Simulated flight cabin

Abstract

The utility model discloses a simulated flight cabin, which comprises a base, a mounting seat is fixed on the inner wall of the top surface of the base, a connecting plate is connected to the outer wall of the top surface of the mounting seat through an adjusting assembly, a seat is fixed on the top surface of the connecting plate, and the adjusting assembly comprises a bidirectional screw rod and a rotating shaft. The two-way lead screw is relatively and rotatably connected to the two ends of the inner wall of the mounting base, a connecting groove is formed in the outer wall of the bottom face of the connecting plate, sliding blocks are slidably connected to the two ends of the inner wall of the connecting groove, moving blocks are arranged at the two ends of the two-way lead screw, and connecting rods are rotatably connected to the top ends of the moving blocks. The adjusting assembly is arranged, the rotating handle is rotated, the rotating shaft rotates, the two-way screw rod is driven to rotate through transmission between the driving bevel gear and the driven bevel gear, the movable block moves along the two-way screw rod, the connecting rod drives the connecting plate to ascend and descend through the sliding block, and the height of the seat is changed. A user can adjust the height of the seat according to the height of the user.

Description

Technical Field

[0001] The utility model relates to the technical field of simulation training, in particular to a simulated flight cockpit. Background Technique

[0002] A simulated flight cockpit is a device that can simulate the scene of an airplane during flight and can control the simulated airplane. Simulated flight cockpits are usually used in occasions such as pilot training, entertainment and learning for flight enthusiasts. Due to the high risks and costs of actual flight, flight simulation can reduce the risks and costs of flight training, and at the same time improve the skills and emergency response capabilities of pilots.

[0003] After retrieval, a patent with the Chinese patent publication number CN214955466U discloses a simulated flight cockpit, including a storage board and a crank. The upper surface of the storage board is fixed with an operation console, and a display screen is arranged on the upper surface of the operation console. A control board is arranged on the surface of the operation console, and a steering wheel is arranged on the operation console. The upper surface of the storage board is fixed with a seat, and a pedal is fixed at the upper end of the storage board. A slideway is fixed inside the storage board, and the slideway is slidably connected to a first moving block and a second moving block. The lower ends of the first moving block and the second moving block are axially connected to a connecting rod, and the lower end of the connecting rod is axially connected to a connecting block.

[0004] This patent can quickly move the simulated flight cockpit by setting universal wheels, telescopic rods and springs, and the telescopic rods and springs inside the pulleys can play a shock-absorbing role when encountering bumpy roads, thus avoiding damage to the devices on the simulated flight cockpit. However, its seat cannot be adjusted. When the user is relatively tall, the user's legs cannot bend normally due to the short seat, causing discomfort. When the user is relatively short, it will affect the user's driving line of sight. Content of the Utility Model

[0005] The purpose of the utility model is to solve the defects existing in the prior art, and to propose a simulated flight cockpit.

[0006] In order to achieve the above purpose, the utility model adopts the following technical scheme:

[0007] A simulated flight cockpit includes a base, and an installation seat is fixed on the inner wall of the top surface of the base. The outer wall of the top surface of the installation seat is connected to a connecting plate through an adjusting component, and a seat is fixed on the top surface of the connecting plate.

[0008] As a further scheme of the utility model: The adjusting component includes a bidirectional lead screw and a rotating shaft. The two ends of the bidirectional lead screw are relatively rotatably connected to both ends of the inner wall of the installation seat, the rotating shaft is rotatably connected to one side of the inner wall of the installation seat, the rotating shaft and the bidirectional lead screw are arranged in a staggered manner, and one end of the rotating shaft is connected to a turning handle.

[0009] As a further solution of the present utility model: a driving bevel gear is fixed on the rotating shaft, a driven bevel gear is fixed at one end of the bidirectional lead screw, and the driving bevel gear is in transmission engagement with the driven bevel gear.

[0010] As a further solution of the present utility model: a connecting groove is formed on the outer wall of the bottom surface of the connecting plate, sliders are slidably connected to both ends of the inner wall of the connecting groove, limiting blocks are fixed on both inner walls of the connecting groove, and limiting grooves slidably matched with the limiting blocks are formed on the outer walls of both sides of the slider.

[0011] As a further solution of the present utility model: moving blocks are arranged at both ends of the bidirectional lead screw, and the two moving blocks are respectively connected to both ends of the bidirectional lead screw through threads with opposite helix directions. A connecting rod is rotatably connected to the top end of the moving block, both connecting rods are rotatably connected to the connecting shaft, and the other end of the connecting rod is rotatably connected to the slider.

[0012] As a further solution of the present utility model: a connecting rod is fixed on the side wall of the seat, a sliding groove is formed on the outer wall of one side of the mounting seat, and the connecting rod is slidably matched with the sliding groove.

[0013] As a further solution of the present utility model: the seat and the connecting plate are connected through a quick-release component. The quick-release component includes a connecting block and a clamping block. The connecting block is relatively fixed on the outer wall of the bottom surface of the seat, a slot matched with the connecting block is formed on the outer wall of the top surface of the connecting plate, a cavity is formed on the outer wall of one side of the connecting plate, and the clamping block is slidably matched with the inner wall of the cavity.

[0014] As a further solution of the present utility model: a clamping groove is formed on the outer wall of one side of the connecting block, the clamping block is in limit fit with the clamping groove, the side wall of the clamping block near the clamping groove is inclined, and a push plate is fixed on the outer wall of one side of the clamping block.

[0015] Compared with the prior art, the present utility model provides a simulated flight cockpit, which has the following beneficial effects:

[0016] 1. In the present utility model, by providing an adjusting component, rotating the turning handle makes the rotating shaft rotate. The rotation of the bidirectional lead screw is driven by the transmission between the driving bevel gear and the driven bevel gear, so that the moving block moves along the bidirectional lead screw, and the connecting rod drives the connecting plate to rise and fall through the slider, changing the height of the seat, enabling the user to adjust the seat height according to their own height.

[0017] 2. In the present utility model, by providing a connecting rod and a sliding groove, the seat can be limited, improving the stability of the seat.

[0018] 3. In this utility model, by providing a quick-release component, when disassembling the seat, move the push plate to one side, drive the latch away from the card slot, compress the fixing spring, release the fixation of the seat, and then move the seat upward to remove the seat. Compared with bolt fixation, it is convenient to disassemble and assemble the seat.

[0019] The parts not involved in this device are the same as or can be implemented using the prior art. This utility model has a simple structure and convenient operation. Description of the Drawings

[0020] Figure 1 It is a schematic diagram of the overall structure of a simulated flight cockpit proposed by this utility model;

[0021] Figure 2 It is a schematic diagram of the internal structure of a simulated flight cockpit proposed by this utility model;

[0022] Figure 3 It is a schematic diagram of the lifting structure of the adjustment component of a simulated flight cockpit proposed by this utility model;

[0023] Figure 4 It is a schematic diagram of the transmission structure of the adjustment component of a simulated flight cockpit proposed by this utility model;

[0024] Figure 5 It is a partial cross-sectional view of a simulated flight cockpit proposed by this utility model;

[0025] Figure 6 It is a schematic diagram of the quick-release component structure of a simulated flight cockpit proposed by this utility model.

[0026] In the figure: 1 - base, 2 - mounting seat, 3 - connecting rod, 4 - sliding groove, 5 - connecting plate, 6 - bidirectional lead screw, 7 - moving block, 8 - connecting shaft, 9 - connecting groove, 10 - slider, 11 - limiting block, 12 - driven bevel gear, 13 - driving bevel gear, 14 - rotating shaft, 15 - turning handle, 16 - seat, 17 - connecting block, 18 - cavity, 19 - fixing spring, 20 - latch, 21 - card slot, 22 - push plate, 23 - connecting rod. Detailed Implementation Modes

[0027] Next, the technical solutions in the embodiments of this utility model will be clearly and completely described in conjunction with the drawings in the embodiments of this utility model. Obviously, the described embodiments are only a part of the embodiments of this utility model, rather than all of the embodiments.

[0028] In the description of the present utility model, it should be understood that the orientation or positional relationship indicated by the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings. It is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation. Therefore, it should not be construed as a limitation to the present utility model.

[0029] Embodiment 1

[0030] A simulated flight cockpit, as Figures 1 to 4 shown, includes a base 1. An installation seat 2 is fixed to the inner wall of the top surface of the base 1. A connecting plate 5 is connected to the outer wall of the top surface of the installation seat 2 through an adjusting assembly. A seat 16 is fixed to the top surface of the connecting plate 5. The adjusting assembly includes a bidirectional lead screw 6 and a rotating shaft 14. The two ends of the bidirectional lead screw 6 are relatively rotatably connected to both ends of the inner wall of the installation seat 2. The rotating shaft 14 is rotatably connected to one side of the inner wall of the installation seat 2. The rotating shaft 14 and the bidirectional lead screw 6 are arranged in a staggered manner. One end of the rotating shaft 14 is connected to a turning handle 15. A driving bevel gear 13 is fixed to the rotating shaft 14. A driven bevel gear 12 is fixed to one end of the bidirectional lead screw 6. The driving bevel gear 13 and the driven bevel gear 12 are in transmission engagement. Two moving blocks 7 are arranged at both ends of the bidirectional lead screw 6. The two moving blocks 7 are respectively connected to both ends of the bidirectional lead screw 6 through threads with opposite helix directions. The top end of the moving block 7 is rotatably connected to a connecting rod 23. Both of the two connecting rods 23 are rotatably connected to a connecting shaft 8. A connecting groove 9 is formed in the outer wall of the bottom surface of the connecting plate 5. Both ends of the inner wall of the connecting groove 9 are slidably connected with sliding blocks 10. Limiting blocks 11 are fixed to both inner walls of the connecting groove 9. Limiting grooves slidably matched with the limiting blocks 11 are formed in the outer walls on both sides of the sliding block 10. The other end of the connecting rod 23 is rotatably connected to the sliding block 10. A connecting rod 3 is fixed to the side wall of the seat 16. A sliding groove 4 is formed in the outer wall on one side of the installation seat 2. The connecting rod 3 is slidably matched with the sliding groove 4.

[0031] During adjustment, rotate the turning handle 15 to make the rotating shaft 14 rotate. Drive the bidirectional lead screw 6 to rotate through the transmission between the driving bevel gear 13 and the driven bevel gear 12, so that the moving block 7 moves along the bidirectional lead screw 6, and make the connecting rod 23 drive the connecting plate 5 to rise and fall through the sliding block 10, changing the height of the seat 16. During the rising and falling process of the seat 16, the connecting rod 3 slides in the sliding groove 4 along with the seat 16. The connecting rod 3 can limit the seat 16 and improve the stability of the seat 16.

[0032] By setting the adjusting component, turning the handle 15 causes the rotating shaft 14 to rotate. The rotation of the bidirectional lead screw 6 is driven by the transmission between the driving bevel gear 13 and the driven bevel gear 12. The moving block 7 moves along the bidirectional lead screw 6, and the connecting rod 23 drives the connecting plate 5 to rise and fall through the slider 10, changing the height of the seat 16, so that the user can adjust the height of the seat 16 according to their own height.

[0033] By setting the connecting rod 3 and the chute 4, the seat 16 can be limited, improving the stability of the seat 16.

[0034] Embodiment 2

[0035] A simulated flight cockpit. In this embodiment, the following improvements are made on the basis of Embodiment 1. As Figure 5 、 Figure 6 shown, the seat 16 is connected to the connecting plate 5 through a quick-release component. The quick-release component includes a connecting block 17 and a clamping block 20. The connecting block 17 is relatively fixed to the outer wall of the bottom surface of the seat 16. A slot matching the connecting block 17 is provided on the outer wall of the top surface of the connecting plate 5. A cavity 18 is provided on one outer wall of the connecting plate 5. The clamping block 20 is slidably fitted to the inner wall of the cavity 18. A fixing spring 19 is fixed to one outer wall of the clamping block 20, and the other end of the fixing spring 19 is connected to the inner wall of the cavity 18. A clamping groove 21 is provided on one outer wall of the connecting block 17. The clamping block 20 is in limit fit with the clamping groove 21. One end side wall of the clamping block 20 close to the clamping groove 21 is inclined, and a push plate 22 is fixed to one outer wall of the clamping block 20.

[0036] When disassembling the seat 16, move the push plate 22 to one side, driving the clamping block 20 away from the clamping groove 21, and the fixing spring 19 is compressed, releasing the fixation of the seat 16. Move the seat 16 upward to remove the seat 16. When installing, insert the connecting block 17 into the slot. The clamping block 20 is pushed by the connecting block 17 to move away from the connecting block 17, and the fixing spring 19 is compressed. When the clamping groove 21 is aligned with the clamping block 20, the fixing spring 19 pushes the clamping block 20 into the clamping groove 21 to complete the installation.

[0037] By setting the quick-release component, when disassembling the seat 16, move the push plate 22 to one side, driving the clamping block 20 away from the clamping groove 21, and the fixing spring 19 is compressed, releasing the fixation of the seat 16. Move the seat 16 upward to remove the seat 16. Compared with bolt fixation, it is convenient for disassembling and assembling the seat 16.

[0038] Working principle: During adjustment, turn the throttle grip 15 to rotate the rotating shaft 14. Through the transmission between the driving bevel gear 13 and the driven bevel gear 12, drive the bidirectional lead screw 6 to rotate, causing the moving block 7 to move along the bidirectional lead screw 6. Make the connecting rod 23 drive the connecting plate 5 to rise and fall through the slider 10, changing the height of the seat 16. During the lifting and lowering process of the seat 16, the connecting rod 3 slides in the chute 4 along with the seat 16. The connecting rod 3 can limit the position of the seat 16, improving the stability of the seat 16; when disassembling the seat 16, move the push plate 22 to one side, driving the latch 20 away from the card slot 21, compressing the fixing spring 19, releasing the fixation of the seat 16, move the seat 16 upward to remove the seat 16. During installation, insert the connecting block 17 into the slot. The latch 20 is pushed by the connecting block 17 to move away from the connecting block 17, compressing the fixing spring 19. When the card slot 21 is aligned with the latch 20, the fixing spring 19 pushes the latch 20 into the card slot 21 to complete the installation.

[0039] The above are only the preferred specific embodiments of the present invention, but the protection scope of the present invention is not limited thereto. Any person skilled in the art within the technical scope disclosed by the present invention, according to the technical solution and inventive concept of the present invention, making equivalent replacements or changes should be covered within the protection scope of the present invention.

Claims

1. A simulated flight cockpit, comprising a base (1), characterized in that: A mounting seat (2) is fixed on the inner wall of the top surface of the base (1); a connecting plate (5) is connected to the outer wall of the top surface of the mounting seat (2) via an adjustment component; a seat (16) is fixed on the top surface of the connecting plate (5); a connecting rod (3) is fixed to the side wall of the seat (16); a sliding groove (4) is provided on the outer wall of one side of the mounting seat (2); and the connecting rod (3) is slidably matched with the sliding groove (4).

2. A simulated flight cockpit according to claim 1, characterized in that: The adjustment assembly comprises a bidirectional screw rod (6) and a rotating shaft (14); the bidirectional screw rod (6) is rotatably connected to two ends of the inner wall of the mounting seat (2); the rotating shaft (14) is rotatably connected to one side of the inner wall of the mounting seat (2); the rotating shaft (14) and the bidirectional screw rod (6) are arranged alternately; one end of the rotating shaft (14) is connected to a turning handle (15).

3. A simulated flight cockpit according to claim 2, characterized in that: A driving bevel gear (13) is fixed on the rotating shaft (14), a driven bevel gear (12) is fixed on one end of the bidirectional screw rod (6), and the driving bevel gear (13) is in transmission meshing engagement with the driven bevel gear (12).

4. A simulated flight cockpit according to claim 1, characterized in that: The outer wall of the bottom surface of the connecting plate (5) is provided with a connecting groove (9), and sliding blocks (10) are slidably connected to the inner walls of the connecting groove (9) at both ends. Limiting blocks (11) are fixed to the inner walls on both sides of the connecting groove (9), and the outer walls on both sides of the sliding block (10) are provided with limiting grooves that slidably cooperate with the limiting blocks (11).

5. A simulated flight cockpit according to claim 2, characterized in that: A moving block (7) is provided at both ends of the bidirectional screw rod (6); the two moving blocks (7) are respectively connected to the two ends of the bidirectional screw rod (6) via threads with opposite rotation directions; the top end of the moving block (7) is rotatably connected to a connecting rod (23); the two connecting rods (23) are both rotatably connected to a connecting shaft (8); and the other end of the connecting rod (23) is rotatably connected to a slider (10).

6. A simulated flight cockpit according to claim 1, characterized in that: The seat (16) and the connecting plate (5) are connected via a quick-release assembly, wherein the quick-release assembly comprises a connecting block (17) and a clamping block (20), wherein the connecting block (17) is relatively fixed to the outer wall of the bottom surface of the seat (16), a slot matching with the connecting block (17) is provided on the outer wall of the top surface of the connecting plate (5), a cavity (18) is provided on the outer wall of one side of the connecting plate (5), and the clamping block (20) is slidably matched with the inner wall of the cavity (18).

7. A simulated flight cockpit according to claim 6, characterized in that: A slot (21) is provided on an outer wall of one side of the connection block (17), the slot (20) and the slot (21) are limitedly matched, the slot (20) is inclined near a side wall of one end of the slot (21), and a push plate (22) is fixed on an outer wall of one side of the slot (20).

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