CN110435899A - The mounting structure of electron speed regulator in a kind of unmanned plane - Google Patents
The mounting structure of electron speed regulator in a kind of unmanned plane Download PDFInfo
- Publication number
- CN110435899A CN110435899A CN201910603975.6A CN201910603975A CN110435899A CN 110435899 A CN110435899 A CN 110435899A CN 201910603975 A CN201910603975 A CN 201910603975A CN 110435899 A CN110435899 A CN 110435899A
- Authority
- CN
- China
- Prior art keywords
- speed regulator
- electron speed
- heat
- unmanned plane
- structural body
- 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
- 229920001821 foam rubber Polymers 0.000 claims abstract description 7
- 238000009434 installation Methods 0.000 claims description 12
- 239000000463 material Substances 0.000 claims description 10
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 4
- 239000000741 silica gel Substances 0.000 claims description 4
- 229910002027 silica gel Inorganic materials 0.000 claims description 4
- 239000003973 paint Substances 0.000 claims description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 2
- 229910052802 copper Inorganic materials 0.000 claims description 2
- 239000010949 copper Substances 0.000 claims description 2
- 239000002184 metal Substances 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 6
- 239000000428 dust Substances 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000032683 aging Effects 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- QRJOYPHTNNOAOJ-UHFFFAOYSA-N copper gold Chemical compound [Cu].[Au] QRJOYPHTNNOAOJ-UHFFFAOYSA-N 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- 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
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Dc Machiner (AREA)
- Motor Or Generator Current Collectors (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of mounting structures of electron speed regulator in unmanned plane, belong to air vehicle technique field.The mounting structure of electron speed regulator in this unmanned plane, including the structural body with rectangular enclosure, the inner upper of the structural body is fixed with buckle, electron speed regulator is provided with below the buckle, the top two sides of the electron speed regulator pass through bolt and are connected with buckle, the lower inside of the structural body is connected with heat-conducting layer, and the bottom side of the structural body, which is connected by a hinge, commutator segment, is connected with foam-rubber cushion and heat conducting bar between the commutator segment and heat-conducting layer.The present invention is provided with commutator segment, heat-conducting layer and heat conducting bar, when user is when using this kind of mounting structure, electron speed regulator can be first mounted on to the inside of structural body by bolt and buckle, so that electron speed regulator is located at the confined space of a safety with this, while passing through the outer gas stream passed through on commutator segment and radiating to electron speed regulator.
Description
Technical field
The invention belongs to air vehicle technique fields, are related to a kind of unmanned plane, electron speed regulator in especially a kind of unmanned plane
Mounting structure.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, without cockpit on machine, but the equipment such as presetting apparatus are installed, ground staff passes through remotely monitored sensor etc.
Equipment tracks it, is positioned, is remotely controlled, telemetering and Digital Transmission, can be reused several times, and aerial reconnaissance, prison are widely used in
It surveys and takes photo by plane.
The mounting structure of electron speed regulator in existing unmanned plane, in order to radiate when working electron speed regulator
When, it is all to be mounted on electron speed regulator is directly exposed outer or partly bury installation in the structure mostly, but this exposed installation
Mode not only increases the flight resistance of unmanned plane when in use, and electron speed regulator is easily caused to damage because of rainwater dust,
To largely effecting on the service life of electron speed regulator, and installation is then higher to surrounding structure intensity requirement when partly burying, and its heat
Radiation may act on adjacent structure, the aging of material be caused, to influence the working condition of electron speed regulator.
Summary of the invention
The purpose of the present invention is there is the above problem in view of the prior art, electron speed regulator in a kind of unmanned plane is proposed
Mounting structure cause electronics tune to solve to propose electron speed regulator exposed installation increase flight resistance in above-mentioned background technique
Fast device is damaged because of rainwater dust, and semi-buried higher to material requirements, heat radiation easily causes aging to adjacent material, influences electronics
The problems such as behaviour in service of governor.
Object of the invention can be realized by the following technical scheme: the installation knot of electron speed regulator in a kind of unmanned plane
Structure, including the structural body with rectangular enclosure, the inner upper of the structural body is fixed with buckle, the lower section of the buckle
It is provided with electron speed regulator, the top two sides of the electron speed regulator pass through bolt and are connected with buckle, the structural body
Lower inside be connected with heat-conducting layer, and the top of the heat-conducting layer is in contact with electron speed regulator, the bottom of the structural body
Portion side, which is connected by a hinge, commutator segment, foam-rubber cushion and heat conducting bar is connected between the commutator segment and heat-conducting layer, and described
The top of heat conducting bar is in contact with heat-conducting layer, and the bottom end of the heat conducting bar is in contact with commutator segment.
In above-mentioned unmanned plane in the mounting structure of electron speed regulator, the top two sides of the structural body are fixed respectively
It is connected with installation bolt.
In above-mentioned unmanned plane in the mounting structure of electron speed regulator, the both sides of the structural body are fixed respectively to be connected
It is connected to connector.
In above-mentioned unmanned plane in the mounting structure of electron speed regulator, the bottom of the commutator segment is uniformly coated with one layer
Anti-decaying paint.
In above-mentioned unmanned plane in the mounting structure of electron speed regulator, the making material of the heat-conducting layer includes thermal conductive silicon
Glue.
In above-mentioned unmanned plane in the mounting structure of electron speed regulator, the making material of the heat conducting bar includes copper gold
Belong to.
In above-mentioned unmanned plane in the mounting structure of electron speed regulator, the bottom of the commutator segment is in " arc ", and institute
The side for stating commutator segment is connected by fastening bolt with structural body.
In above-mentioned unmanned plane in the mounting structure of electron speed regulator, the bolt is adapted with buckle.
Compared with prior art, the invention has the following advantages that
1, the present invention is provided with hinge, commutator segment, heat-conducting layer and heat conducting bar, when user is using this kind of mounting structure
When, electron speed regulator can be first mounted on to the inside of structural body by bolt and buckle, so that electron speed regulator is located at one with this
A safe confined space can effectively completely cut off rainwater dust foreign matter, and carry out waterproof to electron speed regulator to a certain extent
Protection increases the flight resistance of unmanned plane when to avoiding the exposed installation of electron speed regulator, and causes electron speed regulator because of rainwater
Dust and damage, to greatly increase the service life of electron speed regulator；
2, the present invention is provided with hinge, commutator segment, heat-conducting layer and heat conducting bar, after electron speed regulator installs, bottom
It is in contact with the heat-conducting layer in structural body, and the bottom of heat-conducting layer is in contact by heat conducting bar with commutator segment, and due to thermally conductive
The making material of layer includes heat conductive silica gel, therefore electron speed regulator can directly will at work by heat conductive silica gel and heat conducting bar
Heat is transferred out to the commutator segment of wing, the radiating efficiency of electron speed regulator is greatly improved with this, and due to structural body
Installation site can protect electron speed regulator far from the wireless line electricity transmitting module of unmanned plane, avoid electron speed regulator
Normal work be interfered.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is schematic diagram of internal structure of the invention；
Fig. 3 is the partial structurtes enlarged diagram in Fig. 2 at A.
In figure: 1, structural body；2, bolt is installed；3, connector；4, it buckles；5, electron speed regulator；6, hinge；7, it rectifies
Piece；8, heat-conducting layer；9, heat conducting bar；10, foam-rubber cushion；11, fastening bolt；12, bolt.
Specific embodiment
Following is a specific embodiment of the present invention in conjunction with the accompanying drawings, technical scheme of the present invention will be further described,
However, the present invention is not limited to these examples.
As shown in Figure 1-3, in a kind of unmanned plane electron speed regulator mounting structure, including the structure sheet with rectangular enclosure
Body 1, installation bolt 2, connector 3, buckle 4, electron speed regulator 5, hinge 6, commutator segment 7, heat-conducting layer 8, heat conducting bar 9, foam-rubber cushion
10, fastening bolt 11 and bolt 12, the inner upper of the structural body 1 are fixed with buckle 4, the lower section setting of the buckle 4
There is electron speed regulator 5, the top two sides of the electron speed regulator 5 pass through bolt 12 and are connected with buckle 4, the structural body
1 lower inside is connected with heat-conducting layer 8, and the top of the heat-conducting layer 8 is in contact with electron speed regulator 5, the structural body 1
Bottom side commutator segment 7 is connected with by hinge 6, the top of the commutator segment 7 is connected separately with foam-rubber cushion 10 and heat conducting bar
9, and the top of the heat conducting bar 9 is in contact with heat-conducting layer 8, when working convenient for heat conducting bar 9 and heat-conducting layer 8 electron speed regulator 5
The heat of generation is conducted.
As illustrated in fig. 1 and 2, the top two sides of structural body 1, which have been respectively fixedly connected with, installs bolt 2, and the two of structural body 1
Side is fixedly connected with connector 3 respectively, and structural body 1 is mounted on nothing by installation bolt 2 and connector 3 convenient for user
Inside man-machine wing.The bottom of the commutator segment 7 is uniformly coated with one layer of anti-decaying paint, avoids commutator segment 7 in prolonged use
Rust corrosion occurs in the process, to greatly increase the service life of commutator segment 7.
As illustrated in fig. 1 and 2, the making material of the heat-conducting layer 8 includes heat conductive silica gel, the making material of the heat conducting bar 9
Including copper metal, convenient for increasing the thermal conductivity of heat-conducting layer 8 and heat conducting bar 9, so that its heat that can generate electron speed regulator 5 is fast
In speed conduction to commutator segment 7.The bottom of the commutator segment 7 is in " arc ", and the side of the commutator segment 7 passes through fastening bolt
11 are connected with structural body 1, and convenient for reducing the air drag of commutator segment 7, and the setting of fastening bolt 11 can help to whole
Flow 7 is fixed.
As shown in Figures 2 and 3, the bolt 12 is adapted with buckle 4, and electron speed regulator 5 is passed through bolt convenient for user
In 12 insertion buckles 4, electron speed regulator 5 is quick installed to the inside of structural body 1 with this.
Working principle: firstly, when user is when using this kind of mounting structure, can first the outer surface to structural body 1 into
Row detection, it is ensured that the outer surface of structural body 1 is intact, avoids structural body 1 that accident occurs when in use, when detecting
Afterwards, using the overturning opening commutator segment 7 of hinge 6 can be being passed through, electron speed regulator 5 by bolt 12 and is buckled 4 for electronics with this
The inside of 5 mounting structure ontology 1 of governor, after electron speed regulator 5 installs, heat-conducting layer 8 can be applied to electronics by user
The bottom of governor 5, after the painting of heat-conducting layer 8 wipes, user can overturn commutator segment 7 again by hinge 6, make commutator segment with this
7 are closed, and after commutator segment 7 is closed, user can be fixed commutator segment 7 by fastening bolt 11, when commutator segment 7 is solid
After setting, structural body 1 can be mounted on the bottom of wing by user by installation bolt 2 and connector 3, when structural body 1
After installing, when electron speed regulator 5 generates heat at work, heat can be transferred out by heat-conducting layer 8 and heat conducting bar 9 to machine
On the commutator segment 7 of the wing, outer gas stream when commutator segment 7 passes through unmanned plane during flying radiates, and increases electron speed regulator 5 with this
Radiating efficiency.
Specific embodiment described herein is only an example for the spirit of the invention.The neck of technology belonging to the present invention
The technical staff in domain can make various modifications or additions to the described embodiments or replace by a similar method
In generation, however, it does not deviate from the spirit of the invention or beyond the scope of the appended claims.
Although 1, structural body is used more herein；2, bolt is installed；3, connector；4, it buckles；5, electronic speed regulation
Device；6, hinge；7, commutator segment；8, heat-conducting layer；9, heat conducting bar；10, foam-rubber cushion；11, fastening bolt；12, the terms such as bolt, but simultaneously
A possibility that being not excluded for using other terms.The use of these items is only for be more convenient to describe and explain sheet of the invention
Matter；Being construed as any additional limitation is disagreed with spirit of that invention.
Claims (8)
1. the mounting structure of electron speed regulator in a kind of unmanned plane, including the structural body (1) with rectangular enclosure, feature exists
In: the inner upper of the structural body (1) is fixed with buckle (4), is provided with electron speed regulator below the buckle (4)
(5), the top two sides of the electron speed regulator (5) pass through bolt (12) and are connected with buckle (4), the structural body (1)
Lower inside be connected with heat-conducting layer (8), and the top of the heat-conducting layer (8) is in contact with electron speed regulator (5), the structure
The bottom side of ontology (1) is connected with commutator segment (7) by hinge (6), is connected between the commutator segment (7) and heat-conducting layer (8)
There are foam-rubber cushion (10) and heat conducting bar (9), and the top of the heat conducting bar (9) is in contact with heat-conducting layer (8), the heat conducting bar (9)
Bottom end be in contact with commutator segment (7).
2. the mounting structure of electron speed regulator in unmanned plane according to claim 1, which is characterized in that the structural body
(1) top two sides have been respectively fixedly connected with installation bolt (2).
3. the mounting structure of electron speed regulator in unmanned plane according to claim 1, which is characterized in that the structural body
(1) both sides are fixedly connected with connector (3) respectively.
4. the mounting structure of electron speed regulator in unmanned plane according to claim 1, which is characterized in that the commutator segment
(7) bottom is uniformly coated with one layer of anti-decaying paint.
5. the mounting structure of electron speed regulator in unmanned plane according to claim 1, which is characterized in that the heat-conducting layer
(8) making material includes heat conductive silica gel.
6. the mounting structure of electron speed regulator in unmanned plane according to claim 1, which is characterized in that the heat conducting bar
(9) making material includes copper metal.
7. the mounting structure of electron speed regulator in unmanned plane according to claim 1, which is characterized in that the commutator segment
(7) bottom is in " arc ", and the side of the commutator segment (7) is connected by fastening bolt (11) with structural body (1).
8. the mounting structure of electron speed regulator in unmanned plane according to claim 1, which is characterized in that the bolt (12)
It is adapted with buckle (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910603975.6A CN110435899B (en) | 2019-07-05 | 2019-07-05 | Mounting structure of electronic governor in unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910603975.6A CN110435899B (en) | 2019-07-05 | 2019-07-05 | Mounting structure of electronic governor in unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110435899A true CN110435899A (en) | 2019-11-12 |
| CN110435899B CN110435899B (en) | 2020-11-20 |
Family
ID=68429096
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910603975.6A Active CN110435899B (en) | 2019-07-05 | 2019-07-05 | Mounting structure of electronic governor in unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110435899B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116002052A (en) * | 2022-12-14 | 2023-04-25 | 嘉兴安行信息科技有限公司 | Plant protection unmanned aerial vehicle with multi-functional atomizer |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100258088A1 (en) * | 2009-07-01 | 2010-10-14 | Harrison Edward H | Speed and position sensing device for emd two-cycle diesel engines |
| CN206821134U (en) * | 2017-04-24 | 2017-12-29 | 深圳市大疆创新科技有限公司 | Electron speed regulator and unmanned plane |
| CN208127028U (en) * | 2018-05-08 | 2018-11-20 | 江苏华锋新能源科技有限公司 | A kind of capacitor mounting box of high efficiency and heat radiation |
| CN109720558A (en) * | 2019-02-19 | 2019-05-07 | 深圳市翔农创新科技有限公司 | The unmanned plane of layout is adjusted based on electricity |
| CN210246959U (en) * | 2019-09-16 | 2020-04-03 | 咸阳师范学院 | Wireless router mounting box |
-
2019
- 2019-07-05 CN CN201910603975.6A patent/CN110435899B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100258088A1 (en) * | 2009-07-01 | 2010-10-14 | Harrison Edward H | Speed and position sensing device for emd two-cycle diesel engines |
| CN206821134U (en) * | 2017-04-24 | 2017-12-29 | 深圳市大疆创新科技有限公司 | Electron speed regulator and unmanned plane |
| CN208127028U (en) * | 2018-05-08 | 2018-11-20 | 江苏华锋新能源科技有限公司 | A kind of capacitor mounting box of high efficiency and heat radiation |
| CN109720558A (en) * | 2019-02-19 | 2019-05-07 | 深圳市翔农创新科技有限公司 | The unmanned plane of layout is adjusted based on electricity |
| CN210246959U (en) * | 2019-09-16 | 2020-04-03 | 咸阳师范学院 | Wireless router mounting box |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116002052A (en) * | 2022-12-14 | 2023-04-25 | 嘉兴安行信息科技有限公司 | Plant protection unmanned aerial vehicle with multi-functional atomizer |
| CN116002052B (en) * | 2022-12-14 | 2024-05-14 | 嘉兴安行信息科技有限公司 | Plant protection unmanned aerial vehicle with multi-functional atomizer |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110435899B (en) | 2020-11-20 |
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