CN214604285U

CN214604285U - Storage cabinet for storing aerospace electronic instruments

Info

Publication number: CN214604285U
Application number: CN202120483727.5U
Authority: CN
Inventors: 郜丹睿; 郜睿特; 马倩一
Original assignee: Hebei Fuzhen Industry Co ltd
Current assignee: Hebei Fuzhen Industry Co ltd
Priority date: 2021-03-06
Filing date: 2021-03-06
Publication date: 2021-11-05
Anticipated expiration: 2031-03-06

Abstract

The utility model relates to a deposit storage cabinet of space flight electronic instrument belongs to the electronic instrument and deposits technical field, and it includes the cabinet body, can dismantle on the internal wall of cabinet and be connected with vertical backup pad, is connected with a plurality of faying plates along vertical direction in the backup pad, and the faying plate goes up the overlap joint and has the board of holding. This application has the effect of being convenient for place the space flight electronic instrument of equidimension not in the cabinet body.

Description

Storage cabinet for storing aerospace electronic instruments

Technical Field

The application relates to the field of electronic instrument storage, in particular to a storage cabinet for storing aerospace electronic instruments.

Background

Aerospace electronic instruments are generally precise, and are generally placed in a storage cabinet for storage after being processed in order to prevent the aerospace electronic instruments from being damaged.

Referring to fig. 1, the existing storage cabinet generally includes a cabinet body 1, a containing opening 11 is opened on one side of the cabinet body 1, a plurality of containing plates 31 are fixedly connected to the inner wall of the cabinet body 1 along the vertical direction, and the space electronic instrument is placed on the containing plates 31 for storage.

In view of the above-mentioned related art, the inventors consider that there is a drawback that it is inconvenient to place a large space electronic instrument.

SUMMERY OF THE UTILITY MODEL

In order to place the space electronic instrument of equidimension not in the cabinet body in the ease, this application provides a deposit storage cabinet of space electronic instrument.

The application provides a deposit storage cabinet of space electron instrument adopts following technical scheme:

the utility model provides a deposit storage cabinet of space flight electronic instrument, includes the cabinet body, can dismantle on the internal wall of cabinet and be connected with vertical backup pad, be connected with a plurality of faying plates along vertical direction in the backup pad, the faying plate goes up the overlap joint and has the board of holding.

By adopting the technical scheme, when in use, the space electronic instrument is placed on the containing plate, and the space electronic instrument is stored in the cabinet body; when a larger space electronic instrument needs to be placed, part of the containing plates can be taken down from the lapping plates, so that the distance between the adjacent containing plates is increased, and the larger space electronic instrument can be stored; in addition, the supporting plate is detachably connected with the cabinet body, and the supporting plate can be detached from the cabinet body so as to store larger space electronic instruments. Therefore, the technical scheme of this application can deposit the space flight electronic instrument of equidimension not, improves the convenience when using.

Preferably, a plurality of jacks are formed in the supporting plate, one end of the lapping plate is inserted into the jack and is bent downwards to form the inserting plate, and a shielding plate is arranged on one side, away from the supporting plate, of the inserting plate and is connected with the supporting plate.

By adopting the technical scheme, the inserting plate is inserted into the inserting hole and abutted against the shielding plate, and then slides downwards, so that the inserting plate is positioned between the shielding plate and the supporting plate, the inserting plate is clamped and fixed, and the lap plate and the supporting plate are clamped and fixed, and the structure is simple and the connection is convenient; simultaneously, when needing to place great space flight electronic instrument, with part hold the board and take off the back, can take off the overlap joint board that is used for accepting the board that holds from the backup pad, further increase the space between the adjacent board that holds, conveniently place space flight electronic instrument.

Preferably, the inner wall of the cabinet body is connected with a vertical partition board, the cabinet body is divided into two chambers by the partition board, and the same supporting plate is connected to the partition board.

Through adopting above-mentioned technical scheme, the setting of baffle is cut apart into two cavities with the cabinet body, and the space flight electronic instrument classification of being convenient for is deposited, improves the regularity that the space flight electronic instrument was deposited.

Preferably, the cabinet body is provided with a containing opening, and one end of the lapping plate close to the containing opening is provided with an arc chamfer.

Through adopting above-mentioned technical scheme, fish tail staff when access space flight electronic instrument is avoided in the setting of circular arc chamfer, security when improving the use. Meanwhile, the aerospace electronic instrument is prevented from being damaged after the aerospace electronic instrument collides with the end part of the lap joint plate.

Preferably, the place of holding is provided with two shielding doors for shielding the place of holding, and the two shielding doors are arranged in an overlapping mode, and a cabinet lock is arranged at the overlapping position.

Through adopting above-mentioned technical scheme, when getting the internal space flight electronic instrument of cabinet of putting, it is fixed to the locking of sheltering from the door to remove the cabinet lock, then slides and shelter from the door, makes two shelter from the door and overlap completely to remove and hold sheltering from of mouthful, be convenient for get and put space flight electronic instrument. The cabinet lock locks and fixes the two shielding plates, so that the stability of the shielding door can be improved, and the two shielding doors are prevented from sliding randomly.

Preferably, the partition plate is connected with the cabinet body in a sliding manner and is connected with a driving assembly for driving the partition plate to move, the driving assembly comprises a driving screw and a driving sliding block, the driving screw is rotatably connected with the cabinet body, and the driving sliding block is fixedly connected with the partition plate and sleeved on the driving screw and in threaded connection with the driving screw.

Through adopting above-mentioned technical scheme, rotate drive screw, drive screw rotates and makes drive slider drive the baffle and remove, thereby the space size that the baffle removed two cavities can be changed, the cavity size is adjusted according to actual need conveniently, convenience when further improving the cabinet body and using.

Preferably, one end of the lapping plate close to the containing opening is connected with a limiting block in a sliding mode, and the limiting block is connected with an elastic piece for driving the limiting block to move up and down.

Through adopting above-mentioned technical scheme, the stopper shelters from the board of holding of overlap joint on the lapping plate, increases the stability of lapping plate, can prevent to hold the board from the tip roll-off of lapping plate to further prevent that space flight electronic instrument from dropping and damaging from the cabinet internal. When the containing plate needs to be taken out, the limiting block is compressed, so that the elastic piece is compressed, the limiting block moves downwards to remove the shielding of the containing plate, and the containing plate is convenient to take out.

Preferably, the elastic part is a limiting spring, one end of the limiting spring is fixedly connected with the limiting block, and the other end of the limiting spring is fixedly connected with the lapping plate.

By adopting the technical scheme, downward pressure is applied to the limiting block, so that the limiting spring is compressed, the limiting block moves downwards, and the shielding of the containing plate is removed; after the pressure on the limiting block is relieved, the limiting spring drives the limiting block to move upwards, so that the limiting block is reset, and the containing plate is shielded conveniently. In addition, the limiting spring has larger elasticity, simple structure and low price.

In summary, the present application includes at least one of the following beneficial technical effects:

1. the distance between two adjacent containing plates can be adjusted by arranging the supporting plate and the butt plate, so that space electronic instruments of different sizes can be stored, and convenience in use is improved.

2. The cabinet body is divided into two chambers by the arrangement of the partition plates, so that the aerospace electronic instruments can be conveniently stored in a classified manner, and the storage uniformity of the aerospace electronic instruments is improved;

3. the limiting blocks are matched with the driving springs, so that the containing plate can be shielded, the stability of the containing plate is increased, and the stability of the aerospace electronic instrument is improved.

Drawings

Fig. 1 is a schematic structural diagram of a related art in the background art.

Fig. 2 is a schematic structural diagram of embodiment 1 of the present application.

Fig. 3 is a schematic structural view of a hidden shielding door according to embodiment 1 of the present application.

Fig. 4 is a schematic structural view for showing the connection relationship between the strap and the support plate in embodiment 1 of the present application.

Fig. 5 is a partial structural schematic view intended to show a glide assembly in embodiment 1 of the present application.

Fig. 6 is a schematic structural diagram of embodiment 2 of the present application.

Fig. 7 is a partial schematic structural view for showing a drive assembly in embodiment 2 of the present application.

Fig. 8 is a partial structural view at a in fig. 7.

Description of reference numerals: 1. a cabinet body; 11. a holding opening; 12. a shutter door; 13. a containing groove; 14. a guide groove; 141. a guide block; 2. a support plate; 21. a jack; 22. a shielding plate; 3. a lap plate; 31. a holding plate; 32. a plugboard; 33. accommodating grooves; 331. a limiting block; 332. a limiting spring; 4. a partition plate; 41. a chamber; 5. a cabinet lock; 6. a slipping component; 61. a slide rail; 62. a pulley; 7. a drive assembly; 71. a drive screw; 72. the slider is driven.

Detailed Description

The present application is described in further detail below with reference to figures 2-8.

Example 1

The embodiment of the application discloses a storage cabinet for storing aerospace electronic instruments. Referring to fig. 2, the storage cabinet for storing the aerospace electronic instrument comprises a cubic cabinet body 1, wherein a containing opening 11 is formed in one side of the cabinet body 1 in the length direction, and a shielding door 12 is arranged at the containing opening 11; referring to fig. 3, a vertical partition plate 4 is fixedly connected in the cabinet 1, and the cabinet 1 is divided into two chambers 41 by the partition plate 4; two support plates 2 are vertically arranged in each chamber 41, wherein one support plate 2 is connected with one side of the cabinet body 1 far away from the partition plate 4 through a bolt, and the other support plate 2 is connected with the partition plate 4 through a bolt; be equipped with a plurality of overlap joint boards 3 along vertical direction on the backup pad 2, the overlap joint has the horizontally to hold board 31 on the overlap joint board 3. When the spaceflight electronic instrument is used, the containing plate 31 is lapped on the lapping plate 3, the spaceflight electronic instrument is placed on the containing plate 31, and the shielding door 12 is closed.

Referring to fig. 3 and 4, a plurality of insertion holes 21 are formed in the surface of one side of the support plate 2 in the length direction, the insertion holes 21 are distributed in the vertical direction, the length direction of the insertion holes 21 is the same as the length direction of the support plate 2, and the insertion holes 21 penetrate through the thickness of the support plate 2. The lapping plate 3 is a horizontally arranged rectangular plate-shaped structure, the length direction of the lapping plate is the same as that of the insertion hole 21, and chamfers are arranged at two ends of the lapping plate 3 in the length direction. One side of the length direction of the bridging plate 3 is inserted into the insertion hole 21 and bent downwards to form the insertion plate 32, the insertion plate 32 is abutted against the support plate 2, and the height of the insertion plate 32 is smaller than that of the insertion hole 21. The side of the insertion plate 32, which is far away from the support plate 2, is provided with two shielding plates 22, the two shielding plates 22 are vertically arranged and distributed along the length direction of the insertion hole 21, and the shielding plates 22 are abutted against the insertion plate 32; the two ends of the shielding plate 22 are bent towards the direction close to the supporting plate 2 and fixedly connected with the supporting plate 2. The supporting plate 2, the lapping plate 3, the inserting plate 32 and the shielding plate 22 are made of metal materials, and zinc layers are plated on the surfaces of the supporting plate, the lapping plate 3, the inserting plate 32 and the shielding plate 22 to achieve an anti-corrosion effect.

When the fixing device is used, the inserting plate 32 penetrates through the inserting hole 21 to be abutted with the shielding plate 22 and then slides downwards, so that the lapping plate 3 is abutted with the bottom wall of the inserting hole 21, and the lapping plate 3 is fixed; then, after the holding plate 31 is lapped on the lapping plate 3, the space electronic instrument is placed on the holding plate 31. When needing to place great space flight electronic instrument, will partly hold board 31 and take off from the overlap joint, then after rebound bridging plate 3 and jack 21 roof butt, again to keeping away from shielding plate 22 direction removal bridging plate 3, take off bridging plate 3 from backup pad 2, increase the space between the adjacent board 31 of holding, be convenient for place great space flight electronic instrument.

Referring back to fig. 1, two shielding doors 12 are provided, the two shielding doors 12 are both slidably connected to the cabinet 1 and are distributed along the width direction of the cabinet 1 and partially overlapped, the two shielding doors 12 are used for shielding the two chambers 41, and a cabinet lock 5 is provided at the overlapping position of the two shielding doors 12. Referring to fig. 5, a group of sliding assemblies 6 is arranged between each shielding door 12 and the cabinet 1, each sliding assembly 6 includes a sliding rail 61 and a pulley 62, the length direction of each sliding rail 61 is the same as the length direction of the cabinet door, and each sliding rail 61 is fixedly connected with the bottom wall of the cabinet 1; the pulley 62 is a spool, is installed at the bottom of the shielding door 12, is located on the slide rail 61, and slides along the slide rail 61, and a plurality of pulleys 62 are arranged along the length direction of the shielding door 12.

When the device is used, the cabinet lock 5 is released from fixing the shielding doors 12, then one of the shielding doors 12 is slid, so that the shielding of one of the chambers 41 is released after the two shielding doors 12 are completely overlapped, and then the aerospace electronic instrument is stored on the containing plate 31.

The implementation principle of the storage cabinet for storing the aerospace electronic instrument in the embodiment of the application is as follows: when in use, firstly, the required number of the lapping plates 3 are fixed on the supporting plate 2 according to the requirement; then, the holding plate 31 is lapped on the lapping plate 3; then, the space electronic instrument is placed on the holding plate 31; finally, the shielding door 12 is slid, and after the shielding opening is shielded, the shielding door 12 is locked by the cabinet lock 5.

Example 2

The embodiment of the application discloses a storage cabinet for storing aerospace electronic instruments. Referring to fig. 6, the difference from embodiment 1 is that the shielding door 12 is used for shielding the containing opening 11, one end of the shielding door 12 in the vertical direction is hinged to the cabinet 1, the hinge shaft is in the vertical direction, and a cabinet lock 5 is arranged between one end of the shielding door 12 far away from the hinge shaft and the cabinet 1.

With reference to fig. 6 and 7, the partition plate 4 is slidably connected to the cabinet 1, a containing groove 13 is formed in the bottom surface of the cabinet 1, and the length direction of the containing groove 13 is the same as the length direction of the cabinet 1. A driving assembly 7 for driving the partition plate 4 to move is arranged in the containing groove 13, the driving assembly 7 comprises a driving screw rod 71 and a driving slide block 72, the driving screw rod 71 is embedded in the containing groove 13 and is rotatably connected with the cabinet body 1, and one end of the driving screw rod 71 extends out of the cabinet body 1; the driving slide block 72 is fixedly connected with the bottom surface of the partition board 4 and is sleeved on the driving screw rod 71 to be in threaded connection with the driving screw rod 71.

Referring to fig. 7, a guide groove 14 is formed in the bottom surface of the cabinet 1, the length direction of the guide groove 14 is the same as the length direction of the containing groove 13, a guide block 141 is slidably connected in the guide groove 14, and the guide block 141 is fixedly connected with the partition plate 4.

When the sizes of the two chambers 41 need to be adjusted, the driving screw 71 is rotated, and the driving screw 71 rotates to enable the driving slider 72 to drive the partition plate 4 to move, so that the position of the partition plate 4 is changed, the sizes of the two chambers 41 are adjusted, and the aerospace electronic instruments with different sizes can be conveniently placed.

Referring to fig. 8, holding tank 33 has been seted up to 3 top surfaces of fagging, holding tank 33 is located the one end that fagging 3 is close to and holds mouthful 11, sliding connection has stopper 331 in holding tank 33, stopper 331 is close to the one side that holds mouthful 11 and is the inclined plane, and stopper 331's bottom surface is connected with the elastic component that the drive reciprocated for limiting spring 332, limiting spring 332's flexible direction is vertical direction, and limiting spring 332's top and stopper 331 fixed connection, bottom and holding tank 33 diapire fixed connection, limiting spring 332 is compressed back stopper 331 and can inlay completely in holding tank 33.

When placing holding plate 31 on lapping plate 3, compress stopper 331, inlay stopper 331 in holding tank 33, then to the inside back that slides in holding plate 31 of cabinet 1, spacing spring 332 drive stopper 331 rebound shelters from holding plate 31, increases holding plate 31's stability. When the containing plate 31 needs to be taken out, the limiting block 331 is compressed, so that the limiting spring 332 is compressed, the limiting block 331 moves downwards to remove the shielding of the containing plate 31, and the containing plate 31 is convenient to take out.

The above embodiments are preferred embodiments of the present application, and the protection scope of the present application is not limited by the above embodiments, so: all equivalent changes made according to the structure, shape and principle of the present application shall be covered by the protection scope of the present application.

Claims

1. The utility model provides a deposit storage cabinet of space flight electronic instrument, includes the cabinet body (1), its characterized in that: the cabinet is characterized in that a vertical supporting plate (2) is detachably connected to the inner wall of the cabinet body (1), a plurality of lapping plates (3) are connected to the supporting plate (2) in the vertical direction, and containing plates (31) are lapped on the lapping plates (3).

2. A storage case for aerospace electronics according to claim 1 and further comprising: a plurality of insertion holes (21) are formed in the supporting plate (2), one end of the lapping plate (3) is inserted into the insertion holes (21) and is bent downwards to form an insertion plate (32), a shielding plate (22) is arranged on one side, far away from the supporting plate (2), of the insertion plate (32), and the shielding plate (22) is connected with the supporting plate (2).

3. A storage case for aerospace electronics according to claim 1 and further comprising: the cabinet is characterized in that the inner wall of the cabinet body (1) is connected with a vertical partition plate (4), the cabinet body (1) is divided into two chambers (41) by the partition plate (4), and the same supporting plate (2) is connected onto the partition plate (4).

4. A storage case for aerospace electronics according to claim 1 and further comprising: the cabinet body (1) is provided with a containing opening (11), and one end of the lapping plate (3) close to the containing opening (11) is provided with an arc chamfer.

5. A storage case for aerospace electronics according to claim 4 and further comprising: the storage opening (11) is provided with two shielding doors (12) for shielding the storage opening (11) in a sliding manner, the two shielding doors (12) are partially overlapped, and the overlapped part is provided with a cabinet lock (5).

6. A storage case for aerospace electronics according to claim 3 and further comprising: baffle (4) and the cabinet body (1) sliding connection to be connected with drive assembly (7) of its removal of drive, drive assembly (7) include drive screw (71) and drive slider (72), and drive screw (71) rotate with the cabinet body (1) and are connected, drive slider (72) and baffle (4) fixed connection, and the cover is established on drive screw (71) and is connected with drive screw (71) threaded connection.

7. A storage case for aerospace electronics according to claim 4 and further comprising: one end of the lap joint plate (3) close to the containing opening (11) is connected with a limiting block (331) in a sliding mode, and the limiting block (331) is connected with an elastic piece for driving the elastic piece to move up and down.

8. A storage case for aerospace electronics according to claim 7 and further comprising: the elastic piece is a limiting spring (332), one end of the limiting spring (332) is fixedly connected with a limiting block (331), and the other end of the limiting spring (332) is fixedly connected with the lapping plate (3).