CN106275366A - A kind of small-sized unmanned plane of excellent radiation performance - Google Patents

A kind of small-sized unmanned plane of excellent radiation performance Download PDF

Info

Publication number
CN106275366A
CN106275366A CN201610770988.9A CN201610770988A CN106275366A CN 106275366 A CN106275366 A CN 106275366A CN 201610770988 A CN201610770988 A CN 201610770988A CN 106275366 A CN106275366 A CN 106275366A
Authority
CN
China
Prior art keywords
electricity
adjusted
installing plate
adjusts
fuselage
Prior art date
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.)
Granted
Application number
CN201610770988.9A
Other languages
Chinese (zh)
Other versions
CN106275366B (en
Inventor
周烈
崔艳鸿
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.)
Beijing Qizheng Polytron Technologies Inc A Few Dollars
Original Assignee
Beijing Qizheng Polytron Technologies Inc A Few Dollars
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Beijing Qizheng Polytron Technologies Inc A Few Dollars filed Critical Beijing Qizheng Polytron Technologies Inc A Few Dollars
Priority to CN201610770988.9A priority Critical patent/CN106275366B/en
Publication of CN106275366A publication Critical patent/CN106275366A/en
Application granted granted Critical
Publication of CN106275366B publication Critical patent/CN106275366B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00Constructional details common to different types of electric apparatus
    • H05K7/20Modifications to facilitate cooling, ventilating, or heating
    • H05K7/20009Modifications to facilitate cooling, ventilating, or heating using a gaseous coolant in electronic enclosures
    • H05K7/20127Natural convection
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00Constructional details common to different types of electric apparatus
    • H05K7/20Modifications to facilitate cooling, ventilating, or heating
    • H05K7/20845Modifications to facilitate cooling, ventilating, or heating for automotive electronic casings

Landscapes

  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)

Abstract

The invention discloses the small-sized unmanned plane of a kind of excellent radiation performance, it is characterized in that, electricity adjusts assembly to be arranged on inside body nacelle, this electricity adjusts assembly to include: electricity adjusts installing plate, heat conductive silica gel, electricity mediation electricity to adjust and install lid (side has vent), electricity is adjusted installing plate to glued joint and is fixed under fuselage on eyelid covering, heat conductive silica gel and electricity are adjusted to be sequentially placed and are adjusted on installing plate in electricity, electricity adjusts installation lid and electricity to adjust installing plate fastening, and after installing, electricity is adjusted to install and covered through eyelid covering on fuselage and expose vent.The invention have benefit that: electricity is adjusted and is arranged on inside body nacelle by (1), the temperature making interior of aircraft cavity keeps relatively small temperature rise, and a good environment has been built in the temperature sensor flown in control and remaining hardware for internal body;(2) heat produced during the air-flow band leakage of electricity tune work formed at eyelid covering on eyelid covering and fuselage under fuselage when utilizing aircraft flight so that life-span and the using effect of the components and parts that electricity is adjusted get a promotion.

Description

A kind of small-sized unmanned plane of excellent radiation performance
Technical field
The present invention relates to a kind of small-sized unmanned plane, be specifically related to the small-sized unmanned plane of a kind of excellent radiation performance, belong to In unmanned air vehicle technique field.
Background technology
Small-sized unmanned plane power current is adjusted and is installed in internal body, and heat dispersion is poor, causes heat build-up, in aircraft Portion's cavity temperature raises, and not only makes the use flying temperature sensor and remaining hardware in control be affected, also makes electricity tune Life-span and the using effect of components and parts are affected.
Summary of the invention
For solving the deficiencies in the prior art, it is an object of the invention to provide the small-sized unmanned of a kind of excellent radiation performance Machine.
In order to realize above-mentioned target, the present invention adopts the following technical scheme that:
The small-sized unmanned plane of a kind of excellent radiation performance, it is characterised in that it is short that electricity adjusts assembly (1) to be arranged on body power Inside cabin, aforementioned electricity adjusts assembly (1) to include: electricity is adjusted installing plate (11), heat conductive silica gel (12), electricity to adjust (13) and electricity to adjust and installed lid (14), wherein, electricity adjusts the side installing lid (14) to have vent,
Aforementioned electricity is adjusted installing plate (11) to glued joint and is fixed on eyelid covering under fuselage (2), and heat conductive silica gel (12) and electricity adjust (13) to depend on The secondary electricity that is positioned over is adjusted on installing plate (11), and electricity is adjusted and installed lid (14) and threaded pretension with electricity tune installing plate (11), installs Its electricity tune of electricity tune assembly (1) finished is installed lid (14) and is passed eyelid covering (3) on fuselage, and exposes vent, and electricity tune assembly (1) utilizes The air-flow band leakage of electricity that during aircraft flight, on eyelid covering (2) and fuselage, eyelid covering (3) place is formed under fuselage produces when adjusting (13) work Heat.
The small-sized unmanned plane of aforesaid excellent radiation performance, it is characterised in that aforementioned electricity adjusts installing plate (11) and electricity to adjust Installing lid (14) all uses aluminum alloy materials to make.
The small-sized unmanned plane of aforesaid excellent radiation performance, it is characterised in that aforementioned electricity is adjusted (13) and electricity to adjust and installed lid (14) it is screwed and links together.
The invention have benefit that:
(1) electricity tune is arranged on inside body nacelle, makes the temperature rise that the temperature holding of interior of aircraft cavity is relatively small, A good environment has been built in the temperature sensor flown in control and remaining hardware for internal body;
(2) produce during the air-flow band leakage of electricity tune work formed at eyelid covering on eyelid covering and fuselage under fuselage when utilizing aircraft flight Raw heat so that life-span and the using effect of the components and parts that electricity is adjusted get a promotion.
Accompanying drawing explanation
Fig. 1 is the structural representation that electricity adjusts assembly;
Fig. 2 is that electricity adjusts assembly scheme of installation on small-sized unmanned plane.
The implication of reference in figure: 1-electricity adjusts eyelid covering, the tune installation of 11-electricity on eyelid covering, 3-fuselage under assembly, 2-fuselage Plate, 12-heat conductive silica gel, 13-electricity are adjusted, 14-electricity is adjusted and installed lid.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the present invention made concrete introduction.
Seeing figures.1.and.2, the small-sized unmanned plane of the excellent radiation performance of the present invention, its electricity adjusts assembly 1 to be arranged on body Inside nacelle.
Electric tune assembly 1 includes: electricity adjusts installing plate 11, heat conductive silica gel 12, electricity tune 13 and electric tune to install lid 14.Wherein, electricity is adjusted The side installing lid 14 has vent.
Electricity is adjusted installing plate 11 and electricity tune to install lid 14 all employing aluminum alloy materials and is made.
Installation method: first electricity is adjusted installing plate 11 glued joint and is fixed under fuselage on eyelid covering 2, then by eyelid covering 3 on fuselage Glued joint matched moulds with eyelid covering under fuselage 2, next heat conductive silica gel 12 is placed on electricity and adjusts on installing plate 11, electricity tune 13 is installed, finally Electricity is adjusted and lid 14 is installed adjusts installing plate 11 to threaded pretension with electricity, electricity adjust 13 and electricity adjust to install and cover 14 and be screwed connection Together.
Electricity its electricity of tune assembly 1 installed adjusts installation lid 14 to pass eyelid covering 3 on fuselage, and exposes vent, and such one Come, when electricity adjusts assembly 1 just can utilize aircraft flight under fuselage the air-flow band leakage of electricity of formation at eyelid covering 3 on eyelid covering 2 and fuselage The heat produced when adjusting 13 work.
Electricity tune 13 has been arranged on inside body nacelle by the present invention, makes the temperature of interior of aircraft cavity maintain relatively Little temperature rise, a good environment has been built in the temperature sensor flown in control and remaining hardware for internal body.
Additionally, due to the heat that produces when adjusting 13 work of electricity by during aircraft flight under fuselage on eyelid covering and fuselage at eyelid covering The air-flow formed is taken away, so that electricity adjusts the life-span of the components and parts of 13 and using effect to be improved.
Become it should be noted that above-described embodiment limits the present invention, all employing equivalents or equivalence the most in any form The technical scheme that the mode changed is obtained, all falls within protection scope of the present invention.

Claims (3)

1. the small-sized unmanned plane of an excellent radiation performance, it is characterised in that electricity adjusts assembly (1) to be arranged on body nacelle Inside, described electricity tune assembly (1) including: electricity adjusts installing plate (11), heat conductive silica gel (12), electricity to adjust (13) and electric tune to install lid (14), wherein, electricity adjusts the side installing lid (14) to have vent,
Described electricity is adjusted installing plate (11) to glued joint and is fixed on eyelid covering under fuselage (2), and heat conductive silica gel (12) and electricity adjust (13) to put successively Being placed in electricity and adjust on installing plate (11), electricity is adjusted and is installed lid (14) and threaded pretension with electricity tune installing plate (11), installs Its electricity of electricity tune assembly (1) adjusts installation lid (14) to pass eyelid covering (3) on fuselage, and exposes vent, and electricity adjusts assembly (1) to utilize aircraft The heat that the air-flow band leakage of electricity that during flight, on eyelid covering (2) and fuselage, eyelid covering (3) place is formed under fuselage produces when adjusting (13) work.
The small-sized unmanned plane of excellent radiation performance the most according to claim 1, it is characterised in that described electricity adjusts installing plate (11) lid (14) is installed all uses aluminum alloy materials to make with electricity tune.
The small-sized unmanned plane of excellent radiation performance the most according to claim 1, it is characterised in that described electricity adjust (13) and Electricity is adjusted installation lid (14) to be screwed and is linked together.
CN201610770988.9A 2016-08-30 2016-08-30 A kind of small-sized unmanned plane of excellent radiation performance Active CN106275366B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610770988.9A CN106275366B (en) 2016-08-30 2016-08-30 A kind of small-sized unmanned plane of excellent radiation performance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610770988.9A CN106275366B (en) 2016-08-30 2016-08-30 A kind of small-sized unmanned plane of excellent radiation performance

Publications (2)

Publication Number Publication Date
CN106275366A true CN106275366A (en) 2017-01-04
CN106275366B CN106275366B (en) 2018-05-04

Family

ID=57675856

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610770988.9A Active CN106275366B (en) 2016-08-30 2016-08-30 A kind of small-sized unmanned plane of excellent radiation performance

Country Status (1)

Country Link
CN (1) CN106275366B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107140222A (en) * 2017-04-18 2017-09-08 河南翱翔多旋翼科技有限公司 A kind of anti-water power of many rotor plant protection unmanned planes is adjusted
CN107585310A (en) * 2017-07-21 2018-01-16 泰华伟业科技有限责任公司 A kind of nobody electromechanical cold cooling system of water transfer of plant protection
WO2022062194A1 (en) * 2020-09-27 2022-03-31 深圳市大疆创新科技有限公司 Unmanned aerial vehicle

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203353030U (en) * 2013-07-16 2013-12-18 成都新洲航空设备有限责任公司 ESC heat dissipation device for aircraft
CN205203388U (en) * 2015-10-30 2016-05-04 湖北易瓦特科技股份有限公司 Power system for unmanned aerial vehicle
CN205396558U (en) * 2016-03-21 2016-07-27 零度智控(北京)智能科技有限公司 Unmanned aerial vehicle of motor device and applied this motor device
CN205952283U (en) * 2016-08-30 2017-02-15 北京奇正数元科技股份有限公司 Good light unmanned aerial vehicle of heat dispersion

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107140222A (en) * 2017-04-18 2017-09-08 河南翱翔多旋翼科技有限公司 A kind of anti-water power of many rotor plant protection unmanned planes is adjusted
CN107585310A (en) * 2017-07-21 2018-01-16 泰华伟业科技有限责任公司 A kind of nobody electromechanical cold cooling system of water transfer of plant protection
WO2022062194A1 (en) * 2020-09-27 2022-03-31 深圳市大疆创新科技有限公司 Unmanned aerial vehicle

Also Published As

Publication number Publication date
CN106275366B (en) 2018-05-04

Similar Documents

Publication Publication Date Title
CN204489178U (en) High efficiency and heat radiation unmanned plane
CN106275366A (en) A kind of small-sized unmanned plane of excellent radiation performance
JP2019177865A5 (en)
CN205952283U (en) Good light unmanned aerial vehicle of heat dispersion
CN108146648A (en) A kind of unattended unmanned plane base station
CN205801511U (en) A kind of aircraft and power set, Power Component
CN205044948U (en) Solar energy unmanned aerial vehicle
CN113716019B (en) Battery array capable of being quickly assembled and disassembled, aircraft wing structure and manufacturing method thereof
CN106394858A (en) Folded six-rotor unmanned plane
CN206557371U (en) Individual soldier's mobile model unmanned plane breaks through trapping system
CN205574251U (en) Organism is four rotor unmanned aerial vehicle of streamlined
CN209617488U (en) A kind of modularization head
CN205418067U (en) Aircraft afterbody radome fairing
CN205418094U (en) Push -button aircraft
CN108082519A (en) One kind is suitable for small drone landing positioning charging platform
CN110435899B (en) Mounting structure of electronic governor in unmanned aerial vehicle
CN205406707U (en) Aircraft antenna setting support and quick -witted connection structure who carries on back
CN204489185U (en) Possesses the unmanned plane of water-proof function
CN205366073U (en) Integrated into one piece unmanned aerial vehicle carbon fiber horn
CN209693339U (en) One kind being tethered at unmanned aerial vehicle onboard power-supply radiator
CN211671671U (en) Aircraft flare spreader
CN206939075U (en) A kind of strong unmanned plane of endurance
US10604227B2 (en) Solar panel window assembly and method of forming the same
CN207354799U (en) Electric-regulating device and there is its unmanned plane
CN112407279A (en) Modular patrol and use unmanned aerial vehicle

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant