34results about How to "Realize air rescue" patented technology

The invention provides a zero backward thrust composite wing aircraft with ducted fan composite ailerons. The zero backward thrust composite wing aircraft with the ducted fan composite ailerons comprises an aircraft body and composite lift wings which are fixedly mounted on the two sides of the aircraft body, wherein the aircraft body is arranged as a deck platform; self-sealing ducted fans are embedded in the composite lift wings; wing hinges are designed on the external sides of the composite lift wings; ducted fan propellers are arranged at the front ends of ducted fan thrust self-energizedcomposite ailerons; the self-sealing ducted fans are arranged in the ducted fan thrust self-energized composite ailerons; electricity, liquid and gas ports and the wing hinges are arranged on one sides or two sides of the ducted fan thrust self-energized composite ailerons; and the ducted fan thrust self-energized composite ailerons are movably connected with the composite lift wings through thewing hinges. The zero backward thrust composite wing aircraft with the ducted fan composite ailerons has the characteristics that the taking-off and landing distance is short, the flying speed is high, the structural strength of the wings is high, the wings can store energy, the flying energy consumption is low, the hang time is long, the safety is high and so on; and the ailerons adopt compositelift forces to guarantee appropriate power.

The invention provides a foldable composite wing aircraft with twin-propeller thrust composite ailerons. The foldable composite wing aircraft with the twin-propeller thrust composite ailerons comprises an aircraft body and composite lift wings, wherein the composite lift wings are mounted on the two sides of the aircraft body in a foldable manner; the aircraft body is arranged as a deck platform;self-sealing ducted fans are embedded in the composite lift wings; wing hinges are designed on the external sides of the composite lift wings; propellers are arranged at the front ends of propeller thrust self-energized composite ailerons; self-sealing ducted fans are arranged in the propeller thrust self-energized composite ailerons; electricity, liquid and gas ports and wing hinges are arrangedon one side or two sides of the propeller thrust self-energized composite ailerons; and the propeller thrust self-energized composite ailerons are movably connected with the composite lift wings through the wing hinges. The foldable composite wing aircraft with the twin-propeller thrust composite ailerons has the advantages that the take-off and landing distance is short, the flying speed is high,the structural intensity of the wings is high, the wings can store energy, the flying energy consumption is low, the hang time is long, the safety is high and so on; the ailerons adopt composite lifts so that the adaption range of the power is guaranteed.

The invention provides a thrust compound auxiliary wing with double ducts and a rear single-propeller type compound wing man carrying aircraft with the auxiliary wings. The rear single-propeller typecompound wing man carrying aircraft is composed of a rear single-propeller type compound wing aircraft and the ducted fan thrust self-energy-supply compound auxiliary wings arranged on the two sides of wings of the rear single-propeller type compound wing aircraft. The rear single-propeller type compound wing aircraft comprises an aircraft body, the compound lift force wings fixedly installed on the two sides of the aircraft body and a thruster. The aircraft body is arranged as a deck platform; self-sealed ducted fans are arranged in the compound lift force wings, and wing hinges are arrangedon the outer sides of the compound lift force wings; and the thruster is a propeller thruster. The rear single-propeller type compound wing man carrying aircraft has the beneficial effects that the take-off and landing distance is short, the flight speed is high, the wing structural strength is high, the wings can store energy, flight energy consumption is low, and the hang time is long, the auxiliary wings adopt compound lift force, the adaption range of power is guaranteed, meanwhile, the large-area compound lift force wings can achieve the effect of a glider under an emergency, the safety of the aircraft is greatly improved, and safety of personnel, goods and materials is guaranteed.

The invention discloses a rear single-paddle type compound wing airplane with twin-duct thrust compound auxiliary wings and additional wings. The rear single-paddle type compound wing airplane comprises an airplane body, compound lift force wings fixedly mounted on two sides of the airplane body and ducted fan propellers, wherein self-enclosed ducted fans are arranged in the compound lift force wings; wing hinges are designed on the outer sides of the compound lift force wings; the ducted fan propellers are arranged at the front ends of propeller thrust self-powered compound auxiliary wings; self-enclosed ducted fans are arranged in the propeller thrust self-powered compound auxiliary wings; electricity liquid gas connection ports and the wing hinges are arranged on both sides of the propeller thrust self-powered compound auxiliary wings which are movably connected with the compound lift force wings through the wing hinges on one sides. The rear single-paddle type compound wing airplane has the characteristics of short take-off and landing distance, high flying speed, high wing structure strength, capability of energy storage in the wings, low flying energy consumption, long hang time, high safety and the like; the auxiliary wings adopt compound lift force to guarantee an application range of power.

The invention provides a rear single-duct fan type combined wing manned aircraft which is composed of a rear single-duct fan type combined wing aircraft and a manned cabin. The rear single-duct fan type combined wing aircraft comprises an aircraft body, combined lift force wings fixedly installed on the two sides of the aircraft body and a ducted fan propeller. The aircraft body is arranged to bea deck platform. Self-closed ducted fans are arranged in the combined lift force wings, and wing hinges are designed on the outer sides of the combined lift force wings. The manned cabin is installedbelow the aircraft body. The rear single-duct fan type combined wing manned aircraft has the beneficial effects of being short in take-off and landing distance, high in flight speed, high in wing structural strength, capable of storing energy through the wings, low in flight energy consumption, long in hang time, high in safety and the like.

The invention discloses a rear single-vortex type composite wing manned aircraft. The rear single-vortex type composite wing manned aircraft comprises a rear single-vortex type composite wing aircraftand a manned bin, wherein the rear single-vortex type composite wing aircraft comprises a machine body, composite lifting wings fixedly mounted at the two sides of the machine body, and a propeller;the machine body is a deck platform; vertical tail wings are further arranged above or below the machine body; the vertical tail wings are arranged at the two sides of the wings; the vertical tail wings can realize folding; the rear surfaces of the vertical tail wings are equipped with movable vertical rudder wings; self-sealed duct fans are arranged in the composite lifting wings; wing hinges andelectrical gas interfaces are designed at the outer sides of the composite lifting wings; the propeller is a turbine jet engine; and the manned bin is mounted below the machine body. The rear single-vortex type composite wing manned aircraft integrates characteristics of the turbine jet engine, and has the characteristics of being short in lifting distance, rapid in flight speed, high in wing structural strength, capable of storing energy through the wings, low in flight energy consumption, long in hang time, high in safety and the like.

The invention provides a foldable composite-wing cargo aircraft provided with single rear propeller. The foldable composite-wing cargo aircraft comprises a single rear propeller type composite-wing aircraft and a cargo bin, wherein the single rear propeller type composite-wing aircraft comprises an aircraft body, composite lift wings mounted on two sides of the aircraft body in a foldable manner and a thruster; the aircraft body is set as a deck platform; a self-sealing ducted fan is arranged in each composite lift wing, and a wing hinge (1028) is designed on the outer side of the composite lift wing; a magnetic type automatic interlocking port male head and a magnetic type automatic interlocking port female head are arranged on the front and rear sides of each composite lift wing respectively and are of the same size; the thruster is the propeller; the cargo bin is mounted at the lower part of the aircraft body. The foldable composite-wing cargo aircraft has the characteristics of short taking-off and landing distance, high flying speed, high wing structural strength, low flying energy consumption, long hang time and high safety, and the wings can store energy.

The invention discloses a propeller-thrusted composite wing manned aircraft with additional wings. A composite wing aircraft with a rear single-propeller comprises an airframe, additional wings assembled on two sides of a wing, and a manned cabin; a self-enclosed ducted fan is arranged in the composite lift wing, and wing hinges are designed on the outside of the composite lift wing; the wing hinge and an electro-hydraulic gas interface are arranged on one side, towards the airframe, of each additional wing, and the additional wing is arranged on the outside of the composite lift wing in a folding way through the hinge wing; the electro-hydraulic gas interface is provided with a cover, and battery and fuel are built in the additional wing; and the manned cabin is arranged below the airframe. The composite wing manned aircraft disclosed by the invention is not only short in take off and land distance, fast in flight speed, high in wing structure intensity, low in flight energy consumption, long in hang time and high in security, and the wing can store energy; the electro-hydraulic gas interface is arranged on one side or two sides of the additional wing, the energy intercommunication between the additional wing and the composite lift aircraft airfoil is realized, and the flexibility of the whole aircraft is improved since the action is controlled by the composite lift aircraft.

The invention discloses a composite lift force aircraft with a development platform. The composite lift force aircraft consist of a rear single-propeller type composite wing aircraft, thrust-free self-powered composite auxiliary wings assembled at the two sides of the rear single-propeller type composite wing aircraft and an manned bin, wherein the rear single-propeller type composite wing aircraft comprises a machine body, composite lift force wings which are mounted at the two sides of the machine body in a foldable mode, and a propeller; the machine body is a deck platform; self-sealing ducted fans are arranged in the composite lift force wings; wing hinges are designed at the outer sides of the composite lift force wings; self-sealing ducted fans are arranged in the thrust-free self-powered composite auxiliary wings; an electric-liquid gas interface and a wing hinge are arranged at one side or the two sides of each propeller thrust self-powered composite auxiliary wing, and are movably connected with the composite lift force wings through the wing hinges; and the manned bin 112 is mounted below the machine body. The composite lift force aircraft has the characteristics of beingshort in takeoff and landing distance, high in flying speed, high in wing structural strength, capable of storing energy by wings, low in flying energy consumption, long in hang time, high in safetyand the like.

The invention relates to a rear single screw foldable composite wing manned craft with an additional wing. The rear single screw foldable composite wing manned craft comprises a craft body, the composite lift force wings mounted at the two sides of the craft body in a foldable manner and a propeller, wherein the craft body is arranged as a deck platform, the self-sealing ducted fans are arranged in the composite lift force wings, and the wing hinges are designed at the outer sides of the composite lift force wings; a manned cabin is arranged below the craft body, a magnetic type automatic interlocking interface male connector and a magnetic type automatic interlocking interface female connector are respectively arranged in front of and behind the composite lift force wings, and the magnetic type automatic interlocking interface male connector and the magnetic type automatic interlocking interface female connector have the same size. A wing hinge and an electric-hydraulic-gas interfaceare arranged on one side, facing the craft body, of the additional wing, and the additional wings are installed at the outer sides of the composite lift force wings in a foldable manner through the wing hinges. The craft has the characteristics of short take-off and landing distances, high flight speed, high structural strength of the wings, energy storage wings, low flight energy consumption, long hang time, high safety and the like.

A foldable composite-wing manned aircraft with double-propeller-thrust composite auxiliary wings is provided. A rear-thrust-free type composite-wing aircraft includes a fuselage and composite liftingwings mounted, in a foldable manner, at two sides of the fuselage. The fuselage is a deck platform. Self-sealing ducted fans are disposed in the composite lifting wings. Hinges are arranged at outer sides of the composite lifting wings. Front ends of propeller-thrust self-powered composite auxiliary wings are provided with propellers. Self-sealing ducted fans are disposed in the propeller-thrust self-powered composite auxiliary wings. Electro-hydraulic gas connectors and wing hinges are disposed on one or two sides of the propeller-thrust self-powered composite auxiliary wings. The composite auxiliary wings are movably connected to the composite lifting wings through the wing hinges. A manned bin is mounted at the lower part of the fuselage. The aircraft has characteristics of short take-off and landing distances, a high flight speed, high wing structural strength, a characteristic that the wings can store energy, low flight energy consumption, long flying time, high safety, and the like. Composite lifting force is adopted by the auxiliary wings, thus ensuring the adaptive range of power.

The invention provides a rear-single-propeller-type composite wing airplane with double-duct thrust composite auxiliary wings. The rear-single-propeller-type composite wing airplane is composed of a rear-single-propeller-type composite wing aircraft and the duct fan thrust self-energy-supply composite auxiliary wings assembled on the two sides of wings of the rear-single-propeller-type composite wing aircraft. The rear-single-propeller-type composite wing aircraft comprises an aircraft body, the composite lifting force wings fixedly mounted on the two sides of the aircraft body and a thruster.The aircraft body is arranged to be a deck platform, the composite lifting force wings are internally provided with self-sealing duct fans, and wing hinges are designed on the outer sides of the composite lifting force wings. The thruster is a propeller thruster. The rear-single-propeller-type composite wing airplane with the double-duct thrust composite auxiliary wings have the characteristics that the taking-off and landing distance is short, the flying speed is high, the wing structural strength is high, the wings can store energy, the flying energy consumption is low, the hang time is long, and the safety is high, the auxiliary wings adopt composite lifting force, and the power application range is ensured.

The invention provides a composite lift force aircraft with an extended platform. The aircraft is composed of a rear single-propeller type composite wing aircraft, non-thrust self-energy-supply composite auxiliary wings assembled on the two sides of the rear single-propeller type composite wing aircraft and a freight transport bin. The rear single-propeller type composite wing aircraft comprises an aircraft body, composite lift force wings installed on the two sides of the aircraft body in a foldable mode and a propeller thruster. The aircraft body is arranged as a deck platform; self-sealingducted fans are arranged in the composite lift force wings, and wing hinges are designed on the outer sides of the composite lift force wings; and self-sealing ducted fans are arranged in the non-thrust self-energy-supply composite auxiliary wings, an electro-hydraulic-gas interface and a wing hinge are arranged on one side or two sides of each non-thrust self-energy-supply composite auxiliary wing, the non-thrust self-energy-supply composite auxiliary wings are movably connected with the composite lift force wings through the wing hinges, and the freight transport bin is installed below the aircraft body. The composite lift force aircraft has the advantages that the take-off and landing distance is short, the flight speed is high, the wing structural strength is high, the wings can storeenergy, flight energy consumption is low, the hang time is long, and safety is high.

The invention relates to a combined-wing cargo aircraft with double propeller thrust combined ailerons. A rear thrust-free combined-wing aircraft comprises a body, combined lift wings fixedly mountedon two sides of the body, and a freight cabin, wherein the body is a deck platform; self-sealing ducted fans are arranged in the combined lift wings; wing hinges are designed outside the combined liftwings; propellers are arranged at the front ends of propeller thrust self-energizing combined ailerons; self-sealing ducted fans are arranged in the propeller thrust self-energizing combined ailerons; an electro-hydraulic gas interface and a wing hinge are arranged on one side or both sides of each propeller thrust self-energizing combined aileron; the propeller thrust self-energizing combined ailerons are movably connected to the combined lift wings through the wing hinges; the freight cabin is mounted below the body. The invention has the characteristics of being short in take-off and landing distances, fast in flying speed, high in wing structural strength, capable of storing energy in the wings, low in flight energy consumption, long in hang time, and high in safety; the ailerons adopt combined lift, to ensure power adaptability.

The invention provides a zero rear thrust composite-wing cargo aircraft with turbofan composite ailerons and additional wings. An aircraft body is arranged as a deck platform; a self-sealing ducted fans are embedded in composite lift wings; wing hinges are designed on the external sides of the composite lift wings; turbofan propellers are arranged under turbofan thrust self-energized composite ailerons; self-sealing ducted fans are arranged in the turbofan thrust self-energized composite ailerons; electricity, liquid and gas interfaces and wing hinges are arranged on one sides or two sides ofthe turbofan thrust self-energized composite ailerons; the turbofan thrust self-energized composite ailerons are movably connected with the composite lift wings through the wing hinges; wing hinges are arranged on one sides, facing towards the aircraft body, of the additional wings; the additional wings are mounted on the external sides of the composie lift wings through the wing hinges in a foldable manner; and a cargo compartment is mounted at the bottom of the aircraft body. The zero rear thrust composite-wing cargo aircraft with the turbofan composite ailerons and the additional wings hasthe advantages that the taking-off and landing distance is short, the flying speed is high, the structural strength of the wings is high, the wings can store energy, the flying energy consumption is low, the hang time is long, the safety is high, the ailerons adopt composite lift forces to guarantee the power application range and so on.

The invention provides a composite lift force aircraft with an expansion platform. The aircraft is composed of a rear single-propeller type composite wing aircraft and propeller thrust self-energy-supply composite auxiliary wings assembled on the two sides of the rear single-propeller type composite wing aircraft. The rear single-propeller type composite wing aircraft comprises an aircraft body, composite lift force wings installed on the two sides of the aircraft body in a foldable mode and a propeller thruster, wherein the aircraft body is arranged to be a deck platform; self-sealed ducted fans are arranged in the composite lift force wings, and wing hinges are arranged on the outer sides of the composite lift force wings; and self-sealed ducted fans are arranged in the propeller thrustself-energy-supply composite auxiliary wings, electro-hydraulic-gas ports and wing hinges are arranged on one side or two sides of each propeller thrust self-energy-supply composite auxiliary wing, and the propeller thrust self-energy-supply composite auxiliary wings are movably connected with the composite lift force wings through the wing hinges. The aircraft has the beneficial effects that thetake-off and landing distance is short, the flight speed is high, the wing structural strength is high, the wings can store energy, the auxiliary wings adopt composite lift force and have propeller power, the flight energy consumption is low, the aerial duration time is long, and safety is high.

The invention relates to a ship-based foldable dual magnetic anomaly detection anti-submarine warfare aircraft with a vertical take-off and landing function. The ship-based foldable dual magnetic anomaly detection anti-submarine warfare aircraft is composed of a composite wing aircraft, self-powered power composite auxiliary wings assembled on both sides of wings, a manned cabin and a telescopic metal detector. The ship-based foldable dual magnetic anomaly detection anti-submarine warfare aircraft is provided with the cruising speed of a fixed wing anti-submarine warfare aircraft, the cruisingspeed is hundreds of times that of ship anti-submarine. The aircraft can hover directly over the sky for a long time or even stay stationary to lock a submarine. At the same time, the difference value can be calculated combined with the coordinates of a cruise satellite and flight trajectory according to the magnitude and difference value of metal induction values on both sides by adopting the scheme of a two-way magnetic anomaly detection rod to directly calculate and locate the underwater submarine. The positioning efficiency can be multiplied many, many times. And the anti-submarine warfare aircraft can hover and lock the submarine for a long time in a low-power gliding state.

The invention relates to a rear-single-propeller-type complex-wing freight transportation aircraft with complex type ailerons and additional wings. The rear-single-propeller-type complex-wing freighttransportation aircraft comprises a rear-single-propeller-type complex-wing aircraft, zero-thrust self-energizing complex ailerons and additional wings, wherein the zero-thrust self-energizing complexailerons and additional wings are assembled at the two sides of each wing of the aircraft; the additional wings are mounted at outer sides of the zero-thrust self-energizing complex ailerons in a foldable manner through wing hinges, and a freight transportation cabin is mounted below a fuselage. The rear-single-propeller-type complex-wing freight transportation aircraft has the characteristics that the taking off and landing distance is short, the flight speed is high, the wings are high in structural strength and can store energy, the energy consumption of flight is low, the hang time is long, and the like; large-area complex lifting wings can exert the action of a glider under emergency conditions, so that the safety of the aircraft is greatly improved, and the safety of personnel and physical resources is guaranteed.

The invention relates to a non-rearward thrust composite wing aircraft with a duct fan composite auxiliary wing and an additional wing, wherein, the non-rearward thrust composite wing aircraft comprises a body, a composite lifting wing fixedly installed on both sides of the body, and an additional wing; Wherein, the airframe is arranged as a deck platform; The compound lift wing has built-in self-enclosed duct fan and wing hinge on the outside of the compound lift wing. Solar cell panels are arranged on a surface if the additiaon wing, and the cargo cabin is arranged on the bottom of the airframe. The invention not only has the characteristics of short take-off and landing distance, fast flight speed, high wing structure strength, energy storage of the wing, low flight energy consumption,long air stagnation time, high safety and the like, but also adopts the compound lift force to ensure the adaptability of the auxiliary wing.

The invention relates to a screw-propelled compound wing air truck with additional wings. The screw-propelled compound wing air truck comprises a rear single propeller type compound wing aircraft, theadditional wings assembled on two sides of wings of the rear single propeller type compound wing aircraft and a cargo cabin, and the rear single propeller type compound wing aircraft comprises a body, wherein self-closing ducted fans are arranged in compound lift wings, and wing hinges are designed on outer sides of the compound lift wings; the wing hinge and an electro-hydraulic gas port are arranged on one side, facing the body, of each additional wing, and the additional wings are mounted on outer sides of the compound lift wings through the wing hinges in a foldable manner; each electro-hydraulic gas port is provided with a cover, and batteries / fuel are / is arranged in the additional wings; the cargo bin is mounted under the body. The air truck has the characteristics of short take-offand landing distance, high flight speed, high wing structural strength, energy storable wings, low flight energy consumption, long hang time, high safety and the like; the electro-hydraulic gas portsare formed in one side or two sides of each additional wing, energy transmission between the additional wings and the main wing surface of the compound lift aircraft is achieved, and action is controlled by the compound lift aircraft, so that flexibility of the whole aircraft is improved.

The invention relates to a rear single-propeller type composite wing manned craft which comprises a rear single-propeller type composite wing craft and a manned bin, wherein the rear single-propellertype composite wing craft comprises a craft body, the composite lift force wings fixedly installed at the two sides of the craft body and a propeller, wherein the craft body is arranged as a deck platform, the self-sealing ducted fans are arranged in the composite lift force wings, and the wing hinges are designed at the outer sides of the composite lift force wings; the wing tails are further arranged at the tail ends of the composite lift force wings, the propeller is a screw propeller, and the manned bin is arranged below the craft body. The craft has the characteristics of short take-off and landing distances, high flight speed, high structural strength of the wings, energy storage wings, low flight energy consumption, long hang time, high safety and the like.

The invention provides a back-thrust-force-free type composite wing manned craft with turbofan thrust composite auxiliary wings. The back-thrust-force-free type composite wing manned craft comprises acraft body and composite elevating force wings fixedly mounted on the two sides of the craft body. The craft body is arranged to be a deck platform. The composite elevating force wings are internallyprovided with self-sealing ducted fans, and wing hinges are designed on the outer sides of the composite elevating force wings. Turbofan thrusters are arranged at the front ends of turbofan thrust self-powered composite auxiliary wings, electricity, liquid and gas interfaces and the wing hinges are arranged on one sides or two sides of the turbofan thrust self-powered composite auxiliary wings, and the turbofan thrust self-powered composite auxiliary wings are connected with the composite elevating force wings through the wing hinges. The back-thrust-force-free type composite wing manned craft has the characteristics of being short in take-off and landing distance, high in flight speed, high in wing structure strength, capable of achieving energy storage through the wings, low in flight energy consumption, long in hovering time, high in safety and the like, the auxiliary wings adopt composite elevating force, and the adaptability of power is guaranteed.

The invention discloses a foldable type composite lifting power aircraft with an extended platform. The foldable type composite lifting power aircraft with the extended platform comprises an aircraftbody, composite lifting power wings which are installed at the two sides of the aircraft body in a foldable mode and a propeller, wherein the aircraft body is arranged as a deck platform; self-sealingducted fans are arranged in the composite lifting power wings; horizontal lifting rudder wings are arranged in the composite lifting power wings, and the composite lifting power wings are externallyprovided with vertical tail wings and vertical rudder wings. Compared with the prior art, the foldable type composite lifting power aircraft with the extended platform has the characteristics that thetake-off and landing distance is short, the loading capacity is large, the flight speed is high, the flight distance is far, the aircraft is maneuverable and flexible, the supermobility of the flightpath can be realized, the obstacle avoidance ability is good, the energy consumption is low, the extended functions are multiple, the hang time is long and space occupation is small; in addition, thestorage and transportation space occupation is reduced and the foldable type composite lifting power aircraft with the extended platform is especially suitable for the environment with limited spacesuch as families and aircraft carriers. According to the scheme, the quantity of carrier based aircrafts can be greatly increased, and the advantages that the number of the aircraft carried by medium-sized carriers is no less than that of large-sized carriers and the like can be achieved.

The invention provides a rear single ducted fan type composite-wing airplane with composite ailerons and additional wings. The rear single ducted fan type composite-wing airplane with the composite aileron and the additional wing is characterized by comprising a rear single ducted fan type composite-wing aircraft, propeller thrust self-energized composite ailerons and additional wings, wherein thepropeller thrust self-energized composite ailerons and the additional wings are assembled on the two sides of wings. The rear single ducted fan type composite-wing airplane with the composite aileronand the additional wing has the advantages that the taking-off and landing distance is short, the flying speed is high, the structural strength of the wings is high, the wings can store energy, the flying energy consumption is low, the hang time is long, the safety is high, the ailerons adopt composite lift forces to guarantee the power application range and so on.

The invention relates to a composite lift aircraft provided with an extended platform. The composite lift aircraft comprises a rear single propeller type composite wing aircraft and propeller thrust self-powering composite auxiliary wings assembled on two sides of the rear single propeller type composite wing aircraft, wherein the rear single propeller type composite wing aircraft comprises a body, composite lift wings mounted on two sides of the body in a foldable manner and a propeller thruster; the body is set as a deck platform; self-closed ducted fans are arranged in the composite lift wings, and wing hinges are designed on the outer sides of the composite lift wings; self-closed ducted fans are arranged in the propeller thrust self-powering composite auxiliary wings, electric liquidgas ports and wing hinges are arranged on one side or two sides of each propeller thrust self-powering composite auxiliary wing, and the propeller thrust self-powering composite auxiliary wings are movably connected with the composite lift wings through the wing hinges. The composite lift aircraft has the characteristics that the take-off and landing distance is short, the flight speed is high, the wing structure strength is high, the wings can store energy, the auxiliary wings adopt composite lift force, the flight energy consumption is low, the hang time is long, the safety is high and the like.

The invention relates to a composite lift aircraft with an expanding platform. A rear single-propeller type composite wing aircraft comprises an aircraft body, composite lift ailerons which are fixedly arranged on two sides of the aircraft body and propeller thrusts, wherein the aircraft body is arranged as a deck platform; self-closed duct fans are arranged inside the composite lift ailerons; aileron hinges are arranged on the outer sides of the composite lift ailerons; self-closed duct fans are arranged inside thrust-free self-energy supplied composite ailerons; electro-hydraulic and pneumatic interfaces and aileron hinges are arranged on one side or two sides of the thrust-free self-energy supplied composite ailerons; the thrust-free self-energy supplied composite ailerons are movably connected with the corresponding composite lift ailerons by the corresponding aileron hinges; a manned capsule is arranged below the aircraft body. The composite lift aircraft disclosed by the invention has the characteristics of short take-off and landing distance, high flight speed, high structural strength of the ailerons, capability of storing energy by the ailerons, low flight energy consumption, long hang time and the like; the large-area composite lift ailerons can be used as a glider under the emergency condition, so that the safety of the aircraft is greatly improved and the safety ofmaterials is ensured.

The invention discloses a non-rear-thrust composite wing aircraft with a ducted fan composite auxiliary wing and an additional wing. An engine body is arranged to be a deck platform. A composite liftwing is internally provided with a self-closed ducted fan, and a wing hinge is designed on the outer side of the composite lift wing. A turbofan propeller is arranged below a turbofan thrust self-power composite auxiliary wing, the turbofan thrust self-power composite auxiliary wing is internally provided with a self-closed ducted fan, an electro-hydraulic gas connecting opening and a wing hinge are arranged one side or two sides of the turbofan thrust self-power composite auxiliary wing, and the electro-hydraulic gas connector and the wing hinge are movably connected with the composite lift wing through the wing hinge. A wing hinge is arranged on one side, facing to the engine body, of the additional wing, and the additional wing is installed on the outer side of the composite lift wing through the wing hinge in a folding mode. The additional wing is internally provided with a battery / fuel. The non-rear-thrust composite wing aircraft with the ducted fan composite auxiliary wing and the additional wing has the characteristics that takeoff and landing distance is short, flight speed is high, wing structure strength is high, wings can store energy, flight energy consumption is low, hang time is long, and safety is high; and the auxiliary wings adopt compound lift to ensure the adaptive range of power.

The invention belongs to a composite lifting force wing aircraft with an expansion platform. The aircraft consists of a rear single screw type composite wing aircraft and zero-thrust self energy supply composite auxiliary wings assembled at the two sides, wherein the rear single screw foldable composite wing aircraft comprises an aircraft body, composite lifting force wings arranged at the two sides of the aircraft body in a foldable way, and a screw thruster; the aircraft body is made into a deck platform; a self sealing duck passage is built in the composite lifting force wing; a wing hingeis designed at the outer side of the composite lifting force wing; the self sealing duct fan is arranged in the zero-thrust self energy supply composite auxiliary wing; an electric liquid gas interface and a wing hinge are arranged at one side or two sides of the zero-thrust self energy supply composite auxiliary wing; the zero-thrust self energy supply composite auxiliary wing is movably connected with the composite lifting force wing through the wing hinge. The composite lifting force wing aircraft has the characteristics that the takeoff and landing distance is short; the flight speed is high; the wing structure intensity is high; the wing can realize the energy storage; the flight energy consumption is low; the air staying time is long; the safety is high, and the like.

The invention discloses a non-rear-thrust-force type composite wing freight aircraft with turbofan pushing composite auxiliary wings. The non-rear-thrust-force type composite wing freight aircraft comprises a machine body and composite lifting wings fixedly mounted at the two sides of the machine body, wherein the machine body is a deck platform; self-sealed duct fans are arranged in the compositelifting wings; wing hinges are designed at the outer sides of the composite lifting wings; the front ends of turbofan thrust self-powered composite auxiliary wings are equipped with turbofan propellers; self-sealed duct fans are arranged inside the turbofan thrust self-powered composite auxiliary wings; and one side or two sides of each turbofan thrust self-powered composite auxiliary wing are equipped with electric-hydraulic gas interfaces and wing hinges, and are movably connected with the composite lifting wings through the wing hinges. The non-rear-thrust-force type composite wing freightaircraft is short in lifting-landing distance, is high in flight speed, is high in wing structural strength, is capable of storing energy through the wings, is low in flight energy consumption, is long in hang time, is high in safety, and the like; and the auxiliary wings adopt composite lifting force, so that applicability of power is ensured.

The invention relates to a compound lift aircraft with an expansion platform. The compound lift aircraft comprises a rear single propeller type compound wing aircraft, thrust-free self-powered compound ailerons assembled on two sides of the rear single propeller type compound wing aircraft and a cargo bin, wherein the rear single propeller type compound wing aircraft comprises a body, compound lift wings fixed on two sides of the body and a propeller; the body is arranged to be a deck platform; self-closing ducted fans I are arranged in the compound lift wings, and hinges are designed on outersides of the compound lift wings; self-closing ducted fans II are arranged in the thrust-free self-powered compound ailerons, electro-hydraulic gas ports and the hinges are arranged on one side or two sides of each thrust-free self-powered compound aileron, and the thrust-free self-powered compound ailerons are movably connected with the compound lift wings through the hinges; the cargo bin is mounted below the body. The aircraft has the characteristics of short take-off and landing distance, high flight speed, high wing structural strength, energy storable wings, low flight energy consumption, long hang time, high safety and the like.