Test box for cabin controller

Abstract

The utility model relates to the technical field of cabin controllers, and discloses a test box for a cabin controller, which comprises a test box body, fixing mechanisms are arranged on both sides in the test box body, and a cabin controller body is arranged between the two fixing mechanisms. According to the test box for the cabin controller, the cabin controller body can be clamped and fixed under the elastic potential energy of the spring through the arranged fixing mechanism, and when the test box body collides, the damage phenomenon of the surface of the internal cabin controller body can be observed, so that the test box body can be conveniently tested. The anti-collision performance of the cockpit controller body is tested through the detection mechanism, the anti-collision degree of the cockpit controller body can be further known, the cover body can be positioned through the installation mechanism by connecting a locking nut to the surface of a limiting rod in a threaded mode, and therefore installation of the cover body is achieved, and the anti-collision performance of the cockpit controller body is improved. And the internal cabin controller body can be further fixed.

Description

Technical Field

[0001] The utility model relates to the technical field of cockpit controllers, and specifically relates to a test box for a cockpit controller. Background Technique

[0002] A cockpit controller is a domain centralized computing platform that integrates multiple independent control units, such as instrument panels, central control display systems, in-vehicle infotainment systems, etc., and integrates more intelligent functions, such as a driver monitoring system (DMS), etc. Cockpit controllers are playing an increasingly important role in intelligent vehicles. With the continuous development of vehicle intelligence and networking, the amount of data that cockpit controllers need to process is increasing, and the requirements for computing power and functions are also getting higher and higher.

[0003] At present, before a cockpit controller is put into use, it does not have the ability to test the anti-collision performance of the cockpit controller, which results in the phenomenon that some unqualified cockpit controllers are easily damaged during use, and there are defects. Content of the Utility Model

[0004] The purpose of the utility model is to provide a test box for a cockpit controller to solve the problems raised in the above background technique.

[0005] To achieve the above purpose, the utility model provides the following technical solution: A test box for a cockpit controller, including a test box body, fixing mechanisms are arranged on both sides inside the test box body, a cockpit controller body is arranged between the two fixing mechanisms, and an installation mechanism is arranged on the top of the test box body.

[0006] The fixing mechanism includes fixing rods, the fixing rods are fixedly connected to both sides inside the test box body, sliding plates are slidably connected to the surfaces of the fixing rods, connecting plates are fixedly connected to the surfaces of the sliding plates, first support rods are rotatably connected inside the connecting plates, support plates are fixedly connected to the surfaces of the first support rods, second support rods are fixedly connected to the sides of the support plates away from the connecting plates, and positioning plates are rotatably connected to the surfaces of the second support rods.

[0007] Preferably, the number of the positioning plates is two, and the cockpit controller body is arranged between the two positioning plates. By arranging the positioning plates, the cockpit controller body can be fixed.

[0008] Preferably, springs are sleeved on the surfaces of the fixing rods, the springs are arranged on one side of the sliding plates, and support members are fixedly connected to the surfaces of the fixing rods, and the support members are fixedly connected to the inner walls of the test box body. By arranging the springs, elastic force can be provided.

[0009] Preferably, the installation mechanism includes a cover body which is arranged on the top of the test box body. Both sides of the top of the cover body are fixedly connected with handles. Through the arranged handles, it is convenient to take the cover body.

[0010] Preferably, both sides of the cover body are fixedly connected with connecting frames. Both sides inside the connecting frames are provided with limiting grooves. Limiting rods are inserted into the limiting grooves. The bottom of the limiting rods is fixedly connected with limiting blocks. The limiting blocks are fixedly connected to both sides of the top of the test box body. Through the arranged limiting rods, the cover body can be preliminarily limited.

[0011] Preferably, the surface of the limiting rod is provided with threads. A locking nut is threadedly connected to the surface of the limiting rod. The locking nut is arranged on the top of the connecting frame. By threadedly connecting the locking nut to the surface of the limiting rod, the cover body can be positioned, thereby realizing the installation of the cover body.

[0012] Compared with the prior art, the present utility model provides a test box for a cockpit controller, which has the following beneficial effects:

[0013] 1. For the test box for the cockpit controller, through the arranged fixing mechanism, under the elastic potential energy of the spring, the cockpit controller body can be clamped and fixed. When the test box body collides, the anti-collision performance of the cockpit controller body itself can be tested by observing the damage phenomenon on the surface of the cockpit controller body inside, and the anti-collision degree of the cockpit controller body itself can be further understood.

[0014] 2. For the test box for the cockpit controller, through the arranged installation mechanism, by threadedly connecting the locking nut to the surface of the limiting rod, the cover body can be positioned, thereby realizing the installation of the cover body, and the cockpit controller body inside can be further fixed. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] In order to more clearly illustrate the technical solutions in the embodiments of the present utility model, the following will briefly introduce the drawings required for the description of the embodiments. Obviously, the following drawings are only some embodiments of the present utility model. For those of ordinary skill in the art, without creative efforts, other drawings can also be obtained according to these drawings:

[0016] Figure 1 It is a schematic diagram of the overall structure of the present utility model;

[0017] Figure 2 It is a schematic diagram of a partial structure of the present utility model;

[0018] Figure 3 It is a schematic diagram of the fixing mechanism of the present utility model;

[0019] Figure 4 This is a schematic diagram of the installation mechanism of the present utility model.

[0020] In the figure: 1. Test box body; 2. Fixing mechanism; 21. Fixing rod; 22. Spring; 23. Sliding plate; 24. Support member; 25. Connecting plate; 26. First support rod; 27. Support plate; 28. Second support rod; 29. Positioning plate; 3. Installation mechanism; 31. Cover body; 32. Handle; 33. Limit block; 34. Limit rod; 35. Connecting frame; 4. Cockpit controller body. Specific implementation manner

[0021] 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 of the present utility model, all other embodiments obtained by those of ordinary skill in the art without making creative efforts shall fall within the protection scope of the present utility model.

[0022] The present utility model provides a technical solution:

[0023] Embodiment 1:

[0024] Combined with Figure 1-2 to Figure 3 , a test box for a cockpit controller includes a test box body 1, fixing mechanisms 2 are arranged on both sides inside the test box body 1, a cockpit controller body 4 is arranged between the two fixing mechanisms 2, and an installation mechanism 3 is arranged on the top of the test box body 1.

[0025] The fixing mechanism 2 includes fixing rods 21, the fixing rods 21 are fixedly connected to both sides inside the test box body 1, a sliding plate 23 is slidably connected to the surface of the fixing rods 21, a connecting plate 25 is fixedly connected to the surface of the sliding plate 23, a first support rod 26 is rotatably connected inside the connecting plate 25, a support plate 27 is fixedly connected to the surface of the first support rod 26, a second support rod 28 is fixedly connected to the side of the support plate 27 away from the connecting plate 25, and a positioning plate 29 is rotatably connected to the surface of the second support rod 28.

[0026] Furthermore, the number of the positioning plates 29 is two, and the cockpit controller body 4 is arranged between the two positioning plates 29. By arranging the positioning plates 29, the cockpit controller body 4 can be fixed.

[0027] Furthermore, a spring 22 is sleeved on the surface of the fixing rod 21, the spring 22 is arranged on one side of the sliding plate 23, and a support member 24 is fixedly connected to the surface of the fixing rod 21, and the support member 24 is fixedly connected to the inner wall of the test box body 1. By arranging the spring 22, elastic force can be provided.

[0028] Embodiment 2:

[0029] Refer to Figure 4 , and on the basis of Embodiment 1, it is further obtained that the installation mechanism 3 includes a cover body 31, the cover body 31 is arranged on the top of the test box body 1, and both sides of the top of the cover body 31 are fixedly connected with handles 32. Through the arranged handles 32, it is convenient to take the cover body 31.

[0030] Furthermore, both sides of the cover body 31 are fixedly connected with connecting frames 35. Limiting grooves are opened on both sides inside the connecting frames 35, limiting rods 34 are inserted into the limiting grooves, the bottom of the limiting rods 34 is fixedly connected with limiting blocks 33, and the limiting blocks 33 are fixedly connected to both sides of the top of the test box body 1. Through the arranged limiting rods 34, the cover body 31 can be preliminarily limited.

[0031] Furthermore, the surface of the limiting rod 34 is provided with threads, and a locking nut is threadedly connected to the surface of the limiting rod 34. The locking nut is arranged on the top of the connecting frame 35. By threadedly connecting the locking nut to the surface of the limiting rod 34, the cover body 31 can be positioned, thereby realizing the installation of the cover body 31.

[0032] In the actual operation process, when this device is used, first place the cockpit controller body 4 between the two positioning plates 29 on both sides. Under the extrusion of the cockpit controller body 4, the two positioning plates 29 on both sides can be driven to move in the direction away from each other. At this time, the sliding plate 23 slides on the surface of the fixed rod 21 and squeezes the spring 22. Under the elastic potential energy of the spring 22, the cockpit controller body 4 can be clamped and fixed. Then place the cover body 31 on the top of the test box body 1. When the limiting rod 34 is inserted into the limiting groove opened inside the connecting frame 35, at this time, by threadedly connecting the locking nut to the surface of the limiting rod 34, the cover body 31 can be positioned, thereby realizing the installation of the cover body 31, and the cockpit controller body 4 inside can be further fixed. When the test box body 1 collides, the anti-collision performance of the cockpit controller body 4 itself can be tested by observing the damage phenomenon on the surface of the cockpit controller body 4 inside, and the anti-collision degree of the cockpit controller body 4 itself can be further understood.

[0033] 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 "include", "comprise" or any other variant thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device comprising a series of elements not only includes those elements, but also includes other elements not expressly listed, or also includes elements inherent to such process, method, article or device. Without further limitation, an element defined by the statement "comprising an..." does not exclude the presence of additional identical elements in the process, method, article or device comprising said element.

Claims

1. A test box for a cockpit controller, comprising a test box body (1), characterized in that: Fixing mechanisms (2) are provided on both sides of the test box body (1), a cockpit controller body (4) is provided between the two fixing mechanisms (2), and a mounting mechanism (3) is provided on the top of the test box body (1); The fixing mechanism (2) comprises a fixing rod (21), the fixing rod (21) being fixedly connected to both sides of the test box body (1), the surface of the fixing rod (21) being slidably connected to a sliding plate (23), the surface of the sliding plate (23) being fixedly connected to a connecting plate (25), the connecting plate (25) being rotatably connected to a first supporting rod (26), the surface of the first supporting rod (26) being fixedly connected to a supporting plate (27), the side of the supporting plate (27) away from the connecting plate (25) being fixedly connected to a second supporting rod (28), the surface of the second supporting rod (28) being rotatably connected to a positioning plate (29).

2. A test box for a cockpit controller according to claim 1, characterized in that: The number of the positioning plates (29) is two, and the cockpit controller body (4) is arranged between the two positioning plates (29).

3. A test box for a cockpit controller according to claim 1, characterized in that: A spring (22) is sleeved on the surface of the fixing rod (21), and the spring (22) is arranged on one side of the sliding plate (23). A support member (24) is fixedly connected to the surface of the fixing rod (21), and the support member (24) is fixedly connected to the inner wall of the test box body (1).

4. A test box for a cockpit controller according to claim 1, characterized in that: The mounting mechanism (3) comprises a cover body (31), the cover body (31) is arranged on the top of the test box body (1), and handles (32) are fixedly connected to both sides of the top of the cover body (31).

5. A test box for a cockpit controller according to claim 4, characterized in that: The cover body (31) is fixedly connected to a connecting frame (35) on both sides, and the connecting frame (35) is provided with limiting grooves on both sides, and limiting rods (34) are inserted into the limiting grooves. The bottom of the limiting rod (34) is fixedly connected to a limiting block (33), and the limiting blocks (33) are fixedly connected to the tops of both sides of the test box body (1).

6. A test box for a cockpit controller according to claim 5, characterized in that: The surface of the limiting rod (34) is provided with a thread, the surface of the limiting rod (34) is threadedly connected with a locking nut, and the locking nut is arranged on the top of the connecting frame (35).

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