CN207234585U - A kind of unmanned plane radiating shell - Google Patents

A kind of unmanned plane radiating shell Download PDF

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Publication number
CN207234585U
CN207234585U CN201720949198.7U CN201720949198U CN207234585U CN 207234585 U CN207234585 U CN 207234585U CN 201720949198 U CN201720949198 U CN 201720949198U CN 207234585 U CN207234585 U CN 207234585U
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CN
China
Prior art keywords
radiating shell
unmanned plane
shell
unmanned
heat emission
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Active
Application number
CN201720949198.7U
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Chinese (zh)
Inventor
安秋霞
刘利波
安明琪
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
WuJie Intelligent Technology (Shenzhen) Co.,Ltd.
Original Assignee
Henan Cool Agricultural Aviation Plant Protection Technology Co Ltd
Shenzhen Agricultural Uav Industrial Development And Application Co Ltd
Xihua Cool Agricultural Uav Industrial Park Operation Co Ltd
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Filing date
Publication date
Application filed by Henan Cool Agricultural Aviation Plant Protection Technology Co Ltd, Shenzhen Agricultural Uav Industrial Development And Application Co Ltd, Xihua Cool Agricultural Uav Industrial Park Operation Co Ltd filed Critical Henan Cool Agricultural Aviation Plant Protection Technology Co Ltd
Priority to CN201720949198.7U priority Critical patent/CN207234585U/en
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Publication of CN207234585U publication Critical patent/CN207234585U/en
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Abstract

A kind of unmanned plane radiating shell, include unmanned electric motor, radiating shell is provided with the outside of the unmanned electric motor, the radiating shell is cylindrical structure, it is hollow-core construction that it is internal, water inlet is both provided with left and right sides of the upper end of the radiating shell, water outlet is both provided with left and right sides of the lower end of the radiating shell, multiple heat emission holes are evenly arranged with the radiating shell, the radiating shell is hollow-core construction, the heat emission hole is cylindrical type groove structure, it is hollow pipe structure inside radiating shell around the heat emission hole, and mutual unicom, the material of the radiating shell is polybutylene terephthalate (PBT), the radiating shell is set on the shell of unmanned motor, it is quicker that the utility model distributes unmanned plane heat.

Description

A kind of unmanned plane radiating shell
Technical field
A kind of radiating shell is the utility model is related to, it particularly relates to a kind of unmanned plane radiating shell.
Background technology
With the development of society, the raising of living standards of the people, the environment that people live oneself has required, the modern times Society rapid development make people to society cognition it is broader, people thirst for explore sky, it is desirable to hover as bird and Sky, then we have an aircraft, anyone has the possibility for the sky that flies up into the sky to but not, and it is winged not to be that everyone can drive Machine, but this is without prejudice to the our own imagination, unmanned plane are that people fly up into the sky sky, explore an invention of sky, it is not necessary to How much is spent, it is possible to fly to sky, even present small drone is relatively conventional, but nor any can possess , and present technology is immature, and unmanned plane is also by motor, to drive propeller, motor rotation, itself meeting Produce heat, if not in time stop flight, radiate, can damage to unmanned plane motor internal, make its can not again into Row flight.
Utility model content
For the above-mentioned unmanned plane being previously mentioned in flying for long time, motor produces heat, especially in summer, heat without Method distributes in time, the problem of causing the excessive damage of unmanned plane temperature, there is provided a kind of unmanned plane radiating shell.
In order to solve the problems, such as it is above-mentioned be previously mentioned, a kind of unmanned plane radiating shell, includes unmanned electric motor, described Radiating shell is provided with the outside of unmanned electric motor, the radiating shell is cylindrical structure, and it is hollow-core construction that it is internal, institute State and water inlet is both provided with left and right sides of the upper end of radiating shell, water outlet is both provided with left and right sides of the lower end of the radiating shell Mouthful, it is evenly arranged with multiple heat emission holes on the radiating shell.
The heat emission hole is circle structure.
It is hollow pipe structure inside radiating shell around the heat emission hole, and mutual unicom.
The material of the radiating shell is polybutylene terephthalate (PBT).
The radiating shell is set on the shell of unmanned electric motor.
The utility model produce beneficial effect be:The utility model provides a kind of unmanned plane radiator, helps nobody Machine carries out distributing for heat, is hollow pipe structure inside radiating shell, end side surface is provided with two water inlets thereon, for leading Enter water, its lower end side is provided with two water outlets, for discharging water, makes water that the heat of unmanned plane motor is led out, side Help unmanned plane to carry out distributing for heat, can distribute heat more quick, and be provided with multiple heat dissipations on radiating shell Hole, for helping unmanned plane to carry out distributing for heat, works along both lines, heat is distributed faster, more rapidly.
The radiating shell material of the utility model is the material of polybutylene terephthalate (PBT), and secondary material is its inside points Minor structure is highly stable, there is preferable electrical insulation characteristics and heat endurance, can distribute heat quicker.
Brief description of the drawings
Fig. 1 is the utility model top surface structure connection diagram.
Fig. 2 is the utility model Facad structure connection diagram.
Embodiment
Below in conjunction with the accompanying drawings to the embodiment further instruction of the utility model.
Embodiment 1:A kind of unmanned plane radiating shell, includes unmanned electric motor 1, the unmanned electric motor 1 Outside is provided with radiating shell 2, and the radiating shell 2 is cylindrical structure, and it is hollow-core construction that it is internal, the radiating shell 2 Upper end at left and right sides of be both provided with water inlet 3, be both provided with water outlet 4 at left and right sides of the lower end of the radiating shell 2, it is described Multiple heat emission holes 5 are evenly arranged with radiating shell 2.
The heat emission hole 5 is circle structure.
The inside of radiating shell 2 around the heat emission hole 5 is hollow pipe structure, and mutual unicom.
The material of the radiating shell 2 is polybutylene terephthalate (PBT).
The radiating shell 2 is set on the shell of unmanned electric motor 1.
The utility model is when in use:The utility model is a kind of radiator, helps unmanned plane to carry out distributing for heat, The temperature of unmanned plane is reduced, prevents that unmanned plane from working long hours the harm to itself, the utility model includes radiating shell, Radiating shell is set on unmanned motor, comes into full contact with the motor casing of itself and unmanned plane, carries out the conduction of heat, and And the upper side of radiating shell is provided with two water inlets, its lower end side is provided with two water outlets, with water to motor Heat is dissipated, and water can take away most of heat, reduces the bulk temperature of unmanned plane, heat emission hole, can accelerate heat Distribute, more quickly reduce bulk temperature.

Claims (5)

1. a kind of unmanned plane radiating shell, includes unmanned electric motor, it is characterised in that:Outside the unmanned electric motor Side is provided with radiating shell, and the radiating shell is cylindrical structure, and it is hollow-core construction that it is internal, the upper end of the radiating shell The left and right sides is both provided with water inlet, and water outlet, the radiating shell are both provided with left and right sides of the lower end of the radiating shell On be evenly arranged with multiple heat emission holes.
A kind of 2. unmanned plane radiating shell according to claim 1, it is characterised in that:The heat emission hole is cylindrical type groove Structure.
A kind of 3. unmanned plane radiating shell according to claim 1, it is characterised in that:Radiation shell around the heat emission hole Internal portion is hollow pipe structure, and mutual unicom.
A kind of 4. unmanned plane radiating shell according to claim 1, it is characterised in that:The material of the radiating shell is poly- Mutual-phenenyl two acid bromide two alcohol ester.
A kind of 5. unmanned plane radiating shell according to claim 1, it is characterised in that:The radiating shell is set in nobody On the shell of motor.
CN201720949198.7U 2017-08-01 2017-08-01 A kind of unmanned plane radiating shell Active CN207234585U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720949198.7U CN207234585U (en) 2017-08-01 2017-08-01 A kind of unmanned plane radiating shell

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720949198.7U CN207234585U (en) 2017-08-01 2017-08-01 A kind of unmanned plane radiating shell

Publications (1)

Publication Number Publication Date
CN207234585U true CN207234585U (en) 2018-04-13

Family

ID=61856202

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720949198.7U Active CN207234585U (en) 2017-08-01 2017-08-01 A kind of unmanned plane radiating shell

Country Status (1)

Country Link
CN (1) CN207234585U (en)

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CP03 Change of name, title or address

Address after: Xihua East Road, Changping County of Zhoukou City, Henan province 466600

Co-patentee after: HENAN KUNONG AVIATION PLANT PROTECTION TECHNOLOGY Co.,Ltd.

Patentee after: Xihua Jiuxiang UAV Industrial Park Operation Co.,Ltd.

Co-patentee after: SHENZHEN KUNONG UAV INDUSTRIAL DEVELOPMENT AND APPLICATION Co.,Ltd.

Address before: 466600 east section of Changping Road, Xihua county, Zhoukou City, Zhoukou City, Henan Province

Co-patentee before: HENAN KUNONG AVIATION PLANT PROTECTION TECHNOLOGY Co.,Ltd.

Patentee before: XIHUA KUNONG UAV INDUSTRIAL PARK OPERATION Co.,Ltd.

Co-patentee before: SHENZHEN KUNONG UAV INDUSTRIAL DEVELOPMENT AND APPLICATION Co.,Ltd.

CP03 Change of name, title or address
TR01 Transfer of patent right

Effective date of registration: 20200703

Address after: 518000 Guangdong Shenzhen Baoan District Fuhai street Xintian community Fu'an two phase industrial city factory building 3 1 stories.

Patentee after: WuJie Intelligent Technology (Shenzhen) Co.,Ltd.

Address before: Xihua East Road, Changping County of Zhoukou City, Henan province 466600

Co-patentee before: HENAN KUNONG AVIATION PLANT PROTECTION TECHNOLOGY Co.,Ltd.

Patentee before: Xihua Jiuxiang UAV Industrial Park Operation Co.,Ltd.

Co-patentee before: SHENZHEN KUNONG UAV INDUSTRIAL DEVELOPMENT AND APPLICATION Co.,Ltd.

TR01 Transfer of patent right