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 PDFInfo
- 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
Links
- 230000005855 radiation Effects 0.000 title claims abstract description 12
- 230000005611 electricity Effects 0.000 claims abstract description 77
- 210000000744 eyelid Anatomy 0.000 claims abstract description 24
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 11
- 239000000741 silica gel Substances 0.000 claims abstract description 9
- 229910002027 silica gel Inorganic materials 0.000 claims abstract description 9
- 238000009434 installation Methods 0.000 claims abstract description 7
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/20009—Modifications to facilitate cooling, ventilating, or heating using a gaseous coolant in electronic enclosures
- H05K7/20127—Natural convection
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/20845—Modifications 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
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.
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)
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)
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 |
-
2016
- 2016-08-30 CN CN201610770988.9A patent/CN106275366B/en active Active
Cited By (3)
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 |