CN210111836U - High stability power supply box structure of civil aircraft display controller - Google Patents
High stability power supply box structure of civil aircraft display controller Download PDFInfo
- Publication number
- CN210111836U CN210111836U CN201921244152.0U CN201921244152U CN210111836U CN 210111836 U CN210111836 U CN 210111836U CN 201921244152 U CN201921244152 U CN 201921244152U CN 210111836 U CN210111836 U CN 210111836U
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- screw
- mounting
- screws
- box body
- installation
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- Expired - Fee Related
Links
- 238000009434 installation Methods 0.000 claims abstract description 31
- 230000001681 protective effect Effects 0.000 claims abstract description 14
- 229920000742 Cotton Polymers 0.000 claims abstract description 11
- 238000013016 damping Methods 0.000 claims abstract description 6
- 238000009423 ventilation Methods 0.000 claims description 6
- 230000000712 assembly Effects 0.000 claims 4
- 238000000429 assembly Methods 0.000 claims 4
- 238000003780 insertion Methods 0.000 description 8
- 230000037431 insertion Effects 0.000 description 8
- 230000035939 shock Effects 0.000 description 5
- 230000000694 effects Effects 0.000 description 3
- 238000012856 packing Methods 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000004146 energy storage Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model discloses a high-stability power box structure of a civil aircraft display controller, which comprises an installation panel, an installation component, a fixing frame, an installation clamping groove, a connecting slot, a first screw hole, a fastening screw rod, a protective component, a box body, a supporting frame, damping cotton, a vent hole, a storage battery, a wiring board, an operation indicator lamp and a socket, wherein the installation component is arranged on both sides of the installation panel, the fixing frame is arranged on both sides of the back of the installation panel through screws, the protective component is arranged at one end of the fixing frame, the protective component comprises a protective bottom plate, an anti-collision pad, a connecting plug block and a second screw hole, the periphery of one surface of the protective bottom plate is fixedly provided with the connecting plug block through screws, the connecting plug block is inserted and installed inside the connecting slot, the second screw hole is arranged on the connecting plug block, and the high-stability power box, when being installed, the fixing is firm, the installation is convenient, and the structure stability is good.
Description
Technical Field
The utility model relates to a power supply box equipment field specifically is a high stability power supply box structure of civil aircraft display controller.
Background
The power box is mainly used for providing an operating power supply for the vacuum circuit breaker and other high-voltage switches; when the civil aircraft display controller works, the power box can be used; the power box in the prior art is inconvenient to mount when being mounted, has poor stability of the whole structure and is not fastened in connection, so that when the power box is vibrated, parts inside the power box are easily damaged, and the normal work of the power box is influenced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a civil aircraft display controller's high stability power supply box structure to solve the problem that proposes among the above-mentioned background art.
The purpose of the utility model can be realized by the following technical scheme:
a high-stability power box structure of a civil aircraft display controller comprises a mounting panel, a mounting assembly, a fixing frame, a mounting clamping groove, a connecting slot, a first screw hole, a fastening screw rod, a protective assembly, a box body, a supporting frame, damping cotton, a ventilation hole, a storage battery, a wiring board, an operation indicator lamp and a socket, wherein the mounting assembly is arranged on each side of the mounting panel, the fixing frame is mounted on each side of the back of the mounting panel through screws, the connecting slot is formed in the bottom and the top of the back of the fixing frame, the box body is arranged between the two fixing frames, the protective assembly is arranged at one end of the fixing frame and comprises a protective bottom plate, an anti-collision pad, a connecting plug-in block and a second screw hole, the periphery of one surface of the protective bottom plate is fixedly provided with the connecting plug-in block through screws, the connecting plug block is provided with a second screw hole, one end of the top and the bottom of the fixing frame is provided with a first screw hole, the first screw hole corresponds to the second screw hole in position, the fastening screw is sequentially in threaded connection with the first screw hole and the second screw hole, the center of one surface of the protective bottom plate is provided with an anti-collision pad through screws, and the top of the box body is provided with a ventilation hole.
As a further aspect of the present invention: the mounting assembly comprises a connecting plate and mounting positioning holes, the connecting plate is fixedly mounted on one side of the mounting panel through screws, and the mounting positioning holes are formed in the top and the bottom of the surface of the connecting plate.
As a further aspect of the present invention: the mounting clamping groove is formed in one side of the inside of the fixing frame, and the two sides of the box body are installed in the mounting clamping groove in an inserted mode.
As a further aspect of the present invention: the anti-collision pad is attached to the box body.
As a further aspect of the present invention: the utility model discloses a solar energy storage battery, including mounting panel, wiring board, mounting panel, socket, support frame, shock attenuation cotton, the inside of box has the support frame through the mounting screw, there is the wiring board front end one side of mounting panel through the mounting screw, the socket is installed through the mounting screw to the front end opposite side of mounting panel, and the outside of socket is provided with the operation pilot lamp, the inside of box has the support frame through the mounting screw, and the bottom packing of support frame has the shock attenuation cotton, the inside of box is provided with the battery, the battery passes through the top.
The utility model has the advantages that: this civil aircraft display controller's high stability power supply box structure, small in size, moreover, the steam generator is simple in structure, when the installation, install between installation panel and mount through pegging graft the box, rethread protection component fixes the box spacing, make the fixed effect of box firm, can not take place to drop, and simultaneously, when taking place vibrations, because box overall structure is stable, and, the cotton and the anticollision strip of protection bottom plate one side of shock attenuation through the support frame bottom can effectively absorb vibrations and impact, thereby have good protection effect to the box, the security of using has been improved.
Drawings
In order to facilitate understanding for those skilled in the art, the present invention will be further described with reference to the accompanying drawings.
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of a partial structure of the present invention;
fig. 3 is a sectional view of the fixing frame of the present invention;
FIG. 4 is a cross-sectional view of the case of the present invention;
in the figure: 1. installing a panel; 2. mounting the component; 3. a connecting plate; 4. installing a positioning hole; 5. a fixed mount; 6. installing a clamping groove; 7. connecting the slots; 8. a first screw hole; 9. fastening a screw rod; 10. a guard assembly; 11. a protective base plate; 12. an anti-collision pad; 13. connecting the plug blocks; 14. a second screw hole; 15. a box body; 16. a support frame; 17. damping cotton; 18. a vent hole; 19. a storage battery; 20. a wiring board; 21. an operation indicator light; 22. a socket is provided.
Detailed Description
The technical solution of the present invention will be described clearly and completely with reference to the following embodiments, and it should be understood that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
As shown in fig. 1-4, a high-stability power box structure of a civil aircraft display controller comprises an installation panel 1, an installation component 2, a fixing frame 5, an installation clamping groove 6, a connecting slot 7, a first screw hole 8, a fastening screw 9, a protection component 10, a box body 15, a supporting frame 16, damping cotton 17, a vent hole 18, a storage battery 19, a wiring board 20, an operation indicator lamp 21 and a socket 22, wherein the installation component 2 is arranged on both sides of the installation panel 1, the installation component 2 comprises a connecting plate 3 and an installation positioning hole 4, the connecting plate 3 is fixedly installed on one side of the installation panel 1 through a screw, and the installation positioning holes 4 are formed in the top and the bottom of the surface of the connecting plate 3, so that; fixing frames 5 are installed on two sides of the back of the installation panel 1 through screws, connecting slots 7 are formed in the bottom and the top of the back of each fixing frame 5, a box body 15 is arranged between the two fixing frames 5, an installation clamping groove 6 is formed in one side of the inside of each fixing frame 5, and two sides of each box body 15 are installed in the installation clamping grooves 6 in an inserted mode, so that the box body 15 can be installed conveniently; one end of the fixing frame 5 is provided with a protection assembly 10, the protection assembly 10 comprises a protection bottom plate 11, an anti-collision pad 12, a connecting insert block 13 and a second screw hole 14, the periphery of one surface of the protection bottom plate 11 is fixedly provided with the connecting insert block 13 through screws, the connecting insert block 13 is inserted and installed inside the connecting slot 7, the connecting insert block 13 is provided with the second screw hole 14, one ends of the top and the bottom of the fixing frame 5 are provided with first screw holes 8, each first screw hole 8 corresponds to one second screw hole 14 in position, and a fastening screw 9 is sequentially in threaded connection with the first screw holes 8 and the second screw holes 14, so that the fastening screw 9 is conveniently fixed with the first screw holes 8 and the second screw holes 14; the center of one surface of the protective bottom plate 11 is provided with an anti-collision pad 12 through a screw, and the anti-collision pad 12 is attached and connected with the box body 15, so that the anti-collision effect is improved; the top of the box body 15 is provided with a vent hole 18; there is wiring board 20 front end one side of installation panel 1 through the mounting screw, there is socket 22 front end opposite side of installation panel 1 through the mounting screw, and socket 22's outside is provided with operation pilot lamp 21, there is support frame 16 inside of box 15 through the mounting screw, and the bottom packing of support frame 16 has shock attenuation cotton 17, the inside of box 15 is provided with battery 19, battery 19 passes through the mounting screw at the top of support frame 16, battery 19 passes through wire and wiring board 20, operation pilot lamp 21 and socket 22 electricity are even, be convenient for battery 19 normal work.
The utility model discloses a theory of operation: when the anti-collision device is used, two ends of the box body 15 are respectively placed in the installation clamping grooves 6 of the fixing frame 5, the box body 15 is pushed to enable the box body 15 to slide between the fixing frame 5, after the box body 15 is contacted with the installation panel 1, the position of the box body 15 is fixed by using the protection component 10, after the connection insertion blocks 13 on the periphery of the protection bottom plate 11 are aligned with the connection insertion grooves 7 of the fixing frame 5, the connection insertion blocks 13 are inserted into the connection insertion grooves 7, the anti-collision pads 12 are attached and connected with the side walls of the box body 15, after the connection insertion blocks 13 are inserted into the connection insertion grooves 7, the first screw holes 8 are aligned with the second screw holes 14, the fastening screws 9 are inserted into the first screw holes 8 and the second screw holes 14, so that the connection insertion blocks 13 are fixed inside the connection insertion grooves 7, after the box body 15 is fixed, the installation panel 1 is fixed by using the installation component 2, the screws penetrate through, the connection plate 3 is fixed, the mounting panel 1 can be fixed, and the wiring is performed through the wiring board 20, so that the power can be supplied through the storage battery 19; the running state can be observed through the running indicator lamp 21, and the power connection operation can be carried out through the socket 22; when vibration occurs, the box body 15 is arranged between the fixed frame 5 and the installation panel 1 and is fixed through the protection assembly 10, so that the structural stability is good, and meanwhile, the shock absorption cotton 17 at the bottom of the support frame 16 and the anti-collision strip on one side of the box body 15 can absorb part of impact, so that the vibration is reduced; the ventilation holes 18 can facilitate ventilation and heat dissipation inside the case 15.
The preferred embodiments of the present invention disclosed above are intended only to help illustrate the present invention. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and its practical applications, to thereby enable others skilled in the art to best understand the invention for and utilize the invention. The present invention is limited only by the claims and their full scope and equivalents.
Claims (5)
1. A high-stability power box structure of a civil aircraft display controller is characterized by comprising a mounting panel (1), mounting assemblies (2), fixing frames (5), mounting clamping grooves (6), connecting slots (7), first screw holes (8), fastening screws (9), protective assemblies (10), a box body (15), a supporting frame (16), damping cotton (17), ventilation holes (18), a storage battery (19), a wiring board (20), an operation indicator lamp (21) and a socket (22), wherein the mounting assemblies (2) are arranged on two sides of the mounting panel (1), the fixing frames (5) are mounted on two sides of the back of the mounting panel (1) through screws, the connecting slots (7) are formed in the bottom and the top of the back of each fixing frame (5), the box body (15) is arranged between the two fixing frames (5), the protective assemblies (10) are arranged at one end of each fixing frame (5), protection component (10) are including protection bottom plate (11), crashproof pad (12), connect inserted block (13) and second screw (14), all there is connection inserted block (13) one side of protection bottom plate (11) all around through screw fixed mounting, and connects inserted block (13) grafting and install the inside in connection slot (7), second screw (14) have been seted up on connecting inserted block (13), first screw (8) have been seted up to the top of mount (5) and bottom one end, and every first screw (8) are corresponding with a second screw (14) position, fastening screw (9) in proper order with first screw (8) and second screw (14) threaded connection, there is crashproof pad (12) through the screw installation in the one side central authorities of protection bottom plate (11), ventilation hole (18) have been seted up at the top of box (15).
2. The high-stability power box structure of the civil aircraft display controller according to claim 1, wherein the mounting assembly (2) comprises a connecting plate (3) and mounting positioning holes (4), the connecting plate (3) is fixedly mounted on one side of the mounting panel (1) through screws, and the mounting positioning holes (4) are formed in the top and the bottom of the surface of the connecting plate (3).
3. The high-stability power box structure of the civil aircraft display controller according to claim 1, wherein a mounting slot (6) is formed in one side of the inside of the fixing frame (5), and two sides of the box body (15) are inserted and mounted in the mounting slot (6).
4. The civil aircraft display controller high-stability power box structure as claimed in claim 1, wherein the crash pad (12) is attached to the box body (15).
5. The high-stability power box structure of the civil aircraft display controller according to claim 1, wherein a wiring board (20) is installed on one side of the front end of the installation panel (1) through screws, a socket (22) is installed on the other side of the front end of the installation panel (1) through screws, an operation indicator lamp (21) is arranged outside the socket (22), a support frame (16) is installed inside the box body (15) through screws, damping cotton (17) is filled at the bottom of the support frame (16), a storage battery (19) is arranged inside the box body (15), the storage battery (19) is installed at the top of the support frame (16) through screws, and the storage battery (19) is electrically connected with the wiring board (20), the operation indicator lamp (21) and the socket (22) through wires.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921244152.0U CN210111836U (en) | 2019-08-02 | 2019-08-02 | High stability power supply box structure of civil aircraft display controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921244152.0U CN210111836U (en) | 2019-08-02 | 2019-08-02 | High stability power supply box structure of civil aircraft display controller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210111836U true CN210111836U (en) | 2020-02-21 |
Family
ID=69567622
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921244152.0U Expired - Fee Related CN210111836U (en) | 2019-08-02 | 2019-08-02 | High stability power supply box structure of civil aircraft display controller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210111836U (en) |
-
2019
- 2019-08-02 CN CN201921244152.0U patent/CN210111836U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200221 |