CN207045759U - A kind of unmanned plane radiator - Google Patents

A kind of unmanned plane radiator Download PDF

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Publication number
CN207045759U
CN207045759U CN201720901884.7U CN201720901884U CN207045759U CN 207045759 U CN207045759 U CN 207045759U CN 201720901884 U CN201720901884 U CN 201720901884U CN 207045759 U CN207045759 U CN 207045759U
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China
Prior art keywords
radiating
heat
heat sink
unmanned plane
plate
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CN201720901884.7U
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Chinese (zh)
Inventor
俞阿丹
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Hebei Xiangtuo Aviation Technology Co Ltd
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Hebei Xiangtuo Aviation Technology Co Ltd
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Priority to CN201720901884.7U priority Critical patent/CN207045759U/en
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Abstract

The utility model discloses a kind of unmanned plane radiator, its structure includes contiguous block, installing plate, heat sink, radiating tube, heat extraction mouth, heat sink top both sides are provided with radiating tube, heat extraction mouth is installed inside the heat sink, the heat sink both sides are provided with contiguous block, the contiguous block both sides are provided with installing plate, and the heat sink includes radiating bottom plate, fin, air inlet, air outlet, and both sides are provided with fin inside the radiating bottom plate.A kind of unmanned plane radiator of the present utility model, pass through being used cooperatively there is provided radiating tube and heat extraction mouth, radiating tube can effectively be absorbed to the heat inside unmanned plane when in use, heat on radiating tube is carried out by quick heat radiating by heat extraction mouth, solves the phenomenon of radiating effect difference, by the way that there is provided heat sink, the radiating bottom plate set inside heat sink and the heat sink material quality that fin uses are light, thickness of thin, the weight inside unmanned plane can effectively be mitigated, solve excessively heavy phenomenon.

Description

A kind of unmanned plane radiator
Technical field
The utility model is a kind of unmanned plane radiator, belongs to radiator field.
Background technology
Radiator is used to reduce caused heat during equipment operation when being the operating of machinery equipment part, so as to plant equipment Part radiating is freezed to increase the mechanical action life-span, so the quality of radiator directly affects the longevity of operating mechanical equipment component Life, with the rapid development of science and technology, a kind of unmanned plane radiator has also obtained technological improvement, has passed through radiator when in use Unmanned plane is carried out much time using, and the service life of unmanned plane can be increased, but prior art radiating effect Difference is excessively heavy.
Utility model content
In view of the deficienciess of the prior art, the utility model purpose is to provide a kind of unmanned plane radiator, it is existing to solve There is poor, the excessively heavy phenomenon of technology radiating effect.
To achieve these goals, the utility model is to realize by the following technical solutions:A kind of unmanned plane radiating Device, including contiguous block, installing plate, heat sink, radiating tube, heat extraction mouth, heat sink top both sides are provided with radiating tube, described Heat extraction mouth is installed inside heat sink, the heat sink both sides are provided with contiguous block, and the contiguous block both sides are provided with installing plate, The heat sink includes radiating bottom plate, fin, air inlet, air outlet, and both sides are provided with fin, institute inside the radiating bottom plate State and air inlet is connected with the left of radiating bottom plate front end, air outlet, the radiating bottom plate are connected with the right side of the radiating bottom plate front end Both sides are connected with contiguous block.
Further, the radiating tube is provided with two.
Further, the radiating tube is provided with small interior big circular hole outside two or more.
Further, the heat extraction mouth is provided with two.
Further, the fin is provided with four.
Further, the radiating tube uses copper material, and copper material can carry out quick heat radiating.
Further, the fin uses aluminum alloy material, has the advantages of cheap, in light weight.
A kind of unmanned plane radiator of the present utility model, by being used cooperatively there is provided radiating tube and heat extraction mouth, make Used time radiating tube can effectively be absorbed to the heat inside unmanned plane, be carried out the heat on radiating tube soon by heat extraction mouth Speed radiating, solves the phenomenon of radiating effect difference, by the way that there is provided heat sink, the radiating bottom plate set inside heat sink is with dissipating The heat sink material quality that backing uses is light, thickness of thin, can effectively mitigate the weight inside unmanned plane, solve excessively heavy Phenomenon.
Brief description of the drawings
By reading the detailed description made with reference to the following drawings to non-limiting example, other spies of the present utility model Sign, objects and advantages will become more apparent upon:
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of the utility model heat sink;
Fig. 3 is principle schematic of the present utility model.
In figure:Heat sink -1, radiating tube -2, heat extraction mouth -3, contiguous block -4, installing plate -5, radiating bottom plate -101, radiating Piece -102, air inlet -103, air outlet -104.
Embodiment
Technological means, creation characteristic, reached purpose and effect to realize the utility model are easy to understand, below With reference to embodiment, the utility model is expanded on further.
Fig. 1, Fig. 2 and Fig. 3 are referred to, the utility model provides a kind of unmanned plane radiator:Including contiguous block 4, installing plate 5th, heat sink 1, radiating tube 2, heat extraction mouth 3, the top both sides of heat sink 1 are provided with radiating tube 2, heat extraction are provided with inside heat sink 1 Mouthfuls 3, the both sides of heat sink 1 are provided with contiguous block 4, and the both sides of contiguous block 4 are provided with installing plate 5, heat sink 1 include radiating bottom plate 101, Fin 102, air inlet 103, air outlet 104, the inside both sides of radiating bottom plate 101 are provided with fin 102, before radiating bottom plate 101 End left side is connected with air inlet 103, and air outlet 104, the both sides of radiating bottom plate 101 and company are connected with the right side of the front end of radiating bottom plate 101 Connect block 4 to be connected, radiating tube 2 is provided with two, and radiating tube 2 is provided with small interior big circular hole outside two or more, and heat extraction mouth 3 is provided with two Individual, fin 102 is provided with four.Radiating tube 2 uses copper material, and copper material can carry out quick heat radiating, and fin 102 is adopted With aluminum alloy material, there is the advantages of cheap, in light weight.
Fin 102 described in this patent is a kind of device of the easy heat-generating electronic elements radiating in electrical equipment, more by aluminium Alloy, brass or bronze make tabular, sheet, splintery etc., as cpu central processing unit will use sizable radiating in computer Piece, power supply pipe in television set, row pipe, the power tube in amplifirer will use fin, and radiating tube 2 is to pass caused heat The part of water is passed, existing radiating tube lumen diameter is consistent.
When user wants to use this patent, when unmanned plane usage time is long, certain heat will be produced, At this moment radiating tube 2 will be by way of absorbing heat to carry out heat extraction inside unmanned plane, and the heat of absorption is entered by heat extraction mouth 3 Row discharge, when heat sink 1 is installed on inside unmanned plane, can be absorbed by fin 102 to the heat inside unmanned plane, By there is provided air inlet 103 and air outlet 104, when unmanned plane using when made by the cooperation of air inlet 103 and air outlet 104 With, make wind discharge when drive unmanned plane inside heat discharge, effectively unmanned plane can be radiated, by there is provided dissipate Hot plate 1, the radiating bottom plate 101 set inside heat sink and the heat sink material quality that fin 102 uses are light, and thickness of thin can Effectively to mitigate the weight inside unmanned plane, solves excessively heavy phenomenon, by the way that there is provided radiating tube 2 and heat extraction mouth 3 It is used cooperatively, radiating tube 2 can effectively be absorbed to the heat inside unmanned plane when in use, will be radiated by heat extraction mouth 3 Heat on pipe 2 carries out quick heat radiating, and the phenomenon for solving radiating effect difference, contiguous block 4 plays connection function, the side of installing plate 5 Just user is fixedly mounted.
The utility model heat sink 1, radiating tube 2, heat extraction mouth 3, contiguous block 4, installing plate 5, radiating bottom plate 101, fin 102nd, air inlet 103, the part of air outlet 104 are universal standard part, and the especially inside both sides of radiating bottom plate 101 are provided with fin 102, the front end of radiating bottom plate 101 left side is connected with air inlet 103, and air outlet 104 is connected with the right side of the front end of radiating bottom plate 101, dissipates The hot both sides of bottom plate 101 are connected with contiguous block 4, can reach good heat dissipation effect, effect in light weight, so as to be effectively prevented from dissipating Thermal effect is poor, it is excessively heavy the shortcomings that.
The advantages of general principle and principal character of the present utility model and the utility model has been shown and described above, for For those skilled in the art, it is clear that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and without departing substantially from this In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter From the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, the scope of the utility model is by institute Attached claim rather than described above limit, it is intended that will fall in the implication and scope of the equivalency of claim All changes are included in the utility model.Any reference in claim should not be considered as to the involved right of limitation It is required that.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art It is appreciated that other embodiment.

Claims (5)

1. a kind of unmanned plane radiator, including contiguous block (4), installing plate (5), it is characterised in that:Also include heat sink (1), dissipate Heat pipe (2), heat extraction mouth (3), heat sink (1) the top both sides are provided with radiating tube (2), installed inside the heat sink (1) There is heat extraction mouth (3), heat sink (1) both sides are provided with contiguous block (4), and contiguous block (4) both sides are provided with installing plate (5), the heat sink (1) includes radiating bottom plate (101), fin (102), air inlet (103), air outlet (104), described to dissipate The internal both sides of hot bottom plate (101) are provided with fin (102), and air inlet is connected with the left of radiating bottom plate (101) front end (103) air outlet (104), is connected with the right side of radiating bottom plate (101) front end, radiating bottom plate (101) both sides are with being connected Block (4) is connected.
A kind of 2. unmanned plane radiator according to claim 1, it is characterised in that:The radiating tube (2) is provided with two.
A kind of 3. unmanned plane radiator according to claim 1, it is characterised in that:The radiating tube (2) is provided with two Outer small interior big circular hole above.
A kind of 4. unmanned plane radiator according to claim 1, it is characterised in that:The heat extraction mouth (3) is provided with two.
A kind of 5. unmanned plane radiator according to claim 1, it is characterised in that:The fin (102) is provided with Four.
CN201720901884.7U 2017-07-24 2017-07-24 A kind of unmanned plane radiator Active CN207045759U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720901884.7U CN207045759U (en) 2017-07-24 2017-07-24 A kind of unmanned plane radiator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720901884.7U CN207045759U (en) 2017-07-24 2017-07-24 A kind of unmanned plane radiator

Publications (1)

Publication Number Publication Date
CN207045759U true CN207045759U (en) 2018-02-27

Family

ID=61497807

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720901884.7U Active CN207045759U (en) 2017-07-24 2017-07-24 A kind of unmanned plane radiator

Country Status (1)

Country Link
CN (1) CN207045759U (en)

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