68results about How to "Strong obstacle avoidance ability" patented technology

The invention discloses a central air conditioner intelligent control system based on a wireless sensor network and a method, and belongs to the technical field of central air conditioner control. The central air conditioner intelligent control system comprises an intelligent information management center, wireless communication devices, a central air conditioner information monitoring and control module, a room information monitoring and control module and the like. The invention adopts the method that the central air conditioner intelligent control system is used to monitor information, build a data base, calculate current load of the system, and realize advance, accurate and optimized control of a central air conditioner system by combining a short-term loading forecasting method based on similar dates and fuzzy control technology, as well as taking the temperature variation of supply / return chilled / cooling water of a central air conditioner as the manipulated variable. The central air conditioner intelligent control system has the characteristics of great communication capacity, guaranteed communication quality, powerful network functions, wide monitoring range and extensive control quantity of the central air conditioner system, optimized control, high control accuracy, good energy saving effect and the like, and can be widely used in energy-saving optimizing control of various buildings, and is particularly suitable for energy-saving optimizing control of central air conditioners of intelligent buildings.

The invention provides a power pipeline route inspection robot and belongs to the field of power engineering. The power pipeline route inspection robot comprises a snake head (1), a snake body (2) and a snake tail (3); the snake head (1) and the snake body (2) are modular in design; the snake head (1) is connected with the snake body (2) through two pins arranged on two sides of the snake body, modules are also connected through pins, the modules and the snake tail (3) are also connected through pins, the snake tail (3) is mainly powered by a steering engine rocking up and down to move, each part is provided with a backup battery, and battery life is longer. The power pipeline route inspection robot is compact in structure, small in size, light in weight, highly controllable, convenient to demount and safe and reliable and has flexible joints.

The invention provides a multi-joint service robot arm which can achieve translational decoupling along the Z direction; the structure of the arm uses a U RR+R type which consists of a shoulder joint which has two swing pairs, an elbow joint which has a swing pair, a wrist joint which has a rotation pair and a swing pair, a large arm which is connected between the shoulder joint and the elbow joint, a small arm which is connected between the elbow joint and the wrist joint, and paws which are connected with the wrist joint; the shoulder joint comprises a parallelogram mechanism and a shoulder connecting body; the driving arm of the shoulder joint is connected with a motor connecting shaft sleeve which is connected with the motor output shaft; the shoulder connecting body is arranged on the connecting arm of the parallelogram mechanism; the shoulder connecting body comprises a bracket which consists of a supporting plate and a supporting angle aluminium; the bracket is connected with a shoulder actuator and a transmission plate; the actuator is fixed on the bracket; the shoulder transmission plate is connected with the bracket; the actuator output shaft is connected with the transmission plate; the transmission plate is connected with one end of the large arm.

The invention discloses a rope-driven multi-joint flexible mechanical arm. The rope-driven multi-joint flexible mechanical arm comprises a plurality of joint rod units connected in series in the axialdirection, wherein in any two adjacent joint rod units, the bottom end part of one joint rod unit is sleeved with the top end of the other joint rod unit, the top end of one joint rod unit is flexibly connected with the top end of the other joint rod unit through a spring assembly, the bottom end of one joint rod unit is flexibly connected with the top end of the other joint rod unit through a spring assembly, and a plurality of rope penetrating holes are formed in each joint rod unit. External contact or collision force of the mechanical arm can be rapidly dispersed through a load path formed by the joint rod units and the spring assemblies, so that rigid collision impact between the mechanical arm and a target is avoided, and the mechanical arm is suitable for non-cooperative target capture; and by elastically deforming the spring assemblies, relative rotation between the joint rod units is driven, so that bending deformation of the mechanical arm is controlled.

The invention relates to a four-wheel independent steering robot chassis which comprises a frame, a driving mechanism, a suspension mechanism, a steering mechanism and a control mechanism, wherein thedriving mechanism, the suspension mechanism, the steering mechanism and the control mechanism are all connected to the frame, and the steering mechanism and the driving mechanism are both connected with the suspension mechanism; the suspension mechanism comprises a lower suspension, an upper suspension, a steering knuckle, a plurality of knuckle bearings, a lower suspension shaft, a shock absorber shaft, an upper suspension shaft and a shock absorber; the lower suspension and the upper suspension are connected to the frame; the lower suspension shaft and the shock absorber shaft are connectedto the lower suspension; the upper suspension shaft is connected to the upper suspension; and the lower end of the shock absorber is connected with the shock absorber shaft. According to the four-wheel independent steering robot chassis, independent driving, independent steering and independent suspension of the four wheels are achieved, the robot chassis can rotate in situ, multiple operation modes such as front wheel steering and rear wheel driving and four-wheel steering and four-wheel driving are achieved, and the robot chassis is compact in structure, free in movement mode, high in movement speed, stable in movement and high in obstacle avoidance capacity.

The invention relates to a spider-like glass facade cleaning robot. The spider-like glass facade cleaning robot comprises a robot shell, a control device, a motion mechanism, a water flow channel anda cleaning mechanism, wherein rods transversely and longitudinally penetrating through the shell are arranged on the robot shell, a carrying platform is arranged on the robot shell, a motor, a singlechip microcontroller unit and a sensor are arranged on the carrying platform, and the motor and the sensor are connected with the single chip microcontroller unit; the motion mechanism comprises a crank-link mechanism, a rack and pinion mechanism and suction discs, and the suction discs are installed at the tail ends on the inner sides of the crank-link mechanism and the rack and pinion mechanismrespectively, the robot moves up and down through the advance and return movement of the crank-link mechanism, and the robot translates left and right through the rack and pinion mechanism; the cleaning mechanisms are symmetrically arranged at the two ends of the robot shell. The spider-like glass facade cleaning robot has a high obstacle crossing performance, the robot can automatically cross a certain obstacle without assisting, and trackless cleaning can be achieved, so that the cost is reduced; the robot can be suitable for glass facades of different buildings.

The invention discloses a wheel and crawler composite type pipeline robot. The wheel and crawler composite type pipeline robot comprises a crawler type traveling drive device, two driven wheel deviceand a controller; two L-type supports are arranged on the traveling drive device in a bilateral symmetry mode; one ends of the two L-type supports are fixed to the traveling drive device, and the other ends of the two L-type supports are vertically downward; the two driven wheel devices are installed on the two L-type supports; the driven wheel devices comprise driven wheels, lifting mechanisms for driving the driven wheels to lift and steering mechanisms for driving the driven wheels to turn; the lifting mechanisms comprise first motors, first drive gears, first driven gears, lead screws andguide rods; the steering mechanisms comprise second motors, second drive gears, second driven gears and rotary shafts; the driven wheels are provided with pressure sensors; and the controller is connected with the traveling drive device, the first motors, the second motors and the pressure sensors. The wheel and crawler composite type pipeline robot has the excellent pipe diameter adaption ability, obstacle climbing ability and traction ability.

The invention provides a method for butting a robot with a charging device, which comprises the following steps of: when the robot moves in a charging area of the charging device, recognizing feature information of the charging device; when the feature information is recognized, planning a docking path of the robot and the charging device; following the optimal path in the butt joint paths, and driving the robot to move to the butt joint position of the charging device through the optimal path; and triggering the charging device to charge the robot at the butt joint position. The invention further provides a system for butting the robot with the charging device, the robot and a computer storage medium. According to the method and system for butting the robot with the charging device, the robot and the computer storage medium, the characteristic information of the charging device can be recognized from different positions and angles, the recognition result is accurate, the problem that the robot stops halfway is avoided, and the obstacle avoidance capacity of the robot is high.

The invention discloses a forklift device with a high degree of freedom. The forklift device with the high degree of freedom comprises a car body and a lifting mechanism for up-and-down loading and unloading cargoes, wherein a steering mechanism for supporting, moving and steering the car body is arranged on the lower part of the car body; a rotation frame mechanism is connected between the car body and the lifting mechanism and is fixedly connected with the lifting mechanism; the rotating frame mechanism is rotatably connected with the car body; the lifting mechanism rotates around the car body through the rotating frame mechanism; a groove matched with the car body is formed in the rotation frame mechanism; at least one roller is arranged on each of two opposite side surfaces of the groove; annular rail grooves are formed in the opposite upper and lower surfaces of the car body; the rollers can be rotatably arranged in the annular rail grooves; and the rotation frame mechanism rotates relative to the annular rail grooves through the rollers. Through the cooperation of the lifting mechanism, the steering mechanism and the rotation frame mechanism, the adjustment of a forklift in multiple degrees of freedom is realized, and the forklift is good in flexibility, high in obstacle avoidance capacity, and capable of meeting the requirement of a complicated carrying environment for modern logistics storage.

The invention discloses a remote sensing surveying and mapping unmanned aerial vehicle with high safety, which comprises a vehicle body, wings are arranged on the two sides of the vehicle body, a front propeller is arranged in the front of the vehicle body, and a tail vane is arranged at the tail of the vehicle body; wherein a fixed rod parallel to the aircraft body is symmetrically fixed in each of the two wings, vertical propellers are rotatably arranged at the two ends of each fixed rod, and each vertical propeller can be driven by a vertical motor fixed in the corresponding fixed rod to rotate; a plurality of arc-shaped protection blocking pieces are distributed at the bottom of the vertical propeller in the circumferential direction of the vertical propeller, the protection blocking pieces are connected with the fixing rod through protection rods, and the protection rods can adjust the distance between the protection blocking pieces and the center of the vertical propeller; compared with the prior art, the unmanned aerial vehicle can be in a vertical lifting mode and a fixed wing mode and is good in maneuverability, high in surveying and mapping efficiency and large in activity range. And the protection blocking pieces can be opened and closed, a protection net is formed between the protection blocking pieces and the protection ropes, safety is high when the device is close to the ground, and air resistance is small when the unmanned aerial vehicle is high.

The invention discloses a hydraulic drive type foot type bionic humanoid robot and relates to the field of fluid transmission and control innovation. The robot comprises leg mechanical structures andhydraulic systems; the leg mechanical structures are used for being installed on an upper limb connecting frame of the robot in pairs, and each leg mechanical structure comprises a hip joint, a thighplate, a knee joint, a shank plate, an ankle joint and a foot plate which are sequentially connected from top to bottom; under the control of the hydraulic systems, the hip joints can achieve rotation, side swing and / or pitching actions, the knee joints can achieve pitching actions, and the ankle joints can achieve front-back pitching and / or left-right side swing actions. The robot is higher in movement flexibility, higher in obstacle avoidance capacity, higher in whole machine integration power-to-weight ratio, stable in work, small in reversing impact, quick in response, large in thrust andhigher in load capacity, overall components of the pump station system are vertically and integrally installed and arranged, the size of a robot pump station is effectively reduced, connecting pipes are conveniently connected with an oil way of a lower limb mechanism, and practicability is higher.

The invention discloses a four-degree-of-freedom multi-eye visual rotary flight type picking robot and a picking method thereof. The picking robot comprises an unmanned aerial vehicle, a picking mechanism and a multi-eye visual device, wherein the picking mechanism comprises a telescopic rod and a picking mechanical hand, and the picking mechanism and the multi-eye visual device are mounted on theunmanned aerial vehicle; and the unmanned aerial vehicle communicates with an industrial control computer and a computer through a cable or wireless manner for data transmission and system control. Integrated design of the unmanned aerial vehicle and the picking mechanism is realized, the four-degree-of-freedom multi-eye visual rotary flight type picking robot is a four-degree-of-freedom pickingrobot, multiple-oriented picking can be realized, the picking range is extended, and the picking efficiency is improved; and the designed picking mechanical hand can dynamically change free expandingand contracting of middle finger joints of three fingers according to the size of fruits, the holding capacity of the mechanical hand on the fruits is improved, and the applicability is high.

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 wall-climbing robot and a wall surface transition method thereof. The wall-climbing robot comprises two single robots, each single robot comprises a chassis, a reverse thrust mechanism and three groups of translation mechanisms, each reverse thrust mechanism comprises a main rotor wing, an outer frame and a first driving mechanism, the main rotor wings are fixed in the outer frames, and the first driving mechanisms are suitable for driving the main rotor wings and the outer frames to rotate; the translation mechanisms comprise translation wheel sets and second driving mechanisms, the translation wheel sets comprise hubs and tires, the hubs are connected with the second driving mechanisms, and the multiple tires are suitable for being distributed in the circumferential directions of the hubs and suitable for rotating around the center shaft hole direction of the tires. According to the wall-climbing robot, the front-back and left-right translation, oblique translation, in-situ turning and other movements of the wall-climbing robot and movement of the wall-climbing robot between different wall surfaces can be achieved, the movement is flexible, and the obstacle avoidance capacity is high.

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 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 unmanned robot comprises a vehicle body, a movement mechanism and a mechanical gripper, a controller and a first detector are arranged on the vehicle body, a driving mechanism is arranged at the bottom of the vehicle body, the mechanical gripper comprises a fixed rod, a rotating rod and a gripper, a first driver is arranged on the fixed rod, and a second driver is arranged on the rotating rod. The first driver controls the rotating rod to rotate, the gripper is installed at the end of the rotating rod, a second driver is arranged in the rotating rod to control opening and closing of the gripper, a second detector is installed on the fixed rod, and the detection area of the second detector is located in front of the gripper. A collecting box used for storing fruits is installed on the vehicle body, and lossless fruit picking can be achieved.

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 belongs to the related technical field of robots and discloses a multifunctional rescue rear-conveying robot. The robot comprises wheels, a box body, a detection module, a measurement module and a control module, wherein the wheels comprise the front wheel and the rear wheel; the box body is arranged on the wheels, a sliding rail, a lifting motor, a dragging motor and a hinge are arranged in the box body, a stretcher is arranged on the sliding rail, the hinge is controlled by the dragging motor to achieve lowering and retracting of the stretcher, and the lifting motor is arranged at the other end of the box body and used for achieving lifting of the stretcher; a pressure sensor is arranged on the stretcher; the detection module comprises a binocular holder and a multi-line laser radar; the measurement module is used for detecting the identity and physical signs of the wounded on the stretcher; the control module is in communication connection with the lifting motor, the dragging motor, the pressure sensor, the detection module and the measurement module. According to the method, a wounded person can be rescued without manual participation, the automation degree is high, manual participation is not needed, and safety of rescuers is guaranteed.

The invention relates to a rear single ducted fan type composite wing aircraft with double ducted fan composite ailerons. The rear single ducted fan type composite wing aircraft with the double ductedfan composite ailerons comprises a rear single ducted fan type composite wing aircraft and ducted fan thrust self-energized composite ailerons which are assembled on the two sides of the rear singleducted fan type composite wing aircraft, wherein the rear single ducted fan type composite wing aircraft comprises an aircraft body, composite lift wings and a propeller, wherein the composite lift wings are fixedly mounted on the two sides of the aircraft body; the aircraft body is a deck platform; self-sealed ducted fans are placed in the composite lift wings; wing hinges are designed on the external sides of the composite lift wings; self-sealed ducted fans are arranged in the ducted fan thrust self-energized composite ailerons; electric, liquid and gas interfaces and 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 wingsthrough the wing hinges. The rear single ducted fan type composite wing aircraft with the double ducted fan composite ailerons has the advantages of short takeoff and landing distance, high flying speed, high wing structural strength, energy storage ability of the wing, low flying energy consumption, long hang time and so on; and the large-area composite lift wings can have effects of gliders inan emergency case, the safety of the aircraft is greatly enhanced, and safeties of personnel and materials are guaranteed.

The invention discloses a path planning method an device for a mobile robot, and a storage medium. The method comprises the steps of: S1, obtaining a starting point and a target point of the mobile robot, and building a first random tree and a second random tree; S2, respectively carrying out collision detection on the first random tree and the second random tree, and determining a first to-be-grown node and a second to-be-grown node which are closest to an obstacle; S3, obtaining random probability values of random sampling of the two random trees, and obtaining random sampling points according to the random probability values of the two random trees and a preset fixed probability; S4, obtaining new nodes according to the random sampling points, improving the new nodes, and adding the improved new nodes to the corresponding random trees; and S5, repeating the steps S3 to S4 until the newest nodes on the first random tree and the second random tree meet, and selecting an optimal path generated after the newest nodes on the two random trees are communicated with each other. According to the path planning method and device for the mobile robot, and the storage medium, the defects of blindness, strong randomness and poor stability during path planning are overcome.

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 provides a rear single ducted fan type composite-wing aircraft with zero thrust composite ailerons and additional wings. The rear single ducted fan type composite-wing aircraft with thezero thrust composite ailerons and the additional wings comprises a rear single ducted fan type composite-wing aircraft, zero thrust self-energized ailerons and additional wings, wherein the zero thrust self-energized ailerons and the additional wings are assembled on the two sides of wings; the additional wings are mounted on the external sides of the zero thrust self-energized ailerons through wing hinges in a foldable manner. The rear single ducted fan type composite-wing aircraft with the zero thrust composite ailerons and the additional wings 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, large-compositelift wings can have effects of gliders in the case of emergency, the safety of the aircraft is greatly enhanced, and safeties of personnel and materials are guaranteed.

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.