CN215004308U - Quick framework device of test equipment of aviation simulation mechanism - Google Patents
Quick framework device of test equipment of aviation simulation mechanism Download PDFInfo
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- CN215004308U CN215004308U CN202121218749.5U CN202121218749U CN215004308U CN 215004308 U CN215004308 U CN 215004308U CN 202121218749 U CN202121218749 U CN 202121218749U CN 215004308 U CN215004308 U CN 215004308U
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Abstract
The utility model discloses a quick framework device of test equipment of an aviation simulation mechanism, which comprises a carrying box for loading the test equipment, wherein the carrying box comprises a containing cavity, the carrying box comprises a bottom plate, movable side plates and fixed side plates, two groups of the fixed side plates are oppositely and symmetrically arranged on the bottom plate, two movable side plates are movably arranged on two edges of the bottom plate corresponding to an operation panel and a back plate of the test equipment, and at least two movable side plates are vertically turned in the vertical direction or vertically displaced and adjusted in the vertical direction; the bottom plate is through the upset of activity curb plate or displacement bearing about or to breaking away from ground, can regard the activity curb plate of delivery box as bearing structure and the test equipment on bearing bottom plate and the bottom plate, and the test platform that carries on that can be quick shortens test preparation cycle, promotes efficiency of software testing, can also reduce outdoor equipment of carrying simultaneously.
Description
Technical Field
The utility model belongs to space flight test field, in particular to test equipment's of aviation analog mechanism quick framework device.
Background
When carrying out outdoor simulation test to the assembly devices of space flight, generally transport test equipment to the outdoor place and test, need be equipped with test platform simultaneously and supply to bear test equipment, the facility is loaded down with trivial details, the test preparation cycle is longer, and efficiency is lower.
Disclosure of Invention
The purpose of the invention is as follows: in order to overcome the not enough of existence among the prior art, the utility model provides an aviation analog mechanism's test equipment's quick framework device can carry on test platform fast, promotes efficiency of software testing.
The technical scheme is as follows: in order to achieve the above purpose, the technical scheme of the utility model is as follows:
a rapid framework device of testing equipment of an aviation simulation mechanism comprises a carrying box used for loading the testing equipment, wherein the carrying box comprises an accommodating cavity, the carrying box comprises a bottom plate, movable side plates and fixed side plates, two groups of the fixed side plates are oppositely and symmetrically arranged on the bottom plate, the two movable side plates are movably arranged on two edges of the bottom plate corresponding to an operation panel and a back plate of the testing equipment, and at least two movable side plates are turned over up and down in the vertical direction or adjusted in a vertical displacement mode in the vertical plane; the bottom plate is supported to be separated from the ground through the turnover or the up-and-down displacement of the movable side plate.
Furthermore, the movable side plate is hinged to the side wall of the bottom plate through a hinge, the movable side plate is turned upwards to abut against the fixed side plate and form an accommodating cavity, or the movable side plate is turned downwards to be below the bottom plate.
Furthermore, the included angle alpha between the movable side plate and the bottom surface of the bottom plate is more than or equal to 90 degrees and less than or equal to 270 degrees.
Further, the hinge member is a hinge member.
The movable side plate is detachably sleeved on the outer ring of the two movable side plates; the two movable side plates limit the outward expansion range through a limiting ring.
Furthermore, the limiting ring is a flexible ring structure, and a limiting clamping groove is concavely arranged on the movable side plate corresponding to the limiting ring.
Furthermore, the support device also comprises a plurality of support columns, wherein the support columns are arranged on the bottom plate at intervals corresponding to the movable side plate and the fixed side plate respectively, the bottom ends of the support columns are hinged to the bottom plate, and the other ends of the support columns are free ends.
Furthermore, an elastic damping plate is arranged on the inner side wall of the movable side plate.
Has the advantages that: the utility model discloses can regard as bearing structure and the test equipment on bearing bottom plate and the bottom plate with the activity curb plate of delivery case, carry on test platform that can be quick shortens the test and prepares the cycle, promotes efficiency of software testing, can also reduce the outdoor equipment of carrying simultaneously.
Drawings
FIG. 1 is a schematic view of the internal structure of the overall structure of the present invention;
FIG. 2 is a schematic half-sectional view of the overall structure of the present invention;
FIG. 3 is a schematic view of the inverted three-dimensional structure of the movable side plate of the present invention;
figure 4 is the utility model discloses an overall structure semi-section sketch map after activity curb plate upset.
Detailed Description
The present invention will be further described with reference to the accompanying drawings.
As shown in fig. 1 to 4, a fast framework device of a testing device of an aviation simulation mechanism includes a carrying box 2 for loading the testing device 1, the carrying box 2 includes an accommodating cavity for accommodating the testing device 1, the carrying box 2 includes a bottom plate 3, movable side plates 4 and fixed side plates 5, two groups of the fixed side plates 5 are oppositely and symmetrically arranged on the bottom plate 3, two of the movable side plates 4 are movably arranged on two edges of the bottom plate 3 corresponding to an operation panel of the testing device 1, and at least two of the movable side plates 4 are turned over up and down in a vertical direction or adjusted by displacement up and down in the vertical plane; the bottom plate 3 is supported to be separated from the ground through the overturning or up-and-down displacement of the movable side plate 4. The utility model discloses can do 4 with the activity curb plate of delivery case 2 and for bearing bottom plate and the test equipment 1 on the bottom plate for bearing structure, can be quick carry on test platform, shorten test preparation cycle, promote test efficiency, can also reduce the outdoor equipment of carrying simultaneously.
The embodiment of this scheme adoption: activity curb plate 4 passes through articulated elements 6 and articulates the setting on the lateral wall of bottom plate 3, articulated elements 6 is hinge spare, activity curb plate 4 upwards overturns to the fixed curb plate 4 of butt and constitutes and hold the chamber, perhaps activity curb plate 4 downwards overturns to the below of bottom plate 3 in order to be used for the bearing bottom plate, and overall structure is simple, easy operation is convenient.
The movable side plate locking device comprises a bottom plate, a movable side plate 4 and a locking bolt, wherein the bottom plate is provided with a vertical sliding groove corresponding to the vertical displacement of the movable side plate 4, and the locking bolt is arranged on the bottom plate corresponding to the movable side plate 4 and the sliding groove and used for locking the adjusted movable side plate.
The included angle alpha range of the movable side plate 4 and the bottom surface of the bottom plate 3 is more than or equal to 90 degrees and less than or equal to 270 degrees, namely the maximum overturning movable range of the movable side plate 4, when the alpha is within the angle range of 90 degrees to 180 degrees, the movable side plate and the bottom plate are obliquely arranged, a larger effective supporting area can be provided, the gravity center of the whole device is lower, and the supporting is stable.
The device also comprises a limiting ring 7, wherein the limiting ring 7 is detachably sleeved on the outer rings of the two movable side plates 4; the two movable side plates 4 limit the outward expansion range through the limiting rings 7, and support stability is guaranteed.
The limiting ring 7 is a flexible ring structure, such as an iron wire ring, and a limiting clamping groove 8 is concavely arranged on the movable side plate 4 corresponding to the limiting ring 7 for clamping the limiting ring 7 in order to prevent the limiting ring from slipping.
Still include a plurality of support post 9, it is a plurality of support post 9 sets up on bottom plate 3 corresponding to the interval of activity curb plate 4 and fixed curb plate 5 respectively, the bottom of support post 9 articulates on the bottom plate, just the other end of support post is the free end, and support stability is guaranteed to further promotion support intensity through support post 9.
Be provided with elasticity shock attenuation board 10 on the inside wall of activity curb plate 4, enclose synthetic the chamber that holds when activity curb plate butt in fixed curb plate, elasticity shock attenuation board 10 supports to press in test equipment 1, promotes shock attenuation, resistance to compression protection.
Bottom plate 3 is provided with a plurality of supporting backing plates 11 corresponding to the interval on the wall that holds the chamber to be used for bearing and built on stilts test equipment 1, leave bottom heat dissipation channel, the thermovent has been seted up on bottom plate 3, be provided with heat dissipation fan 12 in the thermovent, promote test equipment 1's radiating efficiency through heat dissipation.
The above description is only a preferred embodiment of the present invention, and it should be noted that: for those skilled in the art, without departing from the principle of the present invention, several improvements and modifications can be made, and these improvements and modifications should also be considered as the protection scope of the present invention.
Claims (8)
1. The utility model provides a quick framework device of test equipment of aviation analog mechanism which characterized in that: the carrying box comprises a carrying box (2) used for loading test equipment (1), wherein the carrying box (2) comprises an accommodating cavity, the carrying box (2) comprises a bottom plate (3), movable side plates (4) and fixed side plates (5), the two groups of fixed side plates (5) are oppositely and symmetrically arranged on the bottom plate (3), the two movable side plates (4) are movably arranged on two edges of the bottom plate (3) corresponding to an operation panel and a back plate of the test equipment (1), and at least two movable side plates (4) are turned over up and down in the vertical direction or adjusted in a vertical plane in a vertical displacement mode; the bottom plate (3) is supported to be separated from the ground through the overturning or the vertical displacement of the movable side plate (4).
2. The device for rapidly constructing the test equipment of the aviation simulation mechanism according to claim 1, wherein: the movable side plate (4) is hinged to the side wall of the bottom plate (3) through a hinge piece (6), the movable side plate (4) is upwards overturned to the butt fixed side plate (5) to form an accommodating cavity, or the movable side plate (4) is downwards overturned to the lower side of the bottom plate (3).
3. The device for rapidly constructing the test equipment of the aviation simulation mechanism, according to claim 2, is characterized in that: the included angle alpha between the movable side plate (4) and the bottom surface of the bottom plate (3) is more than or equal to 90 degrees and less than or equal to 270 degrees.
4. The device for rapidly constructing the test equipment of the aviation simulation mechanism, according to claim 2, is characterized in that: the hinge piece (6) is a hinge piece.
5. The device for fast construction of test equipment for aeronautical simulation institutions according to claim 1 or 2, characterized in that: the device also comprises a limiting ring (7), wherein the limiting ring (7) is detachably sleeved on the outer rings of the two movable side plates (4); the two movable side plates (4) limit the outward expansion range through a limiting ring (7).
6. The rapid architecture device of test equipment of an aviation simulation mechanism according to claim 5, wherein: the limiting ring (7) is a flexible ring structure, and a limiting clamping groove (8) is concavely arranged on the movable side plate (4) corresponding to the limiting ring (7).
7. The device for rapidly constructing the test equipment of the aviation simulation mechanism according to claim 1, wherein: the supporting device is characterized by further comprising a plurality of supporting upright columns (9), wherein the supporting upright columns (9) are arranged on the bottom plate (3) at intervals corresponding to the movable side plate (4) and the fixed side plate (5) respectively, the bottom ends of the supporting upright columns (9) are hinged to the bottom plate, and the other ends of the supporting upright columns are free ends.
8. The device for rapidly constructing the test equipment of the aviation simulation mechanism according to claim 1, wherein: and an elastic damping plate (10) is arranged on the inner side wall of the movable side plate (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121218749.5U CN215004308U (en) | 2021-06-02 | 2021-06-02 | Quick framework device of test equipment of aviation simulation mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121218749.5U CN215004308U (en) | 2021-06-02 | 2021-06-02 | Quick framework device of test equipment of aviation simulation mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215004308U true CN215004308U (en) | 2021-12-03 |
Family
ID=79085882
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121218749.5U Active CN215004308U (en) | 2021-06-02 | 2021-06-02 | Quick framework device of test equipment of aviation simulation mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215004308U (en) |
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2021
- 2021-06-02 CN CN202121218749.5U patent/CN215004308U/en active Active
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