CN205952283U - Good light unmanned aerial vehicle of heat dispersion - Google Patents
Good light unmanned aerial vehicle of heat dispersion Download PDFInfo
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- CN205952283U CN205952283U CN201620996949.6U CN201620996949U CN205952283U CN 205952283 U CN205952283 U CN 205952283U CN 201620996949 U CN201620996949 U CN 201620996949U CN 205952283 U CN205952283 U CN 205952283U
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- electricity
- adjusts
- fuselage
- lid
- transferred
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Abstract
The utility model discloses a good light unmanned aerial vehicle of heat dispersion, its characterized in that, electricity transfer the unit mount inside organism power nacelle, and the electricity transfers the subassembly to include: the electricity is transferred mounting panel, series thermal silica, electricity to mediate the electricity and is transferred installation lid (the side has the vent), and the electricity is transferred the mounting panel to splice and is fixed under the fuselage on the covering, and series thermal silica and electric accent are placed in proper order on the mounting panel is transferred to the electricity, and the electricity transfers installation lid and electricity to transfer the mounting panel lock, and the installation finishes the back electricity and transfers the installation lid to pass on the fuselage covering and expose the vent. The utility model has the beneficial effects of: (1 )Transferring the electricity and installing inside organism power nacelle, the temperature that makes the inside cavity of aircraft keeps relatively little temperature rise, has built a fine environment with all the other hardware for the temperature sensor who flies in the accuse of organism inside, (2 )The heat that the electricity transferred the during operation to produce is taken away to the air current of locating to form at fuselage skin when utilizing aircraft flight for the life -span and the result of use of the components and parts that the electricity was transferred get a promotion.
Description
Technical field
This utility model be related to a kind of small-sized unmanned plane and in particular to a kind of excellent radiation performance small-sized unmanned
Machine, belongs to 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, leads to heat build-up, in aircraft
Portion's cavity temperature raises, not only so that the temperature sensor flying in control is affected with the use of remaining hardware, also so that electricity is adjusted
The life-span of components and parts and using effect are affected.
Utility model content
For solving the deficiencies in the prior art, the purpose of this utility model is to provide a kind of the small-sized of excellent radiation performance
Unmanned plane.
In order to realize above-mentioned target, this utility model adopts the following technical scheme that：
A kind of small-sized unmanned plane of excellent radiation performance it is characterised in that electricity to adjust assembly (1) to be arranged on body power short
Inside cabin, aforementioned electricity adjusts assembly (1) to include：Electricity adjusts installing plate (11), heat conductive silica gel (12), electricity to adjust (13) and electricity to adjust and install lid
(14), wherein, electricity adjusts the side installing lid (14) to have vent,
Aforementioned electricity adjust installing plate (11) glued joint be fixed on eyelid covering under fuselage (2), heat conductive silica gel (12) and electricity tune (13) according to
The secondary electricity that is positioned over is adjusted on installing plate (11), and electricity is adjusted and installed lid (14) and threadeded pretension with electricity tune installing plate (11), installs
Complete electricity adjusts its electricity of assembly (1) to adjust installation lid (14) to pass through eyelid covering (3) on fuselage, and exposes vent, and electricity adjusts assembly (1) utilization
The air-flow band leakage of electricity that on eyelid covering (2) and fuselage under fuselage during aircraft flight, eyelid covering (3) place is formed is adjusted and is produced during (13) work
Heat.
The small-sized unmanned plane of aforesaid excellent radiation performance is it is characterised in that aforementioned electricity adjusts installing plate (11) and electricity to adjust
Lid (14) is installed all make using aluminum alloy materials.
The small-sized unmanned plane of aforesaid excellent radiation performance is it is characterised in that aforementioned electricity adjusts (13) and electricity to adjust and install lid
(14) it is screwed and link together.
Of the present utility model it is beneficial in that：
(1) electricity tune is arranged on inside body nacelle, makes the temperature of interior of aircraft cavity keep relatively small temperature rise,
It is that the temperature sensor in the winged control of internal body has built a good environment with remaining hardware；
(2) produce during the air-flow band leakage of electricity tune work being formed at eyelid covering on eyelid covering and fuselage under fuselage when utilizing aircraft flight
Raw heat is so that the life-span of components and parts of electricity tune and using effect get a promotion.
Brief description
Fig. 1 is the structural representation that electricity adjusts assembly；
Fig. 2 is that electricity adjusts scheme of installation on small-sized unmanned plane for the assembly.
The implication of in figure reference：1- electricity adjusts eyelid covering on eyelid covering under assembly, 2- fuselage, 3- fuselage, 11- electricity to adjust and install
Plate, 12- heat conductive silica gel, 13- electricity are adjusted, 14- electricity is adjusted and installed lid.
Specific embodiment
Below in conjunction with the drawings and specific embodiments, this utility model is made with specific introduction.
See figures.1.and.2, the small-sized unmanned plane of excellent radiation performance of the present utility model, its electricity adjusts assembly 1 to be arranged on
Inside body nacelle.
Electricity adjusts assembly 1 to include：Electricity adjusts installing plate 11, heat conductive silica gel 12, electricity tune 13 and electricity to adjust and install lid 14.Wherein, electricity is adjusted
The side installing lid 14 has vent.
Electricity adjusts installing plate 11 and electricity tune to install lid 14 and all make using aluminum alloy materials.
Installation method：First electricity is adjusted installing plate 11 to glued joint to be fixed on eyelid covering 2 under fuselage, 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 is installed and adjusts 13, 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.
The electricity installing adjusts its electricity of assembly 1 to adjust installation lid 14 to pass through eyelid covering 3 on fuselage, and exposes vent, and such one
Come, electricity adjusts the assembly 1 just can be using the air-flow band leakage of electricity of formation at eyelid covering 3 on eyelid covering 2 and fuselage under fuselage during aircraft flight
Adjust the heat producing during 13 work.
Electricity is adjusted 13 to be arranged on inside body nacelle by this utility model, so that the temperature of interior of aircraft cavity is maintained
Relatively small temperature rise, be internal body winged control in temperature sensor and remaining hardware built a good environment.
Further, since the heats that produce are by eyelid covering on eyelid covering and fuselage under fuselage during aircraft flight when electricity adjusts 13 work
The air-flow being formed is taken away, so that electricity adjusts 13 life-span of components and parts and using effect to be improved.
It should be noted that above-described embodiment does not limit this utility model in any form, all using equivalent or wait
The technical scheme that the mode of effect conversion is obtained, all falls within protection domain of the present utility model.
Claims (3)
1. a kind of small-sized unmanned plane of excellent radiation performance is it is characterised in that electricity adjusts assembly (1) to be arranged on body nacelle
Inside, described electricity adjusts assembly (1) to include：Electricity adjusts installing plate (11), heat conductive silica gel (12), electricity to adjust (13) and electricity to adjust and 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
It is placed in electricity and adjusts on installing plate (11), electricity is adjusted and installed lid (14) and threadeded pretension with electricity tune installing plate (11), installs
Electricity adjusts its electricity of assembly (1) to adjust installation lid (14) to pass through eyelid covering (3) on fuselage, and exposes vent, and electricity adjusts assembly (1) to utilize aircraft
The air-flow band leakage of electricity that on eyelid covering (2) and fuselage under fuselage during flight, eyelid covering (3) place is formed adjusts the heat producing during (13) work.
2. the small-sized unmanned plane of excellent radiation performance according to claim 1 is it is characterised in that described electricity adjusts installing plate
(11) lid (14) is installed and is all made using aluminum alloy materials with electricity tune.
3. excellent radiation performance according to claim 1 small-sized unmanned plane 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 |
|---|---|---|---|
| CN201620996949.6U CN205952283U (en) | 2016-08-30 | 2016-08-30 | Good light unmanned aerial vehicle of heat dispersion |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620996949.6U CN205952283U (en) | 2016-08-30 | 2016-08-30 | Good light unmanned aerial vehicle of heat dispersion |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205952283U true CN205952283U (en) | 2017-02-15 |
Family
ID=57978762
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620996949.6U Active CN205952283U (en) | 2016-08-30 | 2016-08-30 | Good light unmanned aerial vehicle of heat dispersion |
Country Status (1)
| Country | Link |
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| CN (1) | CN205952283U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275366B (en) * | 2016-08-30 | 2018-05-04 | 北京奇正数元科技股份有限公司 | A kind of small-sized unmanned plane of excellent radiation performance |
| WO2018195731A1 (en) * | 2017-04-24 | 2018-11-01 | 深圳市大疆创新科技有限公司 | Operation method of electronic speed controller, electronic speed controller, and unmanned aerial vehicle |
| CN113253606A (en) * | 2021-06-11 | 2021-08-13 | 中国空气动力研究与发展中心低速空气动力研究所 | Calibration box high-pressure air supply and vacuum air suction combined control system and method |
-
2016
- 2016-08-30 CN CN201620996949.6U patent/CN205952283U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275366B (en) * | 2016-08-30 | 2018-05-04 | 北京奇正数元科技股份有限公司 | A kind of small-sized unmanned plane of excellent radiation performance |
| WO2018195731A1 (en) * | 2017-04-24 | 2018-11-01 | 深圳市大疆创新科技有限公司 | Operation method of electronic speed controller, electronic speed controller, and unmanned aerial vehicle |
| CN113253606A (en) * | 2021-06-11 | 2021-08-13 | 中国空气动力研究与发展中心低速空气动力研究所 | Calibration box high-pressure air supply and vacuum air suction combined control system and method |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |