CN105592670A - Unmanned plane electronic speed controller heat radiation device - Google Patents
Unmanned plane electronic speed controller heat radiation device Download PDFInfo
- Publication number
- CN105592670A CN105592670A CN201610071477.8A CN201610071477A CN105592670A CN 105592670 A CN105592670 A CN 105592670A CN 201610071477 A CN201610071477 A CN 201610071477A CN 105592670 A CN105592670 A CN 105592670A
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- China
- Prior art keywords
- speed controller
- electronic speed
- heat
- heat radiation
- electricity
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- 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.)
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Classifications
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/2039—Modifications to facilitate cooling, ventilating, or heating characterised by the heat transfer by conduction from the heat generating element to a dissipating body
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- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention relates to an unmanned plane electronic speed controller heat radiation device. The unmanned plane electronic speed controller heat radiation device comprises a plane arm. One end of the plane arm is internally provided with an electronic speed controller, and other end is provided with a rotor swing. The device further comprises an electronic speed controller heat radiation plate. The upper surface of the electronic speed controller heat radiation plate and the plane arm are locked through screws, and the lower surface is bonded and fixed to the electronic speed controller through heat-conducting glue. The contact surface, with the electronic speed controller heat radiation plate, of the plane arm is provided with at least two heat dissipation holes. The electronic speed controller heat radiation plate is provided with grooves communicated with the heat dissipation holes. The electronic speed controller is sealed in the plane arm and is free from the corrosion influences of medicine mist, the heat generated by the electronic speed controller is simultaneously dissipated by the heat dissipation plate, the heat dissipation holes is capable of guiding high-speed air flows generated by the rotor swing to the heat dissipation plate and dissipating the high-speed air flows from two ends of the plane arm, and the heat dissipation effect is good; in addition, the integral structure is simple, and the cost is low.
Description
Technical field
The present invention relates to unmanned plane technical field, more particularly, relate to a kind of unmanned dynamo-electric heat abstractor of adjusting.
Background technology
The unmanned plane of large load electricity tune in the time of flight can send larger heat, and long-time overheated meeting causes electricity to be adjustedExcess temperature is shut down or is burnt; Meanwhile, while work for the unmanned plane of spraying insecticide, medicine mist can be outer to being exposed toElectricity is adjusted to produce and is corroded, and then causes short circuit phenomenon; Thereby need a kind of electricity to adjust sealing to arrange and good heat dissipation effectHeat abstractor.
Summary of the invention
The technical problem to be solved in the present invention is, for the above-mentioned defect of prior art, provides a kind of electricity to adjustSealing arranges and the unmanned electromechanics of good heat dissipation effect is adjusted heat abstractor.
The technical solution adopted for the present invention to solve the technical problems is:
A kind of unmanned dynamo-electric heat abstractor of adjusting of structure, comprises horn; Wherein, described horn one end is inner arrangesHave electricity to adjust, the other end is provided with rotor; Also comprise electricity tune heat sink, described electricity is adjusted heat sink upper surface and instituteState horn by screw locking, lower surface is pasted fixing by heat-conducting glue and described electricity tune; Described horn and instituteStating electricity adjusts heat sink contact-making surface to be provided with at least two louvres; Described electricity is adjusted on heat sink and is provided with describedThe groove of louvre conducting.
The unmanned dynamo-electric heat abstractor of adjusting of the present invention, wherein, described horn is aluminum alloy materials and by aluminiumAlloy extrusion forming process is made.
The unmanned dynamo-electric heat abstractor of adjusting of the present invention, wherein, described horn inside is hollow setting.
The unmanned dynamo-electric heat abstractor of adjusting of the present invention, wherein, described horn is square horn and outer surfaceBe provided with ripple groove.
Beneficial effect of the present invention is: electricity adjusts sealing to be arranged on horn inside, has avoided medicine mist corrosive effect,Meanwhile, electricity adjusts the heat producing to be dispelled the heat by heat sink, and the high velocity air that louvre can produce rotor is ledShed to heat sink and from horn two ends, good heat dissipation effect; Overall structure is simple, and cost is low.
Brief description of the drawings
In order to be illustrated more clearly in the embodiment of the present invention or technical scheme of the prior art, below in conjunction with attachedThe invention will be further described for figure and embodiment, and the accompanying drawing in the following describes is only that part of the present invention is realExecute example, for those of ordinary skill in the art, not paying under the prerequisite of creative work, all rightObtain other accompanying drawings according to these accompanying drawings:
Fig. 1 is the unmanned dynamo-electric construction for heat radiating device schematic diagram of adjusting of preferred embodiment of the present invention.
Detailed description of the invention
In order to make object, technical scheme and the advantage of the embodiment of the present invention clearer, below in conjunction with thisTechnical scheme in bright embodiment is carried out clear, complete description, and obviously, described embodiment is thisBright part embodiment, instead of whole embodiment. Based on embodiments of the invention, ordinary skillThe every other embodiment that personnel obtain under the prerequisite of not paying creative work, belongs to the present inventionProtection domain.
The unmanned dynamo-electric of preferred embodiment of the present invention adjusted heat abstractor as shown in Figure 1, comprises horn 1, horn1 inside, one end is provided with electricity and adjusts 2, and the other end is provided with rotor (not shown); Also comprise the heat radiation of electricity tunePlate 3, electricity adjusts heat sink 3 upper surfaces and horn 1 by screw locking, and lower surface is by heat-conducting glue 4 and electricityTune 2 is pasted fixing; Horn 1 adjusts heat sink 3 contact-making surfaces to be provided with at least two louvres 5 with electricity; Electricity is adjustedOn heat sink 3, be provided with the groove (not shown) with louvre 5 conductings; Electricity adjusts 2 sealings to be arranged onHorn 1 inside, has avoided medicine mist corrosive effect, and meanwhile, electricity adjusts 2 heats that produce to be fallen apart by heat sinkHeat, the high velocity air that louvre 5 can produce rotor (not shown) be directed at heat sink and from horn 1Two ends shed, good heat dissipation effect; Overall structure is simple, and cost is low.
As shown in Figure 1, horn 1 is aluminum alloy materials and is made up aluminum material of aluminium alloy extruded moulding processMaterial is conducive to dispel the heat fast.
As shown in Figure 1, horn 1 inside is hollow setting, is convenient to from horn 1 two ends quick heat radiating.
As shown in Figure 1, horn 1, for square horn and outer surface are provided with ripple groove, is convenient to high speed gasThe conduction of stream.
Should be understood that, for those of ordinary skills, can be improved according to the above descriptionOr conversion, and all these improvement and conversion all should belong to the protection domain of claims of the present invention.
Claims (4)
1. the unmanned dynamo-electric heat abstractor of adjusting, comprises horn; It is characterized in that, in described horn one endPortion is provided with electricity and adjusts, and the other end is provided with rotor; Also comprise electricity tune heat sink, described electricity is adjusted on heat sink and is shownFace and described horn are by screw locking, and lower surface is pasted fixing by heat-conducting glue and described electricity tune; Described machineArm and described electricity adjust heat sink contact-making surface to be provided with at least two louvres; Described electricity is adjusted on heat sink and is provided withGroove with described louvre conducting.
2. the unmanned dynamo-electric heat abstractor of adjusting according to claim 1, is characterized in that described hornMake for aluminum alloy materials and by aluminium alloy extruded moulding process.
3. the unmanned dynamo-electric heat abstractor of adjusting according to claim 1, is characterized in that described hornInside is hollow setting.
4. the unmanned dynamo-electric heat abstractor of adjusting according to claim 1, is characterized in that described hornFor square horn and outer surface are provided with ripple groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610071477.8A CN105592670A (en) | 2016-02-01 | 2016-02-01 | Unmanned plane electronic speed controller heat radiation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610071477.8A CN105592670A (en) | 2016-02-01 | 2016-02-01 | Unmanned plane electronic speed controller heat radiation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105592670A true CN105592670A (en) | 2016-05-18 |
Family
ID=55931752
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610071477.8A Pending CN105592670A (en) | 2016-02-01 | 2016-02-01 | Unmanned plane electronic speed controller heat radiation device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105592670A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107128485A (en) * | 2017-04-18 | 2017-09-05 | 河南翱翔多旋翼科技有限公司 | A kind of multilayer oar plant protection unmanned plane with full protection shell |
| CN107140222A (en) * | 2017-04-18 | 2017-09-08 | 河南翱翔多旋翼科技有限公司 | A kind of anti-water power of many rotor plant protection unmanned planes is adjusted |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204335628U (en) * | 2014-12-23 | 2015-05-20 | 辽宁猎鹰航空科技有限公司 | A kind of electricity of plant protection rotor wing unmanned aerial vehicle adjusts seat |
| CN204489178U (en) * | 2015-02-02 | 2015-07-22 | 深圳市吉田无人机航空科技有限公司 | High efficiency and heat radiation unmanned plane |
| CN204948595U (en) * | 2015-08-24 | 2016-01-06 | 深圳市诺亚星辰科技开发有限公司 | A kind of cooling circuit board for unmanned plane |
| CN205491608U (en) * | 2016-02-01 | 2016-08-17 | 深圳市盛禾农业科技有限公司 | Heat abstractor is transferred to unmanned aerial vehicle electricity |
-
2016
- 2016-02-01 CN CN201610071477.8A patent/CN105592670A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204335628U (en) * | 2014-12-23 | 2015-05-20 | 辽宁猎鹰航空科技有限公司 | A kind of electricity of plant protection rotor wing unmanned aerial vehicle adjusts seat |
| CN204489178U (en) * | 2015-02-02 | 2015-07-22 | 深圳市吉田无人机航空科技有限公司 | High efficiency and heat radiation unmanned plane |
| CN204948595U (en) * | 2015-08-24 | 2016-01-06 | 深圳市诺亚星辰科技开发有限公司 | A kind of cooling circuit board for unmanned plane |
| CN205491608U (en) * | 2016-02-01 | 2016-08-17 | 深圳市盛禾农业科技有限公司 | Heat abstractor is transferred to unmanned aerial vehicle electricity |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107128485A (en) * | 2017-04-18 | 2017-09-05 | 河南翱翔多旋翼科技有限公司 | A kind of multilayer oar plant protection unmanned plane with full protection shell |
| CN107140222A (en) * | 2017-04-18 | 2017-09-08 | 河南翱翔多旋翼科技有限公司 | A kind of anti-water power of many rotor plant protection unmanned planes is adjusted |
| CN107128485B (en) * | 2017-04-18 | 2024-02-23 | 王安民 | Multilayer oar plant protection unmanned aerial vehicle with full protective housing |
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| C10 | Entry into substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160518 |
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| RJ01 | Rejection of invention patent application after publication |