CN207652188U - A kind of unmanned plane motor waterproof heat-dissipation shell - Google Patents
A kind of unmanned plane motor waterproof heat-dissipation shell Download PDFInfo
- Publication number
- CN207652188U CN207652188U CN201721750581.6U CN201721750581U CN207652188U CN 207652188 U CN207652188 U CN 207652188U CN 201721750581 U CN201721750581 U CN 201721750581U CN 207652188 U CN207652188 U CN 207652188U
- Authority
- CN
- China
- Prior art keywords
- shell
- unmanned plane
- end cover
- motor waterproof
- plane motor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 230000017525 heat dissipation Effects 0.000 title claims abstract description 23
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 23
- 238000007789 sealing Methods 0.000 claims abstract description 19
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 18
- 239000007787 solid Substances 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 4
- 239000000498 cooling water Substances 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
Landscapes
- Motor Or Generator Frames (AREA)
Abstract
The utility model discloses a kind of unmanned plane motor waterproof heat-dissipation shells, including shell, the bottom of the shell is equipped with pedestal, the left and right ends of the shell have been respectively fixedly connected with first end cover and second end cover by bolt, the junction of the first end cover and shell is equipped with the first sealing ring, the junction of the second end cover and shell is equipped with the second sealing ring, the shell is internally provided with cycle water layer, the water inlet pipe and outlet pipe for being communicated in cycle water layer are respectively equipped on the left and right sides wall of the shell, radiating fin is uniformly equipped on the side wall of the shell, the section of the radiating fin is in strip.By being internally provided with cycle water layer in shell, the heat in shell is taken away using recirculated cooling water, to reduce enclosure interior temperature, in addition, by the radiating fin for being uniformly equipped with strip on the side wall of shell, the radiating efficiency for improving shell, to reach the heat dissipation effect for ensureing shell in the case where realizing sealing.
Description
Technical field
The utility model is related to air vehicle technique field, specially a kind of unmanned plane motor waterproof heat-dissipation shell.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates.It can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..Unmanned plane presses application field, can be divided into
It is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application are unmanned planes
Really just need；It taking photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring at present
The application in infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, is greatly expanded
The purposes of unmanned plane itself, developed country is also in actively extension sector application and development unmanned air vehicle technique.
With the development of science and technology, unmanned plane field is also rapidly progressed, motor has during unmanned plane use
Very important status, traditional unmanned plane motor waterproof cooling poor performance have certain limitation.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane motor waterproof heat-dissipation shells, to solve above-mentioned background technology
The problem of middle proposition.
To achieve the above object, the utility model provides the following technical solutions：A kind of unmanned plane motor waterproof heat-dissipation shell,
Including shell, the bottom of the shell is equipped with pedestal, and the left and right ends of the shell have been respectively fixedly connected with first by bolt
The junction of end cap and second end cover, the first end cover and shell is equipped with the first sealing ring, the second end cover and shell
Junction is equipped with the second sealing ring, and the shell is internally provided with cycle water layer, is set respectively on the left and right sides wall of the shell
There are the water inlet pipe and outlet pipe for being communicated in cycle water layer, radiating fin, the heat dissipation are uniformly equipped on the side wall of the shell
The section of fin is in strip.
Preferably, the bottom of the pedestal offers location hole, and set square is arranged at left and right sides of the pedestal.
Preferably, the junction of the pedestal and shell is equipped with groove, and the groove is in arc-shaped, the pedestal and shell
Between be welded and fixed.
Preferably, the thickness of the cycle water layer is no more than the half of housing sidewall integral thickness.
Preferably, the end of the water inlet pipe and outlet pipe is respectively connected with flange, and annular spread has bolt on the flange
Hole.
Preferably, hanging ring is connected at the top of the shell, the hanging ring is arranged two groups, and the hanging ring is threadedly connected to shell
Body.
Compared with prior art, the utility model has the beneficial effects that：A kind of unmanned plane motor waterproof of the utility model dissipates
Hot shell, structure novel, by being equipped with the first sealing ring in the junction of first end cover and shell, and in second end cover and shell
Junction be equipped with the second sealing ring, ensure the sealing performance of shell, by being internally provided with cycle water layer in shell, using following
Ring cooling water takes away the heat in shell, to reduce enclosure interior temperature, in addition, by uniform on the side wall of shell
Radiating fin equipped with strip improves the radiating efficiency of shell, ensures shell in the case where realizing sealing to reach
Heat dissipation effect, which has a compact structure and a reasonable design have very high practicability, and it is scattered to greatly improve a kind of unmanned plane motor waterproof
Using for hot shell is functional, ensures its using effect and utilization benefit, is suitble to be widely popularized.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of unmanned plane motor waterproof heat-dissipation shell of the utility model；
Fig. 2 is a kind of A-A schematic cross-sectional views of unmanned plane motor waterproof heat-dissipation shell of the utility model；
Fig. 3 is a kind of schematic diagram of base structure of unmanned plane motor waterproof heat-dissipation shell of the utility model；
Fig. 4 is a kind of flange arrangement schematic diagram of unmanned plane motor waterproof heat-dissipation shell of the utility model.
In figure：1 shell, 2 pedestals, 3 grooves, 4 set squares, 5 cycle water layers, 6 water inlet pipes, 7 outlet pipes, 8 first end covers, 9
Second end cover, 10 first sealing rings, 11 second sealing rings, 12 bolts, 13 radiating fins, 14 hanging rings, 15 flanges.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
- 3 are please referred to Fig.1, the utility model provides a kind of technical solution：A kind of unmanned plane motor waterproof heat-dissipation shell, packet
Shell 1 is included, the bottom of the shell 1 is equipped with pedestal 2, and the left and right ends of the shell 1 have been respectively fixedly connected with by bolt 12
The junction of first end cover 8 and second end cover 9, the first end cover 8 and shell 1 is equipped with the first sealing ring 10, the second end
The junction of lid 9 and shell 1 is equipped with the second sealing ring 11, and the shell 1 is internally provided with cycle water layer 5, a left side for the shell 1
It is respectively equipped with the water inlet pipe 6 and outlet pipe 7 for being communicated in cycle water layer 5 on right two side, is uniformly set on the side wall of the shell 1
There is radiating fin 13, the section of the radiating fin 13 is in strip, and the bottom of the pedestal 2 offers location hole, the bottom
The left and right sides of seat 2 is arranged with set square 4, and the junction of the pedestal 2 and shell 1 is equipped with groove 3, and the groove 3 is in circle
Arcuation is welded and fixed between the pedestal 2 and shell 1, and the thickness of the cycle water layer 5 is no more than 1 side wall integral thickness of shell
Half, the end of the water inlet pipe 6 and outlet pipe 7 is respectively connected with flange 15, and annular spread has spiral shell on the flange 15
The top of keyhole, the shell 1 is connected with hanging ring 14, and the hanging ring 14 is arranged two groups, and the hanging ring 14 is threadedly connected to shell
1。
Operation principle：A kind of unmanned plane motor waterproof heat-dissipation shell of the utility model, in use, by first end cover 8
It is equipped with the first sealing ring 10 with the junction of shell 1, and the second sealing ring 11 is equipped in the junction of second end cover 9 and shell 1,
The sealing performance for ensureing shell 1 will be in shell 1 using recirculated cooling water by being internally provided with cycle water layer 5 in shell 1
Heat is taken away, to reduce by 1 internal temperature of shell, in addition, the heat dissipation by being uniformly equipped with strip on the side wall of shell 1
Fin 13 improves the radiating efficiency of shell 1, to reach the heat dissipation effect for ensureing shell 1 in the case where realizing sealing, structure
Compact, reasonable design has very high practicability.
In the present invention unless specifically defined or limited otherwise, term " installation ", " connected ", " connection ", " Gu
It is fixed " etc. terms shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
Can also be electrical connection to be mechanical connection；It can be directly connected, can also indirectly connected through an intermediary, Ke Yishi
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood as the case may be
Concrete meaning in the present invention.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of unmanned plane motor waterproof heat-dissipation shell, including shell (1), it is characterised in that：The bottom of the shell (1) is equipped with
The left and right ends of pedestal (2), the shell (1) have been respectively fixedly connected with first end cover (8) and second end cover by bolt (12)
(9), the junction of the first end cover (8) and shell (1) is equipped with the first sealing ring (10), the second end cover (9) and shell
(1) junction is equipped with the second sealing ring (11), and the shell (1) is internally provided with cycle water layer (5), the shell (1)
The water inlet pipe (6) and outlet pipe (7) for being communicated in cycle water layer (5), the side wall of the shell (1) are respectively equipped on the wall of the left and right sides
Upper to be uniformly equipped with radiating fin (13), the section of the radiating fin (13) is in strip.
2. a kind of unmanned plane motor waterproof heat-dissipation shell according to claim 1, it is characterised in that：The pedestal (2)
Bottom offers location hole, and set square (4) is arranged at left and right sides of the pedestal (2).
3. a kind of unmanned plane motor waterproof heat-dissipation shell according to claim 1, it is characterised in that：The pedestal (2) and
The junction of shell (1) is equipped with groove (3), and the groove (3) is in arc-shaped, is welded between the pedestal (2) and shell (1) solid
It is fixed.
4. a kind of unmanned plane motor waterproof heat-dissipation shell according to claim 1, it is characterised in that：The cycle water layer
(5) thickness is no more than the half of shell (1) side wall integral thickness.
5. a kind of unmanned plane motor waterproof heat-dissipation shell according to claim 1, it is characterised in that：The water inlet pipe (6)
It is respectively connected with flange (15) with the end of outlet pipe (7), annular spread has bolt hole on the flange (15).
6. a kind of unmanned plane motor waterproof heat-dissipation shell according to claim 1, it is characterised in that：The shell (1)
Top is connected with hanging ring (14), and the hanging ring (14) is arranged two groups, and the hanging ring (14) is threadedly connected to shell (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721750581.6U CN207652188U (en) | 2017-12-15 | 2017-12-15 | A kind of unmanned plane motor waterproof heat-dissipation shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721750581.6U CN207652188U (en) | 2017-12-15 | 2017-12-15 | A kind of unmanned plane motor waterproof heat-dissipation shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207652188U true CN207652188U (en) | 2018-07-24 |
Family
ID=62880800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721750581.6U Expired - Fee Related CN207652188U (en) | 2017-12-15 | 2017-12-15 | A kind of unmanned plane motor waterproof heat-dissipation shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207652188U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110920911A (en) * | 2019-12-10 | 2020-03-27 | 之江实验室 | High-efficient heat dissipation aircraft motor cabinet with self-loopa liquid cooling structure |
-
2017
- 2017-12-15 CN CN201721750581.6U patent/CN207652188U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110920911A (en) * | 2019-12-10 | 2020-03-27 | 之江实验室 | High-efficient heat dissipation aircraft motor cabinet with self-loopa liquid cooling structure |
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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: 20180724 Termination date: 20181215 |