CN206885366U - A kind of multi-functional model plane unmanned plane heat abstractor - Google Patents
A kind of multi-functional model plane unmanned plane heat abstractor Download PDFInfo
- Publication number
- CN206885366U CN206885366U CN201720552118.4U CN201720552118U CN206885366U CN 206885366 U CN206885366 U CN 206885366U CN 201720552118 U CN201720552118 U CN 201720552118U CN 206885366 U CN206885366 U CN 206885366U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- protection network
- housing
- cover body
- fixed mounting
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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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Abstract
The utility model discloses a kind of multi-functional model plane unmanned plane heat abstractor, including unmanned plane housing, on the outer wall of the unmanned plane housing fixed mounting is equipped with the inside of air vent and heat emission hole, one end of fixedly connected part extends to the bottom of fixed mounting, the other end of fixedly connected part extends to the outside of protection network mounting bracket, protection network mounting bracket is provided with by fixedly connected part on fixed mounting, protection network mounting bracket is provided with protection network in one end away from fixed mounting, the inwall of unmanned plane housing is installed with radiating cover body by support frame, the inner chamber of radiating cover body is provided with engine, the one end of radiating cover body away from unmanned plane rotor is fixedly connected with connecting tube, the inner chamber of unmanned plane housing is provided with heat abstractor.The utility model is reasonable in design, good heat dissipation effect, can prevent debris from entering in unmanned plane housing, reliable and stable, extends the service life of unmanned plane, is not susceptible to the security incidents such as air crash.
Description
Technical field
Unmanned air vehicle technique field is the utility model is related to, specifically a kind of multi-functional model plane unmanned plane heat abstractor.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates.It can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..Unmanned plane presses application field, can be divided into
It is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Unmanned plane sector application, it is that unmanned plane has really just needed；
At present take photo by plane, agricultural, plant protection, self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news
The application in report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded the use of unmanned plane in itself
On the way, developed country is also in actively extension sector application and development unmanned air vehicle technique.
The engine cool of existing unmanned plane is using being air cooling engine technology, and some unmanned plane working environments are in high temperature
Under, equipment working strength is big, the time is long, it is big to carry medicine weight, and the engine of unmanned plane is often caused under this working condition
Overheat, so as to cause engine cavity to stop working；In addition, traditional unmanned plane is spread all in flight using exposed electric elements or fuselage
The mode that heat emission hole is radiated, so can not be flown under sleety weather.
Utility model content
The purpose of this utility model is to provide a kind of multi-functional model plane unmanned plane heat abstractor, to solve above-mentioned background skill
The problem of being proposed in art.
To achieve the above object, the utility model provides following technical scheme：
A kind of multi-functional model plane unmanned plane heat abstractor, including unmanned plane housing, the bottom of the unmanned plane housing are set
There is the support that rises and falls for supporting unmanned plane housing, the outer wall of the unmanned plane housing is provided with what is balanced for keeping unmanned plane
Unmanned airplane empennage, the outer wall of the unmanned plane housing are provided with heat emission hole, the outer wall of unmanned plane housing or so at the support that rises and falls
Both sides symmetrically offer air vent, and the opening of heat emission hole is provided with the deflector of arc, the air vent and heat emission hole it is interior
Side is equipped with fixed mounting, and fixed mounting is arranged with two groups, and one end of fixedly connected part extends to fixed mounting
Bottom, the other end of fixedly connected part extend to the outside of protection network mounting bracket, pacified on fixed mounting by fixedly connected part
Equipped with protection network mounting bracket, protection network mounting bracket is provided with protection network, the outside of protection network in one end away from fixed mounting
Provided with Vinylidene Chloride anticorrosive coat, the inwall of the unmanned plane housing is installed with radiating cover body by support frame, and radiate cover body
Inner chamber be provided with engine, the rotating shaft on engine extends to unmanned plane hull outside and is fixedly connected with unmanned plane rotor,
The one end of radiating cover body away from unmanned plane rotor is fixedly connected with connecting tube, and the inner chamber of unmanned plane housing is provided with heat abstractor,
Heat abstractor includes the hollow heat sink of polylith, is connected with conduit between the hollow heat sink of polylith, its in the hollow heat sink of polylith
In two pieces of outer wall offer spliced eye with connecting tube grafting, the cavity of radiating cover body and engine outer wall composition and hollow dissipate
Conduction oil is injected with hot plate, the inner chamber of the unmanned plane housing is installed with upper spacer and lower clapboard, and starts seat in the plane
In the cavity that upper spacer and lower clapboard are formed.
As further program of the utility model：The protection network is that fiberglass weaving reticulates, and protection network
Through-hole aperture be 0.2~1.0 centimetre, and the inner side of protection network is provided with rubber blanket.
As further program of the utility model：The radiating cover body is circular radiating cover, and the inwall for the cover body that radiates
It is bonded with the outer wall of engine.
As further program of the utility model：The hollow heat sink is copper cored slab, and the hollow radiating of polylith
Plate is set in qually spaced in the inner chamber of unmanned plane housing.
Compared with prior art, the beneficial effects of the utility model are：The multi-functional model plane unmanned plane heat abstractor, structure
It is reasonable in design, good heat dissipation effect, it can prevent debris from entering in unmanned plane housing, reliable and stable, extend unmanned plane uses the longevity
Life, is not susceptible to the security incidents such as air crash.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is side structure schematic view of the present utility model.
Fig. 3 is protection network scheme of installation in the utility model.
In figure：1- unmanned plane housings, 2- engines, 3- rise and fall support, 4- support frames, 5- radiating cover bodies, 6- connecting tubes, 7-
Heat abstractor, 8- upper spacers, 9- unmanned plane rotors, 10- air vents, 11- lower clapboards, 12- heat emission holes, 13- deflectors, 14- without
Man-machine empennage, 15- fixedly connected parts, 16- protection network mounting brackets, 17- Vinylidene Chloride anticorrosive coats, 18- protection networks, 19- fix peace
Fill seat.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Refer to Fig. 1~3, in the utility model embodiment, a kind of multi-functional model plane unmanned plane heat abstractor, including nobody
Casing body 1, the bottom of the unmanned plane housing 1 are provided with the support 3 that rises and falls for supporting unmanned plane housing 1, the unmanned plane
The outer wall of housing 1 is provided with the unmanned airplane empennage 14 for keeping unmanned plane to balance, and the outer wall of the unmanned plane housing 1 is close to be risen
Fall and heat emission hole 12 is provided with support 3, symmetrically air vent 10 is offered at left and right sides of the outer wall of unmanned plane housing 1, heat emission hole 12
Opening is provided with the deflector 13 of arc, sets deflector 13 to play a part of water conservancy diversion, prevents what is come out from heat emission hole 12
Hot-air gets muddled and causes unmanned plane during flying unstable, improves the security performance of unmanned plane.
The inner side of the air vent 10 and heat emission hole 12 is equipped with fixed mounting 19, and fixed mounting 19 is arranged with two
Group, one end of fixedly connected part 15 extend to the bottom of fixed mounting 19, and the other end of fixedly connected part 15 extends to protection
The outside of net mounting bracket 16, protection network mounting bracket 16, protection network peace are provided with by fixedly connected part 15 on fixed mounting 19
To shelve and protection network 18 is installed in 16 one end away from fixed mounting 19, protection network 18 is that fiberglass weaving reticulates,
And the through-hole aperture of protection network 18 is 0.2~1.0 centimetre, and the inner side of protection network 18 is provided with rubber blanket, the outside of protection network 18
Provided with Vinylidene Chloride anticorrosive coat 17, protection network 18 can prevent debris from entering in unmanned plane housing 1, reach and keep unmanned plane housing 1
The effect of interior cleaning.
The inwall of the unmanned plane housing 1 is installed with radiating cover body 5 by support frame 4, and radiating cover body 5 dissipates for annular
Heat cover, and the inwall for the cover body 5 that radiates is bonded with the outer wall of engine 2, the inner chamber of radiating cover body 5 is provided with engine 2, engine
Rotating shaft on 2 extends to the outside of unmanned plane housing 1 and is fixedly connected with unmanned plane rotor 9, and radiating cover body 5 is away from unmanned plane rotor
9 one end is fixedly connected with connecting tube 6, and the inner chamber of unmanned plane housing 1 is provided with heat abstractor 7, and it is empty that heat abstractor 7 includes polylith
Heart heat sink, hollow heat sink is copper cored slab, and the hollow heat sink of polylith is set in qually spaced in the interior of unmanned plane housing 1
Chamber, and conduit is connected between the hollow heat sink of polylith, wherein two pieces of outer wall in the hollow heat sink of polylith is offered with connecting
The spliced eye of the grafting of adapter 6, radiating cover body 5 in the cavity of the outer wall of engine 2 composition and hollow heat sink with being injected with heat conduction
Oil, improve the heat-sinking capability of the device.
The inner chamber of the unmanned plane housing 1 is installed with upper spacer 8 and lower clapboard 11, and engine 2 is located at upper spacer 8
In the cavity formed with lower clapboard 11, the effective electronics for preventing heat caused by engine 2 from influenceing unmanned plane enclosure
Element, the service life of unmanned plane is extended, more securely and reliably, be not susceptible to the security incidents such as air crash.
During unmanned plane flight in the air, engine 2 work caused by heat through radiate cover body 5 be collected in heat abstractor 7
Portion, air enter inside unmanned plane housing 1 from air vent 10, the heat being collected inside heat abstractor 7 are blown from heat emission hole 12
Outside to unmanned plane shell 1 completes radiating work.
The multi-functional model plane unmanned plane heat abstractor, reasonable in design, good heat dissipation effect, can prevent debris from entering nobody
It is reliable and stable in casing body, the service life of unmanned plane is extended, is not susceptible to the security incidents such as air crash.
The above is only preferred embodiment of the present utility model, it is noted that for those skilled in the art,
Without departing from the concept of the premise utility, several modifications and improvements can also be made, these should also be considered as this practicality
New protection domain, these are all without the effect and practical applicability for influenceing the utility model implementation.
Claims (4)
1. a kind of multi-functional model plane unmanned plane heat abstractor, including unmanned plane housing（1）, it is characterised in that the unmanned casing
Body（1）Bottom be provided with for supporting unmanned plane housing（1）The support that rises and falls（3）, the unmanned plane housing（1）Outer wall set
It is equipped with the unmanned airplane empennage for keeping unmanned plane to balance（14）, the unmanned plane housing（1）Outer wall close to rising and falling support（3）
Place is provided with heat emission hole（12）, unmanned plane housing（1）Outer wall at left and right sides of symmetrically offer air vent（10）, heat emission hole（12）'s
Opening is provided with the deflector of arc（13）, the air vent（10）And heat emission hole（12）Inner side be equipped with fixed mounting
（19）, fixed mounting（19）Two groups are arranged with, fixedly connected part（15）One end extend to fixed mounting（19）Bottom
Portion, fixedly connected part（15）The other end extend to protection network mounting bracket（16）Outside, fixed mounting（19）It is upper to pass through admittedly
Determine connector（15）Protection network mounting bracket is installed（16）, protection network mounting bracket（16）Away from fixed mounting（19）One end in
Protection network is installed（18）, protection network（18）Outside be provided with Vinylidene Chloride anticorrosive coat（17）, the unmanned plane housing（1）It is interior
Wall passes through support frame（4）It is installed with radiating cover body（5）, radiate cover body（5）Inner chamber be provided with engine（2）, engine
（2）On rotating shaft extend to unmanned plane housing（1）It is outside and with unmanned plane rotor（9）It is fixedly connected, radiate cover body（5）Away from nothing
Man-machine rotor（9）One end be fixedly connected with connecting tube（6）, unmanned plane housing（1）Inner chamber be provided with heat abstractor（7）, dissipate
Thermal（7）Including the hollow heat sink of polylith, conduit is connected between the hollow heat sink of polylith, its in the hollow heat sink of polylith
In two pieces of outer wall offer and connecting tube（6）The spliced eye of grafting, radiate cover body（5）With engine（2）The sky of outer wall composition
Conduction oil, the unmanned plane housing are injected with chamber and hollow heat sink（1）Inner chamber be installed with upper spacer（8）With under
Dividing plate（11）, and engine（2）Positioned at upper spacer（8）And lower clapboard（11）In the cavity formed.
2. multi-functional model plane unmanned plane heat abstractor according to claim 1, it is characterised in that the protection network（18）For
Fiberglass weaving reticulates, and protection network（18）Through-hole aperture be 0.2~1.0 centimetre, and protection network（18）Inner side
Provided with rubber blanket.
3. multi-functional model plane unmanned plane heat abstractor according to claim 1, it is characterised in that the radiating cover body（5）
For circular radiating cover, and the cover body that radiates（5）Inwall and engine（2）Outer wall fitting.
4. multi-functional model plane unmanned plane heat abstractor according to claim 1, it is characterised in that the hollow heat sink is
Copper cored slab, and the hollow heat sink of polylith is set in qually spaced in unmanned plane housing（1）Inner chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720552118.4U CN206885366U (en) | 2017-05-18 | 2017-05-18 | A kind of multi-functional model plane unmanned plane heat abstractor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720552118.4U CN206885366U (en) | 2017-05-18 | 2017-05-18 | A kind of multi-functional model plane unmanned plane heat abstractor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206885366U true CN206885366U (en) | 2018-01-16 |
Family
ID=61342125
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720552118.4U Expired - Fee Related CN206885366U (en) | 2017-05-18 | 2017-05-18 | A kind of multi-functional model plane unmanned plane heat abstractor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206885366U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111591452A (en) * | 2020-04-03 | 2020-08-28 | 湖北吉利太力飞车有限公司 | Ventilating device of vertical take-off device and control method |
-
2017
- 2017-05-18 CN CN201720552118.4U patent/CN206885366U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111591452A (en) * | 2020-04-03 | 2020-08-28 | 湖北吉利太力飞车有限公司 | Ventilating device of vertical take-off device and control method |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180116 Termination date: 20180518 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |