CN206111317U - Unmanned aerial vehicle engine water -cooling heat -radiating devices - Google Patents
Unmanned aerial vehicle engine water -cooling heat -radiating devices Download PDFInfo
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- CN206111317U CN206111317U CN201621077087.3U CN201621077087U CN206111317U CN 206111317 U CN206111317 U CN 206111317U CN 201621077087 U CN201621077087 U CN 201621077087U CN 206111317 U CN206111317 U CN 206111317U
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- water
- vehicle engine
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- cooling heat
- cooling cylinder
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Abstract
The utility model provides an unmanned aerial vehicle engine water -cooling heat -radiating devices, by a plurality of partial constitutions, water -cooling heat -radiating devices includes: the water cold cylinder body, water cold cylinder lid, spark plug, water inlet, delivery port, spiral water channel, cylinder block and screw, the utility model has the advantages of through the spiral water channel and the outside fin of the internal portion of unmanned aerial vehicle engine water -cooling heat -radiating devices normal water cold cylinder can be effectual last heat dissipation to unmanned aerial vehicle engine, and the assurance engine uses for a long time, the production of reduction potential safety hazard.
Description
Technical field
This utility model is related to a kind of heat abstractor, more particularly, to a kind of unmanned vehicle engine water-cooling heat radiating device.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel by the equipment such as radar, it is tracked, is positioned, remote control, remote measurement and Digital Transmission.Can be in radio
Take off or launched with booster rocket as conventional airplane under remote control, also aerial input can be taken to by machine tool and be flown.Reclaim
When, also can be reclaimed by remote control parachute or block with the mode automatic Landing as conventional airplane landing mission, can
Repetitiousness uses multiple.
Electromotor is the heart of unmanned plane, and operationally, the temperature of electromotor can be very high for unmanned plane, if without good
Heat abstractor, will cause unmanned plane to use for a long time, and indicating oven temp. of engine can cause to coordinate between mutual moving parts
Gap reduces, and hinders the proper motion of parts, even causes movement parts stuck when serious, produces potential safety hazard.
Utility model content
Based on the overheated problem of unmanned vehicle engine, the purpose of this utility model is to provide a kind of unmanned vehicle engine water
Cooling and radiation device.
The purpose of this utility model is mainly realized by following technical scheme.
A kind of unmanned vehicle engine water-cooling heat radiating device, it includes：Water cooling cylinder, water cooling cylinder cover, spark plug, water inlet,
Outlet, spiral channel, cylinder block and screw, the top of the water cooling cylinder is provided with water cooling cylinder cover, and bottom is pacified by screw
Equipped with cylinder block, spark plug is installed on the water cooling cylinder cover, the water inlet is arranged on the left end of water cooling cylinder, outlet peace
The right-hand member of water cooling cylinder is mounted in, it is middle to be connected by spiral channel, and spiral channel is arranged on inside water cooling cylinder.
Preferably, the outside of the water cooling cylinder is provided with some groups of parallel fins.
Preferably, between the water cooling cylinder and water cooling cylinder cover, sealing ring is installed between water cooling cylinder and cylinder block.
Preferably, under, outlet is upper for the water inlet.
Compared with prior art, a kind of beneficial effect of unmanned vehicle engine water-cooling heat radiating device of the present utility model exists
In：
By the radiating of the spiral channel inside water cooling cylinder in the unmanned vehicle engine water-cooling heat radiating device and outside
Piece, effectively can persistently be radiated, it is ensured that the engine long time uses to unmanned vehicle engine, reduce the product of potential safety hazard
It is raw.
Description of the drawings
Fig. 1 is the structural representation of the unmanned vehicle engine water-cooling heat radiating device constituted according to this utility model preferred embodiment
Figure.
In figure：
1- water cooling cylinders；2- water cooling cylinder covers；3- spark plugs；4- water inlets；5- outlets；6- spiral channels；7- cylinder block；
8- screws.
Specific embodiment
Hereinafter, refer to the attached drawing is described in detail to specific embodiment of the utility model, it is detailed according to these
Thin description, one of ordinary skill in the art can implement this utility model it can be clearly understood that this utility model.Do not disobeying
In the case of back of the body this utility model principle, the feature in each different embodiment can be combined to obtain new embodiment party
Formula, or some of some embodiments feature is substituted, obtain other preferred embodiment.
Embodiment 1：Fig. 1 shows that a kind of unmanned vehicle engine water-cooled constituted according to this utility model preferred embodiment dissipates
The structural representation of thermal.It is made up of some.The water-cooling heat radiating device includes：Water cooling cylinder 1, water cooling cylinder cover 2,
Spark plug 3, water inlet 4, outlet 5, spiral channel 6, cylinder block 7 and screw 8, the top of the water cooling cylinder 1 is spirally connected installation
There is water cooling cylinder cover 2, bottom is provided with cylinder block 7 by screw 8, and internal welding is connected to spiral channel 6, and outside weldings have multigroup parallel
Between fin, and water cooling cylinder 1 and water cooling cylinder cover 2, sealing ring is installed between water cooling cylinder 1 and cylinder block 7, prevents gas
Into inside water cooling cylinder 1, it is spirally connected on the water cooling cylinder cover 2 and spark plug 3 is installed, the welded and installed of the water inlet 4 is in water-cooled
The left side lower end of cylinder body 1, the welded and installed of outlet 5 is middle to be connected by spiral channel 6 in the right side upper end of water cooling cylinder 1.
During work, struck sparks by spark plug 3, cylinder block 7 is started working, cooling water is from cooling cylinder body 1 left side lower end
Water inlet 4 enter, by spiral channel 6, flow out from the outlet 5 of cooling cylinder body 1 right side upper end, cylinder block 7 is carried out cold
But, amount of residual heat is shed by cooling down the fin outside cylinder body 1, completes to operate the cooling down of unmanned vehicle engine.
Although being described to this utility model above by referring to specific embodiment, art technology people
Member for this utility model is disclosed it should be appreciated that in this utility model principle disclosed and scope, can configure and details
Make many modifications.Protection domain of the present utility model is determined by appended claim, and claim is intended to
Whole modifications that the equivalent literal meaning or scope of technical characteristic is included in claim.
Claims (4)
1. a kind of unmanned vehicle engine water-cooling heat radiating device, is made up of some, and the water-cooling heat radiating device includes：Water-cooled cylinder
Body (1), water cooling cylinder cover (2), spark plug (3), water inlet (4), outlet (5), spiral channel (6), cylinder block (7) and screw
(8), it is characterised in that the top of the water cooling cylinder (1) is provided with water cooling cylinder cover (2), bottom is provided with gas by screw (8)
Cylinder body (7), is provided with spark plug (3), a left side of the water inlet (4) installed in water cooling cylinder (1) on the water cooling cylinder cover (2)
End, installed in the right-hand member of water cooling cylinder (1), centre is connected outlet (5) by spiral channel (6), and spiral channel (6) is pacified
It is mounted in water cooling cylinder (1) internal.
2. unmanned vehicle engine water-cooling heat radiating device as claimed in claim 1, it is characterised in that the outside of water cooling cylinder (1)
It is provided with some groups of parallel fins.
3. unmanned vehicle engine water-cooling heat radiating device as claimed in claim 1, it is characterised in that water cooling cylinder (1) and water-cooled
Between cylinder cap (2), sealing ring is installed between water cooling cylinder (1) and cylinder block (7).
4. unmanned vehicle engine water-cooling heat radiating device as claimed in claim 1, it is characterised in that water inlet (4) under, water outlet
Mouth (5) is upper.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621077087.3U CN206111317U (en) | 2016-09-23 | 2016-09-23 | Unmanned aerial vehicle engine water -cooling heat -radiating devices |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621077087.3U CN206111317U (en) | 2016-09-23 | 2016-09-23 | Unmanned aerial vehicle engine water -cooling heat -radiating devices |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206111317U true CN206111317U (en) | 2017-04-19 |
Family
ID=58520752
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621077087.3U Active CN206111317U (en) | 2016-09-23 | 2016-09-23 | Unmanned aerial vehicle engine water -cooling heat -radiating devices |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206111317U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106988855A (en) * | 2017-05-11 | 2017-07-28 | 廖兴池 | Special engine heat dissipating device on a kind of unmanned plane |
| CN113482827A (en) * | 2021-05-26 | 2021-10-08 | 珠海天晴航空航天科技有限公司 | Engine for unmanned aerial vehicle and control method thereof |
-
2016
- 2016-09-23 CN CN201621077087.3U patent/CN206111317U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106988855A (en) * | 2017-05-11 | 2017-07-28 | 廖兴池 | Special engine heat dissipating device on a kind of unmanned plane |
| CN113482827A (en) * | 2021-05-26 | 2021-10-08 | 珠海天晴航空航天科技有限公司 | Engine for unmanned aerial vehicle and control method thereof |
| CN113482827B (en) * | 2021-05-26 | 2022-07-12 | 珠海天晴航空航天科技有限公司 | Engine for unmanned aerial vehicle and control method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180404 Address after: 276801 production and development building No. 2, No. 2, No. 177, Rizhao City Donggang District, Shandong Province Patentee after: Shandong flying Aero Engine Co., Ltd. Address before: 710003 Gaoling District, Xi'an City, Shaanxi Province, Rong Hao industrial city (twenty-third 02 1 - 4 layers) in the demonstration garden of small and medium enterprises Patentee before: Xi'an flying Aviation Technology Co., Ltd. |