Large-scale collecting and distributing integrated manned aircraft

Abstract

The invention belongs to the technical field of aircrafts, and discloses a large collecting and distributing integrated manned aircraft which comprises an aircraft body, and the bottom of the aircraft body is fixedly connected with a bottom plate. Through the arrangement of the intelligent unmanned vehicle, an I-shaped clamping plate, a fixed clamping block and an inclined clamping block, after a passenger takes the intelligent unmanned vehicle, the intelligent unmanned vehicle moves through a preset route, the I-shaped clamping plate is inserted into a clamping groove, then butt joint of the intelligent unmanned vehicle and the aircraft body is completed, at the moment, a telescopic rod is started, a sleeve is pushed to move downwards, and the intelligent unmanned vehicle is driven to move; when the fixing clamping block moves to the position above the inclined clamping block, the inclined surface of the inclined clamping block makes contact with the inclined surface of the side surface of the fixing clamping block, so that the inclined clamping block moves towards the interior of the sleeve, and when the fixing clamping block moves to the position above the inclined clamping block, the inclined clamping block is pushed to reset under the elastic force recovery effect of a spring, so that the inclined clamping block can play a supporting role on the fixing clamping block; and then the vertical rod is locked, so that a multi-locking effect on the intelligent unmanned vehicle is achieved.

Description

Technical Field

[0001] The present invention belongs to the technical field of aircraft, and specifically relates to a large-scale integrated manned aircraft for gathering and distributing passengers. Background Art

[0002] A manned aircraft is a device used to carry people and fly within the atmosphere or outer space, achieving flight through a power system or by means of aerodynamic force. Its core functions include personnel transportation, space exploration, scientific research experiments, and the execution of special tasks.

[0003] With the acceleration of the urbanization process and the booming development of regional economies, the society's demand for efficient transportation technologies has become increasingly urgent. However, the existing transportation system appears inadequate in coping with the growing demand for rapid travel. On the one hand, intercity travel still highly relies on traditional transportation means such as high-speed railways and airplanes. Although they play an important role in long-distance transportation, within the medium and short-distance range of 100 to 1500 kilometers, it is difficult to achieve a truly rapid and direct connection. This limitation not only increases the transfer costs and waiting times for passengers but also erects an invisible barrier between cities with relatively weak transportation networks, seriously hindering the flow of talents and economic cooperation between regions. On the other hand, as a large-capacity and high-efficiency public transportation mode, rail transit has high construction costs, a long cycle, and is restricted by geographical conditions and urban planning, making it difficult to achieve wide coverage in a short period. Short-distance travel tools such as shared bicycles and electric scooters, although flexible and convenient, have too limited a service range to meet the travel needs for cross-city or medium and long-distance trips. This mismatch between travel efficiency and resource utilization not only exacerbates urban traffic congestion problems but also restricts the sustainable development of the social economy, and there is an urgent need to break this deadlock through technological innovation and model upgrades. Summary of the Invention

[0004] The purpose of the present invention is to provide a large-scale integrated manned aircraft for gathering and distributing passengers to solve the problems raised in the above background art.

[0005] To achieve the above object, the present invention provides the following technical solution: a large-scale distributed integrated manned aircraft, including an aircraft body, a bottom plate is fixedly connected to the bottom of the aircraft body, a card slot is opened on the side surface of the bottom plate, an I-shaped clamping plate is movably connected inside the card slot, a smart unmanned vehicle is fixedly connected to the bottom of the I-shaped clamping plate, vertical rods are fixedly connected to the left and right sides of the top of the smart unmanned vehicle, a fixed clamping block is fixedly sleeved on the top surface of the outer surface of the vertical rod, a movable clamping block is movably sleeved on the outer surface of the vertical rod below the fixed clamping block, a telescopic rod is fixedly installed on the top surface of the inner surface of the aircraft body, a sleeve is fixedly connected to the bottom of the telescopic rod, cross rods are movably sleeved on the left and right sides inside the sleeve, an inclined clamping block is fixedly connected to the inner end of the cross rod, the top of the inclined clamping block is movably connected to the bottom of the fixed clamping block, a fixed sleeve is fixedly sleeved on the outer end of the cross rod, a spring is movably sleeved on the outer surface of the cross rod, the inner end of the spring is fixedly connected to the outer surface of the inclined clamping block, and the outer end of the spring is fixedly connected to the inner surface of the sleeve.

[0006] Preferably, a partition is fixedly sleeved inside the aircraft body above the bottom plate, and a first air cylinder is fixedly connected to the side surface of the partition.

[0007] Preferably, a side plate is fixedly connected to the top of the bottom plate, a chute is opened inside the side plate, slide rails are fixedly connected to the top and bottom of the inner side of the side plate, a sliding plate is movably connected to the outer surface of the slide rail, and the right side of the sliding plate is hinged to the left end of the first air cylinder.

[0008] Preferably, a double-shaft motor is fixedly installed on the inner side of the sliding plate, rotating shafts are fixedly connected to both ends of the output shaft of the double-shaft motor, the outer ends of the rotating shafts penetrate through the sliding plate and extend to the outside of the sliding plate and are movably sleeved with the inner wall of the sliding plate, and a baffle is fixedly sleeved on the inner surface of the inner end of the rotating shaft.

[0009] Preferably, a rotating plate is fixedly connected to the outer end of the rotating shaft, a round block is fixedly connected to the bottom of the outer side of the rotating plate, and the outer surface of the round block is movably connected to the inner surface of the chute.

[0010] Preferably, a mounting plate is fixedly installed on the bottom of the bottom plate, the number of the mounting plates is three, second air cylinders are fixedly sleeved inside the three mounting plates, a first moving rod is fixedly connected to the left end of the second air cylinder, and the outer surface of the first moving rod is movably connected to the inner wall of the mounting plate.

[0011] Preferably, hinge rods are hinged to the front and back sides of the right side of the mounting plate, rotating rods are movably sleeved on the front and back sides of the outer surface of the first moving rod, and the hinge rods and the rotating rods are hinged to each other.

[0012] Preferably, scissors brace brackets are hinged to the bottoms of the articulated rod and the rotating rod. A rotating rod is hinged to the right end of the bottom of the scissors brace bracket, and a support plate is hinged to the bottom of the rotating rod.

[0013] Preferably, a connecting rod is hinged to the left end of the bottom of the scissors brace bracket. A round rod is movably sleeved inside the bottom end of the connecting rod. The outer surface of the round rod is movably sleeved with the inner surface of the support plate, and the connecting rod and the rotating rod are hinged to each other.

[0014] The beneficial effects of the present invention are as follows:

[0015] 1. By providing the intelligent unmanned vehicle, the I-shaped clamping plate, the fixed clamping block and the inclined clamping block in the present invention, after the passenger takes the intelligent unmanned vehicle, the intelligent unmanned vehicle moves along a preset route, so that the I-shaped clamping plate is inserted into the inside of the clamping groove, thereby completing the docking between the intelligent unmanned vehicle and the aircraft body. At this time, the telescopic rod is activated to push the sleeve downward, which will cause the inclined surface of the inclined clamping block to contact the inclined surface of the side of the fixed clamping block, so that the inclined clamping block moves into the inside of the sleeve. When the fixed clamping block moves above the inclined clamping block, at this time, the inclined clamping block is pushed to reset under the action of the elastic force recovery of the spring, so that the inclined clamping block can support the fixed clamping block, and further lock the vertical rod, thereby playing a multiple locking role on the intelligent unmanned vehicle, ensuring the stability of the intelligent unmanned vehicle when the aircraft body is flying, and improving the convenience of medium and short-distance transportation.

[0016] 2. By providing the baffle in the present invention, due to the design of the baffle, after the I-shaped clamping plate is engaged with the clamping groove, the baffle can block in front of the clamping groove, thereby resisting the I-shaped clamping plate and preventing the I-shaped clamping plate from moving, improving the stability after the connection between the intelligent unmanned vehicle and the aircraft body.

[0017] 3. By providing the second air cylinder, the first moving rod, the scissors brace bracket and the support plate in the present invention, when the second air cylinder is activated, it will drive the first moving rod to move to the right, so that the first moving rod can drive the rotating rod to rotate, causing the rotating rod and the articulated rod to unfold, thereby driving the scissors brace bracket to unfold, enabling the rotating rod and the connecting rod to cooperate to push the support plate downward, so that the support plate contacts the ground, thereby supporting the aircraft body, enabling the aircraft body to stay stably on the ground and improving the stability when the aircraft body is docked with the intelligent unmanned vehicle. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 is a schematic structural diagram of the present invention;

[0019] Figure 2 is a bottom-up structural schematic diagram of the present invention;

[0020] Figure 3 Schematic structural diagram of the cross bracing bracket of the present invention;

[0021] Figure 4 Bottom view structural diagram of the cross bracing bracket of the present invention;

[0022] Figure 5 Schematic structural diagram of the top of the partition board of the present invention;

[0023] Figure 6 Schematic structural diagram of the intelligent unmanned vehicle of the present invention;

[0024] Figure 7 Schematic structural diagram of the telescopic rod of the present invention;

[0025] Figure 8 Cross-sectional structural diagram of the telescopic rod of the present invention;

[0026] Figure 9 is Figure 8 Partial enlarged structural diagram at position A in;

[0027] Figure 10 Schematic structural diagram of the partition board of the present invention;

[0028] Figure 11 Schematic structural diagram of the side plate of the present invention;

[0029] Figure 12 Cross-sectional structural diagram of the top of the side plate of the present invention;

[0030] Figure 13 Schematic structural diagram of the side of the side plate of the present invention;

[0031] Figure 14 Schematic structural diagram of the round block of the present invention;

[0032] Figure 15 Schematic structural diagram of the card slot of the present invention.

[0033] In the figure: 1, aircraft body; 2, bottom plate; 3, card slot; 4, intelligent unmanned vehicle; 5, I-shaped clamping plate; 6, vertical rod; 7, fixed clamping block; 8, movable clamping block; 9, telescopic rod; 10, sleeve; 11, cross bar; 12, inclined clamping block; 13, fixed sleeve; 14, spring; 15, side plate; 16, slide rail; 17, slide plate; 18, double-shaft motor; 19, rotating shaft; 20, baffle; 21, rotating plate; 22, round block; 23, chute; 24, first air cylinder; 25, mounting plate; 26, second air cylinder; 27, first moving rod; 28, rotating rod; 29, hinged rod; 30, cross bracing bracket; 31, rotating rod; 32, connecting rod; 33, support plate; 34, round rod; 35, partition board. Detailed implementation manners

[0034] 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. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts shall fall within the protection scope of the present invention.

[0035] As Figures 1 to 15 shown, the embodiment of the present invention provides a large-scale centralized and integrated manned aircraft, including an aircraft body 1. A bottom plate 2 is fixedly connected to the bottom of the aircraft body 1. A card slot 3 is formed on the side surface of the bottom plate 2. An I-shaped clamping plate 5 is movably connected inside the card slot 3. A smart unmanned vehicle 4 is fixedly connected to the bottom of the I-shaped clamping plate 5. Vertical rods 6 are fixedly connected to both the left and right sides of the top of the smart unmanned vehicle 4. A fixed clamping block 7 is fixedly sleeved on the top surface of the outer surface of the vertical rod 6. A movable clamping block 8 is movably sleeved on the outer surface of the vertical rod 6 and is located below the fixed clamping block 7. A telescopic rod 9 is fixedly installed on the top surface of the inner surface of the aircraft body 1. A sleeve 10 is fixedly connected to the bottom of the telescopic rod 9. Cross bars 11 are movably sleeved on both the left and right sides inside the sleeve 10. An inclined clamping block 12 is fixedly connected to the inner end of the cross bar 11. The top of the inclined clamping block 12 is movably connected to the bottom of the fixed clamping block 7. A fixed sleeve 13 is fixedly sleeved on the outer end of the cross bar 11. A spring 14 is movably sleeved on the outer surface of the cross bar 11. The inner end of the spring 14 is fixedly connected to the outer surface of the inclined clamping block 12. The outer end of the spring 14 is fixedly connected to the inner surface of the sleeve 10.

[0036] The smart unmanned vehicle 4 moves along a preset route, so that the I-shaped clamping plate 5 is inserted into the card slot 3, thereby completing the docking of the smart unmanned vehicle 4 and the aircraft body 1. At this time, the telescopic rod 9 is activated, so that the sleeve 10 moves downward. When the sleeve 10 moves downward, the inclined surface of the inclined clamping block 12 will contact the inclined surface of the side of the fixed clamping block 7, so that the inclined clamping block 12 moves into the sleeve 10, and then the sleeve 10 can move downward smoothly. When the fixed clamping block 7 moves above the inclined clamping block 12, at this time, the inclined clamping block 12 is pushed to reset under the action of the elastic force recovery of the spring 14, so that the inclined clamping block 12 can support the fixed clamping block 7, and then lock the vertical rod 6, thereby playing a multiple locking role on the smart unmanned vehicle 4.

[0037] Among them, a partition plate 35 is fixedly sleeved inside the aircraft body 1 and is located above the bottom plate 2. A first air cylinder 24 is fixedly connected to the side surface of the partition plate 35.

[0038] By providing the partition plate 35, the partition plate 35 can play a role in fixing the first air cylinder 24.

[0039] Among them, a side plate 15 is fixedly connected to the top of the bottom plate 2. A sliding groove 23 is formed inside the side plate 15. Sliding rails 16 are fixedly connected to both the top and the bottom on the inner side of the side plate 15. The outer surface of the sliding rail 16 is movably connected with a sliding plate 17. The right side of the sliding plate 17 is hinged to the left end of the first air cylinder 24.

[0040] By arranging the sliding rail 16, the sliding plate 17 can move along the outer surface of the sliding rail 16, thus playing a role in limiting the sliding plate 17.

[0041] Among them, a dual-axis motor 18 is fixedly installed inside the sliding plate 17. Both ends of the output shaft of the dual-axis motor 18 are fixedly connected with a rotating shaft 19. The outer ends of the rotating shafts 19 penetrate through the sliding plate 17 and extend to the outside of the sliding plate 17 and are movably sleeved with the inner wall of the sliding plate 17. A baffle 20 is fixedly sleeved on the inner surface of the inner end of the rotating shaft 19.

[0042] When the dual-axis motor 18 is started, it will drive the baffle 20 to rotate, making the baffle 20 rotate to a vertical state, so that the baffle 20 can block in front of the clamping groove 3, thus resisting the I-shaped clamping plate 5 and preventing the I-shaped clamping plate 5 from moving, improving the stability after the intelligent unmanned vehicle 4 is connected to the aircraft body 1.

[0043] Among them, the outer end of the rotating shaft 19 is fixedly connected with a rotating plate 21. The bottom of the outside of the rotating plate 21 is fixedly connected with a round block 22. The outer surface of the round block 22 is movably connected with the inner surface of the sliding groove 23.

[0044] When the dual-axis motor 18 is started, it will make the rotating shaft 19 drive the baffle 20 to rotate upward to separate from the contact with the I-shaped clamping plate 5 and make the rotating shaft 19 drive the rotating plate 21 to rotate, so that the round block 22 can move along the inner surface of the sliding groove 23 during the leftward movement of the sliding plate 17.

[0045] Among them, a mounting plate 25 is fixedly installed at the bottom of the bottom plate 2. The number of the mounting plates 25 is three. Second air cylinders 26 are fixedly sleeved inside the three mounting plates 25. The left end of the second air cylinder 26 is fixedly connected with a first moving rod 27. The outer surface of the first moving rod 27 is movably connected with the inner wall of the mounting plate 25.

[0046] When the second air cylinder 26 is started, it will push the first moving rod 27 to move leftward along the inner wall of the mounting plate 25.

[0047] Among them, hinge rods 29 are hinged to both the front and the back on the right side of the mounting plate 25. Rotating rods 28 are movably sleeved on both the front and the back sides of the outer surface of the first moving rod 27. The hinge rod 29 and the rotating rod 28 are hinged to each other.

[0048] When the second air cylinder 26 pushes the first moving rod 27 to move leftward, it will cause the rotating rod 28 to drive the hinged rod 29 to rotate, so that the rotating rod 28 and the hinged rod 29 fold, and the height of the rotating rod 28 and the hinged rod 29 in the vertical direction is reduced.

[0049] Wherein, scissor brace brackets 30 are hinged at the bottoms of both the hinged rod 29 and the rotating rod 28. The right end of the bottom of the scissor brace bracket 30 is hinged with a rotating rod 31, and the bottom of the rotating rod 31 is hinged with a support plate 33.

[0050] When the rotating rod 28 and the rotating rod 28 fold, it will drive the scissor brace bracket 30 to fold, so that the rotating rod 31 drives the support plate 33 to rise.

[0051] Wherein, a connecting rod 32 is hinged at the left end of the bottom of the scissor brace bracket 30. A round rod 34 is movably sleeved inside the bottom end of the connecting rod 32. The outer surface of the round rod 34 is movably sleeved with the inner surface of the support plate 33, and the connecting rod 32 and the rotating rod 31 are hinged to each other.

[0052] When the scissor brace bracket 30 folds, it will drive the connecting rod 32 to rotate, so that the connecting rod 32 pushes the round rod 34 to move rightward inside the support plate 33, and thus drives the support plate 33 to rise through the rotating rod 31 and the connecting rod 32.

[0053] Working principle and usage process:

[0054] When the aircraft body 1 stays on the ground, at this time, the support plate 33 and the scissor brace bracket 30 cooperate to support the aircraft body 1, so that the aircraft body 1 can stay stably on the ground and improve the stability when the aircraft body 1 is docked with the intelligent unmanned vehicle 4. When the passenger rides on the intelligent unmanned vehicle 4, the intelligent unmanned vehicle 4 will move along the preset route, so that the I-shaped clamping plate 5 is inserted into the inside of the card slot 3, thus completing the docking of the intelligent unmanned vehicle 4 and the aircraft body 1. At this time, the telescopic rod 9 is activated to push the sleeve 10 downward, which will cause the inclined surface of the inclined clamping block 12 to contact the inclined surface of the side of the fixed clamping block 7, so that the inclined clamping block 12 moves into the inside of the sleeve 10. When the fixed clamping block 7 moves above the inclined clamping block 12, at this time, the inclined clamping block 12 is pushed to reset under the elastic recovery action of the spring 14, so that the inclined clamping block 12 can support the fixed clamping block 7, and further lock the vertical rod 6, thus playing a multiple locking role on the intelligent unmanned vehicle 4.

[0055] Subsequently, the biaxial motor 18 will be activated, causing the rotating shaft 19 to drive the baffle 20 to rotate, enabling the baffle 20 to rotate to a vertical state. The rotation of the rotating shaft 19 will simultaneously drive the rotating plate 21 to rotate downward. At this time, the activation of the first pneumatic cylinder 24 will drive the sliding plate 17 to move to the right along the outer surface of the slide rail 16, causing the rotating plate 21 to drive the round block 22 to move while rotating and enabling the round block 22 to move along the inner surface of the chute 23. At this time, the baffle 20 will block the front side of the card slot 3, thereby resisting the I-shaped clamping plate 5 and preventing the I-shaped clamping plate 5 from moving, improving the stability of the intelligent unmanned vehicle 4 after being connected to the aircraft body 1. The round block 22 will move to the far right inside the chute 23, making the rotating plate 21 unable to rotate further, thus ensuring that the baffle 20 can remain in a vertical state and enabling the baffle 20 to continuously and stably resist the I-shaped clamping plate 5.

[0056] After the intelligent unmanned vehicle 4 is connected to the aircraft body 1, the aircraft body 1 will take off. At this time, the second pneumatic cylinder 26 is activated, which will drive the first moving rod 27 to move to the left, thereby enabling the first moving rod 27 to drive the rotating rod 28 to rotate, causing the rotating rod 28 and the articulated rod 29 to fold, thereby driving the scissors brace 30 to fold, enabling the rotating rod 31 to cooperate with the connecting rod 32, and thus driving the support plate 33 to move upward.

[0057] When the aircraft body 1 is about to land, the second air cylinder 26 is activated at this time, causing the first moving rod 27 to move to the right, thereby causing the scissors brace 30 to unfold, and then causing the support plate 33 to move downward, playing a supporting role for the aircraft body 1 when it lands. Subsequently, the double-shaft motor 18 and the first air cylinder 24 are activated. After the first air cylinder 24 is activated, it will push the sliding plate 17 to move to the left. When the double-shaft motor 18 is activated, the rotating shaft 19 will drive the baffle 20 to rotate upward to disengage from the contact with the I-shaped clamping plate 5 and cause the rotating shaft 19 to drive the rotating plate 21 to rotate, enabling the round block 22 to move along the inner surface of the sliding groove 23 during the leftward movement of the sliding plate 17, thereby releasing the enclosure of the I-shaped clamping plate 5. Subsequently, the telescopic rod 9 is activated to push the sleeve 10 downward, causing the inclined surface of the inclined clamping block 12 to contact the top of the movable clamping block 8, thereby causing the inclined clamping block 12 to move into the sleeve 10. When the inclined clamping block 12 moves below the movable clamping block 8, the inclined clamping block 12 will be pushed back to its original position under the elastic recovery of the spring 14, causing the top of the inclined clamping block 12 to contact the bottom of the movable clamping block 8. Then, the telescopic rod 9 is activated to drive the sleeve 10 to rise, causing the inclined clamping block 12 to drive the movable clamping block 8 to rise along the outer surface of the vertical rod 6. When the top of the movable clamping block 8 contacts the bottom of the fixed clamping block 7, the inclined clamping block 12 will move into the sleeve 10 along the inclined surface at the bottom of the movable clamping block 8. As the sleeve 10 rises, the inclined clamping block 12 will move to the side of the fixed clamping block 7 and disengage from the contact with the fixed clamping block 7 as it rises, thereby releasing the fixing effect on the vertical rod 6, and further releasing the fixing of the intelligent unmanned vehicle 4. At this time, the intelligent unmanned vehicle 4 can move outward to disconnect from the aircraft body 1.

[0058] It should be noted that in this article, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "comprising", "including" or any other variation thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements not only includes those elements, but also includes other elements not explicitly listed, or elements inherent to such process, method, article or device.

[0059] Although the embodiments of the present invention have been shown and described, it will be understood by those of ordinary skill in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. Large-scale centralized and integrated manned aircraft, comprising an aircraft body (1), characterized in that: The bottom of the aircraft body (1) is fixedly connected with a bottom plate (2). A clamping groove (3) is formed on the side surface of the bottom plate (2). An I-shaped clamping plate (5) is movably connected inside the clamping groove (3). The bottom of the I-shaped clamping plate (5) is fixedly connected with an intelligent unmanned vehicle (4). Vertical rods (6) are fixedly connected to both the left and right sides of the top of the intelligent unmanned vehicle (4). A fixed clamping block (7) is fixedly sleeved on the top of the outer surface of the vertical rod (6). A movable clamping block (8) is movably sleeved on the outer surface of the vertical rod (6) and is located below the fixed clamping block (7). A telescopic rod (9) is fixedly installed on the top of the inner surface of the aircraft body (1). The bottom of the telescopic rod (9) is fixedly connected with a sleeve (10). Cross rods (11) are movably sleeved on both the left and right sides inside the sleeve (10). The inner end of the cross rod (11) is fixedly connected with an inclined clamping block (12). The top of the inclined clamping block (12) is movably connected with the bottom of the fixed clamping block (7). A fixed sleeve (13) is fixedly sleeved on the outer end of the cross rod (11). A spring (14) is movably sleeved on the outer surface of the cross rod (11). The inner end of the spring (14) is fixedly connected with the outer surface of the inclined clamping block (12). The outer end of the spring (14) is fixedly connected with the inner surface of the sleeve (10).

2. The large-scale distributed integrated manned aircraft according to claim 1, wherein: A partition plate (35) is fixedly sleeved inside the aircraft body (1) and is located above the bottom plate (2). A first air cylinder (24) is fixedly connected to the side surface of the partition plate (35).

3. The large-scale distributed integrated manned aircraft according to claim 1, characterized in that: A side plate (15) is fixedly connected to the top of the bottom plate (2). A sliding groove (23) is formed inside the side plate (15). Slide rails (16) are fixedly connected to both the top and bottom of the inner side of the side plate (15). A sliding plate (17) is movably connected to the outer surface of the slide rail (16). The right side of the sliding plate (17) is hinged to the left end of the first air cylinder (24).

4. The large-scale decentralized integrated manned aircraft according to claim 3, characterized in that: A double-shaft motor (18) is fixedly installed inside the sliding plate (17). Rotating shafts (19) are fixedly connected to both ends of the output shaft of the double-shaft motor (18). The outer ends of the rotating shafts (19) penetrate through the sliding plate (17) and extend to the outside of the sliding plate (17) and are movably sleeved with the inner wall of the sliding plate (17). A baffle (20) is fixedly sleeved on the inner surface of the inner end of the rotating shaft (19).

5. The large-scale decentralized integrated manned aircraft according to claim 4, wherein: The outer end of the rotating shaft (19) is fixedly connected with a rotating plate (21). A circular block (22) is fixedly connected to the bottom of the outside of the rotating plate (21). The outer surface of the circular block (22) is movably connected with the inner surface of the sliding groove (23).

6. The large-scale distributed integrated manned aircraft according to claim 1, characterized in that: Mounting plates (25) are fixedly installed on the bottom of the bottom plate (2). The number of the mounting plates (25) is three. Second air cylinders (26) are fixedly sleeved inside all three mounting plates (25). The left end of the second air cylinder (26) is fixedly connected with a first moving rod (27). The outer surface of the first moving rod (27) is movably connected with the inner wall of the mounting plate (25).

7. The large-scale distributed integrated manned aircraft according to claim 6, characterized in that: Hinged rods (29) are hinged on both the front and back right sides of the mounting plate (25). Rotating rods (28) are movably sleeved on the front and back sides of the outer surface of the first moving rod (27). The hinged rod (29) and the rotating rod (28) are hinged to each other.

8. The large-scale distributed integrated manned aircraft according to claim 7, characterized in that: Scissor brace brackets (30) are hinged at the bottoms of both the hinged rod (29) and the rotating rod (28). A rotating rod (31) is hinged to the right end of the bottom of the scissor brace bracket (30). A support plate (33) is hinged to the bottom of the rotating rod (31).

9. The large-scale distributed integrated manned aircraft according to claim 8, characterized in that: A connecting rod (32) is hinged to the left end of the bottom of the scissor brace bracket (30). A round rod (34) is movably sleeved inside the bottom end of the connecting rod (32). The outer surface of the round rod (34) is movably sleeved with the inner surface of the support plate (33). The connecting rod (32) and the rotating rod (31) are hinged to each other.

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