Aircraft capable of realizing free flight of human beings

Abstract

The invention relates to the technical field of flight, and discloses an aircraft capable of realizing free flight of human beings, the aircraft comprises an aircraft main body, when the aircraft is used, a micro turbine engine, a wing I and a wing II are arranged, a vector micro turbine engine is carried on the waist of the human beings, and the micro turbine engine generates vertical lifting force, so that the free flight of the human beings is realized. About 95% of the dead weight of the human body can be effectively counteracted, in-situ take-off of the human body is helped, meanwhile, the movable bionic wing membranes from the shoulders to the wrists adopt carbon fiber frameworks and self-adaptive skin structures, the first wing and the second wing are driven to do wing flapping motion through waving of back muscle groups and arms, and the wing flapping effect is achieved. Therefore, the high-efficiency thrust device fixed on the human body can help the human to take off in situ, and the wing I and the wing II can fly in the air like a bird, so that the flat-bottom take-off can be realized, and the free flying of the human in the true sense can be realized.

Description

Technical Field

[0001] The present invention relates to the technical field of human flight technology, and specifically relates to an aircraft capable of realizing human free flight. Background Art

[0002] Humans are the most intelligent creatures existing on the earth, belonging to the family Hominidae of the order Primates. We have highly developed brains, capable of abstract thinking, language communication, and tool manufacturing. By walking upright and liberating our hands, humans have created a splendid civilization and established a complex social structure. From a biological perspective, humans originated in Africa about 200,000 years ago and have developed a unique cultural inheritance ability through long-term evolution. Modern humans are distributed all over the world, forming diverse races and cultures. We can not only transform the natural environment but also face global challenges such as ecological protection. As the only species on earth that can massively change the ecosystem, humans are constantly exploring their position and responsibility in the universe.

[0003] However, there are still some disadvantages. For example: Since humans live on the earth and are affected by the earth's gravity, they cannot fly in place like birds and need to overcome their own body weight to achieve flight. The streamlined cross-section and feather arrangement of bird wings can generate vortex lift, while the shape and surface area of human arms are far from reaching the aerodynamic efficiency required for flight. Even through a running jump, the hang time is still less than one second, far lower than the flight requirements.

[0004] To solve the above problems, an aircraft capable of realizing human free flight is proposed in this application. Summary of the Invention

[0005] The purpose of the present invention is to provide an aircraft capable of realizing human free flight, so as to solve the problems mentioned in the above background art, that is, since humans live on the earth and are affected by the earth's gravity, they cannot fly in place like birds and need to overcome their own body weight to achieve flight. The streamlined cross-section and feather arrangement of bird wings can generate vortex lift, while the shape and surface area of human arms are far from reaching the aerodynamic efficiency required for flight. Even through a running jump, the hang time is still less than one second, far lower than the flight requirements.

[0006] To achieve the above purpose, the technical solution adopted by the present invention is: an aircraft capable of realizing human free flight, including an aircraft main body. On both sides of the rear end of the aircraft main body, a first wing and a second wing are respectively movably connected, and the first wing is located on one side of the second wing. On the outer surfaces of the left and right sides of the lower end of the aircraft main body, an engine fixing outer frame is fixedly connected, and a micro-turbine engine is detachably connected to the inner surface of the engine fixing outer frame.

[0007] Preferably, a connecting block is fixedly connected to the outer surface of one side of the first wing and the second wing. A connecting shaft is movably connected to the lower outer surface of the connecting block. A connecting rod is fixedly connected to the outer wall of the connecting shaft. A spherical connecting head is fixedly connected to the outer surface of one end of the connecting rod.

[0008] Preferably, a connecting sleeve is movably connected to the outer wall of the spherical connecting head. The other end of the connecting sleeve is fixedly connected to a fixing plate, and the fixing plate is fixedly connected to the outer surface of the rear end of the aircraft body.

[0009] Preferably, a connecting wire is fixedly connected to the outer surface of one side of the micro-turbine engine. A driving switch is fixedly connected to the outer surface of one end of the connecting wire. A connecting wire buckle is clamped on the outer wall of the connecting wire, and the connecting wire buckle is fixedly connected to the outer surface of the front end of the second wing. A driving button is movably connected to the upper outer surface of the driving switch.

[0010] Preferably, a connecting ring is fixedly connected to the outer surface of the front end of the first wing. A first connecting belt is fixedly connected to the outer surface of one end of the connecting ring. A second connecting belt is fixedly connected to the outer surface of the other end of the connecting ring. A plug buckle shell is fixedly connected to the outer surface of one end of the second connecting belt. A connecting belt adjusting buckle is arranged on the outer surface of the second connecting belt.

[0011] Preferably, a plug buckle is fixedly connected to the outer surface of one end of the first connecting belt, and the plug buckle is clamped with the plug buckle shell.

[0012] Compared with the prior art, the beneficial effects of the present invention are:

[0013] Through the micro-turbine engine, the first wing and the second wing provided by the present invention, by carrying a vector micro-turbine engine on the human waist, the vertical upward lift generated by the micro-turbine engine can effectively offset about 95% of the human body weight, helping humans achieve takeoff in place. At the same time, the movable bionic wing membranes from the shoulders to the wrists adopt a carbon fiber skeleton and an adaptive skin structure. Driven by the back muscle group and the waving of the arms, the first wing and the second wing are driven to perform flapping wing movements. Thus, by installing an efficient thrust device fixed on the human body, it can help humans achieve takeoff in place, and through the first wing and the second wing, fly in the air like a bird, and can achieve flat takeoff, and then realize the real free flight of humans. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 It is a schematic diagram of the overall structure of an aircraft capable of realizing the free flight of humans according to the present invention;

[0015] Figure 2 It is a schematic diagram of the structure of the first wing and the second wing in an aircraft capable of realizing the free flight of humans according to the present invention;

[0016] Figure 3 It is a partial enlarged view of B in an aircraft capable of realizing human free flight according to the present invention;

[0017] Figure 4 It is a partial enlarged view of A in an aircraft capable of realizing human free flight according to the present invention.

[0018] In the figure: 1. Aircraft main body; 2. First wing; 3. Second wing; 4. Engine fixed outer frame; 5. Micro turbine engine; 6. Connecting block; 7. Connecting shaft; 8. Connecting rod; 9. Spherical connector; 10. Connecting sleeve; 11. Fixed plate; 12. Connecting wire; 13. Connecting wire buckle; 14. Driving switch; 15. Driving button; 16. Connecting ring; 17. First connecting belt; 18. Second connecting belt; 19. Plug buckle shell; 20. Connecting belt adjusting buckle; 21. Plug buckle. Specific embodiments

[0019] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments.

[0020] Please refer to Figures 1-4 , an aircraft capable of realizing human free flight, including an aircraft main body 1, the first wing 2 and the second wing 3 are symmetrically distributed on both sides of the rear end of the aircraft main body 1. The first wing 2 and the second wing 3 adopt a bionic linkage structure. The connecting block 6 is made of high-strength carbon fiber, embedded in the root of the wing, and hinged to the titanium alloy connecting rod 8 through the connecting shaft 7 to realize the adjustment of the wing surface pitch angle. The connecting block 6 is fixed on the sides of the first wing 2 and the second wing 3, and its lower end is hinged to the connecting rod 8 through the connecting shaft 7. The end of the connecting rod 8 is embedded in the connecting sleeve 10 through the spherical connector 9, and finally fixed to the rear end of the main body by the fixed plate 11 to form a multi-degree-of-freedom moving structure. The micro turbine engine 5 is embedded in the engine fixed outer frames 4 on the left and right sides of the lower end of the main body, and the micro turbine engine 5 is fixed through a detachable interface. The micro turbine engine extends to the driving switch 14 through the connecting wire 12, and the cable is fixed to the front surface of the second wing 3 by the connecting wire buckle 13. A pressable driving button 15 is provided on the top of the driving switch.

[0021] In this embodiment, as Figure 4 shown, the connecting ring 16 is fixed to the front part of the first wing 2, and is respectively connected to two belt bodies. One end of the first connecting belt 17 is fixed to the connecting ring, and a plug buckle 21 is provided at the end. The second connecting belt 18, the other end extends to the plug buckle shell 19, and the length is adjusted through the connecting belt adjusting buckle 20, and finally locked with the plug buckle 21 to fix the first wing 2 and the second wing to the human arm.

[0022] Working principle

[0023] An aircraft capable of enabling humans to fly freely. By setting up a micro-turbine engine, wing one 2 and wing two 3, first wear the aircraft main body 1 on the body, and then fix wing one 2 and wing two to the human arm through connecting belt one 17 and connecting belt two 18. At this time, start the micro-turbine engine 5. By installing a vector micro-turbine engine on the human waist, the micro-turbine engine generates a vertical upward lift force, which can effectively offset about 95% of the human body weight and help humans achieve takeoff in place. At the same time, the movable bionic wing membrane from the shoulders to the wrists adopts a carbon fiber skeleton and an adaptive skin structure. Driven by the back muscle group and the waving of the arms, wing one and wing two perform flapping wing movements. Thus, by installing an efficient thrust device fixed on the human body, it can help humans achieve takeoff in place, and through wing one 2 and wing two 3, fly in the air like a bird, enabling flat takeoff, and further realizing the real sense of free flight for humans.

[0024] Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the scope of protection of the present invention.

Claims

1. An aircraft capable of enabling humans to fly freely, comprising an aircraft body (1), characterized in that: On both sides of the rear end of the aircraft body (1), a first wing (2) and a second wing (3) are respectively movably connected, and the first wing (2) is located on one side of the second wing (3). On the outer surfaces of the left and right sides of the lower end of the aircraft body (1), an engine fixing outer frame (4) is fixedly connected, and a micro-turbine engine (5) is detachably connected to the inner surface of the engine fixing outer frame (4).

2. The aircraft capable of realizing human free flight according to claim 1, characterized in that: On the outer surface of one side of the first wing (2) and the second wing (3), a connecting block (6) is fixedly connected. On the outer surface of the lower end of the connecting block (6), a connecting shaft (7) is movably connected. On the outer wall of the connecting shaft (7), a connecting rod (8) is fixedly connected. On the outer surface of one end of the connecting rod (8), a spherical connecting head (9) is fixedly connected.

3. The aircraft capable of enabling human free flight according to claim 2, wherein: On the outer wall of the spherical connecting head (9), a connecting sleeve (10) is movably connected. On the outer surface of the other end of the connecting sleeve (10), a fixing plate (11) is fixedly connected, and the fixing plate (11) is fixedly connected to the outer surface of the rear end of the aircraft body (1).

4. A flying vehicle capable of enabling humans to fly freely according to claim 1, characterized in that: On the outer surface of one side of the micro-turbine engine (5), a connecting wire (12) is fixedly connected. On the outer surface of one end of the connecting wire (12), a driving switch (14) is fixedly connected. A connecting wire buckle (13) is clamped on the outer wall of the connecting wire (12), and the connecting wire buckle (13) is fixedly connected to the outer surface of the front end of the second wing (3). On the outer surface of the upper end of the driving switch (14), a driving button (15) is movably connected.

5. The aircraft capable of realizing human free flight according to claim 1, characterized in that: On the outer surface of the front end of the first wing (2), a connecting ring (16) is fixedly connected. On the outer surface of one end of the connecting ring (16), a first connecting belt (17) is fixedly connected. On the outer surface of the other end of the connecting ring (16), a second connecting belt (18) is fixedly connected. On the outer surface of one end of the second connecting belt (18), a plug buckle shell (19) is fixedly connected. A connecting belt adjusting buckle (20) is arranged on the outer surface of the second connecting belt (18).

6. The aircraft capable of realizing human free flight according to claim 5, characterized in that: On the outer surface of one end of the first connecting belt (17), a plug buckle (21) is fixedly connected, and the plug buckle (21) is connected with the plug buckle shell (19) in a clamping manner.

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