Low-altitude manned flight device

Abstract

The invention discloses a low-altitude manned flight device, and particularly relates to the technical field of aircrafts, the low-altitude manned flight device comprises a flight device body, a fixed seat is fixedly connected in the flight device body, the top of the fixed seat is fixedly connected with a supporting seat, and two dovetail grooves are formed in the top of the fixed seat; and the moving assembly comprises a first electric push rod fixedly connected in the supporting seat. Through cooperation of the electric push rod and the piston rod, automation of seat cleaning is achieved, manual intervention is reduced, various stains can be efficiently removed through the design of the cleaning rod, the cleaning efficiency is improved, an operator does not need to manually wipe the seat and only needs to control starting and stopping of the cleaning assembly, the cleaning work intensity is reduced, and the cleaning efficiency is improved. The cleaning assembly is easy to maintain and replace, the reliability of long-term use is guaranteed, through the design, the seat cleaning work of the low-altitude manned flight device becomes simpler, more convenient and more efficient, and more comfortable and convenient use experience is provided for a user.

Description

Technical Field

[0001] The present invention relates to the technical field of aircraft, and in particular to a low-altitude manned flying device. Background Art

[0002] A low-altitude manned flying device is a device that can carry out manned flights in low-altitude areas (usually no more than 1,000 meters above the ground). It combines advanced technologies in multiple fields such as aviation, electronics, and materials. The origin of low-altitude manned flying devices can be traced back to the early 20th century. With the continuous development of aviation technology, people began to try to apply aircraft to low-altitude areas. In recent years, with the maturity of technologies such as drones and electric aircraft, low-altitude manned flying devices have gradually become a research hotspot.

[0003] After long-term use, the devices in the prior art usually need to use cleaning tools to clean and maintain the seats and other parts. Not only is the operation not convenient, but it also often makes the cleaning work more arduous, thereby weakening the automation advantages of the existing devices to a certain extent. Summary of the invention

[0004] The purpose of the present invention is to provide a low altitude manned flying device to solve the above-mentioned deficiencies in the technology.

[0005] In order to achieve the above-mentioned object, the present invention provides the following technical solution: a low-altitude manned flying device, comprising: a flying device body, a fixing seat fixedly connected to the flying device body, a supporting seat fixedly connected to the top of the fixing seat, and two dovetail grooves being provided on the top of the fixing seat;

[0006] A moving assembly, the moving assembly comprising a first electric push rod fixedly connected to a support seat, a front end of the first electric push rod fixedly connected to a moving plate, a bottom end of the moving plate fixedly connected to two dovetail blocks, a top of the moving plate fixedly connected to two second electric push rods, and tops of the two second electric push rods fixedly connected to the same support plate;

[0007] A rotating assembly, wherein the rotating assembly comprises two supporting rods fixedly connected to the top of the supporting plate, wherein the two supporting rods are rotatably connected to the same fixed shaft, and the fixed shaft is fixedly connected to a rotating seat, and a plurality of card slots are provided on the front side of the rotating seat, and an elastic telescopic rod is fixedly connected to the front supporting rod, and a card block is fixedly connected to the rear end of the elastic telescopic rod, and a handle is fixedly connected to the card block;

[0008] A buffer assembly, the buffer assembly includes a support platform fixedly connected to the top of the rotating seat, two slide grooves are provided on the top of the support platform, two first springs are fixedly connected to the top of the support platform, the tops of the two first springs are fixedly connected to the same connecting plate, the top of the connecting plate is fixedly connected to the same seat, the bottom of the connecting plate is fixedly connected to two fixed blocks, the two fixed blocks are hinged to the rotating rod through the pin shaft, and the two ends of the two rotating rods that are far away from each other are hinged to the connecting blocks through the pin shaft;

[0009] A cleaning assembly, the cleaning assembly includes baffles fixedly connected to the two connecting blocks on both sides away from each other, cleaning rods are fixedly connected to the right sides of the two baffles, piston rods are fixedly connected to the two sides away from each other of the two baffles, piston cylinders are fixedly connected to the front and rear sides of the support platform, and fixed pipes are connected to the two sides away from each other of the piston cylinders.

[0010] Preferably, the piston rod is slidably connected to the piston cylinder, and the piston cylinder and the baffle are fixedly connected to the same second spring on both sides thereof.

[0011] Preferably, the second spring is sleeved on the outside of the piston rod, and a one-way air intake valve is provided outside the piston cylinder.

[0012] Preferably, a slider is fixedly connected to the bottom end of the baffle, and the bottom end of the slider is slidably connected in a slide groove.

[0013] Preferably, the plurality of slots are distributed in a ring shape at equal distances in the rotating seat, and the clamping blocks are slidably connected in the corresponding slots.

[0014] Preferably, a plurality of air outlets are provided outside the fixed pipe, and the fixed pipe is in an L-shape.

[0015] Preferably, the dovetail block is slidably connected in the corresponding dovetail groove, and a support frame is provided at the bottom of the flying device body.

[0016] Preferably, fan blades are provided on the top of the flying device body, and a windshield is provided on the front side of the flying device body.

[0017] In the above technical solution, the technical effects and advantages provided by the present invention are:

[0018] 1. Through the cooperation of the electric push rod and the piston rod, the seat cleaning is automated and manual intervention is reduced. The design of the cleaning rod can effectively remove various stains and improve the cleaning efficiency. The operator does not need to wipe the seat manually, but only needs to control the start and stop of the cleaning component, which greatly reduces the intensity of the cleaning work. The design of the cleaning component is easy to maintain and replace, ensuring the reliability of long-term use. Through this design, the seat cleaning work of the low-altitude manned flight device becomes simpler and more efficient, providing users with a more comfortable and convenient use experience.

[0019] 2. Through the cooperation of electric push rods and spring assemblies, the movement and adjustment of the seat do not require manual operation, which greatly improves the automation level of the device. Ergonomics is taken into consideration to ensure that users get the best comfort when adjusting the seat. It can be personalized according to the height, body shape and preferences of different users, and has strong adaptability. Through this design, the seat system of the low-altitude manned flying device not only improves the user's riding experience, but also reduces the complexity of operation, making the flying device more intelligent and humane. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in the present invention. For ordinary technicians in this field, other drawings can also be obtained based on these drawings.

[0021] Figure 1 It is a schematic diagram of the overall structure of the present invention;

[0022] Figure 2 It is a schematic diagram of the structure of the connection between the flying device body and the supporting frame of the present invention;

[0023] Figure 3 It is a schematic diagram of the structure of the connection between the movable plate and the dovetail block of the present invention;

[0024] Figure 4 It is a structural schematic diagram of the connection between the movable plate and the second electric push rod of the present invention;

[0025] Figure 5 This is a schematic diagram of the structure of the connection between the support plate and the support rod of the present invention;

[0026] Figure 6 It is a structural schematic diagram of the connection between the first spring and the connecting plate of the present invention;

[0027] Figure 7 It is a structural schematic diagram of the connection between the support seat and the first electric push rod of the present invention.

[0028] Description of reference numerals:

[0029] 1. The flying device body; 2. The fixing seat; 3. The supporting seat; 4. The dovetail groove; 5. The first electric push rod; 6. The moving plate; 7. The dovetail block; 8. The second electric push rod; 9. The supporting plate; 10. The supporting rod; 11. The fixed axis; 12. The rotating seat; 13. The card slot; 14. The elastic telescopic rod; 15. The card block; 16. The handle; 17. The supporting platform; 18. The slide groove; 19. The first spring; 20. The connecting plate; 21. The seat; 22. The fixing block; 23. The rotating rod; 24. The connecting block; 25. The baffle; 26. The cleaning rod; 27. The piston rod; 28. The piston cylinder; 29. ​​The fixed pipe; 30. The second spring; 31. The slider; 32. The supporting frame; 33. The fan blade. DETAILED DESCRIPTION

[0030] In order to enable those skilled in the art to better understand the technical solution of the present invention, the present invention will be further described in detail below with reference to the accompanying drawings.

[0031] The present invention provides Figures 1 to 7 A low-altitude manned flying device shown in the figure comprises: a flying device body 1, a fixing seat 2 is fixedly connected inside the flying device body 1, a supporting seat 3 is fixedly connected to the top of the fixing seat 2, and two dovetail grooves 4 are provided on the top of the fixing seat 2;

[0032] The moving assembly includes a first electric push rod 5 fixedly connected to the support seat 3, a moving plate 6 fixedly connected to the front end of the first electric push rod 5, two dovetail blocks 7 fixedly connected to the bottom end of the moving plate 6, two second electric push rods 8 fixedly connected to the top of the moving plate 6, and the tops of the two second electric push rods 8 fixedly connected to the same support plate 9;

[0033] The rotating assembly includes two support rods 10 fixedly connected to the top of the support plate 9. By providing the support rods 10, the support rods 10 can support the fixed shaft 11 to avoid the fixed shaft 11 from shaking during use, thereby ensuring the stable use of the fixed shaft 11;

[0034] The two support rods 10 are rotatably connected to the same fixed shaft 11, and the fixed shaft 11 is fixedly connected to the rotating seat 12. A plurality of slots 13 are provided on the front side of the rotating seat 12. By providing the slots 13 and cooperating with the slots 13 and the blocks 15, the angle of the rotating seat 12 can be fixed and limited, so as to avoid the deviation and rotation, and ensure the stability of the rotating seat 12.

[0035] An elastic telescopic rod 14 is fixedly connected inside the support rod 10 at the front, a clamping block 15 is fixedly connected to the rear end of the elastic telescopic rod 14, and a handle 16 is fixedly connected to the outside of the clamping block 15;

[0036] The buffer assembly includes a support platform 17 fixedly connected to the top of the rotating seat 12. Two slide grooves 18 are provided on the top of the support platform 17. By providing the slide grooves 18, the slide grooves 18 and the slider 31 cooperate with each other to avoid the slider 31 from being offset and stuck during the sliding process, thereby ensuring the stable movement of the slider 31.

[0037] Two first springs 19 are fixedly connected to the top of the support platform 17, and the top ends of the two first springs 19 are fixedly connected to the same connecting plate 20, and the top of the connecting plate 20 is fixedly connected to the same seat 21, and the bottom end of the connecting plate 20 is fixedly connected to two fixed blocks 22, and the two fixed blocks 22 are hinged to the rotating rod 23 through the pin shaft, and the two ends of the two rotating rods 23 that are far away from each other are hinged to the connecting blocks 24 through the pin shaft; through effective impact absorption and buffering adjustment, the comfort of the driver during the flight is significantly improved, the impact of vibration on the driver's body is reduced, and the risk of fatigue and injury that may be caused by long-term flight is reduced, and the buffer component helps to maintain the stability of the seat 21, even in bumpy flight conditions, the passenger can remain stable, which can not only provide a more stable riding experience, but also significantly improve the comfort and satisfaction of the passengers while ensuring safety;

[0038] The cleaning component includes a baffle 25 fixedly connected to the two connecting blocks 24 on both sides away from each other, a cleaning rod 26 is fixedly connected to the right side of the two baffles 25, a piston rod 27 is fixedly connected to the two sides away from each other of the two baffles 25, a piston cylinder 28 is fixedly connected to the front and rear sides of the support platform 17, and a fixed pipe 29 is connected to the two sides away from each other of the piston cylinder 28.

[0039] The piston rod 27 is slidably connected in the piston cylinder 28. The piston cylinder 28 and the baffle 25 are fixedly connected to the same second spring 30 on both sides. The second spring 30 is sleeved on the outside of the piston rod 27. A one-way air intake valve is provided outside the piston cylinder 28.

[0040] The bottom end of the baffle 25 is fixedly connected with a slider 31 , the bottom end of the slider 31 is slidably connected in the slide groove 18 , a plurality of slots 13 are distributed in a ring shape at equal distances in the rotating seat 12 , and the block 15 is slidably connected in the corresponding slots 13 .

[0041] A plurality of air outlets are arranged outside the fixed pipe 29, and the shape of the fixed pipe 29 is L-shaped. The dovetail block 7 is slidably connected in the corresponding dovetail groove 4. A support frame 32 is arranged at the bottom of the flying device body 1, a fan blade 33 is arranged at the top of the flying device body 1, and a windshield is arranged on the front side of the flying device body 1.

[0042] Working principle:

[0043] When using the device, firstly, the first electric push rod 5 can be started according to the demand, and the first electric push rod 5 can push the moving plate 6 and the two dovetail blocks 7 to move horizontally in the corresponding dovetail groove 4, and drive the second electric push rod 8, the support plate 9, the support rod 10, the fixed shaft 11, the rotating seat 12 and the seat 21 to move synchronously, and then the two second electric push rods 8 can be started, and the two second electric push rods 8 can push the support plate 9 upward, and the support plate 9 can drive the two support rods 10, the fixed shaft 11, the rotating seat 12 and the seat 21 to move in the vertical direction, and finally the handle 16 can be pulled, and the handle 16 can drive the block 15 to separate from the slot 13 and compress the elastic telescopic rod 14, and then the support platform 17 and the rotating seat 12 can drive the fixed shaft 11 to rotate to a suitable angle, and then the handle 16 can be released, and the block 15 can be stuck in the corresponding slot 13 under the action of the elastic force of the elastic telescopic rod 14 itself;

[0044] When the driver sits on the seat 21, the seat 21 can press the connecting plate 20 and the first spring 19 downwards under the action of its own weight, and drive the fixed block 22 to move downward synchronously, so as to drive the two rotating rods 23 to rotate relative to each other, so as to push the two baffles 25 and the slider 31 to move relative to each other in the slide groove 18, and push the piston rod 27 to move in the piston cylinder 28, and compress the second spring 30, so that the air in the piston cylinder 28 can be discharged from the air outlet of the fixed pipe 29, so as to blow the outer surface of the seat 21, and when the two baffles 25 move relative to each other, they can drive the two cleaning rods 26 to move synchronously, and can clean the outer surface of the seat 21;

[0045] When the driver leaves the seat 21, the seat 21 can rebound under the action of the elastic force of the two first springs 19, so that the connecting plate 20 can drive the two fixed blocks 22 to move upward synchronously, and can drive the rotating rod 23 to rotate towards each other under the action of the pin shaft, thereby driving the two connecting blocks 24, the baffle 25 and the slider 31 to move towards each other in the slide groove 18, and driving the two piston rods 27 to move towards each other in the piston cylinder 28, so that the two cleaning rods 26 can return to their original state, and allow outside air to enter the piston cylinder 28 through the one-way intake valve, and then repeat the above movement.

[0046] The above description is only by way of illustration of certain exemplary embodiments of the present invention. It is undoubted that those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the present invention. Therefore, the above drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of protection of the claims of the present invention.

Claims

1. A low-altitude manned flying device, characterized in that: include: A flying device body (1), wherein a fixing seat (2) is fixedly connected inside the flying device body (1), a supporting seat (3) is fixedly connected to the top of the fixing seat (2), and two dovetail grooves (4) are provided on the top of the fixing seat (2); A moving assembly, the moving assembly comprising a first electric push rod (5) fixedly connected to a support seat (3), a moving plate (6) fixedly connected to the front end of the first electric push rod (5), two dovetail blocks (7) fixedly connected to the bottom end of the moving plate (6), two second electric push rods (8) fixedly connected to the top of the moving plate (6), and the tops of the two second electric push rods (8) fixedly connected to the same support plate (9); A rotating assembly, the rotating assembly comprising two support rods (10) fixedly connected to the top of the support plate (9), the two support rods (10) being rotatably connected to the same fixed shaft (11), the fixed shaft (11) being fixedly connected to a rotating seat (12) outside, the front side of the rotating seat (12) being provided with a plurality of slots (13), the support rod (10) located in the front being fixedly connected to an elastic telescopic rod (14), the rear end of the elastic telescopic rod (14) being fixedly connected to a clamping block (15), the clamping block (15) being fixedly connected to a handle (16) outside; A buffer component, the buffer component comprises a support platform (17) fixedly connected to the top of a rotating seat (12), the top of the support platform (17) is provided with two slide grooves (18), the top of the support platform (17) is fixedly connected to two first springs (19), the top ends of the two first springs (19) are fixedly connected to the same connecting plate (20), the top of the connecting plate (20) is fixedly connected to the same seat (21), the bottom end of the connecting plate (20) is fixedly connected to two fixed blocks (22), the two fixed blocks (22) are hinged to a rotating rod (23) through a pin shaft, and the two ends of the two rotating rods (23) that are far away from each other are hinged to a connecting block (24) through a pin shaft; A cleaning assembly, the cleaning assembly comprising baffles (25) fixedly connected to two sides away from the two connection blocks (24), cleaning rods (26) fixedly connected to the right sides of the two baffles (25), piston rods (27) fixedly connected to the two sides away from the two baffles (25), piston cylinders (28) fixedly connected to the front and rear sides of the support platform (17), and fixed pipes (29) connected to the two sides away from the piston cylinder (28).

2. A low altitude manned flying device according to claim 1, characterized in that: The piston rod (27) penetrates and is slidably connected in the piston cylinder (28), and the piston cylinder (28) and the baffle (25) are fixedly connected to the same second spring (30) on both sides thereof.

3. A low altitude manned flying device according to claim 2, characterized in that: The second spring (30) is sleeved on the outside of the piston rod (27), and a one-way air intake valve is arranged outside the piston cylinder (28).

4. A low altitude manned flying device according to claim 1, characterized in that: The bottom end of the baffle (25) is fixedly connected to a slider (31), and the bottom end of the slider (31) is slidably connected in the slide groove (18).

5. A low altitude manned flying device according to claim 1, characterized in that: The plurality of slots (13) are distributed in a circular shape at equal distances in the rotating seat (12), and the clamping blocks (15) are slidably connected in the corresponding slots (13).

6. A low altitude manned flying device according to claim 1, characterized in that: The fixed pipe (29) is provided with a plurality of air outlets outside, and the fixed pipe (29) is in an L-shape.

7. A low altitude manned flying device according to claim 1, characterized in that: The dovetail block (7) is slidably connected in the corresponding dovetail groove (4), and a support frame (32) is provided at the bottom of the flying device body (1).

8. A low altitude manned flying device according to claim 1, characterized in that: The top of the flying device body (1) is provided with a fan blade (33), and the front side of the flying device body (1) is provided with a windshield.

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