WO2024021319A1

WO2024021319A1 - Turntable type lifting airport for relative motion air kinetic energy aviation aircraft

Info

Publication number: WO2024021319A1
Application number: PCT/CN2022/126102
Authority: WO
Inventors: 易元明
Original assignee: 易元明; 吴桓勋
Priority date: 2022-07-25
Filing date: 2022-10-19
Publication date: 2024-02-01
Also published as: CN117508624A

Abstract

A turntable type lifting airport device for a relative motion air kinetic energy aviation aircraft. A plurality of relative motion air kinetic energy reversal thrust generating devices (3) are provided on the periphery of a lower portion of an aviation aircraft lifting and rotating platform (5), which is arranged on a turntable type lifting airport; a high-pressure air spraying pipe (15) in a reversal thrust structural layer (6) is used for providing early-stage starting thrust, the relative motion air kinetic energy reversal thrust generating devices (3) are used for providing normal reversal thrust, and the aviation aircraft lifting and rotating platform (5) with a large diameter is used for providing an ultra-long force arm; and mechanical kinetic energy for pushing the aviation aircraft lifting and rotating platform (5) is formed by continuously using the rotating speed of the aviation aircraft lifting and rotating platform (5) and the relative motion air kinetic energy expanded by multiple times, so that large-scale power generation and zero-energy-consumption lifting of the aviation aircraft are achieved.

Description

Relative motion aerodynamic aviation aircraft carousel lift airport

Technical field

The invention relates to an aircraft lift airport, and in particular to a relative motion aerodynamic aircraft turntable lift airport.

Background technique

Current aviation aircraft must build airports with longer runways to carry out take-off, take-off and landing. At the same time, the aircraft must be accelerated over a long distance on the airport runway to achieve takeoff; similarly, the aircraft must be decelerated over a long distance on the airport runway to achieve a smooth landing.

Currently, aviation aircraft powered by fuel engines must consume a large amount of fuel during takeoff. In order to achieve lift-off, take-off and landing, expensive landing gear must be installed at the bottom of the aircraft, and aviation accidents usually occur during the take-off and landing stages of aviation aircraft.

The existing "Method and Device for Collecting and Utilizing Relative Motion Kinetic Energy of Vehicles" and "Method and Device for Simultaneously Utilizing Positive and Negative Pressure Relative Motion Kinetic Energy" technical inventions only provide a propeller propeller at the front end of the vehicle, which cannot effectively move all the vehicles. The collected kinetic energy of relative motion is converted into recoil thrust that can propel the vehicle forward.

Contents of the invention

The object of the present invention is to provide a new relative motion aerodynamic energy aircraft rotary table lift airport method and its device, which adopts the lower peripheral portion of the aviation aircraft lifting and lowering rotating platform on the rotary table lift airport, and multiple relative motion aerodynamic energy tools are provided. The recoil thrust generating device allows it to generate recoil thrust when the aircraft lifting and rotating platform rotates rapidly. At the same time, the large-diameter aircraft lifting and rotating platform that rotates around the axis is used to work on the early start-up thrust and the above-mentioned recoil thrust, providing an ultra-long At the same time, the rotational speed of the aircraft lifting and rotating platform and the high-magnification aerodynamic energy of the relative motion are continuously used twice at the same time as the huge mechanical kinetic energy to promote the rotation of the aircraft lifting and rotating platform. Therefore, while ensuring that the aircraft lifting and rotating platform can achieve large-scale power generation through the main shaft and gearbox-driven generator, it can also achieve zero energy consumption for aircraft lift-off, take-off and smooth landing at high speed. Since the aircraft no longer needs to run long distances with load when lifting and landing on the aircraft lifting and rotating platform, the original expensive landing gear is no longer needed. The above-mentioned technical performance, coupled with the propulsion power of aviation aircraft using relative motion aerodynamic energy, huge load capacity, and many outstanding technical advantages of unlimited range, have successfully opened the era of human free flight!

Technical solutions

A process method for relatively moving aerodynamic energy aircraft carousel lifts. The method is to use multiple relative motion aerodynamic energy recoil thrust generating devices at the lower periphery of the aircraft lifting rotating platform on the carousel lift airport, so that It generates recoil thrust when the aircraft lifting and rotating platform rotates rapidly. At the same time, it uses the large-diameter aircraft lifting and rotating platform that rotates around the axis to work on the early starting thrust and the above-mentioned recoil thrust, providing an ultra-long moment arm, and simultaneously performs two consecutive The rotation speed of the aircraft lifting and rotating platform and the high-magnification relative motion aerodynamic energy are used as the huge mechanical kinetic energy to promote the rotation of the aircraft lifting and rotating platform. Thus, while ensuring that the aviation aircraft lifting and rotating platform achieves large-scale power generation through the main shaft and gearbox-driven generator, it also achieves the technical effect of zero energy consumption for aircraft lift-off, take-off and smooth landing at high speed.

In the present invention, the relative motion aerodynamic energy recoil thrust generating device utilizes relative motion aerodynamic energy collecting impellers arranged in the up, down, left and right directions in the open cabin at the front end of the device. The mechanical kinetic energy generated by the positive and negative pressure and the relative movement speed between the aircraft lifting and rotating platform and the air first drives the turbine air compressor set at the rear end of the device to compress the natural air, and then drives the turbine air compressor set at the rear end of the device to compress the natural air. The propeller propeller at the end of the device finally accelerates the compressed air generated by the turbine air compressor to be discharged outward, thereby forming a recoil thrust that promotes the rapid rotation of the aircraft lifting and rotating platform.

In the present invention, the rotation speed of the aircraft lifting and rotating platform and the high magnification of the relative motion aerodynamic energy are continuously used twice at the same time as the huge mechanical kinetic energy to promote the rotation of the aircraft lifting and rotating platform. One of them refers to the basis

The physical formula of The relative motion aerodynamic energy collected in the impeller is proportional to the cube of the rotation speed of the aircraft lifting and rotating platform. That is, the rotation speed of the aircraft lifting and rotating platform is increased by 10 times, and the relative motion aerodynamic energy generated is increased by 1,000 times. Due to the setting of the air downstream automatic opening and closing shutters, the positive and negative sides of the relative motion air kinetic energy collection impeller bear the positive and negative air pressure at the same time, and the collected relative motion air kinetic energy is doubled again. The other time is to use the collected relative motion air kinetic energy to first drive the turbine air compressor to compress the air, and then drive the propeller propeller to accelerate the compressed air and convert it into recoil thrust. This creates mechanical kinetic energy that drives the aircraft lifting and rotating platform to rotate. Its value is equal to the product of the above-mentioned recoil thrust and the rotation speed of the aircraft lifting platform.

A relative motion aerodynamic aircraft turntable lift airport device, including an aircraft, its parking site, and a waiting hall; it also includes an aircraft lifting and rotating platform, and there are generators, gearboxes, and elevators on the ground floor of the waiting hall. Elevator transition zone, temporary upper and lower access channels for aircraft, load-bearing pillars, ring beams of load-bearing runner that support the gravity of the upper floor, large liquid air storage tanks, high-pressure working fluid pumps, and aircraft lifts above the waiting hall The rotating platform, the recoil thrust structural layer, the structural bracket, a plurality of relative motion aerodynamic energy recoil thrust generating devices are provided in the inner peripheral part of the recoil thrust structural layer, and a recoil thrust generating device is provided inside the relative motion aerodynamic energy recoil thrust generating device The casing of the thrust generating device is an open chamber. There are relatively moving air kinetic energy collection and utilization impellers at the upper, lower, left and right positions in the open chamber. The downstream air automatically opens and closes the shutters to carry out kinetic energy transmission and speed changes in rotation speed and rotation direction. The box has an auxiliary shaft that transmits the kinetic energy of the relative motion of the air, a main shaft that drives the turbine air compressor and propeller propeller, an air inlet and compressed air channel that sends air to the turbine air compressor, and a propeller. Recoil exhaust port for propeller exhaust; an airport canopy cover is provided on the aircraft lifting and rotating platform, an aircraft release card sleeve, a landing positioning card sleeve, an aircraft shift tractor, and an aircraft temporary upper and lower position. At the entrance and exit, there is a liquid air heat-absorbing and vaporization pipe network fixedly connected to the platform plate on the lower layer of the aviation aircraft lifting and rotating platform. There are multiple symmetrical high-pressure air nozzles around the recoil thrust structure layer. The recoil thrust There are multiple load-bearing wheels on the bottom plate of the structural layer.

In the present invention, the main engine shaft that drives the turbine air compressor and the propeller propeller can be the same main engine shaft, or it can be a concentric double-layered machine shaft with different rotational speeds.

In the present invention, the multiple load-bearing wheels provided on the bottom plate of the recoil thrust structure layer refer to the method of transmitting the gravity of the upper layer mechanically, or the method of transmitting the gravity of the upper layer using electromagnetic magnetic levitation.

In the present invention, a plurality of left and right symmetrical relative motion aerodynamic energy recoil thrust generating devices are provided at the inner periphery of the recoil thrust structure layer. This means that there can be 8 devices, 16 devices, or 16 devices. Can be more than 16 pieces.

The invention adopts multiple relative motion aerodynamic energy recoil thrust generating devices at the lower peripheral area of the aircraft lifting and rotating platform on the turntable lift airport, allowing them to generate recoil thrust when the aircraft lifting and rotating platform rotates rapidly, and at the same time utilizes The large-diameter aircraft lifting and rotating platform that rotates around the axis provides an ultra-long moment arm for the early start-up thrust and the above-mentioned recoil thrust. At the same time, the rotation speed of the aircraft lifting and rotating platform is continuously used twice to highly amplify the relative motion aerodynamic energy as a propulsion The huge mechanical kinetic energy of the aircraft lifting and rotating platform rotates. This ensures that the aviation aircraft lifting and rotating platform can achieve large-scale power generation through the main shaft and gearbox-driven generator, and at the same time achieve zero energy consumption for aircraft lift-off, take-off and smooth landing at high speed. Since the aircraft no longer needs to run long distances with a load when lifting and landing on the aircraft lifting and rotating platform, the original expensive landing gear is no longer needed. With the technical performance mentioned above, coupled with the fact that aircraft using relative motion aerodynamic energy do not need to burn fuel or consume electricity, their propulsion power and load capacity are huge, and they can have unlimited range and many outstanding technical advantages, thus successfully opening the era of human free flight. !

Description of drawings

The present invention will be described in detail below with reference to the accompanying drawings.

Figure 1 is a schematic structural diagram of a rotary lift airport for relative motion aerodynamic aviation aircraft.

Figure 2 is a schematic top view of the relative motion aerodynamic aviation aircraft turntable lift airport.

Figure 3 is a schematic structural diagram of a relative motion aerodynamic energy recoil thrust generating device.

Detailed ways

Referring to Figures 1, 2, and 3, the relative motion aerodynamic energy aircraft turntable lift airport device of the present invention adopts multiple relative motion aerodynamic energy devices at the lower peripheral portion of the aircraft lift rotating platform in the turntable lift airport. The recoil thrust generating device allows it to generate recoil thrust when the aircraft lifting and rotating platform rotates rapidly. At the same time, the large-diameter aircraft lifting and rotating platform that rotates around the axis provides an ultra-long moment arm for the early start-up thrust and the above-mentioned recoil thrust. At the same time, the rotation speed of the aircraft lifting and rotating platform is continuously used twice to highly amplify the relative motion aerodynamic energy as a huge mechanical kinetic energy to promote the rotation of the aircraft lifting and rotating platform. This ensures that the aviation aircraft lifting and rotating platform can achieve large-scale power generation through the main shaft and gearbox-driven generator, and at the same time achieve zero energy consumption for aircraft lift-off, take-off and smooth landing at high speed. Since the aircraft no longer needs to run long distances with a load when lifting and landing on the aircraft lifting and rotating platform, the original expensive landing gear is no longer needed. The above-mentioned technical performance, coupled with the propulsion power and huge load capacity of aviation aircraft that use relative motion aerodynamic energy, have unlimited range and many excellent range technical advantages, thus successfully opening the era of human free flight!

The characteristic of the process method of the relative motion aerodynamic energy aircraft turntable lift airport according to the present invention is that the lower peripheral part of the aircraft lift rotating platform on the turntable lift airport is used, and multiple relative motion aerodynamic energy recoil thrust generation tools are provided. The device allows it to generate recoil thrust when the aircraft lifting and rotating platform rotates rapidly. At the same time, the large-diameter aircraft lifting and rotating platform that rotates around the axis is used to work on the early start-up thrust and the above-mentioned recoil thrust, and provides an ultra-long moment arm. At the same time, Twice, the rotation speed of the aircraft lifting platform rotating platform and the high-magnification amplified relative motion aerodynamic energy are used as the huge mechanical kinetic energy to promote the rotation of the aircraft lifting platform. This ensures that the aviation aircraft lifting and rotating platform can achieve large-scale power generation through the main shaft and gearbox-driven generator, and at the same time achieve zero energy consumption for aircraft lift-off, take-off and smooth landing at high speed.

In the present invention, the relative motion aerodynamic energy recoil thrust generating device utilizes relative motion aerodynamic energy collection impellers arranged in the up, down, left and right directions in the open cabin at the front end of the device. , the mechanical kinetic energy generated by the negative pressure and the relative movement speed between the aircraft lifting and rotating platform and the air first drives the turbine air compressor set at the rear end of the device to compress the natural air, and then drives the turbine air compressor set at the rear end of the device to compress the natural air. The propeller propeller at the end accelerates the compressed air generated by the turbine air compressor to the outside, thus forming a recoil thrust that promotes the rapid rotation of the aircraft lifting and rotating platform.

The physical formula of The relative motion aerodynamic energy collected by the impeller is proportional to the cube of the rotation speed of the aircraft lifting and rotating platform. That is, the rotation speed of the aircraft lifting and rotating platform is increased by 10 times, and the relative motion aerodynamic energy generated is increased by 1,000 times. Due to the setting of the air downstream automatic opening and closing shutters, the positive and negative sides of the relative motion air kinetic energy collection impeller bear the positive and negative air pressure at the same time, and the collected relative motion air kinetic energy is doubled again. The other time is to use the collected relative motion air kinetic energy to first drive the turbine air compressor to compress the air, and then drive the propeller propeller to accelerate the compressed air and convert it into recoil thrust. This creates mechanical kinetic energy that drives the aircraft lifting and rotating platform to rotate. Its value is equal to the product of the above-mentioned recoil thrust and the rotation speed of the aircraft lifting platform.

The relative motion aerodynamic aircraft turntable lift airport device according to the present invention is implemented using the above method. As shown in Figures 1, 2, and 3, a relative motion aerodynamic aircraft turntable lift airport device includes: an aircraft 22 and its parking site, and also includes an aircraft lifting and rotating platform 5, which is constructed on the ground floor. Airport hall 4 is equipped with a generator 1, a gearbox 2, and a rotating shaft 11 at the center of the airport ground floor. There are multiple elevators 7 near the center, an elevator transition zone 8, and temporary upper and lower access channels for aviation aircraft. 9. A large liquid air storage tank 10, a high-pressure working medium pump 35, a load-bearing pillar 12, a load-bearing ring beam 14 set on the load-bearing pillar 12, an aviation aircraft lifting and rotating platform 5 at the upper part of the terminal hall 4, and a counter-rotating platform 5. The thrust structure layer 6, the structural bracket 23, and the aircraft temporary upper and lower entrances and exits 21 are provided with a plurality of left and right symmetrical relative motion aerodynamic energy recoil thrust generating devices 3 in the surrounding parts of the recoil thrust structure layer 6. , on the vertical edge of the periphery of the aircraft lifting and rotating platform 5, corresponding to the installation section of the relative motion aerodynamic energy recoil thrust generating device 3, an air downstream automatic opening and closing shutter 28 is provided, and the air kinetic energy recoil thrust is generated between the two relatively moving aerodynamic energy recoil thrust generating devices. The recoil thrust structural layer 6 between the devices 3 has openings on the outside for air intake; inside the relative motion aerodynamic energy recoil thrust generating device 3, a recoil thrust generating device housing 24 and an open chamber 27 are provided. , there are relative motion aerodynamic energy collection and utilization impellers 25 in the downward, left and right directions, and at the same time, there are air downstream automatic opening and closing shutters 28, an auxiliary machine shaft 34, a main engine shaft 32, a gearbox for transmitting kinetic energy and converting speed and rotation direction. 26. There is a turbine air compressor 29 and a propeller propeller 30 driven by the main engine shaft 32; there is an air inlet 36 for providing air for the turbine air compressor 29 and a compressed air channel 33 for providing air outlet; there is a propeller propeller. 30 exhaust recoil exhaust port 31; an airport shed cover 17 is provided over the center of the aircraft lifting and rotating platform 5, and a release card sleeve 18 is provided at the periphery of the board surface of the aircraft lifting and rotating platform 5. Landing positioning The ferrule 19 and the aircraft displacement tractor 20 have a plurality of symmetrically arranged high-pressure air nozzles 15 around the recoil thrust structure layer 6 , and a plurality of load-bearing runners 14 are disposed on the bottom plate of the recoil thrust structure layer 6 .

In the present invention, the main engine shaft 32 that drives the turbine air compressor 29 and the propeller propeller 30 may be the same main engine shaft, or may be a concentric double-layered machine shaft with different rotational speeds.

In the present invention, the load-bearing wheels 14 provided below the bottom plate of the recoil thrust structure layer 6 refer to the method of transmitting the gravity of the upper layer mechanically, or the method of transmitting the gravity of the upper layer using magnetic levitation.

In the present invention, a plurality of left and right symmetrical relative motion aerodynamic energy recoil thrust generating devices are provided at the inner peripheral part of the recoil thrust structure layer 6, which means that there can be 8 devices or 16 devices. It can also be more than 16 pieces.

Referring to Figures 1, 2, and 3, the operating procedures for a relative motion aerodynamic aircraft turntable lift airport device according to the present invention are as follows:

1. After all the above-mentioned projects are completed, the temporary upper and lower entrances 21 of the aircraft installed on the lifting and rotating platform 5 will be retained, and the aircraft 22 will be temporarily moved from the ground parking lot to the air flight by the aircraft shift tractor 20 The upper and lower access channels 9 enter the set position on the aircraft lifting and rotating platform 5. After completion, the structural components that fill the temporary upper and lower entrances and exits 21 of the aircraft will be assembled. In the future, when aircraft require major maintenance and new aircraft are admitted, the above procedures will also be followed.

2. Turn on the liquid air production device that is powered by an external power supply and is installed near the relative motion aerodynamic aircraft carousel airport, let it produce liquid air, and inject the produced liquid air into the carousel lift airport ground. The large liquid air storage tank 10 of the first layer is filled until it is full.

3. Turn on the high-pressure working medium pump 35, apply high pressure to the liquid air in the large liquid air storage tank 10, and then pump it into the liquid air arranged under the metal plate surface of the aircraft lifting and rotating platform 5 and fixedly connected to it to absorb heat and vaporize The pipe network 16 allows it to absorb heat and vaporize into high-pressure air. Finally, the high-pressure air is input to the high-pressure air nozzle 15 symmetrically arranged in the recoil thrust structure layer 6, and is ejected into the natural space. The resulting starting thrust and the ultra-long moment arm provided by the large-diameter aircraft lifting and rotating platform jointly form a huge power moment and mechanical kinetic energy that drives the aircraft lifting and rotating platform to rotate.

4. Open the downstream air automatic switch shutters 28 arranged in sections around the recoil thrust structure layer 6, and simultaneously open multiple symmetrically arranged relative moving air kinetic energy recoil thrust generating devices 3 to collect and utilize the relative moving air kinetic energy. The impeller 25 rotates, and at the same time drives the turbine air compressor 29 and the propeller propeller 30 to operate through the gearbox 2 and the main engine shaft 32, generating recoil thrust to promote the aircraft lifting and rotating platform to accelerate rotation.

5. When the rotational speed of the aircraft lifting and rotating platform 5 reaches the set value, the high-pressure air nozzle 15 stops spraying and the high-pressure working medium pump 35 stops working.

6. When the rotation speed of the aviation aircraft lifting and rotating platform 5 reaches the set speed and realizes rapid rotation operation, the recoil thrust generated by the relative motion aerodynamic energy recoil thrust generating device 3 and the large diameter aviation aircraft lifting and rotating platform 5 provide The ultra-long force arms together form a huge power moment and mechanical kinetic energy that promotes the rotation of the aircraft lifting and rotating platform. The resistance torque endured by the aircraft lifting and rotating platform 5 is only the electromagnetic resistance torque, air resistance torque and friction resistance torque in the generator. Once the gravity of the upper equipment is transmitted by the magnetic levitation device, only the air resistance torque and the electromagnetic resistance torque are left. Through multiple settings and multiple openings of the relative motion aerodynamic energy recoil thrust generating device 3, large-scale power generation by the generator 1 can be fully guaranteed. The lift-off, take-off and high-speed landing process of the aircraft 22 will not only increase the resistance moment of the aircraft lifting and rotating platform 5, but on the contrary, can also partially increase the rotational power moment of the aircraft lifting and rotating platform 5. Therefore, the rotation speed of the generator 1 is adjusted through the main shaft 11 and the gearbox 2, so that it can operate under load to generate electricity and at the same time supply a large amount of power to the outside.

7. Powered by the generator 1, start the liquid air production device installed near the relative motion aerodynamic aviation aircraft turntable lift airport, and let it inject the produced liquid air into the large liquid air storage tank 10 installed on the ground floor of the airport. , so that the aircraft lifting and rotating platform 5 can be started to rotate next time.

8. After the rotation speed of the release card sleeve 19 set on the plane lift rotating platform 5 reaches the flight speed of the aircraft, passengers and cargo can enter the elevator 7 through the elevator transition zone 8 and arrive at the airport from the ground. The aircraft lifts and rotates the platform 5, and boardes the aviation aircraft 22. Then, the aircraft 22 is moved to the release card sleeve 19 position by the aircraft shifting tractor 20 . Before the aircraft reaches the position of the release sleeve 19, the wing lift generating device of the aircraft 22 is turned off, and the relative motion aerodynamic energy recoil thrust generating device 3 provided inside the aircraft 22 is also closed.

9. Turn on the wing lift generating device on the aircraft 22 that is staying on the aircraft lifting and rotating platform 5 at the position of the flight card sleeve 19, and at the same time open the relative motion aerodynamic energy recoil thrust generating device 3, so that the aircraft 22 can When the aircraft lift rotating platform 5 rotates rapidly, it generates huge lift and thrust to propel the aircraft into the air and fly. Then the flight card sleeve 19 is opened according to the instructions issued by the aviation dispatch room, allowing the aviation aircraft 22 to take off, take off, and fly quickly with zero energy consumption.

10. After returning to the airport and arriving from the local airport, the aircraft 22 is allowed to adjust the wing lift, and then land smoothly and safely on the aircraft lifting and rotating platform 5 at high speed. After landing, use the positioning ferrule 18 to fix it on the aircraft lifting and rotating platform 5. Then, the wing lift device of the aircraft 22 is closed, and the relative motion aerodynamic energy recoil thrust generating device 3 onboard the aircraft 22 is closed at the same time. Then, use the aircraft mobile tractor 20 to move the landed aircraft 22 to the vicinity of the airport canopy 17 to unload passengers and cargo. Passengers and cargo unloaded from the aircraft arrive at the ground via the elevator 7 and the elevator transition zone 8 to complete their shipping process.

11. When the aircraft 22 landing on the aircraft lifting and rotating platform 5 needs large-scale maintenance, first stop the generator 1 to generate electricity, and gradually close the relative motion aerodynamic energy recoil thrust generating device provided around the recoil thrust structure layer 6 3. Let the aircraft lifting and rotating platform 5 stop operating under the action of air resistance. Then, open the temporary upper and lower entrances and exits 21 of the aircraft, and use the aircraft shift tractor 20 to push the aircraft 22 to the ground through the temporary upper and lower entrances and exits 9 for maintenance.

The present invention adopts multiple relative motion aerodynamic energy recoil thrust generating devices installed at the lower periphery of the aircraft lifting and rotating platform in the rotary lift airport, allowing them to generate recoil thrust when the aircraft lifting and rotating platform rotates rapidly. At the same time, it utilizes the surrounding The axis-rotating large-diameter aircraft lifting and rotating platform provides an ultra-long moment arm for the initial startup thrust and the above-mentioned recoil thrust. At the same time, the rotating speed of the aircraft lifting and rotating platform is continuously used twice to highly amplify the relative motion aerodynamic energy as a propellant for aviation. The huge mechanical kinetic energy of the aircraft lifting and rotating platform. This ensures that the aviation aircraft lifting and rotating platform can achieve large-scale power generation through the main shaft and gearbox-driven generator, and at the same time achieve zero energy consumption for aircraft lift-off, take-off and smooth landing at high speed. Since aviation aircraft no longer need to run long distances with loads when ascending and landing on a rotating platform, the original expensive landing gear is no longer needed. The above-mentioned technical performance, coupled with the propulsion power and huge load capacity of aviation aircraft using relative motion aerodynamic energy, and many excellent technical advantages of unlimited range, thus successfully opened the era of human free flight!

The principle, industrial and commercial application of the present invention are all included in the scope of the claims of the present invention, and any improved technology based on this is taken from the claims of the present invention.

Claims

A relative motion relative motion aerodynamic energy aviation aircraft carousel type lift airport process method, the method adopts starting power equipment in advance to promote the aviation aircraft lifting and rotating platform to rotate rapidly; It is characterized in that the aviation aircraft lifting and landing on the carousel type lift airport is used At the periphery below the rotating platform, there are many relative motion aerodynamic energy recoil thrust generating devices, allowing them to generate recoil thrust when the aircraft lifting and rotating platform rotates rapidly. At the same time, the large-diameter aircraft lifting and rotating platform that rotates around the axis is used as the early stage. The starting thrust and the above-mentioned recoil thrust work together to provide an ultra-long moment arm. At the same time, the rotation speed of the aircraft lifting and rotating platform is continuously used twice to highly expand the relative motion aerodynamic energy as a huge mechanical kinetic energy to promote the rotation of the aircraft lifting and rotating platform. Thus, while ensuring that the aviation aircraft lifting and rotating platform achieves large-scale power generation through the main shaft and gearbox-driven generator, it also achieves the technical effect of zero energy consumption for aircraft lift-off, take-off and smooth landing at high speed.
The method according to claim 1, characterized in that in the present invention, the relative motion aerodynamic energy recoil thrust generating device utilizes relative motions arranged in the up, down, left and right directions in the open cabin at the front end of the device. The moving air kinetic energy is collected by the impeller. The mechanical kinetic energy generated under the combined action of the positive and negative pressures the impeller bears and the relative movement speed between the aircraft's lifting and rotating platform and the air first drives the turbine air turbine installed at the rear end of the device. The compressor compresses the natural air, and then drives the propeller propeller set at the end of the device. Finally, the propeller propeller accelerates the compressed air generated by the turbine air compressor to be discharged, thus forming a mechanism that promotes the rapid rotation of the aircraft lifting and rotating platform. Recoil thrust.
The method according to claim 1, characterized in that in the present invention, the rotating speed of the aircraft lifting and rotating platform and the high magnification of the relative motion aerodynamic energy are used twice and simultaneously as the huge mechanical kinetic energy to promote the rotation of the aircraft lifting and rotating platform. , one of which refers to the basis
The physical formula of The relative motion aerodynamic energy collected in the impeller is proportional to the cube of the rotation speed of the aircraft lifting and rotating platform. That is, the rotation speed of the aircraft lifting and rotating platform is increased by 10 times, and the relative motion aerodynamic energy generated is increased by 1,000 times. Due to the setting of the air downstream automatic opening and closing shutters, the positive and negative sides of the relative motion air kinetic energy collection impeller bear the positive and negative air pressure at the same time, and the collected relative motion air kinetic energy is doubled again. The other time is to use the collected relative motion air kinetic energy to first drive the turbine air compressor to compress the air, and then drive the propeller propeller to accelerate the compressed air and convert it into recoil thrust. This creates mechanical kinetic energy that drives the aircraft lifting and rotating platform to rotate. Its value is equal to the product of the above-mentioned recoil thrust and the rotation speed of the aircraft lifting platform.
A relative motion aerodynamic aircraft turntable airport device, which includes an aircraft, its parking site, and a waiting hall; it is characterized in that it also includes an aircraft lifting and rotating platform, and a generator on the ground floor of the waiting hall , gearbox, elevator, elevator transition zone, temporary upper and lower access channels for aircraft, load-bearing pillars, ring beams of load-bearing runner that support the gravity of the upper floor, large liquid air storage tanks, high-pressure working fluid pumps, in the waiting hall There is an aircraft lifting and rotating platform, a recoil thrust structural layer, and a structural bracket. A plurality of relative motion aerodynamic energy recoil thrust generating devices are provided in the inner peripheral part of the recoil thrust structural layer. When the relative motion air kinetic energy recoil thrust is generated, The device is equipped with a recoil thrust generating device shell and an open chamber. There are relative moving air kinetic energy collection and utilization impellers at the upper, lower, left and right positions in the open chamber. The downstream air automatically opens and closes the shutters to transfer kinetic energy and rotate speed. , a gearbox that changes the direction of rotation, has an auxiliary shaft that transmits the kinetic energy of the relative motion of the air, a main shaft that drives the turbine air compressor and propeller, and an air inlet and compression port that sends air to the turbine air compressor. The air channel has a recoil exhaust port for exhausting the propeller propeller; an airport canopy cover is provided on the lifting and rotating platform of the aviation aircraft, aviation aircraft, flight card sleeves, landing positioning clamps, aviation aircraft shifting tractors, aviation For the temporary upper and lower entrances and exits of the aircraft, a liquid air heat-absorbing and vaporizing pipe network fixedly connected to the platform plate is provided on the lower layer of the aircraft lifting and rotating platform, and multiple symmetrical high-pressure air pipes are installed around the recoil thrust structure layer. The nozzle and the bottom plate of the recoil thrust structure layer are provided with multiple load-bearing runners.
The device according to claim 4, characterized in that in the present invention, the main engine shaft that drives the turbine air compressor and the propeller propeller can be the same main engine shaft, or a concentric, Double-layer crankshafts with different speeds.
The device according to claim 4, characterized in that in the present invention, the load-bearing runner provided on the bottom plate of the recoil thrust structure layer can be a method of mechanically transmitting the gravity of the upper layer, or it can be It uses electromagnetic magnetic levitation to transmit the gravity of the upper layer.
The device according to claim 4, characterized in that in the present invention, a plurality of left and right symmetrical relative motion aerodynamic energy recoil thrust generating devices are provided at the inner periphery of the recoil thrust structure layer. It can be 8, it can be 16, or it can be more than 16.