WO2024021318A1

WO2024021318A1 - Method and device for aviation aircraft to use relative motion air kinetic energy

Info

Publication number: WO2024021318A1
Application number: PCT/CN2022/126101
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: CN117489487A

Abstract

A method and device for an aviation aircraft to use relative motion air kinetic energy, which, by means of a relative motion air kinetic energy recoil thrust generating device (9) provided on an aviation aircraft, highly amplify relative motion air kinetic energy two consecutive times by utilizing the flight speed of the aviation aircraft, and make same into enormous mechanical kinetic energy for propelling the aviation aircraft to travel fast.

Description

Methods and devices for using relative motion aerodynamic energy in aviation aircraft

Technical field

The invention relates to aviation power equipment, and in particular to a method and device for using relative motion aerodynamic energy for an aviation aircraft.

Background technique

Current aviation aircraft generally use fuel turbine engines as aviation power equipment. During their voyages, they must carry and consume a large amount of fuel, and at the same time produce a large amount of carbon dioxide exhaust gas. Due to the limited fuel it carries, its range is limited. Since the propulsion power of existing aviation engines is limited, the load capacity of existing aviation aircraft is also limited.

Currently, aviation aircraft powered by batteries have very limited storage capacity, which determines that the range of existing electric aviation aircraft is very limited.

Since a large amount of combustible fuel is always stored on existing aviation aircraft, once a safety accident occurs, it will usually cause an explosion, leading to aircraft crashes and fatalities.

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 collect the collected energy. The kinetic energy of relative motion is converted into recoil thrust that can propel the aircraft forward.

Contents of the invention

The object of the present invention is to provide a new method and device for using relative motion aerodynamic energy in an aerospace aircraft. A device for generating relative motion aerodynamic energy recoil thrust is provided on the aerospace aircraft so that it can generate a thrust force under fast traveling conditions. The huge recoil thrust propels the aircraft into the air and takes off, and it can have zero energy consumption, huge propulsion power, huge load capacity, and unlimited range and other outstanding technical advantages, thus creating an era of free flight for mankind!

Technical solutions

A technological method for using relative motion aerodynamic energy in an aerospace aircraft. The method is to install a relative motion aerodynamic energy recoil thrust generating device on the aerospace aircraft, so that it can utilize the relative motion aerodynamic energy provided in the aerospace aircraft under fast traveling conditions. The multiple relative motion air kinetic energy in the recoil thrust generating device collects the relative motion air kinetic energy collected by the impeller. While driving the generator to generate electricity, it first drives the turbine air compressor to compress the natural air, and then drives the propeller for propulsion. The device accelerates the compressed air generated by the turbine air compressor to be discharged outward. At the same time, it continuously uses the speed of the aircraft to greatly expand the air kinetic energy of the relative motion as the mechanical kinetic energy to propel the aircraft to travel quickly.

In the present invention, the condition of allowing the aircraft to travel quickly refers to the condition of allowing the aircraft to be parked on a rotating platform in a fast-rotating, relatively moving aerodynamic aircraft turntable lift airport in advance. To achieve lift-off and take-off; it can also be achieved by allowing the aircraft to be quickly pulled to a set speed by a tractor vehicle on the existing airport straight runway to achieve lift-off and take-off.

In the present invention, the aerodynamic energy of relative motion is continuously utilized twice at the same time to increase the speed of the aircraft at high times as a huge mechanical kinetic energy to propel the aircraft. One of them refers to the method based on

The physical formula of Collecting impeller, the collected relative motion aerodynamic energy is proportional to the cube of the aircraft speed. That is, if the speed of an aircraft increases by 10 times, its relative motion aerodynamic energy increases 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. Another one of them refers to using the relative motion air kinetic energy collected above to drive the generator to generate electricity. It first drives the turbine air compressor to compress the air, then drives the propeller propeller, and finally allows the propeller propeller to move the air. The compressed air generated by the turbine air compressor is accelerated and discharged, thereby forming a recoil thrust that propels the aircraft forward. The value of the mechanical kinetic energy formed by the above-mentioned recoil thrust to propel the aircraft forward is equal to the product of the recoil thrust and the aircraft speed.

A device for an aviation aircraft to use relative motion aerodynamic energy. It includes a main body of the aviation aircraft, a main wing, and a tail wing. It also includes a front compartment, a main compartment, and a rear compartment provided in the main body of the aviation aircraft. The lower part of the main body of the aviation aircraft is provided with a The load-bearing wheel is provided with a battery in the main body of the aviation aircraft. The aviation aircraft is provided with a relative motion aerodynamic energy recoil thrust generating device. A recoil thrust generating device shell is provided inside the relative motion aerodynamic energy recoil thrust generating device. The open chamber is equipped with relatively moving air kinetic energy collection impellers, downstream air automatic opening and closing shutters, generators, gearboxes, auxiliary shafts, main engine shafts, and turbine air compressors in the upper, lower, left, and right directions. The propeller propeller, the main engine shaft simultaneously drives the generator, turbine air compressor and propeller propeller, air inlet, compressed air channel, and recoil exhaust port.

In the present invention, the relative motion aerodynamic energy recoil thrust generating device on the aircraft means that it can be specially installed in the rear compartment of the aircraft, or it can be symmetrically placed on the left and right under the main wing of the aircraft. Its special setting can also be placed symmetrically on the left and right under the rear compartment of the aircraft and below the main wing. The relative motion aerodynamic energy recoil thrust generating device installed in the rear compartment of an aviation aircraft has a large volume and a large recoil thrust, and the number is only one. Compared with the relative motion aerodynamic energy recoil thrust generating device installed in the rear compartment, the relative motion aerodynamic energy recoil thrust generating device installed under the main wing of the aviation aircraft is smaller in size, its recoil thrust is smaller, and its number can be It's multiple objects.

In the present invention, the load-bearing wheel provided below the main body of the aircraft refers to a simple load-bearing wheel for the aircraft to rise and fall at the relative motion aerodynamic aircraft turntable lift airport, or it can be a simple load-bearing wheel at an existing airport. Landing gear for runway ascending and descending.

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

The invention adopts a relative motion aerodynamic energy recoil thrust generating device installed on an aviation aircraft, so that it can generate huge recoil thrust under fast traveling conditions, promote the aviation aircraft to quickly lift off and take off, and can have Zero energy consumption, huge propulsion power, huge load capacity, and unlimited range are all outstanding technical advantages, thus creating an 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 top view of the method and device structure for using relative motion aerodynamic energy in aviation aircraft.

Figure 2 is a schematic side view of the structure of a method and device for using relative motion aerodynamic energy in an aircraft.

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 aircraft of the present invention uses a relative motion aerodynamic energy device, and a relative motion aerodynamic energy recoil thrust generating device is provided on the aircraft, so that it can operate under fast traveling conditions. It generates huge recoil thrust, propelling aircraft into the air and take off quickly. At the same time, it can have zero energy consumption, huge propulsion power, huge load capacity, and various excellent technical advantages of unlimited range.

The characteristic of the process method for using relative motion aerodynamic energy in aviation aircraft according to the present invention is to set up a relative motion aerodynamic energy recoil thrust generating device on the aviation aircraft, so that it can use the relative motion aerodynamic energy recoil thrust generating device under fast traveling conditions. The multiple relative motion air kinetic energy in the moving air kinetic energy recoil thrust generating device collects the relative moving air kinetic energy collected by the impeller. While driving the generator to generate electricity, it first drives the turbine air compressor to compress the natural air, and then drives The propeller accelerates the compressed air generated by the turbine air compressor to be discharged outward. At the same time, it continuously uses the traveling speed of the aircraft and highly amplifies the relative motion aerodynamic energy as the mechanical kinetic energy to propel the aircraft forward quickly.

The physical formula of Collecting impeller, the collected relative motion aerodynamic energy is proportional to the cube of the aircraft speed. That is, if the speed of an aircraft increases by 10 times, its relative motion aerodynamic energy increases 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 one is to use the relative motion air kinetic energy collected above to drive the generator to generate electricity, first drive the turbine air compressor to convert it into compressed air, then drive the propeller propeller, and finally let the propeller propel The air compressor accelerates and discharges the compressed air generated by the turbine air compressor, thereby forming a recoil thrust that propels the aircraft forward. The value of the mechanical kinetic energy formed by the above-mentioned recoil thrust to propel the aircraft forward is equal to the product of the recoil thrust and the aircraft speed.

The aviation aircraft according to the present invention adopts the relative motion aerodynamic energy device and is implemented by the above method. As shown in Figures 1, 2, and 3, an aerodynamic device using relative motion for an aircraft includes an aircraft body 1, a main wing 2, and a tail wing 3; it also includes a front compartment provided in the aircraft body 1. 4. Main warehouse 5 and rear warehouse 6. A load-bearing wheel 7 is provided at the lower part of the main body 1 of the aircraft. A battery 8 is provided in the main body 1 of the aircraft. A relative motion aerodynamic energy recoil thrust generating device is provided on the aircraft. 9; A recoil thrust generating device housing 10 and an open chamber 11 are provided inside the relative motion aerodynamic energy recoil thrust generating device 9. In the open chamber, relative motion aerodynamic

energy collection impellers

12, 12, and 12 are arranged in the up, down, left, and right directions. Downstream air automatic opening and closing shutters 13, generator 14, gearbox 15, auxiliary shaft 16, main shaft 17, turbine air compressor 18, propeller propeller 21, main shaft 17 simultaneously drives generator 14, turbine air compressor Machine 18, propeller propeller 21, air inlet 19, compressed air channel 20, recoil exhaust port 22.

In the present invention, the relative motion aerodynamic energy recoil thrust generating device 9 is provided on the aircraft. It means that it can be installed separately in the rear compartment 6 of the aircraft body, or it can be symmetrically installed on the left and right under the main wing 2. It can also be arranged symmetrically on the left and right under the rear compartment 6 of the aircraft and the main wing 2 at the same time. The relative motion aerodynamic energy recoil thrust generating device 9 provided in the rear compartment 6 of the aircraft has a large volume and a large recoil thrust, and the number is only one. The relative motion aerodynamic energy recoil thrust generating device provided below the main wing 2 of the aircraft is smaller in size and smaller in recoil thrust than the relative motion aerodynamic energy recoil thrust generating device 9 provided in the rear compartment 6 . The quantity can be multiple.

In the present invention, the load-bearing wheel 7 provided below the main body 1 of the aircraft refers to a simple load-bearing wheel 7 for the aircraft to rise and fall in a relative motion aerodynamic aircraft turntable lift airport, or it can be an existing wheel 7 Landing gear ascending and descending on airport runway.

In the present invention, the main engine shaft 17 in the relative motion aerodynamic energy recoil thrust generating device 9 simultaneously drives the generator 14, the turbine air compressor 18 and the propeller propeller 21, which means that it can be the same main engine shaft, or it can be the same main engine shaft. It can be a concentric double-layer crankshaft with different speeds.

Referring to Figures 1, 2, and 3, the operating procedures for using a relative motion kinetic energy device in an aviation aircraft according to the present invention are as follows:

1. The aviation aircraft that has been designed and manufactured according to the requirements of this manual is placed in the release card position on the lifting and rotating platform in the relative motion aerodynamic aviation aircraft turntable lift airport, or it can also be placed on the fast-moving traction vehicle on the existing airport runway. in the car.

2. As the lifting rotating platform and the tractor travel, the relative motion aerodynamic energy recoil thrust generating device 9 installed on the aircraft converts the collected relative motion aerodynamic energy into a huge recoil while driving the generator 14 to generate electricity. Thrust, together with the relative motion speed between the aircraft and the air, forms a huge mechanical kinetic energy that propels the aircraft forward.

3. Release the aircraft.

4. The generator 14 and the battery 8 equipped on the aircraft jointly provide power for all electrical equipment on the aircraft. Before the relative motion aerodynamic energy recoil thrust generating device 9 is started, it is powered by the battery. After the relative motion aerodynamic energy recoil thrust generating device 9 is started, the generator 14 supplies power and charges the battery 8 .

5. During the flight of the space shuttle, the faster its speed, the greater the relative motion aerodynamic energy generated by the space shuttle. During its accelerated flight, its air downstream automatic switch shutter 13 is opened to the maximum, and at the same time, the rotation speed of the main engine shaft 17 is increased through the gearbox 15. During the deceleration flight of the aircraft, the opening degree of the air downstream automatic switch shutter 13 is reduced, and at the same time, the rotation speed of the main shaft 17 is slowed down through the gearbox 15.

6. When an aircraft lands on a relative motion aerodynamic aircraft turntable lift airport, it does not need to slow down and lands directly on the rotating platform. When landing on an existing airport runway, first turn off the lift device of the main wing 2 on the aircraft, and then turn off the relative motion aerodynamic energy recoil generating device 9 on the aircraft, allowing the aircraft to slide on the airport runway under the air resistance It slows down due to friction with the ground and finally stops.

The invention adopts a relative motion aerodynamic energy recoil thrust generating device installed on an aviation aircraft, so that it can generate huge recoil thrust under fast traveling conditions, promote the aviation aircraft to quickly lift off and take off, and can have The outstanding technical advantages of huge propulsion power, zero energy consumption, large load capacity, and unlimited range will usher in 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 method for aviation aircraft to use relative motion aerodynamic energy. In the early stage of this method, other mechanical power equipment is used to promote the aviation aircraft to generate a rapid traveling speed before taking off. It is characterized in that the process method of using relative motion aerodynamic energy is to use A relative motion aerodynamic energy recoil thrust generating device is provided on an aviation aircraft, allowing it to collect the energy collected by a plurality of relative motion aerodynamic energy collecting impellers provided in the relative motion aerodynamic energy recoil thrust generating device under fast traveling conditions. The kinetic energy of the relative motion of the air is obtained. While driving the generator to generate electricity, it first drives the turbine air compressor to compress the natural air, and then drives the propeller propeller to accelerate the compressed air generated by the turbine air compressor to be discharged. At the same time, the two For the first time, the aircraft's traveling speed is continuously used to greatly expand the relative motion aerodynamic energy as the mechanical kinetic energy to propel the aircraft forward rapidly.
The method according to claim 1, characterized in that in the present invention, the said allowing it to travel quickly means that the aircraft can be parked in advance on a fast-rotating relative motion aerodynamic aircraft turntable. Lift-off and take-off can be achieved under the working conditions of the rotating platform in the lift airport; it can also be achieved by allowing the aircraft to be quickly pulled to a set speed by a tractor vehicle on the existing straight runway of the airport. take off.
The method according to claim 1, characterized in that, in the present invention, the two simultaneous and continuous use of high-speed aerodynamic energy of the relative motion of the aircraft as a huge mechanical kinetic energy to propel the aircraft, one of which is based on
The physical formula of Collecting impeller, the collected relative motion aerodynamic energy is proportional to the cube of the aircraft speed. That is, if the speed of an aircraft increases by 10 times, its relative motion aerodynamic energy increases 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. Another one of them refers to using the relative motion air kinetic energy collected above to drive the generator to generate electricity. It first drives the turbine air compressor to compress the air, then drives the propeller propeller, and finally allows the propeller propeller to move the air. The compressed air generated by the turbine air compressor is accelerated and discharged, thereby forming a recoil thrust that propels the aircraft forward. The value of the mechanical kinetic energy formed by the above-mentioned recoil thrust to propel the aircraft forward is equal to the product of the recoil thrust and the aircraft speed.
A device for an aviation aircraft to use relative motion aerodynamic energy. It includes a main body of the aviation aircraft, a main wing, and a tail wing. It is characterized in that it also includes a front compartment, a main compartment, and a rear compartment provided in the main body of the aviation aircraft. A load-bearing wheel is provided at the lower part of the main body of the aircraft, a battery is provided in the main body of the aviation aircraft, a relative motion aerodynamic energy recoil thrust generating device is provided on the aviation aircraft, and a recoil thrust is provided inside the relative motion aerodynamic energy recoil thrust generating device. The generating device casing is an open chamber. In the open chamber, there are relatively moving air kinetic energy collection impellers, downstream air automatic opening and closing shutters, generators, gearboxes, auxiliary shafts, main engine shafts, and turbines arranged in the upper, lower, left, and right directions. Type air compressor, propeller propeller, the main shaft simultaneously drives the generator, turbine air compressor and propeller thruster, air inlet, compressed air channel, and recoil exhaust port.
The device according to claim 4, characterized in that in the present invention, the relative motion aerodynamic energy recoil thrust generating device on the aircraft means that it can be specially installed in the rear compartment of the aircraft, or it can It can be specially set up symmetrically on the left and right below the main wing of the aircraft, or it can also be set up symmetrically on the left and right below the rear compartment of the aircraft and below the main wing. The relative motion aerodynamic energy recoil thrust generating device installed in the rear compartment of an aviation aircraft has a large volume and a large recoil thrust, and the number is only one. Compared with the relative motion aerodynamic energy recoil thrust generating device installed in the rear compartment, the relative motion aerodynamic energy recoil thrust generating device installed under the main wing of the aviation aircraft is smaller in size, its recoil thrust is smaller, and its number can be It's multiple objects.
The device according to claim 4, characterized in that in the present invention, the load-bearing wheel is provided below the main body of the aircraft, which can be a simple way for the aircraft to rise and fall at the relative motion aerodynamic aircraft turntable lift airport. It can be a load-bearing wheel or a landing gear that can be lifted and landed on an existing airport runway.
The device according to claim 4, characterized in that in the present invention, the main engine shaft drives the generator, the turbine air compressor and the propeller propeller at the same time, which means that it can be the same main engine shaft, or it can be a kind of main engine shaft. Concentric double-layer crankshaft with different speeds.