Airplane turning system test box convenient to use and having buffering effect

Abstract

The utility model relates to the technical field of airplane turning system test boxes, and discloses an airplane turning system test box which is convenient to use and has a buffering effect, and comprises a bottom box, a soft cushion plate is arranged in the bottom box, a tester is arranged on one side of the outer surface of the soft cushion plate, a cover plate is arranged on one side of the outer surface of the bottom box, and the cover plate is arranged on the bottom box. A limiting block is arranged on one side of the outer surface of the cover plate, a connecting box is arranged on one side of the outer surface of the cover plate, a device pipe is arranged in the connecting box, an inserting rod is arranged in the device pipe, a groove plate is arranged on one side of the outer surface of the inserting rod, a rotating disc is arranged on one side of the outer surface of the groove plate, and an auxiliary groove plate is arranged on one side of the outer surface of the rotating disc. According to the utility model, when the threaded rod rotates, the auxiliary groove plate moves left and right, so that the turntable rotates, when the turntable rotates, the rotating rod drives the groove plate to move left and right, so that the insertion rod moves left and right, and when the insertion rod is disconnected with the bottom box, the cover plate can be taken down, so that the effect of convenient disassembly and repair is realized.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft turning system test boxes, and specifically relates to an aircraft turning system test box which is convenient to use and has a buffering effect. Background Technique

[0002] The aircraft turning system test box is mainly used to test the performance of the aircraft turning system to ensure its reliability and safety during flight.

[0003] With the continuous changes in people's lives, the use of aircraft has become more and more common, which has also made the production of aircraft more and more common. When an aircraft is in use, an aircraft turning system test box needs to be configured to ensure the safety of the aircraft. However, the traditional device is not convenient for internal disassembly and repair during use, which makes its use have great limitations. Therefore, a new structure is proposed now to solve this technical problem. Content of the Utility Model

[0004] (1) Technical Problem to be Solved

[0005] Aiming at the deficiencies of the prior art, the utility model provides an aircraft turning system test box which is convenient to use and has a buffering effect, and has the advantages of being convenient for disassembly and repair, etc., and solves the problem that the traditional device in the above background technique is not convenient for disassembly and repair.

[0006] (2) Technical Solution

[0007] To achieve the purpose of being convenient for disassembly and repair mentioned in the above background technique, the utility model provides the following technical solution: an aircraft turning system test box which is convenient to use and has a buffering effect, including a bottom box, a soft cushion plate is arranged inside the bottom box, a tester is arranged on one side of the outer surface of the soft cushion plate, a cover plate is arranged on one side of the outer surface of the bottom box, a limiting block is arranged on one side of the outer surface of the cover plate, a connecting box is arranged on one side of the outer surface of the cover plate, a device pipe is arranged inside the connecting box, an inserting rod is arranged inside the device pipe, a groove plate is arranged on one side of the outer surface of the inserting rod, a turntable is arranged on one side of the outer surface of the groove plate, an auxiliary groove plate is arranged on one side of the outer surface of the turntable, a threaded rod is arranged on one side of the outer surface of the turntable, and a rotating rod is arranged on one side of the outer surface of the turntable.

[0008] Preferably, the number of the connecting boxes is two, and the two connecting boxes are uniformly arranged on one side of the outer surface of the cover plate.

[0009] Preferably, one side of the outer surface of the connecting box contacts with one side of the outer surface of the cover plate, penetrates through one side of the outer surface of the cover plate to the other side of the outer surface of the cover plate, and is fixedly connected with the cover plate.

[0010] Preferably, the number of the device tubes is two, and the two device tubes are uniformly arranged in the left and right connection boxes.

[0011] Preferably, one end of the device tube contacts one side of the inner wall of the connection box, penetrates one side of the inner wall of the connection box to one side of the outer surface of the connection box, and is fixedly connected to the connection box.

[0012] Preferably, one end of the threaded rod contacts one side of the outer surface of the auxiliary groove plate, penetrates one side of the outer surface of the auxiliary groove plate to the other side of the outer surface of the auxiliary groove plate, and is threadedly connected to the auxiliary groove plate.

[0013] Chutes are arranged on the upper and lower sides of the inner wall of the device tube. One side of the outer surface of the chute contacts one side of the inner wall of the device tube, penetrates one side of the inner wall of the device tube to one side of the outer surface of the device tube. The inserting rod is arranged in the device tube. One side of the outer surface of the inserting rod is provided with a sliding rod. One end of the sliding rod is fixedly connected to one side of the outer surface of the inserting rod, and the other end of the sliding rod is slidably connected to the inner wall of the chute, so that when the inserting rod moves left and right, it has better stability.

[0014] The number of the rotating rods is multiple. Every two rotating rods are uniformly arranged on one side of the outer surface of the turntable. One end of the left rotating rod is slidably connected to the inner wall of the groove plate, and one end of the right rotating rod is slidably connected to the inner wall of the auxiliary groove plate. The auxiliary groove plate is threadedly connected to the threaded rod. When the threaded rod rotates, the auxiliary groove plate moves left and right, so that the turntable rotates. Then the left rotating rod drives the groove plate to move left and right.

[0015] Compared with the prior art, the utility model provides a test box for an aircraft turning system which is convenient to use and has a buffering effect, and has the following beneficial effects:

[0016] 1. In the utility model, by arranging the threaded rod in the device, when the threaded rod rotates, the auxiliary groove plate moves left and right, so that the turntable rotates. When the turntable rotates, the rotating rod drives the groove plate to move left and right, and then the inserting rod moves left and right. When the inserting rod is disconnected from the bottom box, the cover plate can be removed, thus achieving the effect of being convenient for disassembly and repair.

[0017] 2. In the utility model, by arranging the soft cushion plate in the device, one side of the outer surface of the soft cushion plate is fixedly connected to the upper side of the inner bottom wall of the bottom box, and the side of the outer surface of the soft cushion plate far from the inner bottom wall of the bottom box is fixedly connected to the tester, so that the device has a certain protective effect on the tester. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 is a schematic structural diagram of the utility model;

[0019] Figure 2 is a front sectional view of the structure of the utility model;

[0020] Figure 3 This is a partial enlarged front view sectional view of the structure of the present utility model.

[0021] Among them: 1. Bottom box; 2. Soft cushion plate; 3. Tester; 4. Cover plate; 5. Limit block; 6. Connection box; 7. Device tube; 8. Insert rod; 9. Groove plate; 10. Turntable; 11. Auxiliary groove plate; 12. Threaded rod; 13. Rotating rod. Specific implementation manner

[0022] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments in the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0023] Please refer to Figures 1 - 3 , an aircraft turning system test box that is easy to use and has a buffering effect, including a bottom box 1;

[0024] As Figures 1 - 3 shown, a soft cushion plate 2 is arranged inside the bottom box 1, a tester 3 is arranged on one side of the outer surface of the soft cushion plate 2, a cover plate 4 is arranged on one side of the outer surface of the bottom box 1, a limit block 5 is arranged on one side of the outer surface of the cover plate 4, a connection box 6 is arranged on one side of the outer surface of the cover plate 4, a device tube 7 is arranged inside the connection box 6, an insert rod 8 is arranged inside the device tube 7, a groove plate 9 is arranged on one side of the outer surface of the insert rod 8, a turntable 10 is arranged on one side of the outer surface of the groove plate 9, an auxiliary groove plate 11 is arranged on one side of the outer surface of the turntable 10, a threaded rod 12 is arranged on one side of the outer surface of the auxiliary groove plate 11, and a rotating rod 13 is arranged on one side of the outer surface of the turntable 10.

[0025] Specifically, as Figures 1 - 3 shown, the number of connection boxes 6 is two, and the two connection boxes 6 are evenly arranged on one side of the outer surface of the cover plate 4.

[0026] Specifically, as Figures 1 - 3 shown, one side of the outer surface of the connection box 6 is in contact with one side of the outer surface of the cover plate 4, penetrates through one side of the outer surface of the cover plate 4 to the other side of the outer surface of the cover plate 4, and is fixedly connected to the cover plate 4.

[0027] Specifically, as Figures 1 - 3 shown, the number of device tubes 7 is two, and the two device tubes 7 are evenly arranged in the left and right connection boxes 6.

[0028] Specifically, as Figures 1 - 3 shown, one end of the device tube 7 is in contact with one side of the inner wall of the connection box 6, penetrates through one side of the inner wall of the connection box 6 to the outer surface of the connection box 6, and is fixedly connected to the connection box 6.

[0029] Specifically, as Figures 1 - 3 shown, one end of the threaded rod 12 contacts one side of the outer surface of the auxiliary groove plate 11, penetrates through one side of the outer surface of the auxiliary groove plate 11 to the other side of the outer surface of the auxiliary groove plate 11, and is threadedly connected to the auxiliary groove plate 11.

[0030] Through the above technical solution, chutes are provided on the upper and lower sides of the inner wall of the device tube 7, and one side of the outer surface of the chute contacts one side of the inner wall of the device tube 7, penetrates through one side of the inner wall of the device tube 7 to one side of the outer surface of the device tube 7, and the insertion rod 8 is arranged in the device tube 7. A slide bar is arranged on one side of the outer surface of the insertion rod 8, one end of the slide bar is fixedly connected to one side of the outer surface of the insertion rod 8, and the other end of the slide bar is slidably connected to the inner wall of the chute, so that the insertion rod 8 is more stable when moving left and right;

[0031] Moreover, the number of the rotating rods 13 is multiple, and every two rotating rods 13 are evenly arranged on one side of the outer surface of the turntable 10 as a group. One end of the left rotating rod 13 is slidably connected to the inner wall of the groove plate 9, one end of the right rotating rod 13 is slidably connected to the inner wall of the auxiliary groove plate 11, and the auxiliary groove plate 11 is threadedly connected to the threaded rod 12. Therefore, when the threaded rod 12 rotates, the auxiliary groove plate 11 moves left and right, so that the turntable 10 rotates, and thus the left rotating rod 13 drives the groove plate 9 to move left and right.

[0032] During use, by fixedly connecting the tester 3 to the soft cushion plate 2, then connecting the cover plate 4 to the bottom box 1, the limit block 5 contacts the tester 3, and then rotating the threaded rod 12, the auxiliary groove plate 11 moves left and right, so that the turntable 10 rotates, and thus the rotating rod 13 drives the groove plate 9 to move left and right, so that the insertion rod 8 moves left and right. When the insertion rod 8 is inserted into the bottom box 1, the cover plate 4 is connected to the device, and then connecting the device to the aircraft, the device can be used normally.

[0033] Although the embodiments of the present invention have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principle and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An aircraft turning system test box which is easy to use and has a buffering effect, comprising a bottom box (1), characterized in that: A soft pad (2) is arranged inside the bottom box (1), a tester (3) is arranged on one side of the outer surface of the soft pad (2), a cover plate (4) is arranged on one side of the outer surface of the bottom box (1), a limit block (5) is arranged on one side of the outer surface of the cover plate (4), a connection box (6) is arranged on one side of the outer surface of the cover plate (4), a device tube (7) is arranged inside the connection box (6), a plug rod (8) is arranged inside the device tube (7), a slot plate (9) is arranged on one side of the outer surface of the plug rod (8), a turntable (10) is arranged on one side of the outer surface of the slot plate (9), an auxiliary slot plate (11) is arranged on one side of the outer surface of the turntable (10), a threaded rod (12) is arranged on one side of the outer surface of the auxiliary slot plate (11), and a rotating rod (13) is arranged on one side of the outer surface of the turntable (10).

2. The aircraft turning system test box which is easy to use and has a buffering effect according to claim 1 is characterized in that: The number of the connection boxes (6) is two, and the two connection boxes (6) are evenly arranged on one side of the outer surface of the cover plate (4).

3. The aircraft turning system test box which is easy to use and has a buffering effect according to claim 1 is characterized in that: One side of the outer surface of the connection box (6) contacts one side of the outer surface of the cover plate (4), penetrates one side of the outer surface of the cover plate (4), reaches the other side of the outer surface of the cover plate (4), and is fixedly connected to the cover plate (4).

4. The aircraft turning system test box which is easy to use and has a buffering effect according to claim 1 is characterized in that: The number of the device pipes (7) is two, and the two device pipes (7) are evenly arranged in the connection boxes (6) on the left and right sides.

5. The aircraft turning system test box which is easy to use and has a buffering effect according to claim 1, characterized in that: One end of the device pipe (7) contacts one side of the inner wall of the connection box (6), passes through one side of the inner wall of the connection box (6), reaches one side of the outer surface of the connection box (6), and is fixedly connected to the connection box (6).

6. The aircraft turning system test box which is easy to use and has a buffering effect according to claim 1, characterized in that: One end of the threaded rod (12) is connected to one side of the outer surface of the auxiliary groove plate (11). Contacting and penetrating one side of the outer surface of the auxiliary slot plate (11) to the other side of the outer surface of the auxiliary slot plate (11), The auxiliary groove plate (11) is threadedly connected thereto.

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