Parts and components of helicopter with orbiting propeller and non-rotating main shaft

Abstract

The invention relates to parts and structures of a helicopter with a non-rotating main shaft and a revolution propeller. The invention is applied to the field of aerial flight and is intended to solve the drawbacks of parts and structures of traditional helicopters, traditional coaxial helicopters, and various aircraft. By using a better arrangement method, parts and devices of a new structure are designed to enable them to exert and possess epoch-making performance and efficiency, so that traditional helicopters and aircraft using revolution propellers have higher safety, stability and resistance to deformation, and the revolution propeller can become various aircraft with superior carrying capacity and safety.

Description

[0001] Technical field: air flight.

[0002] Background technology: The blades of traditional helicopters are long and elastic, and the whole blade swings freely when it hits the wind, which produces a lot of noise. The original orbiting propeller disc profile is not clearly described, and there are few functions applied in the orbiting propeller disc and functions that are not expected or expressed. The original orbiting propeller disc rotates with the coaxial, which is different from or safer than the original orbiting propeller disc lower layer application or the orbiting propeller disc application between the upper and lower wing orbiting groups. The traditional propeller center axis or known coaxial axis rotates with the propeller, which will cause fatal disadvantages. For example, if the center axis or coaxial axis or bearing has a little gap or bending, even if the external rotating part is well balanced, it will cause fatal problems. If it is in the air, the speed will decrease and even fall. The transmission of the components of the upper and lower drive gear discs at the root of the original orbiting propeller that propels the orbiting group forward is not clearly described or a solution is not thought of. The traditional blade type has one propeller, or the rotation of the propeller causes the aircraft body or tail to tilt or rotate to one side. Existing conductive parts such as conductive bearings are made of metal, and rotational wear will also produce gaps that affect the conductive effect. For example, adding lubricating oil will affect the conductive effect. Moreover, conductive bearings have an uncontrolled medium, that is, the ball. Or other rotating conductive devices have a short service life. Traditional tail rotors or tail wings use levers or wind resistance areas to control the main body of the aircraft, such as the area of ​​the tail rotor of a traditional coaxial helicopter and the area of ​​the tail rotor of a left-right horizontal tilt helicopter. The cross-flow or reverse wind can also use the tail rotor or tail wing to move the main body and lose control. Traditional tilting is tilting from top to front. The forward tilting has a poor vision. As long as there are blades in front, there is a blind spot. The rudder of various traditional helicopters is at the rear, and it is not good if it breaks. Forklifts are rear-steering and cars are front-steering. Front steering is more suitable for forward than rear steering. The external structure of the helicopter is determined by different applications, but most of them are that the airflow compressed by the blades is blocked by the main body. Summary of the invention:

[0003] 1. The parts and composition of the helicopter with a revolution blade and a revolution group and a non-rotating main shaft, the revolution propeller, the propeller having several blades symmetrically mounted on the revolution disk, the revolution disk rotation center being mounted on the upper end of the non-rotating main shaft by means of a bearing, or the propeller having several blades symmetrically mounted on the revolution disk, the revolution disk rotation center being mounted on the upper end of the non-rotating main shaft by means of a bearing sleeve, the non-rotating main shaft being made hollow, the coupling being mounted at the position of the lower revolution disk, the coupling being mounted on the revolution disk or the bearing sleeve, the non-rotating main shaft being mounted together with the coupling by means of a round shaft tube being sleeved into the non-rotating main shaft, the round shaft tube being called an outer coupling shaft tube, and being mounted on the outer coupling shaft tube in the outer shell of the propeller non-rotating main shaft A driving gear ring or a pulley or a chain wheel or a planetary reduction gear is installed, which transmits power to the motor installed on the outer shell, and a lifting and telescopic shaft is inserted into the hollow non-rotating main shaft. The two ends of the lifting and telescopic shaft protrude a certain distance from the two ends of the non-rotating main shaft. A pitch disc is installed at the segmented propeller end of the lifting and telescopic shaft. There are several pitch disc connecting rods installed for each number of blades, which are connected to the blade pitch change arm. The synchronous connecting rod rotates together with the revolving propeller disc, and a motor is installed at the other end of the lifting and telescopic shaft to perform the lifting and telescopic action, or the lifting and telescopic shaft of each propeller is converged in the revolving propeller disc at the coaxial position by levers, pull rods, gears, etc., and the pitch change of multiple propeller blades is synchronously processed by the pitch disc, motor, etc. The propeller non-rotating main shaft housing is installed on the stress transfer revolution hub, and the propellers of the wing revolution group arranged up and down are installed above the stress transfer revolution hubs of the upper and lower wing revolution groups, or the propellers of the upper wing revolution group are installed above the stress transfer revolution hub, and the propellers of the lower wing revolution group are installed below the stress transfer revolution hub. The section from the propeller blade installation end to the section with lift or wind-flapping angle is the section with a downward bending angle and gradually widens, which is called the blade lift section. Traditional flat blades or lift blades can be used. At the other end of the propeller blade installation end, the flat section that does not bend downward is called the blade tip section, or the windward surface of the blade tip section is gradually changed into a flat rectangular strip, and the gradually changed flat rectangular strip is like the plane of the sword blade gradually changes from a narrow sword tip to a flat rectangular strip. The width and length of the gradually changed flat rectangular strip are based on actual needs. The windward surface of the flat rectangular strip may be a sawtooth shape, a polygonal strip, or a slightly inclined surface. The blade tip end surface, that is, the top, should also be square, rectangular, gradient flat rectangular strip, etc. The angle formed by the windward surface of the blade tip and the two sides of the blade tip end surface is a solid angle, using a right angle, an obtuse angle, an acute angle or an arc, but connected together, they are all flat rectangular strips. Or the entire windward surface of the propeller blade should be a flat rectangular strip.The propeller blades are divided into two sections, and one or more shafts are inserted into the lift section of the blade. This shaft is connected to the blade tip section and the blade tip section is fixed. The blade on the blade lift section of the shaft can swing up and down with variable pitch. This shaft is called the blade shaft. The blade shaft is installed on the central axis of the propeller using a round shaft or a flat shaft with holes at the installation end. The joint between the blade lift section and the blade tip section adopts positive joint, oblique joint, or soft joint. Positive joint is to divide the blade lift section and the blade tip section of the long strip blade into two sections at a right angle to it. Oblique joint is to divide the blade lift section and the blade tip section of the long strip blade into two sections at an oblique angle with an acute or obtuse angle. Positive joint should be used at the variable pitch swing axis. Soft joint joint is to use materials that can stretch, retract, bend, and return to the position to connect the blade lift section and the blade tip section. Or the blade shaft is used as the windward side of the blade, which is called the windward blade shaft. The blade tip section and the windward blade shaft are initially integrated, and the blade lift section is installed behind the windward blade shaft with a shaft or bearing, or the windward blade shaft and the blade lift section are connected to each other by a hinge or chain. A pitch-changing arm is installed on the shaft of the blade lift section or on the blade, so that the blade lift section can swing up and down. Or the blade tip section and the windward blade shaft are made to have a swing amount, and the connection between the blade lift section and the blade tip section or the variable pitch swing shaft of the blade lift section and the windward blade shaft is mutually transmitted by gears, pull rods, pull wires, etc., or the shaft connected to the blade tip section and the variable pitch swing shaft of the blade lift section are separately controlled, and when the windward side of the blade lift section changes pitch upward, the windward side of the blade tip section changes pitch downward. The lift section of the blade generates opposite forces with the tip section of the blade. The blade maintains a constant amplitude. The segmented blades provide more stability, controllability and noise reduction. The propeller with a non-rotating main shaft will not affect the dynamic balance rotation even if the main shaft is bent by centrifugal force.

[0004] 2 The non-rotating main shaft and the electric coaxial shaft, the shaft tube or the outer rotating part installed on the outer periphery of the main shaft, can be self-contained and can be independent. Using a non-rotating main shaft or a hollow shaft tube, the upper wing revolution group revolution disk is installed on the upper end of the main shaft by bearings, and the lower wing revolution group revolution disk is installed on the lower end of the main shaft by bearings. The non-rotating main shaft is arranged in the state of the upper and lower revolution groups and the electric coaxial shaft is collectively referred to as a coaxial shaft. One or more transverse shafts are installed on the non-rotating coaxial shaft between the upper and lower revolution disks. The transverse shaft and the coaxial axis are in a right-angle plane or multiple symmetrical installations. A rotatable gear is installed on the transverse shaft. An external coupling shaft tube is installed downwardly on the outer periphery of the coaxial shaft of the lower revolution disk of the upper wing revolution group. The external coupling shaft tube or the coupling and other soft connections are connected to the revolution disk or the revolution disk bearing jacket. An annular gear ring or an annular gear disk is installed on the external coupling shaft tube. The annular gear ring or annular gear disk is collectively referred to as an annular gear ring. Or the annular gear ring is directly installed on the lower revolving propeller disc or the bearing sleeve of the upper wing revolving group, or the annular gear ring is installed on the lower revolving propeller disc or the bearing sleeve of the upper wing revolving group by using a connecting rod, and the annular gear ring of the lower revolving propeller disc of the upper wing revolving group meshes with the upper part of the gear on the horizontal axis. The upper revolving propeller disc of the lower wing revolving group is upwardly installed with an external coupling shaft tube and a coupling on the outer periphery of the non-rotating coaxial, and the annular gear ring is installed on the external coupling shaft tube, or the annular gear ring is directly installed on the upper revolving propeller disc of the lower wing revolving group, or the annular gear ring is installed on the revolving propeller disc or the bearing sleeve by using a connecting rod, and the annular gear ring of the upper revolving propeller disc of the lower wing revolving group meshes with the lower part of the gear on the horizontal axis. The external coupling shaft tube is downwardly installed with a bearing on the outer periphery of the non-rotating coaxial below the lower revolving propeller disc of the lower wing revolving group, and a driving gear disc is installed on the external coupling shaft tube, or the driving gear disc is directly installed below the lower revolving propeller disc, and the driving gear disc is driven or meshed with the wheel of the power output by using a pulley, a chain wheel, etc. Or one of the horizontal shafts can be made into a transmission shaft, and a driving gear plate can be installed at the other end of the transmission shaft, or it can be made into a tilting horizontal shaft, and the driving gear plate can rotate to drive the upper and lower wing revolution groups to rotate in opposite directions. Or the horizontal shaft can be erected, called a vertical shaft, and non-rotating gears can be installed at both ends. The vertical shaft is installed on the periphery of the non-rotating main shaft, and the gear at one end of the vertical shaft meshes with the outer ring teeth of one of the upper and lower annular gear rings, and the gear at the other end of the vertical shaft meshes with the inner ring teeth of the other annular gear ring. The vertical shaft can use universal joints, telescopic joints, etc. to make the upper and lower wing revolution groups rotate in positive and negative directions. Or multiple folding-type synchronous links are used to connect the upper and lower revolving paddle discs with the annular gear ring, and the synchronous links are supported by springs, or the upper or lower revolving paddle disc is connected to the extended outer connecting shaft tube to connect the annular gear ring of one of them, or a coaxial ball cage is used, or a coaxial spring is used, or a coaxial upper and lower meshing gear ring is used, or a groove is used to insert teeth, or various couplings and other soft connections are used to connect between the outer connecting shaft tube and the upper or lower revolving paddle disc or the revolving paddle disc bearing sleeve.The non-rotating main shaft derives an electric coaxial shaft, and utilizes a non-rotating hollow shaft tube to install a driving gear disc or an annular gear ring of an inner ring tooth on the orbiting propeller disc of the upper wing orbiting group or the rotating center area of ​​the initially integrated stress transfer orbiting propeller hub. A motor is installed inside or outside the upper end of the hollow non-rotating shaft tube, or a planetary reduction device is used to rotate the upper wing orbiting group and drive the lower wing orbiting group to rotate in the opposite direction, or the driving gear disc is installed in one of the orbiting propeller disc cavities, and an intermediate transmission device is used to rotate the upper and lower wing orbiting groups in the forward and reverse directions, or the intermediate horizontal shaft and the transmission part are eliminated, or two driving gear discs are installed in or outside the upper and lower orbiting propeller disc cavities, and the upper and lower motors are installed on a non-rotating hollow shaft to drive the upper and lower driving gear discs, or a motor is installed on the horizontal shaft to drive the gears on the horizontal shaft or directly drive the upper and lower annular gear rings to drive the upper and lower wing orbiting groups to rotate in the opposite direction. Or, a planetary gear reduction device is used on the horizontal axis, and the rotating electric wire at the propeller end is led to the non-rotating hollow electric coaxial shaft. Holes are drilled on the electric coaxial shaft inside or outside the cavity of the revolving propeller disc. As many holes are drilled on the hollow electric coaxial shaft tube, the quality of the hollow shaft tube is affected. Or, another shaft tube or a shaft tube with grooves or multiple wire grooves or multiple thin shaft tubes is inserted into the hollow shaft tube, or the inner wall of the coaxial shaft tube is made with multiple wire grooves, or the outer wall of the coaxial shaft tube is made into a groove to insert the wire round tube, or the inner shaft tube is an oblate ring shaft tube with holes, and the wire can be inserted into the round hole, and the wire is introduced into the lower body. The double-layer shaft tube can increase the strength of the electric coaxial shaft. The outer connecting shaft tube installed downward on the lower revolving propeller disc is installed with a bearing, which is installed on the aircraft body using a bearing sleeve, and then the non-rotating coaxial shaft is installed on the body using a connecting rod. There are two mounting points for the main body. Imagine that the reciprocating swing of the universal joint cross axis can be formed. The bearing sleeve and the connecting rod connected to the main body with the non-rotating coaxial shaft derive the tilt arm, and the orbiting propeller wing orbiting group and the tilt helicopter. The orbiting propeller non-rotating main shaft can be used to push the orbiting group forward. Moreover, the electric coaxial shaft and the non-rotating main shaft are self-contained, and you can play with it even if the coaxial shaft is bent or there is some clearance in the bearing. The non-rotating coaxial shaft can be manually bent and returned to the desired direction to change the direction and push the main body.

[0005] 3. The orbiting propeller disc, the orbiting propeller blades are symmetrically installed on the orbiting propeller disc, or one or more layers of discs or connecting rods are installed at the coaxial ends of the roots of multiple stress transfer orbiting hubs. The discs or connecting rods are connected at multiple points of extension and shortening on the stress transfer orbiting hub or the transmission shaft, that is, multiple grip points, or the inner and outer layers or the upper and lower layers are interconnected again, etc., to fix the stress transfer orbiting hub and the transmission shaft to withstand more stress. The rotation center of the orbiting propeller disc is directly installed on the rotating coaxial axis and rotates with the coaxial axis, or the rotation center of the orbiting propeller disc is installed on the non-rotating coaxial axis or the main shaft by means of bearings. The rotating part installed on the orbiting propeller disc can rotate on the non-rotating coaxial axis or the main shaft. When the orbiting propeller disc rotates on the coaxial axis or the main shaft, the upper or lower part of the cross-section with the coaxial axis or the main shaft axis is triangular or the upper or lower part is concave semicircular, etc., which is called an orbiting propeller disc. A revolving propeller disc is installed on the upper and lower surfaces of each stress transfer revolving propeller hub connected to each propeller of each revolving group, or the revolving propeller disc is installed on only one side. A cavity is formed between the revolving propeller disc and the coaxial shaft, or one or more layers of flat discs or pull rods are applied in the cavity, and connected to the outer sleeve of the bearing installed on each group of stress transfer revolving propeller hubs and transmission shafts, which are pulled to the coaxial shaft in a straight line or pulled to the coaxial shaft in a plane, to bear some rotational centrifugal force. Or a planetary reduction device is applied in the cavity. The revolving propeller disc uses a connecting rod weaving method or an oblique pulling method to install the stress transfer revolving propeller hub and the transmission shaft, just like the spokes of a wheel are woven and pulled crosswise and obliquely. The orbiting propeller disc is different from the connection point between the traditional blades and their central axis. The traditional connection point does not require or does not have the stability characteristic of the triangle or concave semicircle presented when the orbiting propeller disc rotates. Because the traditional blades require or allow each blade to have uncontrollable swinging up and down or left and right independently, the orbiting propeller disc does not need to produce variables in this position. Even if the stress transfer orbiting propeller hub has a small elasticity, it can be quickly returned to its original position through the stable traction of the orbiting propeller disc. When the rotating part installed on the orbiting propeller disc is in good dynamic balance, the smooth rotation will not be affected by the bending of the coaxial axis or the clearance of the bearing, and it is safe.

[0006] 4. Metal conductive device, using a conductive metal ring installed on the coaxial inside or outside the cavity of the orbiting propeller disk of the wing orbiting group, and the coaxial installation is surrounded by a plane at right angles to the coaxial axis. The conductive metal ring is installed at the corresponding position of the outer wall of the ring and the orbiting propeller disk or the cavity of the orbiting propeller disk, or a disk is used on the top or bottom of the disk to form a disk installed on the coaxial, and the ring or the disk are collectively referred to as a conductive ring. The conductive ring is made into an inner gear ring, one or more conductive gears matching the teeth of the inner gear ring are installed in the inner gear ring, a conductive bearing is installed at the rotation center of the conductive gear, a shaft is installed on the inner wall of the conductive bearing, or a hollow bearing shaft with a diameter larger than the coaxial shaft is encircled by the coaxial shaft, and a conductive bearing with a diameter larger than the coaxial shaft is encircled by the coaxial shaft, a conductive connecting rod is installed on the inner wall shaft of the bearing, or the conductive connecting rod is made to be retractable, and a spring or other elastic material is used to pull or push in the same direction of the rotating centrifugal force, or an electric wire is directly led out from the bearing shaft, the other end of the connecting rod and the electric wire are installed in the corresponding position inside or outside the cavity of the revolving propeller disk, led to the propeller end, and connected to the electric wire of the propeller end motor, or the other end of the connecting rod is installed with the coaxial shaft, the electric wire is led into the coaxial shaft, connected to the electric wire of the power output end, and the electric wire led out of the conductive ring is led into the coaxial shaft or led to the propeller end. Or a groove is made at the tooth position of the inner circle of the conductive ring, and one or more flat cams matching the groove are placed in the groove, or a convex ring of the inner circle of the conductive ring and a concave wheel matching the groove are placed in the groove, a conductive bearing is installed at the rotation center of the cam or the concave wheel, a shaft is installed on the inner wall of the conductive bearing, a conductive connecting rod or a connecting arm or a disc is installed on the bearing shaft, or a hollow bearing shaft with a coaxial diameter larger than the coaxial shaft diameter is surrounded by a coaxial shaft, and a conductive bearing with a coaxial diameter larger than the coaxial shaft diameter is surrounded by a coaxial shaft, or the conductive connecting rod is made to be retractable, or a spring or other elastic material is used to pull or push in the same direction of the rotating centrifugal force, or an electric wire is directly led out from the bearing shaft, and the other end of the connecting rod and the electric wire are installed at the corresponding position in the cavity of the revolving propeller disk and led to the propeller end, or the other end of the connecting rod is installed with the coaxial shaft, and the electric wire is led into the coaxial shaft, and the electric wire led out of the conductive ring is led into the coaxial shaft or led to the propeller end. The conductive ring is coaxially installed with a right-angle plane around the coaxial axis. If several wires are needed in the cavity of the revolving propeller disc, several holes are drilled on the coaxial axis and several sets of metal conductive devices are installed. The metal conductive device is installed in a plane stacking ring manner with one ring inside and one ring inside, or installed on one or more layers of flat discs in the revolving propeller disc. The flat disc can not only pull the revolving propeller hub, but also install the conductive device, or install it in the cavity of the revolving propeller disc in an installation manner of stacking rings arranged up and down. The size of the inner wheel or gear of the conductive ring is related to the number of rotations, or it is installed at an inclined angle or standing to expand its diameter. If the conductive bearing is directly installed on the coaxial wall, the bearing beads will have poor contact after rotation and wear, and it cannot be controlled. If you don't grasp it, you will have no confidence. The centrifugal force of the conductive bearing of the metal conductive device and the action of the spring cause the conductive bearing to generate stress on one side, and its internal ball is in a controlled state on one side. Even if it is worn, it is in a controlled state of extrusion, so it is safer. The metal conductive device derives the liquid conductive device.

[0007] 5 Liquid conductive device, drill holes on the hollow shaft tube in the cavity of the orbiting propeller disc, on the electrical coaxial area above the upper orbiting propeller disc of the upper wing orbiting group or the area outside the single wing orbiting group or other orbiting propeller discs where you want to install, drill as many holes as the motor needs, use conductive metal or anti-corrosion properties to make a thin cylindrical conductive ring, which is installed around the hollow shaft tube, and needs to be rotated or installed with bearings, which is called a conductive ring. The conductive ring is installed on the hollow shaft tube and connected to the power wire, or rotates synchronously with the wing orbiting group and is connected to the motor wire at the propeller, and then use conductive or non-conductive or one of the inner and outer layers of non-conductive metal or non-metallic materials to make a circular ring for storing conductive liquid, or a circular tubular ring, or a circular cylindrical ring with various downward or upward or arc or angle curved shapes on the lower ring surface and the upper ring surface, which is installed around the hollow shaft tube, and needs to be rotated or installed with bearings, which is called a liquid ring. A conductive liquid is injected into the liquid pocket ring, and the conductive ring is inserted into the liquid pocket ring. One or more sealing rings are installed on the outer inner wall of the upper end of the liquid pocket ring and the inner outer wall or the inner and outer walls of the conductive ring to form a seal with the inserted conductive ring. The liquid pocket ring is installed on a hollow shaft tube. The wires drawn from the liquid pocket ring are connected to the power wires, or the liquid pocket ring rotates synchronously with the wing revolution group. The wires drawn from the liquid pocket ring are connected to the motor at the propeller. The positive and negative poles of the wires of the motor of each propeller on a wing revolution group are connected in parallel or in series and converged at the coaxial part to connect with the conductive ring or the wires drawn from the liquid pocket ring. As many conductive rings and liquid pocket rings are installed as many wires as there are. The conductive ring and the liquid pocket ring are installed in the cavity of the revolution propeller disc in an up-and-down arrangement or in a flat stacking arrangement of one ring inside and one ring outside the cavity of the revolution propeller disc. The wires drawn from the generator or battery and the wires drawn from the coaxial part are led to the cab and the control device for corresponding connection. Or add a liquid storage ring to automatically add and store the conductive liquid in the liquid pocket ring, just like the effect of the water tank outside the car tank. Use a tie rod with spaced stakes, wrap the wire around each stake and insert it into the corresponding hollow stress transfer revolving hub, fix the tie rod, and connect it to the propeller end wire. Or place the wire in an S shape in the hollow stress transfer revolving hub, and fix the wire by spraying foam to solidify it to reduce the centrifugal force of the wire. Each set of conductive rings and liquid pocket rings only conducts electricity from one wire, so there will be no boiling of liquid or metal welding effect in liquid metal.In the shape of artillery rifle, on the inner section of the conductive ring inserted into the liquid pocket ring, a circle of strips extending obliquely or standing obliquely on the conductive ring or a groove sunk into the conductive ring is installed around the coaxial ring, which is called a stirring bar. The intermittent stirring bar moves forward to reduce resistance, or a circle of strips extending obliquely or standing obliquely on the inner wall of the liquid pocket ring or a groove sunk into the liquid pocket ring is installed around the coaxial ring in the liquid pocket ring cavity, or stirring bars are installed on both the conductive ring and the liquid pocket ring, or a circular ring is installed at the lower end of the conductive ring inserted into the liquid pocket ring, and the stirring bar is installed on the circular ring. The oblique direction of the stirring bar allows the conductive liquid to flow and roll in the liquid pocket ring. No bubbles are generated and there is no wear except for the sealing ring. The resistance of water is relatively small. The viscosity of the conductive liquid metal depends on the viscosity of it when it is poured out of the bucket. If the large circular ring rotates, the resistance will be very large.

[0008] 6. Propel the revolution group forward, utilize the revolution propeller to utilize several propeller blades to be symmetrically installed on the revolution propeller disc, the revolution propeller disc rotation center is installed on the upper end of the non-rotating main shaft by the bearing, utilize the coupling and the outer coupling shaft tube to be installed on the revolution propeller disc, the outer coupling shaft tube is installed on the revolution propeller disc, and the annular gear ring is installed on the non-rotating coaxial axis in the revolution propeller disc, the transmission shaft gear is meshed with the annular gear ring, a transverse axis is installed on the coaxial axis between the upper and lower revolution propeller discs, and the upper and lower annular gear rings and the outer coupling shaft tube are connected with the upper and lower revolution propeller discs, a driving gear disc is installed on the lower outer coupling shaft tube of the lower revolution propeller disc, a driving gear disc is meshed with the power output gear, and the upper and lower wing revolution groups are driven to rotate in the positive and negative directions, this is the vertical state, it is laid down horizontally, or a propeller blade with a fixed pitch is used, and it is installed at the rear end of the helicopter to propel the revolution group forward. A toothed disc of a driving toothed disc is used with a pulley, a chain wheel, a toothed wheel, a planetary gear, etc., and is mutually transmitted with a power output wheel or a gear. The original coaxial upper and lower wing revolution group has upper and lower driving toothed discs with reverse speed increase, or a bearing is used to install the horizontal axis between the upper and lower driving toothed discs such as the non-rotating coaxial upper and lower revolution propeller discs. The horizontal axis is fixed on the main body and does not rotate. The rotatable gear on the horizontal axis is engaged with the upper and lower driving toothed discs. A power output wheel or gear is used to mutually transmit with one of the driving toothed discs, which can drive the upper and lower wing revolution groups to rotate in the positive and negative directions. This is the vertical state, which is laid down horizontally, or a propeller blade with a fixed pitch is used and installed at the rear end of the helicopter to make a forward propulsion revolution group. The two wing revolution groups above the coaxial helicopter with the forward propulsion revolution group installed are equivalent to the wings, and it is possible to become a gyroscope when combined with the inverted forward propulsion revolution group.

[0009] 7. Wind-holding wing. The older generation said that for water, dry-building walls can annoy the Dragon King, so the wind should also be unblocked. The wind-holding wing of the orbiting propeller helicopter is made into one or more straight narrow and long rods, or narrow and long rods with a certain curvature according to the needs. The front ridge of a narrow and long rod is rectangular, triangular, elliptical, etc. The rod-shaped wing is opened for work when needed, and returns to the initial state of the rod when not needed. It is called the wind-holding wing. The front wing installed on the front side of the helicopter body is the wind-holding front wing, the side wing installed on both sides of the body is the wind-holding side wing, and the tail wing installed at the rear of the body is the wind-holding tail wing. The opening and closing of the wind-holding wing is controlled by a pull rod, a pull wire or a motor, an electric cylinder, an oil cylinder, etc. The tail wing is installed on the tail beam behind the body or protrudes on the shell of the body or extends from the end of the tail beam, or one or more wind-holding wings are installed at the tail corresponding to the up, down, left and right directions. Each wind-holding wing can swing a certain angle in the required direction. Or the narrow long rod is not moved to push and pull the wing hub to expand to one side, or the wing hub is installed on both sides of the inner surface of the narrow long rod, or the wing hub is installed on both sides of the narrow long rod, and the narrow long rod or the wing hub is pushed and pulled to make the wind-holding wing fan-shaped. The length is based on the requirements, and one end of all the wing hubs is condensed on the swing point axis of the narrow long rod and installed, which is called the root. The wing hub and the narrow long rod are connected by folding cloth of good material, or thin and hard metal or non-metallic materials are directly made into narrow and long strip wing hubs or attached to the wing hubs, and they are connected to each other at the top and middle with ropes or steel wires and grooves, embedded and staggered. When a narrow long rod is pulled in the required direction, a fan-shaped windward surface is generated. Or the narrow long rod is initially fixed at the required angle, and a fan-shaped windward surface is generated when the wing hub is pulled. The wing hub and the narrow long rod are made of thin and hard materials. The blades are arranged in overlapping scales one by one. To prevent the air from leaking through the wing surface, the blades are made into flat strips, parallelograms, rhombuses, ellipses, S-shaped, etc., and multiple rows of blades are connected to each other between the wing hubs and the narrow long rods. A retractable wing hub is added between the wing hub and the narrow long rods or between the two. When the narrow long rods or the wing hubs on both sides are turned, all the blades change their tilting direction at the same time, so as to increase the fan-shaped windward area generated when a narrow long rod is turned in the required direction. At the root swing point of the narrow long rod, one or more integral shaft rods are installed at right angles to the narrow long rod using bearings. One shaft rod is connected to the narrow long rod or is initially integrated with the narrow long rod, and the other or more shaft rods extend inward or outward in a "towel" shape. A narrow long rod is erected at the center of the cross, which is called an angle shaft rod. Put the root of the wing hub or the application bearing on the angle shaft rod, install a connecting rod of corresponding length or gear of corresponding size at the root of each wing hub, use pull rod, pull wire, rack and other corresponding installation connections, and fix it on the tail beam or the fixed place of the main body. When the narrow long rod is pulled, the angle shaft rod sleeved on the root of the wing hub forms a fan-shaped stroke, which automatically pulls the wing hub to one side to unfold and tilt, and the narrow long rod unfolds into a fan shape in the required direction. After the work is completed, use a return spring or push-pull rod to return the narrow long rod to its initial state to become a wind-engaging wing.Or the narrow long rod and the root of the wing hub are arranged separately and installed flat on the vertical axis of the "mountain" shape, and the horizontal axis is installed on the main body, or a section of shaft rod is led out from the installation point of the narrow long rod and the root of the wing hub, and a directional angle slide is installed and fixed on the main body or the bracket. The slide is installed on the wing hub, and the two points of the triangular bottom of the slide are installed obliquely on the main body or the bracket, or a cross lever push-pull rod is installed, and the lever is installed on the main body frame, one end of the lever is connected to the root of the opposite wing hub and the other end is connected to the narrow long rod, or a directional angle push-pull rod, the narrow long rod and the wing hub swing by the angle of the installation pull rod, or a directional angle slide groove, the narrow long rod and the wing hub use a section of shaft rod installed at the root, and a concave and convex arc angle slide groove is installed on the main body or the bracket, or a directional angle travel slot, the empty slots with intervals installed on the main body or the bracket have a directional angle, and the narrow long rod and the wing hub are clamped in the slot. All are unidirectional or bidirectional, with the middle being the unfolding stroke or one end being close together and the other end being unfolded, or the middle being the combined angle stroke and the two ends being the unfolding angle stroke, or the two ends being the combined angle stroke and the middle being the unfolding angle stroke, and the narrow long rod or wing hub or moving device can be pushed and pulled to make the wind-holding wing unfold in the required direction and return to the initial narrow long rod state. Or one rod can be rotated to different directions for work, or the wind-holding wing can be fixedly installed at a certain angle, or the fan-shaped large arc surface of the wind-holding wing can be installed in the reverse direction facing the front of the main body, etc., or it can be unfolded or merged by pushing and pulling the wing hub. A narrow long rod can be installed in front of the main body to control up and down, and a narrow long rod can be installed at the tail to control left and right. Or a narrow long rod can be used to control left and right or up and down, and the angle folding connecting rod used by the balance steering wheel can be connected with the connecting rod of the corresponding length installed at the root of each wing hub by a pull rod, etc., so that pushing and pulling a narrow long rod can work in the left and right directions or up and down directions. Or multiple wind-holding wings can be applied in the shape of arrow feathers, and a row of wind-holding wings arranged at an inclined angle can be installed on both sides or one side of the main pole, or arranged in the shape of a fork, and a row of wind-holding wings with one direction can be installed on a main pole using an angle folding connecting rod, and a horizontal tail can be formed by pushing and pulling the wing hub or a narrow long rod, or by pushing and pulling the main rod. When ascending, descending or hovering, it returns to the narrow long rod state, and unfolds into a large area when needed. The pull rods, pull wires, motor cylinders, etc. that control its workmanship are connected to the four-way pedals or the balance steering wheel in the cab to control the direction.

[0010] 8. The front rudder wing is installed at the front end of the main body, or at the periphery of the upper or lower part of the main body, and is called the front rudder wing. The front rudder wing is in a triangular cone shape, with the front end tip facing the front of the main body and having three faces. The rear end is larger than the front end tip and is also triangular. The length and width are determined according to the needs, or the front rudder wing is made into a cone or an oblate cone, or the rear end section is a triangular hub frame. The triangular hub frame is a combination in the middle, and the enclosure and construction area are empty for ventilation. The front end tip faces the front of the main body, and the oblate cone has an olive-shaped cross section. The front end tip is broken into two sections, and the rear end section is made into a hollow circular hole. A telescopic transmission shaft, or motor wires, etc. are inserted into the circular hole. Two or more blades embedded in the rear end section are installed on the front end tip section. When in use, the front end tip section is pushed forward, and the blades are spread open by a connecting rod, or the blades are directly rotated after being pushed forward and thrown away by centrifugal force. A horizontal axis is installed at the rear end of the rear section of the front rudder wing, and a vertical axis is installed on the main body. The lower end of the vertical axis does not rotate, and the upper end is equipped with a connecting arm that rotates and is installed with the horizontal axis using a bearing. An annular gear plate is installed on the non-rotating vertical axis, and a motor is installed on the rotating vertical axis. The motor gear meshes with the teeth of the annular gear plate. A connecting arm is extended from the rear end of the rear section of the front rudder wing. The connecting arm connects the pull rod, the lever, and the lever connects the rack, the motor, the electric cylinder, the oil cylinder, etc. to control the up and down or left and right swing. The three faces of the triangular cone or the three faces are concave, and one of the edges is directly above or directly below the plane of the main body. The strips are drawn out according to the shape to make vertical left and right direction wings. The left and right edges are drawn out according to the shape on the planes on both sides of the main body plane to make up and down direction wings, which can swing up and down or left and right to control the flight attitude. The front end of the triangular cone front rudder wing is an equilateral triangle, and the left and right strips do not need to be equilateral at the position where the strips are drawn out, or the left and right strips are not drawn out at the continuation angle of the equilateral, or the left and right strips are drawn out at the continuation angle of the equilateral. The three surfaces of the triangular cone front rudder wing are made concave, like a triangular scraper, or the front tip is broken and divided into two sections, and the rear section is made into a hollow circular hole, or a triangular hub frame is used to insert a telescopic transmission shaft or a motor wire into the circular hole, and three or more root folding propeller blades are installed on the front tip section, close to the groove of the triangular cone front rudder wing, and a pocket groove, a card slot, a card rod, etc. are set at the groove and the blade tip. When folding, the blade tip is inserted into the card slot. When in use, the front tip section is pushed forward, like an umbrella, and the blade is opened by a connecting rod, or it is pushed forward and directly rotated to use centrifugal force to throw the blade away. The directional wing drawn out or the wind-holding wing is used. It is used as a backup for emergency use. The wind-holding tail wing is installed behind the main body, and the front rudder wing is controlled by a balanced steering wheel, and the rear wind-holding wing is controlled by a four-way pedal. When the front rudder wing is installed above the cab, it blocks the sun and rain, and the front rudder wing reacts faster to the main body direction strain during flight.

[0011] The parts and composition of the orbiting propeller-wing orbiting group non-rotating main shaft helicopter, its overall layout is, using the orbiting propeller propeller several blades, symmetrically installed on the orbiting propeller disk, the orbiting propeller disk rotation center is installed on the upper end of the non-rotating main shaft by means of a bearing, the non-rotating main shaft is made hollow, a coupling is installed at the position of the lower orbiting propeller disk, the coupling is installed on the orbiting propeller disk or the bearing sleeve, an outer coupling shaft tube is used to insert into the non-rotating main shaft and install it together with the coupling, an annular gear ring is installed on the outer coupling shaft tube in the outer casing of the propeller non-rotating main shaft, etc., which transmits to each other with the motor installed on the outer casing, a lifting and telescopic shaft is inserted into the hollow non-rotating main shaft, the two ends of the lifting and telescopic shaft protrude a certain distance from the two ends of the non-rotating main shaft, a pitch disc is installed at the segmented propeller end of the lifting and telescopic shaft, there are several blades Install several pitch disc connecting rods to connect with the pitch arm of the blade, use the synchronous connecting rod to rotate together with the orbiting propeller disc, and use levers, pull rods, gears, etc. to converge the lifting and telescopic shaft of each orbiting propeller in the orbiting propeller disc at the coaxial position at the other end of the lifting and telescopic shaft. Use the pitch disc, motor, etc. to synchronously handle the pitch change of multiple propeller blades at the same time, and use the propeller non-rotating main shaft housing to install it on the stress transfer orbiting hub, pass the wires used at the orbiting propeller end through the hollow stress transfer orbiting hub, and install the stress transfer orbiting hub on the orbiting propeller disc. Install a metal conductive device or a liquid conductive device at the orbiting propeller disc cavity position on the electrical coaxial axis, connect the orbiting propeller end wires to the conductive device wires, and install bearings and bearing sleeves at the corresponding positions of the orbiting propeller disc on the coaxial axis. , the wire of the conductive device is led to the lower end by the drilled hollow electric coaxial shaft, and a shaft tube with a groove is inserted into the hollow electric coaxial shaft, the revolving propeller disc is installed on the bearing sleeve, and a coupling and other soft connections are installed on the bearing sleeve. The coupling is further extended by a section of external coupling shaft tube, and an annular gear ring is installed on the external coupling shaft tube. The transverse shaft is symmetrically installed on the coaxial shaft, and a rotatable gear is installed on the transverse shaft. The lower annular gear ring is installed, and the upper and lower annular gear rings are meshed with the gears on the transverse shaft. The lower wing revolving group is installed in the same way as the upper wing revolving group. The lower annular gear ring leads out a section of external coupling shaft tube, or the lower annular gear ring is directly installed on the upper bearing sleeve of the lower revolving propeller disc, and a section of external coupling shaft tube is installed on the lower layer of the lower revolving propeller disc, or a coupling and other soft connections are installed, and the bearings and shafts installed on the main body are installed on the external coupling shaft tube. A bearing sleeve, or a wing revolution group is coaxially installed above the middle long arm of a "U"-shaped helicopter or above the middle main body of a "turban"-shaped helicopter, and the bearing sleeve is used to install it on the main body, and a driving gear plate is installed on the outer coupling shaft tube. The driving gear plate and the power output shaft teeth transmit each other, and the forward propulsion revolution group is installed on the main body on both sides of the "U"-shaped or "turban"-shaped body, or a main body arranged in a plane such as a "V"-shaped body or an oblate circular ring is used, or a "U"-shaped upper and lower structural main body is laid down, or the upper and lower main body structure is used to install the left and right side main bodies, and a helicopter with left and right multi-layer upper and lower structural bodies, and the non-rotating main shaft is installed together with the main body, and the bearing sleeve is connected to the connecting rod of the main body connected to the outer coupling shaft tube to form the reciprocating swing of the universal joint cross axis, or a tilt arm is installed at the coaxial installation position,The other end of the tilt arm is installed on the helicopter body, so that the orbiting rotor blade orbiting helicopter can realize backward tilting, and become an orbiting rotor blade orbiting helicopter with backward tilting. Or use the tilt arm to tilt the jet engine, and tilt the jet engine from the tail nozzle downward to the tail nozzle facing backward, and become a backward tilting jet engine helicopter. Plastic main body shell, install front rudder wing, wind-holding wing and wind-holding tail wing, connect the wires led out of the generator or battery and the wires led out of the coaxial line accordingly, and then pull it to the cab, and connect it to the accelerator pedal, four-way pedal, sensing lifting wheel, balance steering wheel, etc., and install the landing gear.

[0012] A helicopter with a tilting rotary-wing group that rotates around an axis, applying the components required for a helicopter with a non-rotating main shaft for the rotary-wing group that rotates around an axis, to derive a new tilting method, the required components, and the required main body shape. The tilting method is to install the mounting part of the wing rotary-wing group above, with the propeller blades flapping downward against the wind. The single-wing rotary-wing group or the coaxial-wing rotary-wing group is installed at the mounting end of the tilting arm. The tilting arm is above the main body. The single-wing rotary-wing group or the coaxial-wing rotary-wing group is arranged in the middle part of the main body or at the ends of both sides of the main body. The rotation of the wing rotary-wing group lifts the helicopter main body. The tilting arm tilts the single-wing rotary-wing group or the coaxial-wing rotary-wing group to point to the rear of the helicopter main body. The wing rotary-wing group flaps backward against the wind to push the main body forward. When taking off and landing, it returns to flapping downward against the wind. The helicopter main body is made into a "V" shape, a "U" shape, an oblong circular ring shape, or a "towel" shape. For the "U" shape main body, the two side main bodies extend backward, and the main body is arranged in a plane. Or the "U" shape is laid down to form an upper and lower structure main body. The upper main body of the upper and lower structure main body is shorter, and the lower main body is longer. Or the upper main body is longer and the lower main body is shorter. Or install the left and right side main bodies on the upper and lower main body structures, and the left and right multi-layer upper and lower structure main bodies. When viewed from the front of the helicopter main body, it presents a "T" shape, an inverted "T" shape, an "I" shape, a "soil" shape, a "dry" shape, a "king" shape, a "rich" shape, etc. The two side main bodies extend backward. When viewed from both sides of the helicopter main body, it presents that the upper main body is short and the lower main body is long, or the lower main body is short and the upper main body is long, or the middle main body is short and the upper and lower main bodies are long, or the upper and lower main bodies are short and the middle main body is long, or the upper and lower main bodies are of the same length. The front end of the main body is in a shape that reduces wind resistance. Install inclined long arms on the outer periphery of both side main bodies or on the outer periphery of the center of the front of the main body upward and backward. Install one or more or multiple sections of long arms, or multiple sections of robotic arms. The inclined direction of the long arms is the same inclined direction or one or more of the other long arms are inclined in the opposite direction. These are called tilting arms. The tilting arm may be in a triangular support. The tilting arm presents an "L" shape when viewed from the left or right of the helicopter main body. The tilting arm presents a "Sichuan" shape, a "door" shape, or a "claw" shape when viewed from the front of the helicopter main body. One or more of the tilting arms are made hollow. The outer shape of the tilting arm uses a shape that reduces wind resistance. The cross-section of the tilting arm is an olive shape, a circular shape, a semi-circular shape, a flat rhombus shape, etc. Set one or more as the active arms, and the others as the driven arms. The connection between the tilting arm and the main body is called the mounting end, and it is installed using a bearing or a gear installation method that allows it to swing up and down. Use an electric cylinder, an oil cylinder, a motor, a gear, a lever, a pull rod, etc. to make the active arm swing up and down. The connection between the tilting arm and the single-wing rotary-wing group or the coaxial-wing rotary-wing group is called the end. Or use a rope, a pull rod, and a material with high tensile strength to reinforce the pull between the mounting end and the end of the tilting arm. Or install one or more pull rods on the tilting arm at the mounting end, which is in a cross shape with the tilting arm. Install ropes to pull on both ends of the tilting arm on the cross pull rod. Or install an electric cylinder, an oil cylinder, etc. at one end of the cross pull rod.The tilt arm can be extended and retracted by using a telescopic section, or the tilt arm can be moved forward and backward or bent and extended at the main body installation end, or the end of the tilt arm and the coaxial connection can be rotated, or the left and right sides of the main body can swing up and down, or the wings can be formed to pull the tilt arm. Using a tilt arm to tilt backward, the tilt arm can be installed on the long arm using a lever pull rod. When the long arm swings, the deformation of the two at the end installation point is used to tilt the coaxial wing orbital group downward and backward, or a tilt arm section is installed at the end of the tilt arm using a bearing and a horizontal axis, which is called a second section of the tilt arm. The second section of the tilt arm is bent at a right angle, or an obtuse angle or an acute angle to the front or rear of the main body, and a single-wing orbital group or a coaxial wing orbital group is installed at its end. The coaxial wing revolution group can be installed by various methods by using the coaxiality between the upper and lower wing revolution groups and the end of the tilt arm, or by using three tilt arms, one of which is installed on the outer periphery of the front center of the front main body upward, and the other two tilt arms are installed on the outer periphery of the main body on both sides upward, and the distance difference between the tilt arm and the installation point of the longitudinal axis of the main body is used, that is, one is installed at the front end of the main body and two are installed in the middle part, or two are installed at the front end of the main body and one is installed in the middle part of the main body. By using the misalignment difference of the coaxial installation point at the end of the tilt arm when the tilt arm swings up and down, the single-wing revolution group or the coaxial wing revolution group installed at the end of the tilt arm is tilted from fluttering in the downward direction to fluttering in the rear direction, or the tilt arm in the middle part is installed on the outer periphery of the middle part of the main body and tilted backward and upward, and the tilt arms on the two main bodies are installed on the outer periphery of the rear end of the two main bodies, and are fixed or tilted forward and upward and swing up and down, so that the balance will be better. A transverse symmetry axis is installed on the bearing sleeve at the driving gear disc end of the coaxial drive, and the transverse symmetry axis is installed together with the ends of the tilting arms on both sides by means of bearings. An up-and-down moving position block is set at the installation place of the tilting arm and the main body to control the swing angle required for the tilting arm to rise and fall. An up-and-down angle block is also set at the installation place of the middle tilting arm and the non-rotating axis, and an angle stopper plate or a shaping plug plate is installed. There is transverse symmetry axis control on the left and right, and there is also transverse axis stability at the connection between the coaxial and the tilting arm, or another section of the tilting arm is installed at the end of the middle tilting arm, and a symmetrical transverse axis is installed in the middle part of the second section of the tilting arm. The ends of the tilting arms on both sides are installed with bearings and the transverse axis. A single-wing orbital group or a coaxial wing orbital group is installed on the end. When the middle tilt arm moves downward, the tilt arms on both sides also descend accordingly, causing the coaxis to tilt. The middle active arm continues to descend so that the wing orbital group coaxially points to the rear tail of the helicopter. Before takeoff or landing, the active arm is raised to point the wing orbital group coaxially downward. The middle tilt arm is installed tilted upward and backward, and the tilt arms on both sides are installed tilted upward and forward. The ends of the tilt arms on both sides are installed together with the non-rotating main shaft by means of bearings and transverse axes. The end of the middle tilt arm is divided into two forks and is concave in an upward semicircle, or the ends of the two tilt arms are installed together with the transverse symmetry axes installed on both sides of the bearing sleeve by means of bearings.The "towel" - shaped main body is arranged in a plane. The middle main body can be shorter and made into a shape that reduces wind resistance, while the two "U" - shaped main bodies on both sides are longer. A long arm that slopes backward and upward is installed above or below the periphery of the middle main body. Or the tilting arm in the middle is the driving arm and the tilting arms on both sides are the driven arms, or the tilting arms on both sides are the driving arms and the tilting arm in the middle is the driven arm. Or the middle main body is long and the main bodies on the left and right sides are short, and tilting arms are installed on the periphery or at the ends of the main bodies extending backward on the left and right sides. On the tilting arms, a single - wing revolution group or a co - axial wing revolution group with a non - rotating main shaft that flaps the wind downward is installed. When the tilting arm is installed on the upper main body or the lower main body, or the upper and lower main bodies are installed with tilting arms in an interactive manner, or an over - frame shaft - type tilting device is installed at the end of the tilting arm. For a three - layer or more - layer main body structure (a three - layer structure uses the two outer layers and the ends to install tilting arms and wing revolution groups). The upper and lower layers where the wing revolution groups are installed are pulled apart by a certain distance front and back, which is easy to achieve front - rear balance. The single - wing revolution group and the tilting arm are used to lift the main body, tilt it backward, and move it forward. Or a transmission shaft is installed in the cavity of the tilting arm to be in contact with a driving gear disk or a disk, a wheel, etc. to implement transmission. The blades of the wing revolution group flap the wind downward, the helicopter main body is lifted, and the wing revolution group is tilted backward by the downward movement of the tilting arm to move the helicopter main body forward in flight. When installing the left and right main bodies on the upper and lower main body structures, and on the left - right multi - layer upper - lower structure main bodies, a single - wing revolution group or a co - axial revolution group is installed at the end of the tilting arm, and it is installed at a position where the helicopter main body can be lifted by the rotating wing revolution group and maintain balance. All tilting arms do not tilt simultaneously. First, one or more groups tilt, and then all tilt backward after the lifting speed increases. Or the middle part between the upper and lower co - axial electric wing revolution groups is connected to the end of the tilting arm, and a motor is installed on the horizontal axis of the co - axial electric system. The horizontal axis is made hollow, and wires enter the hollow hole of the horizontal axis. The horizontal axis is used as the tilting axis, or it is connected to the end of the tilting arm of the left and right side main bodies, or one or more ends of the tilting arms are connected to a horizontal transverse axis, and the other one or more are connected to a vertical transverse axis. Or a tilting arm is installed on the outer coupling pipe between the upper and lower revolution paddle disks. Or one or more ends of the tilting arms are connected between the upper and lower revolution paddle disks, and the other one or more ends of the tilting arms are connected to one end of a non - rotating co - axial system. Wings that expand to both sides are installed on the two - side main bodies of the helicopter. The wings expand when the wing revolution group tilts, and they are close to or embedded in the two - side main bodies during takeoff or landing. The tilting arms are operated in the cab using a fan - shaped swinging push - pull rod. When the revolution paddle wing revolution group tilts backward, the helicopter lifts the main body, and there are multiple - point connections and connections with non - rotating main shafts between the main body and the wing revolution group. Unlike traditional helicopters that use rotors to lift the main body, it is safer. The compressed air flow is at the rear end, without the obstruction of the main body, and the flight speed is faster. Description of the Drawings:

[0013] Figure 1: 1. The movable connection point between the tilting arm and the second section of the tilting arm. 2. The second section of the tilting arm. 3. The axis of the single-wing orbiting group or the coaxial orbiting group. 4. The tilting arm. 5. The tilting arm or the main arm. 6. The movable connection point between the tilting arm and the main body. 7. The movable connection point between the tilting arm and the main body. 8. The cross tie rod. 9. The main body frame.

[0014] Figure 2 : 1. Use the positive joint to divide the blade lift section and the blade tip section into two sections. 2. Use the oblique joint to divide the blade lift section and the blade tip section into two sections. 3. Use the oblique joint to make the blade tip section and the windward blade shaft initially integrated, and use gears to make the windward blade shaft and the blade lift section change pitch in opposite directions. 4. Use the oblique joint to connect the windward blade shaft and the blade lift section by hinge type or chain type.

[0015] Figure 3 : 1. Bearings on which the revolving propeller disc is mounted on the coaxial shaft. 2. Liquid pocket ring. 3. Electric wires led from the conductive ring or liquid pocket ring into the coaxial shaft and to the main body. 4. Bearings on which the revolving propeller disc is mounted on the coaxial shaft. 5. Flexible connections such as couplings. 6. External coupling tube. 7. Gears on the transverse shaft. 8. Electrical coaxial shaft. 9. Conductive ring. 10. Revolving propeller disc. 11. Electric wires leading to the propeller end. 12. Transverse shaft. 13. Upper and lower annular gear rings. 14. External coupling tube. 15. Flexible connections such as couplings. 16. Stress transfer revolving propeller hub. 17. Flexible connections such as couplings. 18. External coupling tube. 19. Driving gear disc or wheel. Specific implementation method:

[0016] Apply the original "revolution propeller" and the rotation mode of the revolution group, and apply the "revolution propeller helicopter structure method and parts" to improve it, such as pushing the revolution group and the revolution propeller disc forward, and applying some irreplaceable structural parts, etc., deriving non-rotating coaxial and electric coaxial, and new helicopters and new required helicopter main body shapes, etc. The new helicopter main body shape is also a required part. Or use electricity, motors, etc. as new structures and new parts for driving, etc., or use batteries or generators, etc. as output power sources.

[0017] 1. The parts and composition of the helicopter with a revolution blade and a revolution group and a non-rotating main shaft, the revolution propeller, the propeller having several blades symmetrically mounted on the revolution disk, the revolution disk rotation center being mounted on the upper end of the non-rotating main shaft by means of a bearing, or the propeller having several blades symmetrically mounted on the revolution disk, the revolution disk rotation center being mounted on the upper end of the non-rotating main shaft by means of a bearing sleeve, the non-rotating main shaft being made hollow, the coupling being mounted at the position of the lower revolution disk, the coupling being mounted on the revolution disk or the bearing sleeve, the non-rotating main shaft being mounted together with the coupling by means of a round shaft tube being sleeved into the non-rotating main shaft, the round shaft tube being called an outer coupling shaft tube, and being mounted on the outer coupling shaft tube in the outer shell of the propeller non-rotating main shaft A driving gear ring or a pulley or a chain wheel or a planetary reduction gear is installed, which transmits power to the motor installed on the outer shell, and a lifting and telescopic shaft is inserted into the hollow non-rotating main shaft. The two ends of the lifting and telescopic shaft protrude a certain distance from the two ends of the non-rotating main shaft. A pitch disc is installed at the segmented propeller end of the lifting and telescopic shaft. There are several pitch disc connecting rods installed for each number of blades, which are connected to the blade pitch change arm. The synchronous connecting rod rotates together with the revolving propeller disc, and a motor is installed at the other end of the lifting and telescopic shaft to perform the lifting and telescopic action, or the lifting and telescopic shaft of each propeller is converged in the revolving propeller disc at the coaxial position by levers, pull rods, gears, etc., and the pitch change of multiple propeller blades is synchronously processed by the pitch disc, motor, etc. The propeller non-rotating main shaft housing is installed on the stress transfer revolution hub, and the propellers of the wing revolution group arranged up and down are installed above the stress transfer revolution hubs of the upper and lower wing revolution groups, or the propellers of the upper wing revolution group are installed above the stress transfer revolution hub, and the propellers of the lower wing revolution group are installed below the stress transfer revolution hub. The section from the propeller blade installation end to the section with lift or wind-flapping angle is the section with a downward bending angle and gradually widens, which is called the blade lift section. Traditional flat blades or lift blades can be used. At the other end of the propeller blade installation end, the flat section that does not bend downward is called the blade tip section, or the windward surface of the blade tip section is gradually changed into a flat rectangular strip, and the gradually changed flat rectangular strip is like the plane of the sword blade gradually changes from a narrow sword tip to a flat rectangular strip. The width and length of the gradually changed flat rectangular strip are based on actual needs. The windward surface of the flat rectangular strip may be a sawtooth shape, a polygonal strip, or a slightly inclined surface. The blade tip end surface, that is, the top, should also be square, rectangular, gradient flat rectangular strip, etc. The angle formed by the windward surface of the blade tip and the two sides of the blade tip end surface is a solid angle, using a right angle, an obtuse angle, an acute angle or an arc, but connected together, they are all flat rectangular strips. Or the entire windward surface of the propeller blade should be a flat rectangular strip.The propeller blades are divided into two sections, and one or more shafts are inserted into the lift section of the blade. This shaft is connected to the blade tip section and the blade tip section is fixed. The blade on the blade lift section of the shaft can swing up and down with variable pitch. This shaft is called the blade shaft. The blade shaft is installed on the central axis of the propeller using a round shaft or a flat shaft with holes at the installation end. The joint between the blade lift section and the blade tip section adopts positive joint, oblique joint, or soft joint. Positive joint is to divide the blade lift section and the blade tip section of the long strip blade into two sections at a right angle to it. Oblique joint is to divide the blade lift section and the blade tip section of the long strip blade into two sections at an oblique angle with an acute or obtuse angle. Positive joint should be used at the variable pitch swing axis. Soft joint joint is to use materials that can stretch, retract, bend, and return to the position to connect the blade lift section and the blade tip section. Or the blade shaft is used as the windward side of the blade, which is called the windward blade shaft. The blade tip section and the windward blade shaft are initially integrated, and the blade lift section is installed behind the windward blade shaft with a shaft or bearing, or the windward blade shaft and the blade lift section are connected to each other by a hinge or chain. A pitch-changing arm is installed on the shaft of the blade lift section or on the blade, so that the blade lift section can swing up and down. Or the blade tip section and the windward blade shaft are made to have a swing amount, and the connection between the blade lift section and the blade tip section or the variable pitch swing shaft of the blade lift section and the windward blade shaft is mutually transmitted by gears, pull rods, pull wires, etc., or the shaft connected to the blade tip section and the variable pitch swing shaft of the blade lift section are separately controlled, and when the windward side of the blade lift section changes pitch upward, the windward side of the blade tip section changes pitch downward. The lift section of the blade generates opposite forces with the tip section of the blade. The blade maintains a constant amplitude. The segmented blades provide more stability, controllability and noise reduction. The propeller with a non-rotating main shaft will not affect the dynamic balance rotation even if the main shaft is bent by centrifugal force.

[0018] 2 The non-rotating main shaft and the electric coaxial shaft, the shaft tube or the outer rotating part installed on the outer periphery of the main shaft, can be self-contained and can be independent. Using a non-rotating main shaft or a hollow shaft tube, the upper wing revolution group revolution disk is installed on the upper end of the main shaft by bearings, and the lower wing revolution group revolution disk is installed on the lower end of the main shaft by bearings. The non-rotating main shaft is arranged in the state of the upper and lower revolution groups and the electric coaxial shaft is collectively referred to as a coaxial shaft. One or more transverse shafts are installed on the non-rotating coaxial shaft between the upper and lower revolution disks. The transverse shaft and the coaxial axis are in a right-angle plane or multiple symmetrical installations. A rotatable gear is installed on the transverse shaft. An external coupling shaft tube is installed downwardly on the outer periphery of the coaxial shaft of the lower revolution disk of the upper wing revolution group. The external coupling shaft tube or the coupling and other soft connections are connected to the revolution disk or the revolution disk bearing jacket. An annular gear ring or an annular gear disk is installed on the external coupling shaft tube. The annular gear ring or annular gear disk is collectively referred to as an annular gear ring. Or the annular gear ring is directly installed on the lower revolving propeller disc or the bearing sleeve of the upper wing revolving group, or the annular gear ring is installed on the lower revolving propeller disc or the bearing sleeve of the upper wing revolving group by using a connecting rod, and the annular gear ring of the lower revolving propeller disc of the upper wing revolving group meshes with the upper part of the gear on the horizontal axis. The upper revolving propeller disc of the lower wing revolving group is upwardly installed with an external coupling shaft tube and a coupling on the outer periphery of the non-rotating coaxial, and the annular gear ring is installed on the external coupling shaft tube, or the annular gear ring is directly installed on the upper revolving propeller disc of the lower wing revolving group, or the annular gear ring is installed on the revolving propeller disc or the bearing sleeve by using a connecting rod, and the annular gear ring of the upper revolving propeller disc of the lower wing revolving group meshes with the lower part of the gear on the horizontal axis. The external coupling shaft tube is downwardly installed with a bearing on the outer periphery of the non-rotating coaxial below the lower revolving propeller disc of the lower wing revolving group, and a driving gear disc is installed on the external coupling shaft tube, or the driving gear disc is directly installed below the lower revolving propeller disc, and the driving gear disc is driven or meshed with the wheel of the power output by using a pulley, a chain wheel, etc. Or one of the horizontal shafts can be made into a transmission shaft, and a driving gear plate can be installed at the other end of the transmission shaft, or it can be made into a tilting horizontal shaft, and the driving gear plate can rotate to drive the upper and lower wing revolution groups to rotate in opposite directions. Or the horizontal shaft can be erected, called a vertical shaft, and non-rotating gears can be installed at both ends. The vertical shaft is installed on the periphery of the non-rotating main shaft, and the gear at one end of the vertical shaft meshes with the outer ring teeth of one of the upper and lower annular gear rings, and the gear at the other end of the vertical shaft meshes with the inner ring teeth of the other annular gear ring. The vertical shaft can use universal joints, telescopic joints, etc. to make the upper and lower wing revolution groups rotate in positive and negative directions. Or multiple folding-type synchronous links are used to connect the upper and lower revolving paddle discs with the annular gear ring, and the synchronous links are supported by springs, or the upper or lower revolving paddle disc is connected to the extended outer connecting shaft tube to connect the annular gear ring of one of them, or a coaxial ball cage is used, or a coaxial spring is used, or a coaxial upper and lower meshing gear ring is used, or a groove is used to insert teeth, or various couplings and other soft connections are used to connect between the outer connecting shaft tube and the upper or lower revolving paddle disc or the revolving paddle disc bearing sleeve.The non-rotating main shaft derives an electric coaxial shaft, and utilizes a non-rotating hollow shaft tube to install a driving gear disc or an annular gear ring of an inner ring tooth on the orbiting propeller disc of the upper wing orbiting group or the rotating center area of ​​the initially integrated stress transfer orbiting propeller hub. A motor is installed inside or outside the upper end of the hollow non-rotating shaft tube, or a planetary reduction device is used to rotate the upper wing orbiting group and drive the lower wing orbiting group to rotate in the opposite direction, or the driving gear disc is installed in one of the orbiting propeller disc cavities, and an intermediate transmission device is used to rotate the upper and lower wing orbiting groups in the forward and reverse directions, or the intermediate horizontal shaft and the transmission part are eliminated, or two driving gear discs are installed in or outside the upper and lower orbiting propeller disc cavities, and the upper and lower motors are installed on a non-rotating hollow shaft to drive the upper and lower driving gear discs, or a motor is installed on the horizontal shaft to drive the gears on the horizontal shaft or directly drive the upper and lower annular gear rings to drive the upper and lower wing orbiting groups to rotate in the opposite direction. Or, a planetary gear reduction device is used on the horizontal axis, and the rotating electric wire at the propeller end is led to the non-rotating hollow electric coaxial shaft. Holes are drilled on the electric coaxial shaft inside or outside the cavity of the revolving propeller disc. As many holes are drilled on the hollow electric coaxial shaft tube, the quality of the hollow shaft tube is affected. Or, another shaft tube or a shaft tube with grooves or multiple wire grooves or multiple thin shaft tubes is inserted into the hollow shaft tube, or the inner wall of the coaxial shaft tube is made with multiple wire grooves, or the outer wall of the coaxial shaft tube is made into a groove to insert the wire round tube, or the inner shaft tube is an oblate ring shaft tube with holes, and the wire can be inserted into the round hole, and the wire is introduced into the lower body. The double-layer shaft tube can increase the strength of the electric coaxial shaft. The outer connecting shaft tube installed downward on the lower revolving propeller disc is installed with a bearing, which is installed on the aircraft body using a bearing sleeve, and then the non-rotating coaxial shaft is installed on the body using a connecting rod. There are two mounting points for the main body. Imagine that the reciprocating swing of the universal joint cross axis can be formed. The bearing sleeve and the connecting rod connected to the main body with the non-rotating coaxial shaft derive the tilt arm, and the orbiting propeller wing orbiting group and the tilt helicopter. The orbiting propeller non-rotating main shaft can be used to push the orbiting group forward. Moreover, the electric coaxial shaft and the non-rotating main shaft are self-contained, and you can play with it even if the coaxial shaft is bent or there is some clearance in the bearing. The non-rotating coaxial shaft can be manually bent and returned to the desired direction to change the direction and push the main body.

[0019] 3. The orbiting propeller disc, the orbiting propeller blades are symmetrically installed on the orbiting propeller disc, or one or more layers of discs or connecting rods are installed at the coaxial ends of the roots of multiple stress transfer orbiting hubs. The discs or connecting rods are connected at multiple points of extension and shortening on the stress transfer orbiting hub or the transmission shaft, that is, multiple grip points, or the inner and outer layers or the upper and lower layers are interconnected again, etc., to fix the stress transfer orbiting hub and the transmission shaft to withstand more stress. The rotation center of the orbiting propeller disc is directly installed on the rotating coaxial axis and rotates with the coaxial axis, or the rotation center of the orbiting propeller disc is installed on the non-rotating coaxial axis or the main shaft by means of bearings. The rotating part installed on the orbiting propeller disc can rotate on the non-rotating coaxial axis or the main shaft. When the orbiting propeller disc rotates on the coaxial axis or the main shaft, the upper or lower part of the cross-section with the coaxial axis or the main shaft axis is triangular or the upper or lower part is concave semicircular, etc., which is called an orbiting propeller disc. A revolving propeller disc is installed on the upper and lower surfaces of each stress transfer revolving propeller hub connected to each propeller of each revolving group, or the revolving propeller disc is installed on only one side. A cavity is formed between the revolving propeller disc and the coaxial shaft, or one or more layers of flat discs or pull rods are applied in the cavity, and connected to the outer sleeve of the bearing installed on each group of stress transfer revolving propeller hubs and transmission shafts, which are pulled to the coaxial shaft in a straight line or pulled to the coaxial shaft in a plane, to bear some rotational centrifugal force. Or a planetary reduction device is applied in the cavity. The revolving propeller disc uses a connecting rod weaving method or an oblique pulling method to install the stress transfer revolving propeller hub and the transmission shaft, just like the spokes of a wheel are woven and pulled crosswise and obliquely. The orbiting propeller disc is different from the connection point between the traditional blades and their central axis. The traditional connection point does not require or does not have the stability characteristic of the triangle or concave semicircle presented when the orbiting propeller disc rotates. Because the traditional blades require or allow each blade to have uncontrollable swinging up and down or left and right independently, the orbiting propeller disc does not need to produce variables in this position. Even if the stress transfer orbiting propeller hub has a small elasticity, it can be quickly returned to its original position through the stable traction of the orbiting propeller disc. When the rotating part installed on the orbiting propeller disc is in good dynamic balance, the smooth rotation will not be affected by the bending of the coaxial axis or the clearance of the bearing, and it is safe.

[0020] 4. Metal conductive device, using a conductive metal ring installed on the coaxial inside or outside the cavity of the orbiting propeller disk of the wing orbiting group, and the coaxial installation is surrounded by a plane at right angles to the coaxial axis. The conductive metal ring is installed at the corresponding position of the outer wall of the ring and the orbiting propeller disk or the cavity of the orbiting propeller disk, or a disk is used on the top or bottom of the disk to form a disk installed on the coaxial, and the ring or the disk are collectively referred to as a conductive ring. The conductive ring is made into an inner gear ring, one or more conductive gears matching the teeth of the inner gear ring are installed in the inner gear ring, a conductive bearing is installed at the rotation center of the conductive gear, a shaft is installed on the inner wall of the conductive bearing, or a hollow bearing shaft with a diameter larger than the coaxial shaft is encircled by the coaxial shaft, and a conductive bearing with a diameter larger than the coaxial shaft is encircled by the coaxial shaft, a conductive connecting rod is installed on the inner wall shaft of the bearing, or the conductive connecting rod is made to be retractable, and a spring or other elastic material is used to pull or push in the same direction of the rotating centrifugal force, or an electric wire is directly led out from the bearing shaft, the other end of the connecting rod and the electric wire are installed in the corresponding position inside or outside the cavity of the revolving propeller disk, led to the propeller end, and connected to the electric wire of the propeller end motor, or the other end of the connecting rod is installed with the coaxial shaft, the electric wire is led into the coaxial shaft, connected to the electric wire of the power output end, and the electric wire led out of the conductive ring is led into the coaxial shaft or led to the propeller end. Or a groove is made at the tooth position of the inner circle of the conductive ring, and one or more flat cams matching the groove are placed in the groove, or a convex ring of the inner circle of the conductive ring and a concave wheel matching the groove are placed in the groove, a conductive bearing is installed at the rotation center of the cam or the concave wheel, a shaft is installed on the inner wall of the conductive bearing, a conductive connecting rod or a connecting arm or a disc is installed on the bearing shaft, or a hollow bearing shaft with a coaxial diameter larger than the coaxial shaft diameter is surrounded by a coaxial shaft, and a conductive bearing with a coaxial diameter larger than the coaxial shaft diameter is surrounded by a coaxial shaft, or the conductive connecting rod is made to be retractable, or a spring or other elastic material is used to pull or push in the same direction of the rotating centrifugal force, or an electric wire is directly led out from the bearing shaft, and the other end of the connecting rod and the electric wire are installed at the corresponding position in the cavity of the revolving propeller disk and led to the propeller end, or the other end of the connecting rod is installed with the coaxial shaft, and the electric wire is led into the coaxial shaft, and the electric wire led out of the conductive ring is led into the coaxial shaft or led to the propeller end. The conductive ring is coaxially installed with a right-angle plane around the coaxial axis. If several wires are needed in the cavity of the revolving propeller disc, several holes are drilled on the coaxial axis and several sets of metal conductive devices are installed. The metal conductive device is installed in a plane stacking ring manner with one ring inside and one ring inside, or installed on one or more layers of flat discs in the revolving propeller disc. The flat disc can not only pull the revolving propeller hub, but also install the conductive device, or install it in the cavity of the revolving propeller disc in an installation manner of stacking rings arranged up and down. The size of the inner wheel or gear of the conductive ring is related to the number of rotations, or it is installed at an inclined angle or standing to expand its diameter. If the conductive bearing is directly installed on the coaxial wall, the bearing beads will have poor contact after rotation and wear, and it cannot be controlled. If you don't grasp it, you will have no confidence. The centrifugal force of the conductive bearing of the metal conductive device and the action of the spring cause the conductive bearing to generate stress on one side, and its internal ball is in a controlled state on one side. Even if it is worn, it is in a controlled state of extrusion, so it is safer. The metal conductive device derives the liquid conductive device.

[0021] 5 Liquid conductive device, drill holes on the hollow shaft tube in the cavity of the orbiting propeller disc, on the electrical coaxial area above the upper orbiting propeller disc of the upper wing orbiting group or the area outside the single wing orbiting group or other orbiting propeller discs where you want to install, drill as many holes as the motor needs, use conductive metal or anti-corrosion properties to make a thin cylindrical conductive ring, which is installed around the hollow shaft tube, and needs to be rotated or installed with bearings, which is called a conductive ring. The conductive ring is installed on the hollow shaft tube and connected to the power wire, or rotates synchronously with the wing orbiting group and is connected to the motor wire at the propeller, and then use conductive or non-conductive or one of the inner and outer layers of non-conductive metal or non-metallic materials to make a circular ring for storing conductive liquid, or a circular tubular ring, or a circular cylindrical ring with various downward or upward or arc or angle curved shapes on the lower ring surface and the upper ring surface, which is installed around the hollow shaft tube, and needs to be rotated or installed with bearings, which is called a liquid ring. A conductive liquid is injected into the liquid pocket ring, and the conductive ring is inserted into the liquid pocket ring. One or more sealing rings are installed on the outer inner wall of the upper end of the liquid pocket ring and the inner outer wall or the inner and outer walls of the conductive ring to form a seal with the inserted conductive ring. The liquid pocket ring is installed on a hollow shaft tube. The wires drawn from the liquid pocket ring are connected to the power wires, or the liquid pocket ring rotates synchronously with the wing revolution group. The wires drawn from the liquid pocket ring are connected to the motor at the propeller. The positive and negative poles of the wires of the motor of each propeller on a wing revolution group are connected in parallel or in series and converged at the coaxial part to connect with the conductive ring or the wires drawn from the liquid pocket ring. As many conductive rings and liquid pocket rings are installed as many wires as there are. The conductive ring and the liquid pocket ring are installed in the cavity of the revolution propeller disc in an up-and-down arrangement or in a flat stacking arrangement of one ring inside and one ring outside the cavity of the revolution propeller disc. The wires drawn from the generator or battery and the wires drawn from the coaxial part are led to the cab and the control device for corresponding connection. Or add a liquid storage ring to automatically add and store the conductive liquid in the liquid pocket ring, just like the effect of the water tank outside the car tank. Use a pull rod with spaced stakes, wrap the wire around each stake and then insert it into the corresponding hollow stress transfer revolving hub, fix the pull rod, and connect it to the propeller end wire. Or place the wire in an S shape in the hollow stress transfer revolving hub, and use the spray foam solidification method to fix the wire to reduce the centrifugal force of the wire. Each set of conductive rings and liquid pocket rings only conducts electricity from one wire, so there will be no boiling of the liquid or metal welding effect in the liquid metal. Suddenly I thought that this seems wrong, the light bulb is connected by tungsten filament. When I was working, I used two steel saw blades to boil water in a bucket for bathing. There were positive and negative poles. After the water boiled, there would be a humming sound. Now when you cook and boil water, bubbles will appear in the pot. If you rotate the water, the bubbles will disappear. The faster the rotation, the fewer bubbles there are. On Mount Everest or in space, the water cannot boil because of the rotation of the earth or the movement of space, or the water may boil if it rotates in the opposite direction. Therefore, the liquid in the liquid ring must have not only centrifugal force, but also flowing rotation.In the shape of artillery rifle, on the inner section of the conductive ring inserted into the liquid pocket ring, a circle of strips extending obliquely or standing obliquely on the conductive ring or a groove sunk into the conductive ring is installed around the coaxial ring, which is called a stirring bar. The intermittent stirring bar moves forward to reduce resistance, or a circle of strips extending obliquely or standing obliquely on the inner wall of the liquid pocket ring or a groove sunk into the liquid pocket ring is installed around the coaxial ring in the liquid pocket ring cavity, or stirring bars are installed on both the conductive ring and the liquid pocket ring, or a circular ring is installed at the lower end of the conductive ring inserted into the liquid pocket ring, and the stirring bar is installed on the circular ring. The oblique direction of the stirring bar allows the conductive liquid to flow and roll in the liquid pocket ring. No bubbles are generated and there is no wear except for the sealing ring. The resistance of water is relatively small. The viscosity of the conductive liquid metal depends on the viscosity of it when it is poured out of the bucket. If the large circular ring rotates, the resistance will be very large.

[0022] 6. Propel the revolution group forward, utilize the revolution propeller to utilize several propeller blades to be symmetrically installed on the revolution propeller disc, the revolution propeller disc rotation center is installed on the upper end of the non-rotating main shaft by the bearing, utilize the coupling and the outer coupling shaft tube to be installed on the revolution propeller disc, the outer coupling shaft tube is installed on the revolution propeller disc, and the annular gear ring is installed on the non-rotating coaxial axis in the revolution propeller disc, the transmission shaft gear is meshed with the annular gear ring, a transverse axis is installed on the coaxial axis between the upper and lower revolution propeller discs, and the upper and lower annular gear rings and the outer coupling shaft tube are connected with the upper and lower revolution propeller discs, a driving gear disc is installed on the lower outer coupling shaft tube of the lower revolution propeller disc, a driving gear disc is meshed with the power output gear, and the upper and lower wing revolution groups are driven to rotate in the positive and negative directions, this is the vertical state, it is laid down horizontally, or a propeller blade with a fixed pitch is used, and it is installed at the rear end of the helicopter to propel the revolution group forward. A toothed disc of a driving toothed disc is used with a pulley, a chain wheel, a toothed wheel, a planetary gear, etc., and is mutually transmitted with a power output wheel or a gear. The original coaxial upper and lower wing revolution group has upper and lower driving toothed discs with reverse speed increase, or a bearing is used to install the horizontal axis between the upper and lower driving toothed discs such as the non-rotating coaxial upper and lower revolution propeller discs. The horizontal axis is fixed on the main body and does not rotate. The rotatable gear on the horizontal axis is engaged with the upper and lower driving toothed discs. A power output wheel or gear is used to mutually transmit with one of the driving toothed discs, which can drive the upper and lower wing revolution groups to rotate in the positive and negative directions. This is the vertical state, which is laid down horizontally, or a propeller blade with a fixed pitch is used and installed at the rear end of the helicopter to make a forward propulsion revolution group. The two wing revolution groups above the coaxial helicopter with the forward propulsion revolution group installed are equivalent to the wings, and it is possible to become a gyroscope when combined with the inverted forward propulsion revolution group.

[0023] 7. Wind-holding wing. The older generation said that for water, dry-building walls can annoy the Dragon King, so the wind should also be unblocked. The wind-holding wing of the orbiting propeller helicopter is made into one or more straight narrow and long rods, or narrow and long rods with a certain curvature according to the needs. The front ridge of a narrow and long rod is rectangular, triangular, elliptical, etc. The rod-shaped wing is opened for work when needed, and returns to the initial state of the rod when not needed. It is called the wind-holding wing. The front wing installed on the front side of the helicopter body is the wind-holding front wing, the side wing installed on both sides of the body is the wind-holding side wing, and the tail wing installed at the rear of the body is the wind-holding tail wing. The opening and closing of the wind-holding wing is controlled by a pull rod, a pull wire or a motor, an electric cylinder, an oil cylinder, etc. The tail wing is installed on the tail beam behind the body or protrudes on the shell of the body or extends from the end of the tail beam, or one or more wind-holding wings are installed at the tail corresponding to the up, down, left and right directions. Each wind-holding wing can swing a certain angle in the required direction. Or the narrow long rod is not moved to push and pull the wing hub to expand to one side, or the wing hub is installed on both sides of the inner surface of the narrow long rod, or the wing hub is installed on both sides of the narrow long rod, and the narrow long rod or the wing hub is pushed and pulled to make the wind-holding wing fan-shaped. The length is based on the requirements, and one end of all the wing hubs is condensed on the swing point axis of the narrow long rod and installed, which is called the root. The wing hub and the narrow long rod are connected by folding cloth of good material, or thin and hard metal or non-metallic materials are directly made into narrow and long strip wing hubs or attached to the wing hubs, and they are connected to each other at the top and middle with ropes or steel wires and grooves, embedded and staggered. When a narrow long rod is pulled in the required direction, a fan-shaped windward surface is generated. Or the narrow long rod is initially fixed at the required angle, and a fan-shaped windward surface is generated when the wing hub is pulled. The wing hub and the narrow long rod are made of thin and hard materials. The blades are arranged in overlapping scales one by one. To prevent the air from leaking through the wing surface, the blades are made into flat strips, parallelograms, rhombuses, ellipses, S-shaped, etc., and multiple rows of blades are connected to each other between the wing hubs and the narrow long rods. A retractable wing hub is added between the wing hub and the narrow long rods or between the two. When the narrow long rods or the wing hubs on both sides are turned, all the blades change their tilting direction at the same time, so as to increase the fan-shaped windward area generated when a narrow long rod is turned in the required direction. At the root swing point of the narrow long rod, one or more integral shaft rods are installed at right angles to the narrow long rod using bearings. One shaft rod is connected to the narrow long rod or is initially integrated with the narrow long rod, and the other or more shaft rods extend inward or outward in a "towel" shape. A narrow long rod is erected at the center of the cross, which is called an angle shaft rod. Put the root of the wing hub or the application bearing on the angle shaft rod, install a connecting rod of corresponding length or gear of corresponding size at the root of each wing hub, use pull rod, pull wire, rack and other corresponding installation connections, and fix it on the tail beam or the fixed place of the main body. When the narrow long rod is pulled, the angle shaft rod sleeved on the root of the wing hub forms a fan-shaped stroke, which automatically pulls the wing hub to one side to unfold and tilt, and the narrow long rod unfolds into a fan shape in the required direction. After the work is completed, use a return spring or push-pull rod to return the narrow long rod to its initial state to become a wind-engaging wing.Or the narrow long rod and the root of the wing hub are arranged separately and installed flat on the vertical axis of the "mountain" shape, and the horizontal axis is installed on the main body, or a section of shaft rod is led out from the installation point of the narrow long rod and the root of the wing hub, and a directional angle slide is installed and fixed on the main body or the bracket. The slide is installed on the wing hub, and the two points of the triangular bottom of the slide are installed obliquely on the main body or the bracket, or a cross lever push-pull rod is installed, and the lever is installed on the main body frame, one end of the lever is connected to the root of the opposite wing hub and the other end is connected to the narrow long rod, or a directional angle push-pull rod, the narrow long rod and the wing hub swing by the angle of the installation pull rod, or a directional angle slide groove, the narrow long rod and the wing hub use a section of shaft rod installed at the root, and a concave and convex arc angle slide groove is installed on the main body or the bracket, or a directional angle travel slot, the empty slots with intervals installed on the main body or the bracket have a directional angle, and the narrow long rod and the wing hub are clamped in the slot. All are unidirectional or bidirectional, with the middle being the unfolding stroke or one end being close together and the other end being unfolded, or the middle being the combined angle stroke and the two ends being the unfolding angle stroke, or the two ends being the combined angle stroke and the middle being the unfolding angle stroke, and the narrow long rod or wing hub or moving device can be pushed and pulled to make the wind-holding wing unfold in the required direction and return to the initial narrow long rod state. Or one rod can be rotated to different directions for work, or the wind-holding wing can be fixedly installed at a certain angle, or the fan-shaped large arc surface of the wind-holding wing can be installed in the reverse direction facing the front of the main body, etc., or it can be unfolded or merged by pushing and pulling the wing hub. A narrow long rod can be installed in front of the main body to control up and down, and a narrow long rod can be installed at the tail to control left and right. Or a narrow long rod can be used to control left and right or up and down, and the angle folding connecting rod used by the balance steering wheel can be connected with the connecting rod of the corresponding length installed at the root of each wing hub by a pull rod, etc., so that pushing and pulling a narrow long rod can work in the left and right directions or up and down directions. Or multiple wind-carrying wings can be applied in the shape of arrow feathers, and multiple wind-carrying wings arranged in a row at an inclined angle can be installed on both sides or one side of the main pole, or arranged in the shape of a fork, and multiple wind-carrying wings in a row with one direction can be installed on a main pole by using an angle folding connecting rod, and the wing hub or narrow long rod or the main rod can be pushed and pulled to become a horizontal tail. When ascending, descending or hovering, it returns to the narrow long rod state, and unfolds into a large area when needed. The pull rod, pull wire, motor cylinder, etc. that control its workmanship are connected to the four-way pedals or the balance steering wheel in the cab to control the direction.

[0024] 8. The front rudder wing is installed at the front end of the main body, or at the periphery of the upper or lower part of the main body, and is called the front rudder wing. The front rudder wing is in a triangular cone shape, with the front end tip facing the front of the main body and having three faces. The rear end is larger than the front end tip and is also triangular. The length and width are determined according to the needs, or the front rudder wing is made into a cone or an oblate cone, or the rear end section is a triangular hub frame. The triangular hub frame is a combination in the middle, and the enclosure and construction area are empty for ventilation. The front end tip faces the front of the main body, and the oblate cone has an olive-shaped cross section. The front end tip is broken into two sections, and the rear end section is made into a hollow circular hole. A telescopic transmission shaft, or motor wires, etc. are inserted into the circular hole. Two or more blades embedded in the rear end section are installed on the front end tip section. When in use, the front end tip section is pushed forward, and the blades are spread open by a connecting rod, or the blades are directly rotated after being pushed forward and thrown away by centrifugal force. A horizontal axis is installed at the rear end of the rear section of the front rudder wing, and a vertical axis is installed on the main body. The lower end of the vertical axis does not rotate, and the upper end is equipped with a connecting arm that rotates and is installed with the horizontal axis using a bearing. An annular gear plate is installed on the non-rotating vertical axis, and a motor is installed on the rotating vertical axis. The motor gear meshes with the teeth of the annular gear plate. A connecting arm is extended from the rear end of the rear section of the front rudder wing. The connecting arm connects the pull rod, the lever, and the lever connects the rack, the motor, the electric cylinder, the oil cylinder, etc. to control the up and down or left and right swing. The three faces of the triangular cone or the three faces are concave, and one of the edges is directly above or directly below the plane of the main body. The strips are drawn out according to the shape to make vertical left and right direction wings. The left and right edges are drawn out according to the shape on the planes on both sides of the main body plane to make up and down direction wings, which can swing up and down or left and right to control the flight attitude. The front end of the triangular cone front rudder wing is an equilateral triangle, and the left and right strips do not need to be equilateral at the position where the strips are drawn out, or the left and right strips are not drawn out at the continuation angle of the equilateral, or the left and right strips are drawn out at the continuation angle of the equilateral. The three surfaces of the triangular cone front rudder wing are made concave, like a triangular scraper, or the front tip is broken and divided into two sections, and the rear section is made into a hollow circular hole, or a triangular hub frame is used to insert a telescopic transmission shaft or a motor wire into the circular hole, and three or more root folding propeller blades are installed on the front tip section, close to the groove of the triangular cone front rudder wing, and a pocket groove, a card slot, a card rod, etc. are set at the groove and the blade tip. When folding, the blade tip is inserted into the card slot. When in use, the front tip section is pushed forward, like an umbrella, and the blade is opened by a connecting rod, or it is pushed forward and directly rotated to use centrifugal force to throw the blade away. The directional wing drawn out or the wind-holding wing is used. It is used as a backup for emergency use. The wind-holding tail wing is installed behind the main body, and the front rudder wing is controlled by a balanced steering wheel, and the rear wind-holding wing is controlled by a four-way pedal. When the front rudder wing is installed above the cab, it blocks the sun and rain, and the front rudder wing reacts faster to the main body direction strain during flight.

[0025] The parts and composition of the orbiting propeller-wing orbiting group non-rotating main shaft helicopter, its overall layout is, using the orbiting propeller propeller several blades, symmetrically installed on the orbiting propeller disk, the orbiting propeller disk rotation center is installed on the upper end of the non-rotating main shaft by means of a bearing, the non-rotating main shaft is made hollow, a coupling is installed at the position of the lower orbiting propeller disk, the coupling is installed on the orbiting propeller disk or the bearing sleeve, an outer coupling shaft tube is used to insert into the non-rotating main shaft and install it together with the coupling, an annular gear ring is installed on the outer coupling shaft tube in the outer casing of the propeller non-rotating main shaft, etc., which transmits to each other with the motor installed on the outer casing, a lifting and telescopic shaft is inserted into the hollow non-rotating main shaft, the two ends of the lifting and telescopic shaft protrude a certain distance from the two ends of the non-rotating main shaft, a pitch disc is installed at the segmented propeller end of the lifting and telescopic shaft, there are several blades Install several pitch disc connecting rods to connect with the pitch arm of the blade, use the synchronous connecting rod to rotate together with the orbiting propeller disc, and use levers, pull rods, gears, etc. to converge the lifting and telescopic shaft of each orbiting propeller in the orbiting propeller disc at the coaxial position at the other end of the lifting and telescopic shaft. Use the pitch disc, motor, etc. to synchronously handle the pitch change of multiple propeller blades at the same time, and use the propeller non-rotating main shaft housing to install it on the stress transfer orbiting hub, pass the wires used at the orbiting propeller end through the hollow stress transfer orbiting hub, and install the stress transfer orbiting hub on the orbiting propeller disc. Install a metal conductive device or a liquid conductive device at the orbiting propeller disc cavity position on the electrical coaxial axis, connect the orbiting propeller end wires to the conductive device wires, and install bearings and bearing sleeves at the corresponding positions of the orbiting propeller disc on the coaxial axis. , the wire of the conductive device is led to the lower end by the drilled hollow electric coaxial shaft, and a shaft tube with a groove is inserted into the hollow electric coaxial shaft, the revolving propeller disc is installed on the bearing sleeve, and a coupling and other soft connections are installed on the bearing sleeve. The coupling is further extended by a section of external coupling shaft tube, and an annular gear ring is installed on the external coupling shaft tube. The transverse shaft is symmetrically installed on the coaxial shaft, and a rotatable gear is installed on the transverse shaft. The lower annular gear ring is installed, and the upper and lower annular gear rings are meshed with the gears on the transverse shaft. The lower wing revolving group is installed in the same way as the upper wing revolving group. The lower annular gear ring leads out a section of external coupling shaft tube, or the lower annular gear ring is directly installed on the upper bearing sleeve of the lower revolving propeller disc, and a section of external coupling shaft tube is installed on the lower layer of the lower revolving propeller disc, or a coupling and other soft connections are installed, and the bearings and shafts installed on the main body are installed on the external coupling shaft tube. A bearing sleeve, or a wing revolution group is coaxially installed above the middle long arm of a "U"-shaped helicopter or above the middle main body of a "turban"-shaped helicopter, and the bearing sleeve is used to install it on the main body, and a driving gear plate is installed on the outer coupling shaft tube. The driving gear plate and the power output shaft teeth transmit each other, and the forward propulsion revolution group is installed on the main body on both sides of the "U"-shaped or "turban"-shaped body, or a main body arranged in a plane such as a "V"-shaped body or an oblate circular ring is used, or a "U"-shaped upper and lower structural main body is laid down, or the upper and lower main body structure is used to install the left and right side main bodies, and a helicopter with left and right multi-layer upper and lower structural bodies, and the non-rotating main shaft is installed together with the main body, and the bearing sleeve is connected to the connecting rod of the main body connected to the outer coupling shaft tube to form the reciprocating swing of the universal joint cross axis, or a tilt arm is installed at the coaxial installation position,The other end of the tilt arm is installed on the helicopter body, so that the orbiting rotor blade orbiting helicopter can realize backward tilting, and become an orbiting rotor blade orbiting helicopter with backward tilting. Or use the tilt arm to tilt the jet engine, and tilt the jet engine from the tail nozzle downward to the tail nozzle facing backward, and become a backward tilting jet engine helicopter. Plastic main body shell, install front rudder wing, wind-holding wing and wind-holding tail wing, connect the wires led out of the generator or battery and the wires led out of the coaxial line accordingly, and then pull it to the cab, and connect it to the accelerator pedal, four-way pedal, sensing lifting wheel, balance steering wheel, etc., and install the landing gear.

[0026] A helicopter with a tilting rotor group of revolving paddles, which applies the parts required for a helicopter with a non-rotating main shaft of a revolving paddle rotor group, and derives a new tilting method, required parts and required main body shapes. The tilting method is that the installation part of the wing revolving group is above, the propeller blades flap downwards, the single-wing revolving group or the coaxial-wing revolving group is installed at the installation end of the tilting arm, the tilting arm is above the main body, the single-wing revolving group or the coaxial-wing revolving group is arranged in the middle part of the main body or at the ends of both sides of the main body. The rotation of the wing revolving group lifts the helicopter main body, the tilting arm tilts the single-wing revolving group or the coaxial-wing revolving group to point to the rear of the helicopter main body, and the backward flapping of the wing revolving group pushes the main body forward to fly. When taking off and landing, it returns to flap downwards. The helicopter main body is made into a "V" shape, a "U" shape, an oblong ring shape, or a "towel" shape. The two sides of the "U" shape main body extend backward, and the main body is arranged in a plane. Or the "U" shape is laid down to form an upper and lower structure main body. The upper main body of the upper and lower structure main body is shorter, and the lower main body is longer. Or the upper main body is longer and the lower main body is shorter. Or the left and right side main bodies are installed on the upper and lower main body structures, and the left and right multi-layer upper and lower structure main bodies. When viewed from the front of the helicopter main body, it is in the shape of an inverted "T", or a "worker" shape, or a "soil" shape, or a "dry" shape, or a "king" shape, or a "abundant" shape, etc. The two side main bodies extend backward. When viewed from both sides of the helicopter main body, the upper main body is short and the lower main body is long, or the lower main body is short and the upper main body is long, or the middle main body is short and the upper and lower main bodies are long, or the upper and lower main bodies are short and the middle main body is long, or the upper and lower main bodies are of the same length. The front end of the main body is in a shape that reduces wind resistance. Install inclined long arms on the outer periphery of both side main bodies or on the outer periphery of the center of the front of the main body upward and backward. Install one or more or multiple sections of long arms, or multiple sections of robotic arms. The inclined direction of the long arms is the same inclined direction or one or more of the other long arms are inclined in the opposite direction. It is called the tilting arm. The tilting arm is in the shape of a triangular support. When viewed from the left or right of the helicopter main body, the tilting arm is in the shape of a "factory" character. When viewed from the front of the helicopter main body, the tilting arm is in the shape of a "chuan" character, a "door" character, or a "claw" character. One or more of the tilting arms are made hollow. The outer shape of the tilting arm uses a shape that reduces wind resistance. The cross-section of the tilting arm is in the shape of an olive, a circle, a semi-circle, a flat rhombus, etc. Set one or more as the active arms, and the others as the driven arms. The connection between the tilting arm and the main body is called the installation end, and it is installed by using a bearing or a gear installation method that can swing up and down. Use an electric cylinder, an oil cylinder, a motor, a gear, a lever, a pull rod, etc. to make the active arm swing up and down. The connection between the tilting arm and the single-wing revolving group or the coaxial-wing revolving group is called the end. Or use a rope, a pull rod and a material with high pulling strength to pull and reinforce it from the installation end of the tilting arm to the end. Or install one or more pull rods on the tilting arm at the installation end, which is in the shape of a cross with the tilting arm. Pull ropes on both ends of the cross pull rod and the tilting arm. Or install an electric cylinder, an oil cylinder, etc. at one end of the cross pull rod.The tilt arm can be extended and retracted by using a telescopic section, or the tilt arm can be moved forward and backward or bent and extended at the main body installation end, or the end of the tilt arm and the coaxial connection can be rotated, or the left and right sides of the main body can swing up and down, or the wings can be formed to pull the tilt arm. Using a tilt arm to tilt backward, the tilt arm can be installed on the long arm using a lever pull rod. When the long arm swings, the deformation of the two at the end installation point is used to tilt the coaxial wing orbital group downward and backward, or a tilt arm section is installed at the end of the tilt arm using a bearing and a horizontal axis, which is called a second section of the tilt arm. The second section of the tilt arm is bent at a right angle, or an obtuse angle or an acute angle to the front or rear of the main body, and a single-wing orbital group or a coaxial wing orbital group is installed at its end. The coaxial wing revolution group can be installed by various methods by using the coaxiality between the upper and lower wing revolution groups and the end of the tilt arm, or by using three tilt arms, one of which is installed on the outer periphery of the front center of the front main body upward, and the other two tilt arms are installed on the outer periphery of the main body on both sides upward, and the distance difference between the tilt arm and the installation point of the longitudinal axis of the main body is used, that is, one is installed at the front end of the main body and two are installed in the middle part, or two are installed at the front end of the main body and one is installed in the middle part of the main body. By using the misalignment difference of the coaxial installation point at the end of the tilt arm when the tilt arm swings up and down, the single-wing revolution group or the coaxial wing revolution group installed at the end of the tilt arm is tilted from fluttering in the downward direction to fluttering in the rear direction, or the tilt arm in the middle part is installed on the outer periphery of the middle part of the main body and tilted backward and upward, and the tilt arms on the two main bodies are installed on the outer periphery of the rear end of the two main bodies, and are fixed or tilted forward and upward and swing up and down, so that the balance will be better. A transverse symmetry axis is installed on the bearing sleeve at the driving gear disc end of the coaxial drive, and the transverse symmetry axis is installed together with the ends of the tilting arms on both sides by means of bearings. An up-and-down moving position block is set at the installation place of the tilting arm and the main body to control the swing angle required for the tilting arm to rise and fall. An up-and-down angle block is also set at the installation place of the middle tilting arm and the non-rotating axis, and an angle stopper plate or a shaping plug plate is installed. There is transverse symmetry axis control on the left and right, and there is also transverse axis stability at the connection between the coaxial and the tilting arm, or another section of the tilting arm is installed at the end of the middle tilting arm, and a symmetrical transverse axis is installed in the middle part of the second section of the tilting arm. The ends of the tilting arms on both sides are installed with bearings and the transverse axis. A single-wing orbital group or a coaxial wing orbital group is installed on the end. When the middle tilt arm moves downward, the tilt arms on both sides also descend accordingly, causing the coaxis to tilt. The middle active arm continues to descend so that the wing orbital group coaxially points to the rear tail of the helicopter. Before takeoff or landing, the active arm is raised to point the wing orbital group coaxially downward. The middle tilt arm is installed tilted upward and backward, and the tilt arms on both sides are installed tilted upward and forward. The ends of the tilt arms on both sides are installed together with the non-rotating main shaft by means of bearings and transverse axes. The end of the middle tilt arm is divided into two forks and is concave in an upward semicircle, or the ends of the two tilt arms are installed together with the transverse symmetry axes installed on both sides of the bearing sleeve by means of bearings.The "towel" - shaped main body is arranged in a plane. The middle main body can be shorter and made into a shape that reduces wind resistance, while the two side "U" - shaped main bodies are longer. A long arm that slopes backward and upward is installed above or below the periphery of the middle main body. Or the tilting arm in the middle is the driving arm and the tilting arms on both sides are the driven arms, or the tilting arms on both sides are the driving arms and the tilting arm in the middle is the driven arm. Or the middle main body is long and the main bodies on the left and right sides are short, and tilting arms are installed on the periphery or at the ends of the main bodies extending backward on the left and right sides. On the tilting arms, a single - wing revolution group or a co - axial wing revolution group with a non - rotating main shaft that flaps the wind downward is installed. When the tilting arms are installed on the upper - layer main body or the lower - layer main body, or the upper and lower - layer main bodies are installed with tilting arms in an interactive manner, or an over - frame - shaft type tilting device is installed at the end of the tilting arm. For a three - layer or more - layer main - body structure (a three - layer structure uses the two outer layers and the ends to install tilting arms and wing revolution groups). The upper and lower layers where the wing revolution groups are installed are pulled apart by a certain distance front - to - back, which is easy to achieve front - to - back balance. The single - wing revolution group and the tilting arm are used to lift the main body and tilt it backward, and move forward. Or a transmission shaft is installed in the cavity of the tilting arm and is in contact with a driving gear disc or a disc, a wheel, etc. to implement transmission. The blades of the wing revolution group flap the wind downward, the helicopter main body is lifted, and the wing revolution group is tilted backward by the downward movement of the tilting arm to move the helicopter main body forward in flight. When installing the left and right side main bodies on the upper and lower main - body structure, and on the left - right multi - layer upper - lower - structure main bodies, the single - wing revolution group or the co - axial revolution group is installed at the end of the tilting arm, and is installed at a position where the helicopter main body can be balanced when lifted by the rotating wing revolution group. All tilting arms do not tilt simultaneously. First, one group or multiple groups tilt, and then all tilt backward after the lifting speed is increased. Or the middle part between the upper and lower co - axial electric wing revolution groups is connected to the end of the tilting arm, and a motor is installed on the horizontal axis part of the co - axial electric system. The horizontal axis is made hollow, and wires enter the hollow hole of the horizontal axis. The horizontal axis is used as the tilting axis, or is connected to the end of the tilting arm of the left and right side main bodies, or the ends of one or more tilting arms are connected to a horizontal transverse axis, and the ends of the other one or more tilting arms are connected to a vertical transverse axis. Or tilting arms are installed on the outer coupling pipe between the upper and lower revolution paddle discs. The ends of one or more tilting arms are connected between the upper and lower revolution paddle discs, and the ends of the other one or more tilting arms are connected to one end of the non - rotating co - axial system. Wings that expand to both sides are installed on the two - side main bodies of the helicopter. The wing revolution group expands when tilting and clings to or is embedded in the two - side main bodies during take - off or landing. In the cab, a fan - shaped swinging push - pull rod is used to operate the tilting arm. When the revolution paddle wing revolution group tilts the helicopter backward, the main body is lifted, and there are multiple - point connections and connections with non - rotating main shafts between the main body and the revolution group, unlike traditional helicopters that use rotors to lift the main body, so it is safer. The compressed air flow is at the rear end, without the obstruction of the main body, and the flight speed is faster.

[0027] Revolving paddle wing revolving group rear-tilting helicopter. Its overall layout is that it is better to use a "towel" - shaped main body. Install tilting arms and single - wing revolving groups on both side main bodies. Secondly, install the left - and - right side main bodies and the left - and - right multi - layer up - and - down structure main bodies with the up - and - down main body structure. A single - wing revolving group or a co - axial wing revolving group can be installed on both side main bodies and the middle main body. Install the revolving paddle propeller blades on the revolving paddle disk and at the upper end of the non - rotating main shaft in a way that the blades flap the wind in the opposite direction, and then install them on the stress - transferring revolving paddle hub. Pass the wires used at the end of the revolving paddle propeller through the hollow stress - transferring revolving paddle hub. The stress - transferring revolving paddle hub is installed on the revolving paddle disk. Install a metal conductive device or a liquid conductive device at the cavity position of the co - axial revolving paddle disk. Connect the wires at the end of the revolving paddle propeller to the wires of the conductive device correspondingly. Install bearings and bearing outer sleeves at the corresponding positions of the co - axial revolving paddle disk. Lead the wires of the conductive device downward through the hollow co - axial with holes. Thread a grooved shaft tube into the hollow co - axial. Install the revolving paddle disk on the bearing outer sleeve. Install flexible connections such as couplings on the bearing outer sleeve. Extend a section of shaft tube from the coupling. Install an upper annular gear ring on the shaft tube. Install horizontal shafts symmetrically on the co - axis. Install rotatable gears on the horizontal shafts. Install a lower annular gear ring. The upper and lower annular gear rings mesh with the gears on the horizontal shafts. Install the lower - wing revolving group in the same way as the upper - wing revolving group. Lead a section of shaft tube from the lower annular gear ring, or directly install the lower annular gear ring on the upper - layer bearing outer sleeve of the lower revolving paddle disk. Install a section of shaft tube on the lower layer of the lower revolving paddle disk, or install flexible connections such as couplings. Install bearings and bearing outer sleeves on the shaft tube that are installed on the tilting arms. Point the co - axial wing revolving group downward. Install symmetric horizontal shafts on the bearing outer sleeve. Connect the horizontal shafts and the tilting arms together with bearings. Install a driving gear disk on the shaft tube. The driving gear disk and the power output shaft teeth drive each other. Install a hollow perforated horizontal shaft on the non - rotating main shaft, and then install it together with the hollow perforated tilting arm using bearings. Mold the main body shell. Install a front rudder wing at the front end of the main body. Install wind - catching wings and wind - catching tail wings. Pull the wires led upward inside the co - axis through the hollow - perforated horizontal shaft and the tilting arm into the main body. Connect the wires led out from the generator or battery and the wires led out from the co - axis correspondingly, and then pull them to the cab, and connect them correspondingly to the accelerator pedal, four - way pedal, sensing lifting wheel, balance steering wheel, fan - shaped swinging push - pull rod, etc. Install landing gears.

Claims

1. The parts and composition of the orbiting propeller-wing orbiting group non-rotating main shaft helicopter, whose main features are that several blades of the orbiting propeller are symmetrically installed on the orbiting propeller disc, the rotation center of the orbiting propeller disc is installed on the upper end of the non-rotating main shaft by means of a bearing, the non-rotating main shaft is made hollow, a coupling is installed at the position of the lower orbiting propeller disc, the coupling is installed on the orbiting propeller disc or the bearing sleeve, an outer coupling shaft tube is inserted into the non-rotating main shaft and installed together with the coupling, an annular gear ring is installed on the outer coupling shaft tube in the propeller non-rotating main shaft housing, etc., which transmits mutually with the motor installed on the housing, the orbiting propeller non-rotating main shaft housing is installed on the stress transfer orbiting propeller hub, and the wires used at the orbiting propeller end are passed through the hollow stress transfer orbiting propeller hub. The hub and stress transfer orbiting hub are installed on the orbiting propeller disc, and a metal conductive device or a liquid conductive device is installed at the cavity position of the orbiting propeller disc on the electrical coaxial shaft. The propeller end wire is connected to the conductive device wire, and the bearing and bearing sleeve are installed at the corresponding position of the orbiting propeller disc on the coaxial shaft. The wire of the conductive device is led to the lower end by the drilled hollow coaxial shaft, and a shaft tube with grooves is inserted into the hollow electrical coaxial shaft, and the orbiting propeller disc is installed on the bearing sleeve, and a coupling and other soft connections are installed on the bearing sleeve or the orbiting propeller disc, and an external coupling shaft tube is installed on the coupling, and an annular gear ring is installed on the external coupling shaft tube, and a transverse shaft is symmetrically installed on the coaxial shaft, and a rotatable gear is installed on the transverse shaft, and a lower annular gear ring is installed, and the upper and lower annular gear rings are meshed with the gears on the transverse shaft. The lower wing revolution group is installed in the same way as the upper wing revolution group, and a section of external coupling shaft tube is led out from the lower annular gear ring, or the lower annular gear ring is directly installed on the upper bearing sleeve or revolution blade disc of the lower revolution blade disc, and a section of external coupling shaft tube is installed on the lower layer of the lower revolution blade disc, or a soft connection such as a coupling is installed, and the bearing and bearing sleeve installed on the main body are installed on the external coupling shaft tube, or the wing revolution group is coaxially installed above the middle long arm of the "U"-shaped helicopter or above the middle main body of the "turban"-shaped helicopter, and is installed on the main body by using the bearing sleeve, and a driving gear disc is installed on the external coupling shaft tube, and the driving gear disc and the power output shaft gear are mutually transmitted, and the forward propulsion revolution group is installed on the main bodies on both sides of the "U"-shaped or "turban"-shaped body, or a "V"-shaped main body or an oblate long circular ring and other plane arrangements are applied. The main body, or the upper and lower structure main body of the "U" shape is laid down, or the upper and lower main body structure is used to install the left and right side main bodies, and the helicopter with multiple layers of upper and lower structure main bodies on the left and right sides, and the coaxial body is installed together, the bearing sleeve and the connecting rod connected to the main body with the outer connecting shaft tube form the reciprocating swing of the universal joint cross axis, or a tilt arm is installed at the installation position of the coaxial, and the other end of the tilt arm is installed on the helicopter main body, so that the orbiting rotor blade orbiting group helicopter can be tilted backward, or the tilt arm is used to tilt the jet engine, and the jet engine is tilted from the tail nozzle downward to the tail nozzle facing backward, and the front rudder wing is installed, and the forward propulsion orbiting group is installed at the rear of the main body, and the wind-holding wing and the wind-holding tail wing are installed, and the wires led out of the generator or battery and the wires led out of the coaxial are connected accordingly.

2. The orbiting propeller-wing orbiting group non-rotating main shaft helicopter parts and structure as described in claim 1, its main characteristics are that the orbiting propeller is symmetrically mounted on the orbiting propeller disc by using several propeller blades, the rotation center of the orbiting propeller disc is mounted on the upper end of the non-rotating main shaft by using bearings, or several segmented propeller blades are symmetrically mounted on the orbiting propeller disc, the rotation center of the orbiting propeller disc is mounted on the upper end of the non-rotating main shaft by using bearings, the non-rotating main shaft is made hollow, a coupling is installed at the position of the lower orbiting propeller disc, the coupling is installed on the orbiting propeller disc or the bearing sleeve, a round shaft tube is inserted into the non-rotating main shaft and installed together with the coupling, a driving gear ring or a pulley or a sprocket or a planetary reduction gear, etc. is installed on the outer coupling shaft tube in the outer shell of the propeller non-rotating main shaft, and a gear ring or a pulley or a sprocket or a planetary reduction gear, etc. are installed on the outer coupling shaft tube in the outer shell of the propeller non-rotating main shaft, and a gear ring or a pulley or a sprocket or a planetary reduction gear, etc. are installed on the outer coupling shaft tube The motors on the propellers transmit each other, and the lifting and telescopic shaft is inserted into the hollow non-rotating main shaft, which rotates together with the orbiting propeller disc or the bearing sleeve or the outer connecting shaft tube through a synchronous connecting rod. A motor is installed at the other end of the lifting and telescopic shaft to perform the lifting and telescopic action, or the lifting and telescopic shaft of each propeller is converged in the orbiting propeller disc at the coaxial position by levers, pull rods, gears, etc., and the pitch change of multiple propeller blades is synchronously processed by using a pitch disc, a motor, etc. The outer shell of the propeller non-rotating main shaft is installed on the stress transfer orbiting hub, and the propellers of the wing orbiting group in the upper and lower arrangement are installed above the stress transfer orbiting hubs of the upper and lower wing orbiting groups, or the propellers of the upper wing orbiting group are installed above the stress transfer orbiting hub, and the propellers of the lower wing orbiting group are installed below the stress transfer orbiting hub. The section from the blade mounting end to the section with lift or wind-flapping angle, which has a downward bending angle and gradually widens, is the blade lift section. A traditional flat blade or lift blade can be used. The flat section that does not bend downward at the other end of the propeller blade mounting end is the blade tip section, or the windward surface of the blade tip section can be gradually transformed into a flat rectangular strip. The width and length are based on actual needs. The windward surface of the flat rectangular strip can be serrated, or a polygonal strip, or slightly inclined, etc. The cutoff point of the blade tip section can also be square, rectangular, gradually flat rectangular, etc. The angle formed by the windward surface of the blade tip section and the two sides of the cutoff surface of the blade tip section is a solid angle. They are all flat rectangular strips when connected together using right angles, obtuse angles, acute angles, or circular arcs, or the propeller blades can be The overall windward surface should be in the shape of a flat rectangular strip, and the propeller blades should be divided into two sections. One or more shafts should be inserted into the lift section of the blade. The shaft is connected to the tip section of the blade and the tip section of the blade is fixed. The blades on the lift section of the shaft can swing up and down with variable pitch. The blade shaft should be installed on the propeller revolving disk with a round shaft or a flat shaft with holes at the installation end. The joints between the lift section of the blade and the tip section of the blade should be positively joined, or obliquely joined, or softly joined. Positive joining is to divide the lift section and the tip section of the blade into two sections at a right angle to the long blade. Oblique joining is to divide the lift section and the tip section of the blade into two sections at an oblique angle of an acute or obtuse angle to the long blade. Positive joining should be used at the variable pitch swing axis. Softly joined joints are made by stretching, retracting,The bending and returning material is used to connect the lift section of the blade and the tip section of the blade, or the blade shaft is used as the windward side of the blade, the tip section of the blade and the windward blade shaft are initially integrated, the lift section of the blade is installed behind the windward blade shaft with a shaft and a bearing, or the windward blade shaft and the lift section of the blade are connected to each other by a hinge or chain, and a pitch change arm is installed on the shaft of the lift section of the blade or on the blade, so that the lift section of the blade can Up and down variable pitch swing, or make the blade tip section and the windward blade shaft also have a swing amount, at the border of the blade lift section and the blade tip section or the border of the variable pitch swing shaft of the blade lift section and the windward blade shaft, use gears, pull rods, pull wires, etc. to transmit to each other, or separate the shaft connected to the blade tip section and the variable pitch swing shaft of the blade lift section and control them individually, when the windward side of the blade lift section changes pitch upward, the windward side of the blade tip section changes pitch downward.

3. The non-rotating main shaft helicopter parts and structure of the orbiting propeller-wing orbiting group as described in claim 1 are mainly characterized in that the non-rotating main shaft and the electrical coaxiality are used, and a non-rotating main shaft or hollow shaft tube is used to install the orbiting propeller disc of the upper wing orbiting group on the upper end of the main shaft by using a bearing, and the orbiting propeller disc of the lower wing orbiting group is installed on the lower end of the main shaft by using a bearing, and one or more transverse axes are installed on the non-rotating coaxial between the upper and lower orbiting propeller discs, and the transverse axis and the coaxial axis are in a right-angle plane or multiple symmetrical installations, and a rotatable gear is installed on the transverse axis, and an external connecting shaft tube is installed downwardly on the coaxial periphery of the lower orbiting propeller disc of the upper wing orbiting group, and the external connecting shaft tube or the coupling and other soft connections are interconnected with the orbiting propeller disc or the orbiting propeller disc bearing sleeve, and an annular gear ring is installed on the external connecting shaft tube, or on the lower orbiting propeller disc of the upper wing orbiting group Or directly install the annular gear ring on the bearing sleeve, or install the annular gear ring on the lower orbiting propeller disc of the upper wing orbiting group or the bearing sleeve by using a connecting rod, the annular gear ring of the lower orbiting propeller disc of the upper wing orbiting group meshes with the upper part of the gear on the horizontal shaft, the upper orbiting propeller disc of the lower wing orbiting group is installed with an outer coupling shaft tube and a coupling upward on the outer periphery of the non-rotating coaxial, and the annular gear ring is installed on the outer coupling shaft tube, or directly install the annular gear ring on the upper orbiting propeller disc of the lower wing orbiting group, or install the annular gear ring on the orbiting propeller disc or the bearing sleeve by using a connecting rod, the annular gear ring of the upper orbiting propeller disc of the lower wing orbiting group meshes with the lower part of the gear on the horizontal shaft, the outer coupling shaft tube is installed downward on the outer periphery of the non-rotating coaxial under the lower orbiting propeller disc of the lower wing orbiting group by using a bearing, and the driving gear disc is installed on the outer coupling shaft tube, or the driving gear disc is directly installed Below the lower orbiting propeller disc, a driving gear disc is transmitted or meshed with a wheel or gear for power output by means of a pulley, a chain wheel, etc., or one of the horizontal shafts is made into a transmission shaft, and a driving gear disc is installed at the other end of the transmission shaft, or it is made into a tilting horizontal shaft, or the horizontal shaft is erected to form a vertical shaft, and non-rotating gears are installed at both ends. The vertical shaft is installed on the periphery of the non-rotating main shaft, and the gear at one end of the vertical shaft meshes with the outer ring teeth of one of the upper and lower annular gear rings, and the gear at the other end of the vertical shaft meshes with the inner ring teeth of the other annular gear ring. The vertical shaft may use a universal joint, a telescopic joint, etc. to make the upper and lower wing orbiting groups rotate in the forward and reverse directions, or multiple folding-type synchronous connecting rods are used to connect the upper and lower orbiting propeller discs with the annular gear rings, and the synchronous connecting rods are supported by springs, or the upper or lower orbiting propeller discs are connected with the extended external connecting shaft tube , connect the annular gear ring of one of the parties, or use a coaxial ball cage, or a coaxial spring, or a coaxial upper and lower meshing gear ring, or use a groove toothing method, or various couplings and other soft connections, connect between the outer coupling shaft tube and the upper or lower revolving propeller disc or the revolving propeller disc bearing sleeve, use a non-rotating hollow shaft tube, install the driving gear disc or the annular gear ring of the inner ring teeth on the upper wing revolving group The revolving propeller disc or the initial integrated stress transfer revolving hub rotation center area, install a motor inside or outside the upper end of the hollow non-rotating shaft tube, or use a planetary reduction device to rotate the upper wing revolving group and drive the lower wing revolving group to rotate in the opposite direction, or install the driving gear disc in one of the revolving propeller disc cavities, and use an intermediate transmission device to rotate the upper and lower wing revolving groups in the forward and reverse directions,Or use two drive gear discs installed inside or outside the upper and lower orbiting propeller disc cavities, and install upper and lower motors on a non-rotating hollow shaft to drive the upper and lower drive gear discs, or install a motor on the horizontal shaft to drive the gears on the horizontal shaft or directly drive the upper and lower annular gear rings to drive the upper and lower wing orbiting groups to rotate in the opposite direction, or use a planetary gear reduction device on the horizontal shaft, and lead the rotating wires at the propeller end to the non-rotating hollow electric coaxial shaft, and drill holes on the electric coaxial shaft inside or outside the orbiting propeller disc cavity. Drill as many holes as needed for the wires, or insert another shaft tube or a shaft tube with grooves on the outer wall or multiple wire grooves or multiple thin shaft tubes, or a coaxial shaft tube The inner wall of the shaft tube is made with multiple wire grooves, or the outer wall of the coaxial shaft tube is made into a groove to insert the wire round tube, or the inner shaft tube is an oblate ring shaft tube with a hole, and the round hole of the oblate ring can be inserted into the wire, and the wire is introduced into the lower body. The lower layer of the lower wing revolution group is installed downward with the bearing on the outer connecting shaft tube installed with the bearing, and the bearing sleeve is installed on the helicopter body, and then the non-rotating coaxial is installed on the body with the connecting rod. The bearing sleeve and the connecting rod connected to the non-rotating coaxial body derive the tilt arm, and the revolution blade wing revolution group is derived to tilt the helicopter, and the non-rotating coaxial or artificial active bending and return to the desired direction.

4. The orbiting propeller-wing orbiting group non-rotating main shaft helicopter parts and structure as described in claim 1, its main feature is that the orbiting propeller disc, the orbiting propeller propeller blades are symmetrically installed on the orbiting propeller disc, or one or more layers of discs or connecting rods are installed at the coaxial ends of the roots of multiple stress transfer orbiting hubs, the discs or connecting rods are connected at multiple points of extension and shortening on the stress transfer orbiting hub or the transmission shaft, or the inner and outer layers or the upper and lower layers are interconnected again, etc., to fix the stress transfer orbiting hub and the transmission shaft, the rotation center of the orbiting propeller disc is directly installed on the rotating coaxial axis and rotates with the coaxial axis, or the rotation center of the orbiting propeller disc is installed on the non-rotating coaxial axis or the main shaft using a bearing, and the rotating part installed on the orbiting propeller disc can be on the non-rotating coaxial axis. The revolving propeller disk rotates on the axis or the main axis, and when the revolving propeller disk rotates on the coaxial axis or the main axis, the upper or lower part of the cross-section of the coaxial axis is triangular, or the upper or lower part is concave semicircular, etc. The revolving propeller disk is installed on the upper and lower surfaces of each stress transfer revolving propeller hub connected to the propeller of each revolving group, or the revolving propeller disk is installed on only one side, and a cavity is formed between the revolving propeller disk and the coaxial axis, or one or more layers of flat discs or pull rods are applied in the cavity, and each group of stress transfer revolving propeller hubs and the transmission shaft or the outer edge of the revolving propeller disk are pulled to the coaxial axis in a straight line, or pulled in a plane to the outer sleeve of the bearing installed on the coaxial axis, and the revolving propeller disk is installed with the stress transfer revolving propeller hub and the transmission shaft by using a connecting rod weaving method or an oblique pulling method.

5. The non-rotating main shaft helicopter parts and structure of the orbiting blade group according to claim 1 are mainly characterized in that the metal conductive device is installed on the coaxial inside or outside the cavity of the orbiting blade disk of the wing orbiting group by using a conductive metal ring, and is coaxially installed in a plane at right angles to the coaxial axis, the conductive metal ring is installed at the corresponding position of the orbiting blade disk or the cavity of the orbiting blade disk by using the outer wall of the ring, or is installed on the coaxial by using a disk on the top or bottom of the disk, the conductive ring is made into an inner gear ring, and one or more conductive gears that match the teeth of the inner gear ring are installed in the inner gear ring, a conductive bearing is installed at the rotation center of the conductive gear, and a conductive bearing is installed on the inner wall of the conductive bearing. Install a shaft, or a hollow bearing shaft that embraces the coaxial axis and is larger than the coaxial axis diameter, and a conductive bearing that embraces the coaxial axis and is larger than the coaxial axis diameter, install a conductive connecting rod on the inner wall shaft of the bearing, or make the conductive connecting rod retractable, use springs and other elastic materials to pull or push in the same direction of rotating centrifugal force, or directly lead out wires from the bearing shaft, the other end of the connecting rod and the wires are installed at corresponding positions in the cavity of the revolving propeller disk, lead to the propeller end, and connect with the propeller end motor wire, or the other end of the connecting rod is installed with the coaxial axis, the wires are introduced into the coaxial axis, and connected with the wires at the power output end, the wires led out of the conductive ring are introduced into the coaxial axis or led to the propeller end, or in the inner ring of the conductive ring. A circle of teeth is made into a groove, and one or more flat cams that match the groove are placed in the groove, or a convex ring inside a conductive ring and a concave wheel that matches it. A conductive bearing is installed at the rotation center of the cam or the concave wheel, and a shaft is installed on the inner wall of the conductive bearing, or a hollow bearing shaft that embraces the coaxial axis and is larger than the coaxial axis diameter, and a conductive bearing that embraces the coaxial axis and is larger than the coaxial axis diameter, a conductive connecting rod or connecting arm or disc is installed on the bearing shaft, or the conductive connecting rod is made to be retractable, or a spring or other elastic material is used to pull or push in the same direction of the rotating centrifugal force, or an electric wire is directly led out from the bearing shaft, and the other end of the connecting rod and the electric wire are correspondingly arranged in the cavity of the revolving paddle disc. The conductive ring is installed at the coaxial end and led to the propeller end, or the other end of the connecting rod is installed with the coaxial shaft, the wires are led into the coaxial shaft, the wires led out of the conductive ring are led into the coaxial shaft or led to the propeller end, the conductive ring is installed in a plane at right angles to the coaxial axis and surrounds the coaxial shaft, and several holes are drilled on the coaxial shaft if several wires are needed inside or outside the cavity of the revolving propeller disk, and several groups of metal conductive devices are installed. The metal conductive devices are installed in a plane stacking ring manner with one ring inside and one ring outside, or are installed on one or more layers of flat discs inside the revolving propeller disk, or are installed in an upper and lower stacking ring manner arranged up and down inside or outside the cavity of the revolving propeller disk, or the inner wheel or gear of the conductive ring is installed at an inclined angle or upright to expand its diameter.

6. The parts and structure of the non-rotating main shaft helicopter of the orbiting propeller wing orbiting group as described in claim 1 are mainly characterized in that the liquid conductive device is used to drill holes on the hollow shaft tube in the orbiting propeller disk cavity. As many holes as the motor needs, a conductive metal or a conductive metal with anti-corrosion properties is used to make an annular thin cylindrical conductive ring, which is installed around the hollow shaft tube. If the bearing needs to be rotated or installed, the conductive ring is installed on the hollow shaft tube and connected to the power supply wire, or it rotates synchronously with the wing orbiting group and is connected to the motor wire at the propeller. Then, a conductive or non-conductive or one of the inner and outer layers of a non-conductive metal or non-metal material is used to make a circular ring or a circular tubular ring for storing conductive liquid. A circular ring, or an annular cylindrical ring with various downward or upward or arc or angle curved shapes on the lower ring surface and the upper ring surface, is installed around a hollow shaft tube. It needs to be rotated or installed with a bearing. It is a liquid ring. A conductive liquid is injected into the liquid ring. A conductive ring is inserted into the liquid ring. One or more sealing rings are installed on the outer inner wall of the upper end of the liquid ring and the inner outer wall or the inner and outer walls of the conductive ring to form a seal with the inserted conductive ring. The liquid ring is installed on the hollow shaft tube. The wires led out of the liquid ring are connected to the power wires, or the liquid ring rotates synchronously with the wing revolution group. The wires led out of the liquid ring are connected to the motor at the propeller. The wires of the motor applied to each propeller on a wing revolution group converge on the coaxial The conductive rings and liquid pocket rings are installed in the cavity of the revolving propeller disc in an up-and-down arrangement or in a flat stacking arrangement of one ring inside and one ring outside the cavity of the revolving propeller disc, or a liquid storage ring is added to automatically add and store the conductive liquid in the liquid pocket ring. A pull rod with spaced stakes is used to wrap the wires around the stakes and then pass them into the hollow stress transfer revolving hub. The pull rod is fixed and connected to the corresponding wires at the propeller end, or the wires are placed in an S shape in the hollow stress transfer revolving hub and fixed by spraying foam to solidify. The electric wire is installed on the inner section of the conductive ring inserted into the liquid pocket ring, and a circle of obliquely extended or spaced oblique strips standing on the conductive ring or grooves sunk into the conductive ring are installed around the coaxial ring. The circle of obliquely extended or spaced oblique strips standing or grooves sunk into the conductive ring are installed around the coaxial ring, which are stirring bars. The intermittent stirring bars are in the shape of forward rotation to reduce resistance, or a circle of obliquely extended or spaced oblique strips standing on the inner wall of the liquid pocket ring or grooves sunk into the liquid pocket ring are installed around the coaxial ring in the liquid pocket ring cavity, or stirring bars are installed on both the conductive ring and the liquid pocket ring, or a circular ring is installed at the lower end of the conductive ring inserted into the liquid pocket ring, and the stirring bar is installed on the circular ring.

7. The non-rotating main shaft helicopter parts and structure of the orbiting propeller-wing orbiting group as described in claim 1 are mainly characterized in that the orbiting group is propelled forward, and several propeller blades of the orbiting propeller are symmetrically installed on the orbiting propeller disc, the rotation center of the orbiting propeller disc is installed on the upper end of the non-rotating main shaft by a bearing, and is installed on the orbiting propeller disc by a coupling and an outer coupling shaft tube, an annular gear disc is installed on the outer coupling shaft tube, the propeller is rotated by a motor or a transmission shaft, and the propeller housing is installed on the stress transfer orbiting propeller hub, the stress transfer orbiting propeller hub is installed on the orbiting propeller disc, and a non-rotating annular gear ring is installed on the non-rotating coaxial axis in the orbiting propeller disc, the transmission shaft teeth are meshed with the annular gear ring, a transverse axis is installed on the coaxial axis between the upper and lower orbiting propeller discs, and the upper and lower annular gear rings and the outer coupling shaft tube are connected to the upper and lower orbiting propeller discs, a driving gear disc is installed on the lower outer coupling shaft tube of the lower orbiting propeller disc, and a The driving toothed disc is meshed with the power output gear, driving the upper and lower wing revolution groups to rotate in the positive and negative directions, laying it down horizontally, or using a propeller blade with a fixed pitch, installed at the rear end of the helicopter to propel the revolution group forward. A toothed disc of a driving toothed disc uses a pulley, a chain wheel, a toothed wheel, a planetary gear, etc., and transmits power to each other with a power output wheel or gear. The original coaxial upper and lower wing revolution groups have upper and lower driving toothed discs with reverse speed increase, or a bearing is used between the upper and lower driving toothed discs to install the horizontal axis between the coaxial upper and lower revolution propeller discs such as non-rotating, and the horizontal axis is fixed on the main body and does not rotate. The rotatable gear on the horizontal axis is meshed with the upper and lower driving toothed discs, and a power output wheel or gear is used to transmit power to each other with one of the driving toothed discs, driving the upper and lower wing revolution groups to rotate in the positive and negative directions, laying it down horizontally, or using a propeller blade with a fixed pitch, installed at the rear end of the helicopter to propel the revolution group forward.

8. The parts and structure of the orbiting rotor blade orbiting group non-rotating main axis helicopter as described in claim 1, wherein the main feature is that the fascia wing, the fascia wing of the orbiting rotor helicopter is made into one or more straight narrow and long rods, or narrow and long rods with a certain curvature according to needs, the front ridge of a narrow and long rod is a rectangular strip, a triangle, an ellipse, etc., the rod-shaped wing is opened for work when needed, and returns to the rod shape in the initial state when not needed. The fascia front wing is installed on the front side of the helicopter body, the fascia side wings are installed on both sides of the body, and the fascia tail wing is installed at the rear of the body. The opening and closing of the fascia wing is controlled by a pull rod, a pull wire or a motor, an electric cylinder, an oil cylinder, etc. The fascia tail wing is installed on the tail beam at the rear of the body or protrudes from the body shell or is extended from the end of the tail beam, or one or more fascia tail wings are installed at the tail. The wing hubs are mounted on both sides of the inner surface of the narrow rod, or the wing hubs are installed on both sides of the inner surface of the narrow rod. The wing hubs are pushed and pulled to make the wing hubs unfold in a fan shape. The length is determined according to the requirements. One end of all the wing hubs is condensed on the swing point axis of the narrow rod and installed as the root. The wing hubs and the narrow rods are connected by folding cloth of good material, or thin and hard metal or non-metallic materials are used to directly make narrow and long strip wing hubs or attach them to the wing hubs, and they are connected to each other at the top and middle with ropes, steel wires and grooves, embedded and staggered. When a narrow rod is pulled in the required direction, a fan-shaped windward surface is generated, or the narrow rod is initially fixed at the required angle and pulled. When the wing hub is moved, a fan-shaped windward surface is generated. The blades are made of thin and hard materials between the wing hub, the wing hub and the narrow long rod, and are arranged one by one in a scale-like overlapping manner. The blades are made into flat long strips, parallelograms, rhombuses, ellipses, S shapes, etc., and multiple rows of blades are axially connected to each other between the wing hub, the wing hub and the narrow long rod. A retractable wing hub is added between the wing hub and the narrow long rod and between the two. When the narrow long rod or the wing hubs on both sides are pulled, all the blades change their tilting direction at the same time. One or more integrated shaft rods are installed at the root swing point of the narrow long rod using bearings to form a right angle with the narrow long rod. One shaft rod is connected to the narrow long rod or is initially integrated with the narrow long rod, and the other or more shaft rods extend inward or outward in a "towel" shape. A narrow long rod is erected at the center of the cross to form an angle The shaft rod is used to sleeve the root of the wing hub or the bearing on the angle shaft rod. A connecting rod of corresponding length or a gear of corresponding size is installed at the root of each wing hub, or a pull rod, a pull wire, a rack, etc. are used to install and connect the rods, and the rods are fixed on the tail beam or the fixed part of the main body. When the narrow long rod is pulled, the angle shaft rod sleeved at the root of the wing hub forms a fan-shaped stroke, which automatically pulls the wing hub to one side to unfold and tilt. After the work is completed, the narrow long rod is returned to its initial state by a return spring or a push-pull rod, or the narrow long rod and the root of the wing hub are arranged separately and installed flat on the vertical axis of the "mountain" shape, and the horizontal axis is installed on the main frame, or a shaft rod is led out from the installation point of the narrow long rod and the root of the wing hub, and a directional angle slide is installed and fixed on the main frame, and the slide is installed on the wing hub, and the two points of the triangle bottom of the slide are installed obliquely on the main frame.Or install a cross lever push-pull rod, the lever is installed on the main frame, one end of the lever is connected to the root of the opposite wing hub and the other end is connected to a narrow long rod, or a directional angle push-pull rod, the narrow long rod and the wing hub swing according to the angle of the installed pull rod, or a directional angle slide groove, the narrow long rod and the wing hub use a section of shaft rod installed at the root, install a concave and convex arc angle slide groove on the main frame, or a directional angle stroke slot, the empty slots installed on the main frame have a directional angle, the narrow long rod and the wing hub are clamped in the slot, all are unidirectional or bidirectional, the middle is the expansion stroke or one end is close together and the other end is expanded, or the middle is the combined angle stroke and the two ends are the expansion angle stroke, or the two ends are the combined angle stroke and the middle is the expansion angle stroke, push and pull the narrow long rod or the wing hub or the moving device to make the wind-holding wing expand in the desired direction and return to the initial narrow long rod state, or use a rotating Work in different directions and angles, or install the tuyere wings at a certain angle and in a fixed direction, or install the fan-shaped large arc surface of the tuyere wings in the opposite direction facing the front of the main body, etc., or can be expanded or merged by pushing and pulling the wing hub, a narrow long rod can be installed in front of the main body to control up and down, and a narrow long rod can be installed at the tail to control left and right, or a narrow long rod can be used to control left and right or up and down, and the angle folding connecting rod used by the balance steering wheel can be connected with the connecting rod of the corresponding length installed at the root of each wing hub by a pull rod, etc., or multiple tuyere wings can be applied in the shape of arrow feathers, and a row of multiple tuyere wings arranged at an inclined angle can be installed on both sides or one side of the main pole, or arranged in the shape of a fork, and a row of multiple tuyere wings with one direction can be installed on a main pole using an angle folding connecting rod, and the wing hub or the narrow long rod can be pushed and pulled, or the main pole can be pushed and pulled to return to the narrow long rod state when rising, falling or hovering.

9. The components and structure of the orbiting rotor blade orbiting group non-rotating main shaft helicopter as claimed in claim 1, wherein the main features are that the front rudder wing is installed at the front end of the main body, or at the periphery of the upper or lower part of the main body, and the front rudder wing is in a triangular cone shape, with the front end tip facing the front of the main body, having three faces, and the rear end is larger than the front end tip and also in a triangular shape, and the length and width are determined according to the needs, or the front rudder wing is made into a cone or an oblate cone, or the rear end section is a triangular hub frame, the middle area of ​​the triangular hub frame is empty, the front end tip faces the front of the main body, and the oblate cone has an olive-shaped cross section, or the front end tip is broken into two sections, and the rear end section is made into A hollow circular hole is inserted into the circular hole with a telescopic transmission shaft or a motor wire, etc. Two or more blades embedded in the rear section of the rear end are installed on the front tip section. When in use, the front tip section is pushed forward, and the blades are spread open by a connecting rod, or the blades are directly rotated after being pushed forward to use centrifugal force to throw the blades away. A horizontal axis is installed at the rear end of the rear section of the front rudder wing, and a vertical axis is installed on the main body. The lower end of the vertical axis does not rotate, and the upper end is installed with a connecting arm that rotates and is installed together with the horizontal axis using a bearing. An annular gear plate is installed on the non-rotating vertical axis, and a motor is installed on the rotating vertical axis. The motor gear is meshed with the teeth of the annular gear plate. A connecting arm is extended from the rear end of the rear section of the front rudder wing, and the connecting arm is connected to the pull rod, lever, and the lever is connected to the rack, motor, electric cylinder, oil cylinder, etc. The three faces of the triangular cone are or the three faces are concave, and one of the edges is directly above or below the main plane, and the strips are drawn out according to the shape to make vertical left and right wings. The left and right edges are drawn out according to the shape on the planes on both sides of the main plane to make up and down wings. The front end of the triangular cone front rudder wing is an equilateral triangle, and the left and right strips do not need to be equilateral, or the left and right strips are not drawn out at an equilateral continuation angle, or the left and right strips are drawn out at an equilateral continuation angle. The three surfaces of the triangular cone-shaped front rudder wing are made concave, or the front end tip is disconnected and divided into two sections, and the rear end section is made into a hollow circular hole, or a triangular hub frame is used to insert a telescopic transmission shaft or motor wire into the circular hole, and three or more root folding propeller blades are installed on the front end tip section, close to the groove of the triangular cone-shaped front rudder wing, and pockets, card slots, card rods, etc. are arranged at the groove and the blade tip. The blade tip is inserted into the card slot when folding, and the front end tip section is pushed forward when in use, and the blade is spread open by a connecting rod, or the blade is directly rotated after being pushed forward and the blade is thrown away by centrifugal force, leading out a direction wing or a wind-holding wing.

10. The helicopter parts and structure of the orbiting rotor-wing orbiting group without rotating main axis as described in claim 1 are mainly characterized in that the orbiting rotor-wing orbiting group rearwardly tilts the helicopter, and the tilting method is that the installation part of the wing orbiting group is at the top, and the propeller blades flutter the wind downward, and the installation end of the single-wing orbiting group or the coaxial wing orbiting group is installed on the tilting arm, and the tilting arm is above the main body, and the single-wing orbiting group or the coaxial wing orbiting group is arranged at the middle part of the main body or the ends of the main body on both sides. The wing orbiting group rotates to lift the helicopter main body, and the tilting arm tilts the single-wing orbiting group or the coaxial wing orbiting group to point to the rear of the helicopter main body, and the wing orbiting group flutters the wind backward to push the main body forward to fly, and returns to flutter the wind downward during takeoff and landing, and the helicopter main body is made into a "V" shape or a "U" shape or a flat long circular ring, or into a "towel" shape. The main body, the main bodies on both sides of the "U"-shaped main body extend backwards, the main body plane is arranged, or the "U" shape is turned down to make an upper and lower structural main body, the upper main body of the upper and lower structural main body is shorter, and the lower main body is longer, or the upper main body is long and the lower main body is short, or the upper main body is installed on the upper and lower main body structure and the left and right side main bodies, and the left and right multi-layer upper and lower structural main bodies are visually presented in the front of the helicopter main body. The main body on both sides extends backwards, and the upper body is short and the lower body is long on both sides of the helicopter main body, or the lower body is short and the upper body is long, or the middle body is short and the upper and lower bodies are long, or the upper and lower bodies are short and the middle body is long, or the upper and lower bodies are the same length, and the main bodies on both sides are visually presented in the front of the helicopter main body. A long arm tilted upward or upward and backward on the periphery or on the periphery of the front center of the main body is installed, one or more or multi-section long arms or multi-section mechanical arms are installed, the tilting direction of the long arms is the same tilting direction or the other one or more are tilted in the opposite direction, which is a tilt arm, the tilt arm is supported in a triangular shape, the tilt arm is visually or presents a "factory" shape on the left or right side of the helicopter body, the tilt arm is visually in the shape of a "river" or a "door" or a "claw" shape in front of the helicopter body, one or more of the tilt arms are made hollow, the cross section of the tilt arm is olive-shaped, circular, semicircular, flat diamond-shaped, etc., one or more are set as active arms, and the others are driven arms. The connection between the tilt arm and the main body is the installation end, which is installed by using a bearing or a gear that allows it to swing up and down, and is installed by using an electric cylinder, an oil cylinder, or a motor. , gears, levers, pull rods, etc. enable the main arm to swing up and down, the connection between the tilt arm and the single-wing orbiting group or the coaxial wing orbiting group is the end, or ropes, pull rods and materials with high pulling strength are used from the installation end of the tilt arm to the end to pull and reinforce it, or one or more pull rods are installed on the tilt arm at the installation end, forming a cross shape with the tilt arm, etc., and ropes are pulled mutually at the two ends of the tilt arm on the cross pull rod, or electric cylinders, oil cylinders, etc. are installed on one end of the cross pull rod, the tilt arm may be extended and retracted by using the telescopic section, or the tilt arm may be able to move forward and backward or bend and retract at the main body installation end, or the end of the tilt arm may be able to rotate at the coaxial connection, or the left and right sides of the main body may swing up and down, or form a wing to pull the tilt arm, and use one tilt arm to tilt backward, the tilt arm may be installed on the long arm by using a lever pull rod,When the long arm swings, the deformation of the two at the terminal installation point is utilized to tilt the coaxial wing orbital group downward and backward, or another section of the tilt arm is installed at the terminal of the tilt arm by using bearings and transverse axes, and the second section of the tilt arm is bent in front of or backward of the main body by right angles, or by obtuse or acute angles to install a single-wing orbital group or a coaxial wing orbital group at its terminal. The coaxial wing orbital group can be installed at the terminal of the tilt arm by using the coaxial part between the upper and lower wing orbital groups, or three tilt arms are used, one of which is installed on the outer periphery of the front center of the front main body upward, and the other two tilt arms are installed on the outer peripheries of the main bodies on both sides upward, and the single-wing orbital group or the coaxial wing orbital group installed at the terminal of the tilt arm is installed by using the difference in distance between the tilt arm and the installation point on the longitudinal axis of the main body, and by using the misalignment difference of the terminal installation point when the tilt arm swings up and down. The shaft-wing revolution group is tilted from catching wind downward to catching wind backward, or the tilt arm in the middle part is installed on the periphery of the middle part of the main body and tilted backward and upward, and the tilt arms on the two sides of the main body are installed on the periphery of the rear end of the two sides of the main body, and are fixed or tilted forward and upward to swing up and down. A transverse symmetry axis is installed on the bearing sleeve at the end of the coaxial driving gear disk, and the transverse symmetry axis is installed with the ends of the tilt arms on both sides by bearings. Up and down moving position blocks are set at the installation of the tilt arm and the main body to control the swing angle required for the tilt arm to rise and fall. Up and down angle blocks are also set at the installation of the middle tilt arm and the non-rotating axis, and angle plates or shaping plugs are installed, or another section of the tilt arm is installed at the end of the middle tilt arm, and a transverse symmetry axis is installed in the middle part of the second section of the tilt arm. The single-wing orbital group or the coaxial-wing orbital group is installed on the end of the second section of the tilt arm. The middle tilt arm is installed tilted upward and backward, and the tilt arms on both sides are installed tilted forward and upward. The ends of the tilt arms on both sides are installed together with the non-rotating main shaft by bearings and the transverse symmetry axis. The end of the middle tilt arm is divided into two forks and is concave upward in a semicircle, or the ends of the two tilt arms are installed together with the transverse symmetry axes installed on both sides of the bearing sleeve by bearings. The "towel"-shaped main body is arranged in a plane. The middle main body is shorter and the "U"-shaped main bodies on both sides are longer. A long arm tilted upward and backward is installed above or below the outer periphery of the middle main body, or the middle main body is long and the main bodies on the left and right sides are short. The tilt arms are installed on the outer periphery or ends of the main bodies extending backward on the left and right sides. The upper body or the lower body is installed with a tilt arm, or the upper and lower bodies are installed with interactive tilt arms, or an over-the-axis tilt device is installed at the end of the tilt arm. The upper, middle and lower three-layer main structure or more layers, the three-layer structure uses the outer periphery and the end of the two layers to install the tilt arm and the wing revolution group, the upper and lower layers where the wing revolution group is installed are pulled apart a certain distance, or a transmission shaft is installed in the cavity of the tilt arm to connect with the driving gear plate or plate, wheel, etc. to implement transmission, and the left and right side bodies are installed on the upper and lower main structures, and the left and right multi-layer upper and lower structure bodies are installed, and a single-wing revolution group or a coaxial revolution group is installed on the end of the tilt arm, and it is installed in a position where the helicopter body is lifted by the rotating wing revolution group to maintain balance, all the tilt arms may not tilt at the same time, first tilt one or more groups, and then tilt all after the speed is increased.Or install the middle part between the upper and lower wing revolution groups of the electric coaxial with the end of the tilt arm, install the motor on the horizontal axis of the electric coaxial, make the horizontal axis hollow, and put the wire into the hollow hole of the horizontal axis, or use the horizontal axis as the tilt axis, or connect with the ends of the left and right main body tilt arms, or one or more tilt arms are connected to the horizontal horizontal axis, and another one or more are connected to the longitudinal horizontal axis, or install the tilt arm on the outer coupling shaft tube between the upper and lower revolution propeller discs, or one or more tilt arms are connected between the upper and lower revolution propeller discs, and another one or more tilt arms are connected to one end of the non-rotating coaxial, and the tilt arm is operated in the cab using a fan-shaped swing push-pull rod.

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