CN208924037U - A kind of unmanned plane radiating shell - Google Patents
A kind of unmanned plane radiating shell Download PDFInfo
- Publication number
- CN208924037U CN208924037U CN201821858624.7U CN201821858624U CN208924037U CN 208924037 U CN208924037 U CN 208924037U CN 201821858624 U CN201821858624 U CN 201821858624U CN 208924037 U CN208924037 U CN 208924037U
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- shell
- motor body
- unmanned plane
- conductive rubber
- heat conductive
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Abstract
The utility model relates to unmanned plane radiating shell technical fields, specifically a kind of unmanned plane radiating shell, including motor body and shell, shell is specially the aluminium casing of cylindric setting, the shell is that upper and lower open type is arranged and is socketed on motor body outer wall, the inner walls are equidistantly vertically arranged with the heat conductive rubber item for being tightly attached to the setting of motor body outer wall, and the strip groove being vertically arranged is formed between the two neighboring heat conductive rubber item, the housing exterior walls integration is provided with and the aluminium base cooling fin that is correspondingly arranged inside and outside heat conductive rubber item, through heat conductive rubber item under the premise of can stablize placement by buffer itself effect promoting motor body, thermally conductive processing can also be carried out as heat-conduction medium, by the heat transmission of absorption to aluminium casing and aluminium base cooling fin, thus motor body is distributed Partial heat be discharged in time.
Description
Technical field
The utility model relates to unmanned plane radiating shell technical field, specifically a kind of unmanned plane radiating shell.
Background technique
Unmanned plane is by motor, and to drive propeller, motor rotation, itself can generate heat, if too late
When stop flight, radiate, it can be made not fly again to causing damages inside unmanned plane motor.
In this regard, number of patent application is that CN201720949198.7 proposes a kind of unmanned plane radiating shell, it include nobody
Electric motor is provided with radiating shell on the outside of the unmanned electric motor, and the radiating shell is cylindrical structure, inside
The upper end left and right sides for hollow structure, the radiating shell is provided with water inlet, lower end of the radiating shell or so two
Side is provided with water outlet, and multiple heat release holes are evenly arranged on the radiating shell, and the radiating shell is hollow structure, institute
Stating heat release hole is cylindrical type groove structure, is hollow pipe structure inside the radiating shell around the heat release hole, and mutually interconnect
Logical, the material of the radiating shell is polybutylene terephthalate (PBT), and above scheme makes the more quickening that unmanned plane heat distributes
Speed.
But there is also defects when in use for above scheme:
Heat dissipation effect is undesirable: motor major part heat is taken away using cold water in above scheme, and if in above scheme
If the hydropexis of entrance is not easy that radiating shell is discharged from drainpipe, it is greatly likely to become auxiliary motor heating damage
Leading factor；Above scheme is not easy to carry out motor and radiating shell faster to stablize installation and removal simultaneously, thus
Maintenance cost is promoted.
Utility model content
In order to make up the above deficiency, the utility model provides a kind of unmanned plane radiating shell, to solve above-mentioned background
The problems in technology.
The technical solution of the utility model is: a kind of unmanned plane radiating shell, including motor body and shell, shell
The aluminium casing of specially cylindric setting, the shell are that upper and lower open type is arranged and is socketed on motor body outer wall, institute
It states inner walls and is equidistantly vertically arranged with the heat conductive rubber item for being tightly attached to the setting of motor body outer wall, and two neighboring described lead
The strip groove being vertically arranged is formed between hot rubber strip, the housing exterior walls integration is provided with set corresponding with inside and outside heat conductive rubber item
The aluminium base cooling fin set, the housing bottom are fixedly installed with bottom plate by screw, and the bottom plate top is pacified by screw
Equipped with radiator fan, radiator fan uses model STF1202512VH, and the inner walls, which also equidistantly offer, to be vertically arranged
Heat release hole, integration is provided with support rod at left and right sides of the inner walls bottom, the support rod by screw with
Motor body bottom end is fixed.
In this setting:
1) heat dissipation effect is preferable: can stablized by buffer itself effect promoting motor body by heat conductive rubber item
Under the premise of placement, additionally it is possible to carry out thermally conductive processing as heat-conduction medium, by the heat transmission of absorption to aluminium casing and
Thus aluminium base cooling fin the partial heat that motor body is distributed is discharged in time, while passing through two neighboring heat conductive rubber
The setting of item and shell can form the strip groove being placed equidistant between shell and motor body, by the power supply of radiator fan
Line accesses unmanned plane internal electric source by the wiring hole offered on shell, to blow out cold air, cold sky by radiator fan
Gas first radiates to motor body bottom face, at the same air-flow by motor body bottom stop after along strip groove to
Upper flowing carries out cooling and heat dissipation to motor body side again, and the heat of blowout is by that can flow directly out upwards or pass through shell
The heat release hole of side wall flow to hull outside, realizes and carries out safer radiating treatment to motor body；
2) installation convenience: motor body is placed inside housings, so that motor body bottom end is placed in branch
Strut top, then support rod and motor body are carried out by installation fixation by screw, pass through the compression bar installed by screw
Convenient for motor body upper end is carried out abutting fixation, while support rod and compression bar are copper bar and bottom is coated with abutting
In the heat conductive silica gel of motor body, to be convenient for the heat for preferably carrying out absorbing motor body by heat conductive silica gel, lead to
Support rod and compression bar made of copper are crossed convenient for preferably distributing the heat of absorption.
Preferably, compression bar, and two compression bars are also fixedly installed with by screw at left and right sides of the shell upper end
By being fixedly mounted at left and right sides of screw and motor body upper end, the support rod and compression bar is copper bar and bottom is equal
Coated with abutting in the heat conductive silica gel of motor body.
Preferably, the support rod is located at setting above radiator fan, and the bottom base plate middle position offer with
The ventilation opening of connection setting on rear side of radiator fan.
This setting is convenient for ventilation by the setting of ventilation opening.
Preferably, the shell is identical as the vertical length of heat conductive rubber item and aluminium base cooling fin, and the heat dissipation hole location
It is arranged between two neighboring aluminium base cooling fin.
Preferably, the housing bottom is also provided with the wiring hole for interting radiator fan power supply line.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, before not making the creative labor property
It puts, is also possible to obtain other drawings based on these drawings.
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the left side view in the utility model Fig. 1；
Fig. 3 is the schematic diagram of the section structure at the A-A in the utility model Fig. 2；
Fig. 4 is the schematic diagram of the section structure at the B-B in the utility model Fig. 2.
Wherein, appended drawing reference is summarized as follows: 1 motor body, 2 shells, 3 heat conductive rubber items, 4 strip grooves, the heat dissipation of 5 aluminium bases
Piece, 6 bottom plates, 7 radiator fans, 8 heat release holes, 9 support rods, 10 compression bars.
Specific embodiment
The utility model is further illustrated in the following with reference to the drawings and specific embodiments.
With reference to Fig. 1-4 it is found that a kind of unmanned plane radiating shell of the utility model, including motor body 1 and shell 2,
The shell 2 is that upper and lower open type is arranged and is socketed on 1 outer wall of motor body, and 2 inner wall of shell is equidistantly vertically arranged with
It is tightly attached to the heat conductive rubber item 3 of 1 outer wall of motor body setting, and is formed between the two neighboring heat conductive rubber item 3 and set vertically
The strip groove 4 set, the 2 outer wall integration of shell be provided with the aluminium base cooling fin 5 that is correspondingly arranged inside and outside heat conductive rubber item 3,
2 bottom end of shell is fixedly installed with bottom plate 6 by screw, and 6 top of bottom plate is equipped with radiator fan by screw
7,2 inner wall of shell also equidistantly offers the heat release hole 8 being vertically arranged, and 2 inner wall bottom of the shell left and right sides is whole
Change is provided with support rod 9, and the support rod 9 is fixed by screw and 1 bottom end of motor body.Described 2 upper end of shell or so
Two sides also pass through screw and are fixedly installed with compression bar 10, and two compression bars 10 pass through screw and 1 upper end of motor body
Left and right sides fixed installation, the support rod 9 and compression bar 10 are copper bar and bottom is coated with abutting in motor body
1 heat conductive silica gel.The support rod 9, which is located above radiator fan 7, to be arranged, and 6 bottom middle position of the bottom plate offer with
The ventilation opening of setting is connected on rear side of radiator fan 7.The vertical length of the shell 2 and heat conductive rubber item 3 and aluminium base cooling fin 5
It is identical, and the heat release hole 8 is arranged between two neighboring aluminium base cooling fin 5.2 bottom of shell, which is also provided with, to be used for
The wiring hole of interspersed 7 power supply line of radiator fan.
Motor body 1 is placed on inside shell 2, when implementing so that motor body 1 by the present embodiment
Bottom end is placed in 9 top of support rod, then support rod 9 and motor body 1 are carried out installation fixation by screw, by by spiral shell
The compression bar 10 of adjusting screw installation is convenient for 1 upper end of motor body carrying out abutting fixation；By heat conductive rubber item 3 can by from
Under the premise of body buffering effect promotes the stable placement of motor body 1, additionally it is possible to thermally conductive processing is carried out as heat-conduction medium,
By the heat transmission of absorption to aluminium casing 2 and aluminium base cooling fin 5, the partial heat for thus being distributed motor body 1
Discharge in time, while can be between shell 2 and motor body 1 by the setting of two neighboring heat conductive rubber item 3 and shell 2
The strip groove 4 being placed equidistant with is formed, the power supply line of radiator fan 7 is accessed into unmanned plane by the wiring hole offered on shell 2
Internal electric source, to blow out cold air by radiator fan 7, cold air first radiates to 1 bottom face of motor body, together
When air-flow stopped by 1 bottom of motor body after flow up along strip groove 4 and cool down again to 1 side of motor body
Heat dissipation, the heat of blowout are realized by that can flow directly out upwards or flow to 2 outside of shell by the heat release hole 8 of 2 side wall of shell
Safer radiating treatment is carried out to motor body 1.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above.Current row
The technical staff of industry is described in above embodiments and description it should be appreciated that the present utility model is not limited to the above embodiments
Only illustrate the principles of the present invention, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
It will have various changes and improvements, these various changes and improvements fall within the scope of the claimed invention.The utility model
Claimed range is defined by the appending claims and its equivalent thereof.
Claims (5)
1. a kind of unmanned plane radiating shell, including motor body (1) and shell (2), it is characterised in that: the shell (2)
For the setting of upper and lower open type and it is socketed on motor body (1) outer wall, shell (2) inner wall, which is equidistantly vertically arranged with, to be tightly attached to
The heat conductive rubber item (3) of motor body (1) outer wall setting, and formed between the two neighboring heat conductive rubber item (3) and set vertically
The strip groove (4) set, shell (2) the outer wall integration is provided with to be dissipated with the inside and outside aluminium base being correspondingly arranged of heat conductive rubber item (3)
Backing (5), shell (2) bottom end are fixedly installed with bottom plate (6) by screw, and bottom plate (6) top passes through screw
It is equipped with radiator fan (7), shell (2) inner wall also equidistantly offers the heat release hole (8) being vertically arranged, the shell (2)
Integration is provided with support rod (9) at left and right sides of inner wall bottom, and the support rod (9) passes through screw and motor body
(1) bottom end is fixed.
2. a kind of unmanned plane radiating shell described in accordance with the claim 1, it is characterised in that: described shell (2) upper end or so
Two sides also pass through screw and are fixedly installed with compression bar (10), and two compression bars (10) pass through screw and motor body
(1) be fixedly mounted at left and right sides of upper end, the support rod (9) and compression bar (10) are copper bar and bottom be coated with push against in
The heat conductive silica gel of motor body (1).
3. a kind of unmanned plane radiating shell described in accordance with the claim 1, it is characterised in that: the support rod (9), which is located at, to be dissipated
Setting above Hot-air fan (7), and the bottom plate (6) bottom middle position offers and is connected to setting on rear side of radiator fan (7)
Ventilation opening.
4. a kind of unmanned plane radiating shell described in accordance with the claim 1, it is characterised in that: the shell (2) and thermally conductive rubber
Adhesive tape (3) is identical with the vertical length of aluminium base cooling fin (5), and the heat release hole (8) is located at two neighboring aluminium base cooling fin (5)
Between be arranged.
5. a kind of unmanned plane radiating shell described in accordance with the claim 1, it is characterised in that: also open shell (2) bottom
Equipped with the wiring hole for interting radiator fan (7) power supply line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821858624.7U CN208924037U (en) | 2018-11-12 | 2018-11-12 | A kind of unmanned plane radiating shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821858624.7U CN208924037U (en) | 2018-11-12 | 2018-11-12 | A kind of unmanned plane radiating shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208924037U true CN208924037U (en) | 2019-05-31 |
Family
ID=66711842
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821858624.7U Expired - Fee Related CN208924037U (en) | 2018-11-12 | 2018-11-12 | A kind of unmanned plane radiating shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208924037U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111629545A (en) * | 2020-06-01 | 2020-09-04 | 李克胜 | Heat dissipation fixing device for communication engineering equipment |
| WO2021068476A1 (en) * | 2019-10-10 | 2021-04-15 | 精进电动科技股份有限公司 | Electric motor shell |
-
2018
- 2018-11-12 CN CN201821858624.7U patent/CN208924037U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021068476A1 (en) * | 2019-10-10 | 2021-04-15 | 精进电动科技股份有限公司 | Electric motor shell |
| US11811290B2 (en) | 2019-10-10 | 2023-11-07 | Jing-Jin Electric Technologies Co., Ltd. | Electric-machine housing |
| CN111629545A (en) * | 2020-06-01 | 2020-09-04 | 李克胜 | Heat dissipation fixing device for communication engineering equipment |
| CN111629545B (en) * | 2020-06-01 | 2024-06-04 | 深圳市天建通信有限公司 | Heat dissipation fixing device for communication engineering equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP02 | Change in the address of a patent holder | ||
| CP02 | Change in the address of a patent holder |
Address after: No.5 workshop, No.398, Wenhui Road, Wuyi Town, Chuzhou City, Anhui Province Patentee after: Anhui dream wing UAV Technology Co., Ltd. Address before: No.5 workshop, No.398, Wenhui Road, Wuyi Town, Chuzhou City, Anhui Province Patentee before: Anhui dream wing UAV Technology Co., Ltd. |
|
| 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: 20190531 Termination date: 20201112 |