CN104883863A - Copper pipe heat radiation device of unmanned plane - Google Patents
Copper pipe heat radiation device of unmanned plane Download PDFInfo
- Publication number
- CN104883863A CN104883863A CN201510356106.XA CN201510356106A CN104883863A CN 104883863 A CN104883863 A CN 104883863A CN 201510356106 A CN201510356106 A CN 201510356106A CN 104883863 A CN104883863 A CN 104883863A
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- China
- Prior art keywords
- copper pipe
- unmanned plane
- heat
- conducting copper
- heat radiation
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Abstract
The invention discloses a copper pipe heat radiation device of an unmanned plane. The copper pipe heat radiation device of the unmanned plane comprises a heat conduction copper pipe. One end of the heat conduction copper pipe is in contact with a heating module of the unmanned plane. A main body part of the heat conduction copper pipe extends to an air outlet side below a power propeller of the unmanned plane. The end, in contact with the heating module, of the heat conduction copper pipe is of a flat sheet structure. According to the invention, the heat conduction efficiency of the heat conduction copper pipe is high, so that the layout of the whole structure is easy, and no additional heat radiation fans are needed; in addition, the heat radiation performance is improved, the assembling difficulty is lowered, and the weight is reduced.
Description
Technical field
The present invention relates to unmanned plane heat abstractor technical field, be specifically related to a kind of unmanned plane copper pipe heat abstractor.
Background technology
Inside unmanned plane of the prior art, main heating module is calculate the module concentrated, control module like flying, vision processing module, high definition transport module etc., and in these modules, components and parts and sensor for temperature are very responsive; Existing product on the market, dispel the heat facing to forms such as components and parts blowing, aluminum alloy heat sinks mainly through fan, its radiating effect is bad, also increases flight simultaneously and bears a heavy burden, in addition for hardware designs increases burden.
Summary of the invention
For above-mentioned defect, the invention discloses a kind of unmanned plane copper pipe heat abstractor, the heat transfer efficiency of copper pipe is high, total layout can be made easy, do not need to configure radiator fan in addition, simultaneously heat radiation performance, can reduce assembling difficulty and weight reduction.
Technical scheme of the present invention is as follows:
A kind of unmanned plane copper pipe heat abstractor, comprise heat-conducting copper pipe, one end of described heat-conducting copper pipe contacts with the heating module of unmanned plane, and the main part of heat-conducting copper pipe extends to the air side of unmanned plane power spin oar bottom; One end that described heat-conducting copper pipe contacts with heating module is flat sheet-like structure.
As preferably, described heat-conducting copper pipe is fixed on unmanned plane engine body exterior.
As preferably, described heat-conducting copper pipe is fixed on unmanned plane internal body, and on described unmanned plane body, the position corresponding with described heat-conducting copper pipe is provided with some air-guiding holes for ventilating.
Unmanned plane copper pipe heat abstractor disclosed by the invention is by the ends contact thermal source of heat-conducting copper pipe, the main part of heat-conducting copper pipe extends to the air side of unmanned plane power spin oar bottom, the air-flow utilizing power spin oar to produce realizes wind-cooling heat dissipating, the heat transfer efficiency of copper pipe is high, total layout can be made easy, do not need to configure radiator fan in addition, simultaneously heat radiation performance, assembling difficulty can be reduced and weight reduction.
Accompanying drawing explanation
Fig. 1 is the present invention's structural representation in one embodiment.
Embodiment
Below in conjunction with accompanying drawing, the specific embodiment of the present invention is elaborated.
As shown in Figure 1, unmanned plane copper pipe heat abstractor disclosed by the invention comprises heat-conducting copper pipe 3, and one end of described heat-conducting copper pipe 3 contacts with the heating module 1 of unmanned plane, and the main part of heat-conducting copper pipe 3 extends to the air side of unmanned plane power spin oar 2 bottom; One end that described heat-conducting copper pipe 3 contacts with heating module 1 is flat sheet-like structure, with enlarge active surface, improves radiating efficiency; In concrete enforcement, it is outside that described heat-conducting copper pipe 3 can be fixed on unmanned plane body 4, extend to the air-out side of power spin oar 2, the wind-force heat radiation that power spin oar can be utilized to produce, under some operating mode, it is inner that heat-conducting copper pipe 3 also can be fixed on unmanned plane body 4, and now on unmanned plane body, 4 positions corresponding with described heat-conducting copper pipe 3 are provided with some air-guiding holes for ventilating, formation heat dissipation wind channel;
Unmanned plane copper pipe heat abstractor disclosed by the invention is by the ends contact thermal source of heat-conducting copper pipe 3, the main part of heat-conducting copper pipe 3 extends to the air side of unmanned plane power spin oar 2 bottom, the air-flow utilizing power spin oar to produce realizes wind-cooling heat dissipating, the heat transfer efficiency of copper pipe is high, total layout can be made easy, do not need to configure radiator fan in addition, simultaneously heat radiation performance, assembling difficulty can be reduced and weight reduction.
Above-described embodiment of the present invention, does not form limiting the scope of the present invention.Any amendment done within the spirit and principles in the present invention, equivalent replacement and improvement etc., all should be included within claims of the present invention.
Claims (3)
1. a unmanned plane copper pipe heat abstractor, is characterized in that: comprise heat-conducting copper pipe, one end of described heat-conducting copper pipe contacts with the heating module of unmanned plane, and the main part of heat-conducting copper pipe extends to the air side of unmanned plane power spin oar bottom; One end that described heat-conducting copper pipe contacts with heating module is flat sheet-like structure.
2. unmanned plane copper pipe heat abstractor as claimed in claim 1, is characterized in that: described heat-conducting copper pipe is fixed on unmanned plane engine body exterior.
3. unmanned plane copper pipe heat abstractor as claimed in claim 1, it is characterized in that: described heat-conducting copper pipe is fixed on unmanned plane internal body, on described unmanned plane body, the position corresponding with described heat-conducting copper pipe is provided with some air-guiding holes for ventilating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510356106.XA CN104883863A (en) | 2015-06-25 | 2015-06-25 | Copper pipe heat radiation device of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510356106.XA CN104883863A (en) | 2015-06-25 | 2015-06-25 | Copper pipe heat radiation device of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104883863A true CN104883863A (en) | 2015-09-02 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510356106.XA Pending CN104883863A (en) | 2015-06-25 | 2015-06-25 | Copper pipe heat radiation device of unmanned plane |
Country Status (1)
| Country | Link |
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| CN (1) | CN104883863A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017132805A1 (en) * | 2016-02-01 | 2017-08-10 | 张琬彬 | Unmanned aerial vehicle electronic speed controller heat dissipation device |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102514715A (en) * | 2011-12-19 | 2012-06-27 | 天津全华时代航天科技发展有限公司 | Cooling channel of motor |
| CN203854852U (en) * | 2014-03-28 | 2014-10-01 | 浙江省第二测绘院 | Rain-proof cooling device for unmanned aerial vehicle |
| CN104627366A (en) * | 2015-02-10 | 2015-05-20 | 曹兵 | Oil drive variable pitch quadrotor type multifunctional fire-fighting unmanned aerial vehicle |
| CN204697469U (en) * | 2015-06-25 | 2015-10-07 | 深圳飞马机器人科技有限公司 | Unmanned plane copper pipe heat abstractor |
-
2015
- 2015-06-25 CN CN201510356106.XA patent/CN104883863A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102514715A (en) * | 2011-12-19 | 2012-06-27 | 天津全华时代航天科技发展有限公司 | Cooling channel of motor |
| CN203854852U (en) * | 2014-03-28 | 2014-10-01 | 浙江省第二测绘院 | Rain-proof cooling device for unmanned aerial vehicle |
| CN104627366A (en) * | 2015-02-10 | 2015-05-20 | 曹兵 | Oil drive variable pitch quadrotor type multifunctional fire-fighting unmanned aerial vehicle |
| CN204697469U (en) * | 2015-06-25 | 2015-10-07 | 深圳飞马机器人科技有限公司 | Unmanned plane copper pipe heat abstractor |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017132805A1 (en) * | 2016-02-01 | 2017-08-10 | 张琬彬 | Unmanned aerial vehicle electronic speed controller heat dissipation device |
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| C06 | Publication | ||
| PB01 | Publication | ||
| EXSB | Decision made by sipo to initiate substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150902 |