CN220606149U - Flight control board heat abstractor - Google Patents
Flight control board heat abstractor Download PDFInfo
- Publication number
- CN220606149U CN220606149U CN202322105056.0U CN202322105056U CN220606149U CN 220606149 U CN220606149 U CN 220606149U CN 202322105056 U CN202322105056 U CN 202322105056U CN 220606149 U CN220606149 U CN 220606149U
- Authority
- CN
- China
- Prior art keywords
- control board
- heat dissipation
- flight control
- wall
- plate
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title claims abstract description 28
- 230000007246 mechanism Effects 0.000 claims abstract description 21
- 238000009434 installation Methods 0.000 claims abstract description 14
- 241000883990 Flabellum Species 0.000 claims description 5
- 239000007787 solid Substances 0.000 claims description 3
- 238000001816 cooling Methods 0.000 claims 2
- 230000017525 heat dissipation Effects 0.000 abstract description 32
- 230000000694 effects Effects 0.000 abstract description 8
- 238000000034 method Methods 0.000 abstract description 6
- 230000008569 process Effects 0.000 abstract description 4
- 230000002035 prolonged effect Effects 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 4
- 238000010304 firing Methods 0.000 description 3
- 238000009792 diffusion process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Abstract
The utility model provides a flight control board heat dissipation device, which relates to the technical field of flight control board heat dissipation devices and comprises: the heat dissipation mechanism comprises a control board, a mounting mechanism is arranged at the bottom of the control board, a plurality of fixing rings are arranged on the inner wall of the control board, and a top plate is arranged at the top of the control board. According to the utility model, the heat dissipation area of the aircraft can be increased through the installed heat dissipation mechanism, the heat dissipation effect is improved, so that the normal operation of the flight control board is ensured, the service life is prolonged, the stability of the aircraft can be improved, the aircraft can keep stable temperature in the flight process through controlling the rotation speed of the fan blades, the flight stability of the aircraft is further improved, the direct installation of heat dissipation equipment on the control board can be avoided, air cannot be diffused to the whole control board, the heat dissipation effect of the control board far away from the heat dissipation equipment is reduced, the control board is damaged for a long time, a user is required to maintain, and the use of the user is affected.
Description
Technical Field
The utility model relates to the technical field of flight control board heat dissipation devices, in particular to a flight control board heat dissipation device.
Background
The existing flight control board heat dissipation device is generally provided with a heat dissipation fan at the position close to the flight control board, and the heat dissipation fan is driven to rotate by a small motor and the like, so that the heat dissipation fan transmits external air into the surface of the flight control board, and the heat dissipation effect is achieved by continuously transmitting air to the surface of the flight control board. But install the radiator fan on flight control board surface, the too near air diffusion that can't transmit to the control panel is whole, makes the control panel that keeps away from firing equipment reduce radiating effect, uses the control panel damage for a long time, needs the user to maintain, influences user's use.
Disclosure of Invention
The utility model aims to solve the defects in the prior art and provides a flight control board heat dissipation device.
In order to achieve the above purpose, the present utility model adopts the following technical scheme: a flight control board heat sink comprising: the heat dissipation mechanism comprises a control plate, the control plate bottom is provided with installation mechanism, the control plate inner wall is provided with a plurality of solid fixed rings, the control plate top is provided with the roof, the thread groove inner wall that the roof was seted up is provided with the mounting, the draw-in groove inner wall that the roof was seted up is provided with the dead lever, the dead lever surface is provided with in-wheel motor, in-wheel motor surface is provided with the flabellum, the roof top is provided with the mount, the mount top is provided with the guard plate.
As a preferred implementation mode, the mounting mechanism comprises a mounting plate, wherein one side of the top of the mounting plate is fixedly connected with one side of the bottom of the control plate, a plurality of mounting holes are formed in the mounting plate, and the inner walls of the mounting holes are rotationally connected with the outer surfaces of the fasteners.
As a preferred implementation mode, the outer surface of the fixing ring is fixedly connected with the inner wall of the control panel, the outer surface of the fixing piece is in threaded connection with a threaded groove formed in the fixing piece, the outer surface of the fixing piece is in threaded connection with the inner wall of the fixing ring, and the top plate is fixedly connected with the control panel through the fixing piece and the fixing ring.
As a preferable implementation mode, one end of the fixing rod is fixedly connected with the inner wall of the clamping groove formed in the top of the top plate.
As a preferred implementation mode, the inner wall of the hub motor is rotationally connected with the outer surface of the fixing rod, and the outer surface of the hub motor is fixedly connected with one side of the fan blade.
As a preferred embodiment, one side of the fixing frame is fixedly connected with one side of the top plate. As a preferred implementation mode, compared with the prior art, the fixed connection between one side of the protection plate and one side of the top of the fixing frame has the advantages and positive effects that:
according to the utility model, the heat dissipation area of the aircraft can be increased through the installed heat dissipation mechanism, the heat dissipation effect is improved, so that the normal operation of the flight control board is ensured, the service life is prolonged, the stability of the aircraft can be improved, the aircraft can keep stable temperature in the flight process through controlling the rotation speed of the fan blades, the flight stability of the aircraft is further improved, the direct installation of heat dissipation equipment on the control board can be avoided, air cannot be diffused to the whole control board, the heat dissipation effect of the control board far away from the heat dissipation equipment is reduced, the control board is damaged for a long time, a user is required to maintain, and the use of the user is affected. The installation mechanism through the installation can effectively utilize the space to guarantee the normal operating of system, when staff installs, only need rotate out the mounting hole with the fastener, rethread rotates fastener and wholly carries out threaded connection, just can install and accomplish, can more convenient to use person installs and dismantles.
Drawings
Fig. 1 is a schematic structural diagram of a heat dissipating device of a flight control board according to the present utility model.
Fig. 2 is a schematic structural diagram of a disassembled side view of a heat dissipation mechanism of a heat dissipation device of a flight control board according to the present utility model.
Fig. 3 is a schematic structural diagram of a side of a partially disassembled view of a heat dissipation mechanism of a heat dissipation device of a flight control board according to the present utility model.
Fig. 4 is a schematic structural diagram of a side surface of a mounting mechanism of a heat dissipation device of a flight control board according to the present utility model.
Legend description:
1. a heat dissipation mechanism; 11. a control board; 12. a fixing ring; 13. a top plate; 14. a fixing member; 15. a fixed rod; 16. a hub motor; 17. a fan blade; 18. a fixing frame; 19. a protection plate;
2. a mounting mechanism; 21. a mounting plate; 22. a mounting hole; 23. a fastener.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Example 1
As shown in fig. 1-3, the present utility model provides a technical solution: a flight control board heat sink comprising: the heat dissipation mechanism 1, heat dissipation mechanism 1 includes control panel 11, control panel 11 bottom is provided with installation mechanism 2, control panel 11 inner wall is provided with a plurality of solid fixed rings 12, the control panel 11 top is provided with roof 13, the screw groove inner wall that roof 13 offered is provided with mounting 14, the draw-in groove inner wall that roof 13 offered is provided with dead lever 15, the dead lever 15 surface is provided with in-wheel motor 16, in-wheel motor 16 surface is provided with flabellum 17, roof 13 top is provided with mount 18, the mount 18 top is provided with guard plate 19.
In this embodiment, the outer surface of the fixing member 14 is fixedly connected with the inner wall of the control board 11 through the outer surface of the fixing ring 12, the outer surface of the fixing member 14 is in threaded connection with a threaded groove formed in the fixing member 14, the outer surface of the fixing member 14 is in threaded connection with the inner wall of the fixing ring 12, and the top plate 13 is fixedly connected with the control board 11 through the fixing member 14 and the fixing ring 12; not only can improve its security, avoid the trouble or the accident that lead to because roof 13 is not hard up in the flight in-process, if control panel 11 need maintain or change, the staff only need use the instrument to disassemble mounting 14, just can make roof 13 and control panel 11 separate, dismantles simple more the staff of being convenient for and dismantle inspection or maintenance. One end of the fixed rod 15 is fixedly connected with the inner wall of a clamping groove formed in the top of the top plate 13, the inner wall of the hub motor 16 is rotationally connected with the outer surface of the fixed rod 15, and the outer surface of the hub motor 16 is fixedly connected with one side of the fan blade 17; the roof 13 installation in-wheel motor 16 drive flabellum 17 can increase its radiating area, the radiating effect is improved, thereby guarantee the normal operating and the increase of service life of flight control board, still can improve the stability of aircraft, through control flabellum 17 rotational speed, can make the aircraft keep stable temperature in the flight in-process, further improve the flight stability of aircraft, can avoid direct installation firing equipment on control panel 11, make the unable diffusion of air to control panel 11 whole, make the control panel 11 that keeps away from firing equipment reduce radiating effect, make control panel 11 damage for a long time, the user is required to maintain, influence user's use. One side of the protection plate 19 is fixedly connected with one side of the top of the fixing frame 18 through the fixing frame 18 fixedly connected with one side of the top plate 13; not only can the fan blades 17, the hub motor 16 and the like be protected from collision and damage of external objects, but also faults and accidents caused by external factors in the flying process can be avoided, and the safety of the system is improved.
Example 2
As shown in fig. 1-4, the mounting mechanism 2 comprises a mounting plate 21, wherein one side of the top of the mounting plate 21 is fixedly connected with one side of the bottom of the control plate 11, the mounting plate 21 is provided with a plurality of mounting holes 22, and the inner walls of the mounting holes 22 are rotatably connected with the outer surfaces of the fasteners 23.
In the embodiment, through the fixed connection of the top side of the mounting plate 21 and the bottom side of the control plate 11, the mounting plate 21 is provided with a plurality of mounting holes 22, and the inner walls of the mounting holes 22 are rotationally connected with the outer surfaces of the fasteners 23; the control panel 11 can be tightly combined with the integral installation, so that the stability of the system is improved, the space can be effectively utilized, the normal operation of the system is ensured, when the installation is performed by a worker, the fastener 23 is only required to be rotated out of the installation hole 22, the fastener 23 is rotated to be in threaded connection with the integral body, the installation is completed, and the installation and the disassembly of the system can be more convenient for the user.
Working principle:
as shown in fig. 1-4, when a worker uses the device, firstly, the fixing piece 14 can be used for fixing the top plate 13 and the control plate 11, after the fixing is finished, the safety of the device can be improved, faults or accidents caused by loosening of the top plate 13 in the flying process are avoided, if the control plate 11 needs to be maintained or replaced, the worker only needs to disassemble the fixing piece 14 by using a tool, the top plate 13 and the control plate 11 can be separated, the disassembly is simple, the worker can disassemble and inspect or maintain the device more conveniently, when the device is used, the worker can drive the fan blades 17 to dissipate heat of the whole control plate 11 by starting the hub motor 16, the stability of the aircraft can be improved, and the flying stability of the aircraft can be further improved by controlling the rotating speed of the fan blades 17.
The present utility model is not limited to the above-mentioned embodiments, and any equivalent embodiments which can be changed or modified by the technical content disclosed above can be applied to other fields, but any simple modification, equivalent changes and modification made to the above-mentioned embodiments according to the technical substance of the present utility model without departing from the technical content of the present utility model still belong to the protection scope of the technical solution of the present utility model.
Claims (7)
1. A flight control board heat sink, comprising: the utility model provides a cooling mechanism (1), cooling mechanism (1) includes control panel (11), control panel (11) bottom is provided with installation mechanism (2), control panel (11) inner wall is provided with a plurality of solid fixed ring (12), control panel (11) top is provided with roof (13), the screw groove inner wall that roof (13) were seted up is provided with mounting (14), the draw-in groove inner wall that roof (13) were seted up is provided with dead lever (15), dead lever (15) surface is provided with in-wheel motor (16), in-wheel motor (16) surface is provided with flabellum (17), roof (13) top is provided with mount (18), mount (18) top is provided with guard plate (19).
2. The flight control board heat sink as claimed in claim 1, wherein: the mounting mechanism (2) comprises a mounting plate (21), one side of the top of the mounting plate (21) is fixedly connected with one side of the bottom of the control plate (11), a plurality of mounting holes (22) are formed in the mounting plate (21), and the inner walls of the mounting holes (22) are rotationally connected with the outer surfaces of the fasteners (23).
3. The flight control board heat sink as claimed in claim 2, wherein: the outer surface of the fixed ring (12) is fixedly connected with the inner wall of the control board (11), the outer surface of the fixed piece (14) is in threaded connection with a threaded groove formed in the fixed piece (14), the outer surface of the fixed piece (14) is in threaded connection with the inner wall of the fixed ring (12), and the top plate (13) is fixedly connected with the control board (11) through the fixed piece (14) and the fixed ring (12).
4. The flight control board heat sink as claimed in claim 1, wherein: one end of the fixing rod (15) is fixedly connected with the inner wall of a clamping groove formed in the top of the top plate (13).
5. The flight control board heat sink as claimed in claim 1, wherein: the inner wall of the hub motor (16) is rotationally connected with the outer surface of the fixed rod (15), and the outer surface of the hub motor (16) is fixedly connected with one side of the fan blade (17).
6. The flight control board heat sink as claimed in claim 1, wherein: one side of the fixing frame (18) is fixedly connected with one side of the top plate (13).
7. The flight control board heat sink as claimed in claim 1, wherein: one side of the protection plate (19) is fixedly connected with one side of the top of the fixing frame (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322105056.0U CN220606149U (en) | 2023-08-07 | 2023-08-07 | Flight control board heat abstractor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322105056.0U CN220606149U (en) | 2023-08-07 | 2023-08-07 | Flight control board heat abstractor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220606149U true CN220606149U (en) | 2024-03-15 |
Family
ID=90181867
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322105056.0U Active CN220606149U (en) | 2023-08-07 | 2023-08-07 | Flight control board heat abstractor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220606149U (en) |
-
2023
- 2023-08-07 CN CN202322105056.0U patent/CN220606149U/en active Active
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