47results about How to "Improve handling agility" patented technology

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 relates to a compound lift aircraft with an expanded platform. The compound lift aircraft with the expanded platform is composed of a rear single-propeller compound-wing aircraft and non-thrust self-energized compound ailerons installed on the two sides of the rear single-propeller compound-wing aircraft body; the rear single-propeller compound-wing aircraft comprises a plane, compound lift wings fixedly installed on the two sides of the plane and a propeller; the plane is arranged as a deck platform; self-sealing ducted-fans are arranged in the compound lift wings, and wing hinges are designed on the outer sides of the compound lift wings; self-sealing ducted-fans are arranged in the non-thrust self-energized compound ailerons, power liquid and gas connectors and wing hingesare arranged on one sides or the two sides of the non-thrust self-energized compound ailerons, and the non-thrust self-energized compound ailerons are movably connected with the compound lift wings through the wing hinges. The compound lift aircraft with the expanded platform not only has the advantages of being short in take-off and landing distance, high in flying speed, high in wing structurestrength, capable of energy storage by means of the wings, low in flying energy consumption, long in hang time and the like, but also the large-area compound lift wings can be used as gliders in the emergency situation, thus the safety of the aircraft is greatly improved, and the safety of personnel and materials is ensured.

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 relates to a combined wing aircraft with double-propeller-thrust combined auxiliary wings. The combined wing aircraft comprises a rear-thrust-free type combined wing aircraft and propeller-thrust self-power combined auxiliary wings which are arranged on the two sides of wings of the rear-thrust-free type combined wing aircraft, wherein the rear-thrust-free type combined wing aircraftcomprises a machine body and combined lift force wings fixedly arranged on the two sides of the machine body, the machine body is set as a deck platform, self-sealed 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; propeller thrusters are arranged at the front ends of the propeller-thrust self-power combined auxiliary wings, spaces are reserved between lift force auxiliary wings and balance auxiliary tail wings, and horizontal elevating rudder wings are arranged in the spaces; one or more self-sealed ducted fan is arranged in each lift force auxiliary wings. The combined wing aircraft disclosed by the invention has the characteristics of short rising and landing distance, quick flying speed, high wing structure strength, low flying energy consumption, long hang time, high safety and the like; the wings can be used for storing energy; the auxiliary wings utilize combined lift force, so that a power adaption range is ensured.

The invention discloses a back thrust-free composite wing aircraft with a ducted fan composite auxiliary wing. The back thrust-free composite wing aircraft comprises an engine body and composite liftwings fixed on the two sides of the engine body, wherein the engine body is arranged as a deck platform; a self-sealing ducted fan is arranged in the composite lift wing; a wing hinge is designed on the outer side of the composite lift wing. The back thrust-free composite wing aircraft disclosed by the invention has the characteristics of short takeoff and landing distance, fast flying, high strength of wing structure, energy storage of wing, low energy consumption in flying, long hang time, high safety and the like, wherein the auxiliary wing adopts composite lift.

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 relates to a non-rear-thrust type composite wing aircraft with a ducted fan composite auxiliary wing and an additional wing. A self-sealing ducted fan is arranged in a ducted fan thrustself-energized composite wing; an electrohydraulic gas interface and a wing hinge are arranged on one side or two sides of the ducted fan thrust self-energized composite wing; the ducted fan thrust self-energized composite wing is movably connected with a composite lift force wing through the wing hinge; the wing hinge is arranged on one side, facing towards a machine body, of the additional wing;the additional wing is foldably arranged on the outer side of the composite lift force wing through the wing hinge; a battery / fuel is arranged in the additional wing; and a solar battery panel is arranged on the surface of the additional wing. The non-rear-thrust type composite wing aircraft has the characteristics of short take-off and landing distance, low flight energy consumption, long hang time, high safety and the like; and the auxiliary wing adopts a composite lift force, so that the power application range is guaranteed.

The invention relates to a rear single-propeller type composite wing manned aircraft with propeller thrust composite auxiliary wings. The rear single-propeller type composite wing manned aircraft is composed of a rear single-propeller type composite wing aircraft body and the propeller thrust self-energy-supply composite auxiliary wings assembled on the two sides of wings of the rear single-propeller type composite wing aircraft body. The rear single-propeller type composite wing aircraft body comprises a fuselage, the composite lift wings fixedly mounted on the two sides of the fuselage, anda thruster. The fuselage is arranged as a deck platform. Self-closed culvert fans are arranged in the composite lift wings, and wing hinges are designed on the outer sides of the composite lift wings.The thruster is a propeller thruster. The rear single-propeller type composite wing manned aircraft has the characteristics that the takeoff and landing distance is short, the flight speed is high, the structure strength of the wings is high, the wings can store energy, flight energy consumption is low, and the hang time is long; and the auxiliary wings adopt composite lift to ensure the adaptionrange of power, and meanwhile, the composite lift wings with the large area can achieve the action of a glider under the emergency situations, so that the safety of the aircraft is greatly improved,and the safety of personnel and materials is guaranteed.

The invention discloses a composite wing air freighter with twin-screw composite auxiliary wings with solar additional wings. Rear thrust force-free composite wing aircraft comprises an aircraft body,composite lifting wings which are fixedly arranged at the two sides of the machine body, and additional wings, wherein 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; batteries / fuels are arranged in the additional wings; solar cell panels are arranged on thesurfaces of the additional wings; and a freight bin is mounted below the aircraft body. The composite wing air freighter has the characteristics of being short in takeoff and landing distance, high in flying speed, high in wing structural strength, capable of storing energy by the wing, low in flying energy consumption, long in hang time, high in safety, and the like; and the auxiliary wings adopt composite lift force, so that the applicable range of the power is guaranteed.

The invention relates to a rear single-propeller compound-wing plane with twin-duct compound ailerons and additional wings. A rear single-propeller compound-wing aircraft comprises a plane, compound lift wings fixedly installed on the two sides of the plane and ducted-fan propellers; self-sealing ducted-fans are arranged in the compound lift wings, and wing hinges are designed on the outer sides of the compound lift wings; the ducted-fan propellers are arranged at the front ends of the propeller thrust self-energized compound ailerons, self-sealing ducted fans are arranged in the propeller thrust self-energized compound ailerons, power fluid and gas connectors and the wing hinges are arranged on the two sides of the propeller thrust self-energized compound ailerons, and the airscrew thrustself-energized compound ailerons are movably connected with the compound lift wings through the wing hinges on one sides; a manned cabin is installed on the bottom of the plane. The rear single-propeller compound-wing plane with the twin-duct compound ailerons and the additional wings not only has the advantages of being short in take-off and landing distance, high in flying speed, high in wing structure strength, capable of energy storage by means of the wings, low in flying energy consumption, long in hang time, high in safety and the like, but also compound lift is adopted by the ailerons,so that the power adaptive range is ensured.

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.

A propeller-drive composite-wing manned aircraft provided with two-propeller auxiliary wings and ailerons is provided. A composite-wing aircraft with one rear propeller includes a fuselage, compositelifting wings fixedly mounted at two sides of the fuselage, and a propeller, wherein self-sealing ducted fans are disposed in the composite lifting wings; wing hinges are designed at outsides of the composite lifting wings; the propeller is disposed at the front end of a propeller thrust self-powered composite auxiliary wing; self-sealing ducted fans are disposed in the propeller thrust self-powered composite auxiliary wing; two sides of the propeller thrust self-powered composite auxiliary wing are provided with electro-hydraulic gas connectors and wing hinges and are movably connected to thecomposite lifting wings through the wing hinges; and one side of each aileron, facing the fuselage, is provided with a wing hinge and an electro-hydraulic gas connector, and is mounted, in a foldablemanner, to the outside of the propeller thrust self-powered composite auxiliary wing through the wing hinge. Composite lifting force is adopted by the auxiliary wings to ensure the suitable application range of power.

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 discloses a rear single-ducted fan type composite wing aircraft with propeller thrust composite auxiliary wings. A rear single-ducted fan type composite wing aircraft body comprises a fuselage, composite lift wings fixedly mounted on the two sides of the fuselage, and a ducted fan thruster. The fuselage body is arranged as a deck platform; the composite lift wings are internally provided with self-closed ducted fans, and wing hinges are designed on the outer sides of the composite lift wings; and propeller thrusters are arranged at the front ends of the propeller thrust self-energy-supply composite auxiliary wings, self-closed ducted fans are arranged inside the propeller thrust self-energy-supply composite auxiliary wings, and one sides or the two sides of the propeller thrust self-energy-supply composite auxiliary wings are provided with electro-hydraulic gas connectors and wing hinges, and movably connected with the composite lift wings through the wing hinges. The rear single-ducted fan type composite wing aircraft has the characteristics that the takeoff and landing distance is short, the flight speed is high, the wings are high in structural strength and can store energy, flight energy consumption is low, the hang time is long, and safety is high; and the auxiliary wings adopt composite lift, and the applicable range of power is guaranteed.

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 ship-borne foldable type double-magnetic-anomaly detection antisubmarine warfare airplane with a vertical takeoff and landing function. The ship-borne foldable type double-magnetic-anomaly detection antisubmarine warfare airplane is composed of a composite wing aircraft, self-power-supply composite auxiliary wings assembled at two sides of a wing, a manned cabin and a retractable type metal detector. The ship-borne foldable type double-magnetic-anomaly detection antisubmarine warfare airplane has a cruising speed of a fixed wing antisubmarine warfare airplane and is hundreds of times of that of antisubmarine warfare of a ship. The aircraft provided by the invention can directly hover overhead for long time and even is immobilized to lock a submarine. Meanwhile, a double-path magnetic anomaly detection rod scheme is adopted, and the size and difference value of metal induction numerical values at two sides can be induced and are combined with coordinates of a cruising satellite and a flight track to calculate the difference value; then the underwater submarine is directly calculated and positioned. The positioning efficiency can be increased by a lot of times. The antisubmarine warfare airplane provided by the invention can hover for long time at a low-power-consumption gliding state to lock the submarine.

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 rear single propeller type composite wing aircraft with propeller thrust composite ailerons. The rear single propeller type composite wing aircraft with the propeller thrust composite ailerons comprises a rear single propeller type composite wing aircraft and propeller thrust self-energized composite ailerons which are assembled on a wing, wherein the rear single propellertype composite wing aircraft comprises an aircraft body, composite lift wings and a thruster, wherein the composite lift wings are fixedly mounted on the two sides of aircraft body; the aircraft bodyis arranged as a deck platform; self-sealed ducted fans are embedded in the composite lift wings; wing hinges are designed on the external sides of the composite lift wings; and the thruster is a propeller type thruster. The rear single propeller type composite wing aircraft with the propeller thrust composite ailerons has the advantages that the take-off and landing distance is short, the flyingspeed is high, the wing structural strength is high, the wing can store energy, the flying energy consumption is low, the aircraft can stay in the air for long time, the safety is high and so on; andthe ailerons adopt composite lift forces so that the application range of the power is guaranteed.

The invention discloses a composite lift aircraft with an extended platform. The composite lift aircraft is composed of a rear single-ducted fan type composite wing aircraft body, non-thrust self-energy-supply composite auxiliary wings assembled on the two sides of the rear single-ducted fan type composite wing aircraft body, and a manned bin. The rear single-ducted fan type composite wing aircraft body comprises a fuselage, composite lift wings fixedly mounted on the two sides of the fuselage, and a propeller thruster. The fuselage is arranged as a deck platform; the composite lift wings areinternally provided with self-closed ducted fans, and wing hinges are designed on the outer sides of the composite lift wings; and self-closed ducted fans are arranged inside the non-thrust self-energy-supply composite auxiliary wings, and one sides or the two sides of the non-thrust self-energy-supply composite auxiliary wings are provided with electro-hydraulic gas connectors and wing hinges, and movably connected with the composite lift wings through the wing hinges. The manned bin is mounted on the lower portion of the fuselage. The composite lift aircraft has the characteristics that thetakeoff and landing distance is short, the flight speed is high, the wings are high in structural strength and can store energy, flight energy consumption is low, and the hang time is long; and the large-area composite lift wings can achieve the effect of a glider under the emergency situation, the safety of the aircraft is greatly improved, and the safety of personnel and materials is guaranteed.

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 no-back-thrust-type complex-wing manned aircraft with turbofan complex ailerons and additional wings. A deck platform serves as a fuselage; self-sealing ducted fans are built in complex lifting wings, and wing hinges are designed at outer sides of the complex lifting wings; turbofan propellers are arranged below turbofan thrust self-energizing complex ailerons, self-sealing ducted fans are arranged inside the turbofan thrust self-energizing complex ailerons, electrohydraulic gas interfaces and wing hinges are arranged at one side or two sides of each turbofan thrustself-energizing complex aileron and are movably connected with the complex lifting wings through the wing hinges, the wing hinges are arranged at one side, facing to the fuselage, of each additional wing, and the additional wings are mounted at outer sides of the complex lifting wings in a foldable manner through the wing hinges; a manned cabin is mounted below the fuselage. The no-back-thrust-type complex-wing manned 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, theenergy consumption of flight is low, the hang time is long, the safety is high, and the like; the ailerons adopt a complex lifting force, so that the adaptation range of power is ensured.

The invention discloses a rear single ducted fan type composite wing manned aircraft provided with composite auxiliary wings and additional wings. The rear single ducted fan type composite wing mannedaircraft provided with the composite auxiliary wings and the additional wings is characterized by comprising a rear single ducted fan type composite wing aircraft as well as propeller thrust self-powering composite auxiliary wings, additional wings and manned cabins which are assembled on two sides of wings of the aircraft. The rear single ducted fan type composite wing manned 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 flight energy consumption is low, the hangtime is long, the safety is high and the like, the auxiliary wings adopt composite lift force, and the application range of power is ensured.

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 composite wing manned aircraft having double-propeller composite auxiliary wings with solar additional wings. The pushback-free composite wing aircraft comprises an aircraftbody, composite lift force wings fixedly mounted on two sides of the aircraft body, and additional wings, wherein the aircraft body adopts a deck platform; self-closing ducted fans are arranged in the composite lift force wings; wing hinges are designed on the outer sides of the composite lift force wings; batteries / fuels are arranged in the additional wings; solar battery panels are arranged onthe surfaces of the additional wings; a manned bin is mounted below the aircraft body. The composite wing manned aircraft disclosed by the invention has the characteristics of short take-off and landdistances, high flying speed, high wing structure intensity, capability of enabling the wings to store energy, low flying energy consumption, long hang time, high safety and the like; the auxiliary wings adopt composite lift force, so as to guarantee the application range of power.

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 back single ducted fan type compound wing manned craft with a propeller thrust compound auxiliary wing. The back single ducted fan type compound wing manned craft comprisesa body, compound lift force wings and a manned cabin fixedly mounted on two sides of the body, wherein the body is arranged as a deck platform; a self-closed ducted fan is arranged in the compound lift force wing, and a wing hinge is designed on the outer side of the compound lift force wing; a propeller thruster is arranged at the front end of the propeller thrust self energy-supplying compound auxiliary wing, the self-closed ducted fan is arranged in the propeller thrust self energy-supplying compound auxiliary wing, an electro-hydraulic-gas interface and the wing hinge are arranged on one side or two sides of the propeller thrust self energy-supplying compound auxiliary wing and are movably connected to the compound lift force wing through the wing hinge, and the manned cabin is mountedbelow the body. The back single ducted fan type compound wing manned craft not only has the characteristics of being short in landing and take-off distance, high in flying speed, high in strength ofwing structure, capable of storing energy by the wing, low in flying energy consumption, long in hang time, high in safety and the like. The auxiliary wing employs a compound lift force, so that the application range of power is ensured.

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.