CN206255185U - A kind of dismountable rotor wing unmanned aerial vehicle of horn - Google Patents
A kind of dismountable rotor wing unmanned aerial vehicle of horn Download PDFInfo
- Publication number
- CN206255185U CN206255185U CN201621388943.7U CN201621388943U CN206255185U CN 206255185 U CN206255185 U CN 206255185U CN 201621388943 U CN201621388943 U CN 201621388943U CN 206255185 U CN206255185 U CN 206255185U
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- Prior art keywords
- horn
- locating piece
- frame
- housing
- locating slot
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- 210000002683 foot Anatomy 0.000 claims abstract description 12
- 238000009434 installation Methods 0.000 claims abstract description 6
- 244000273618 Sphenoclea zeylanica Species 0.000 claims description 3
- 238000003780 insertion Methods 0.000 claims description 3
- 230000037431 insertion Effects 0.000 claims description 3
- 241000196324 Embryophyta Species 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000004806 packaging method and process Methods 0.000 description 2
- 238000005070 sampling Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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Abstract
The utility model discloses a kind of dismountable rotor wing unmanned aerial vehicle of horn, including frame, housing, many support feets, many horns, frame is located in housing, horn is through housing and is installed on frame, the sidepiece of frame is provided with multiple horn positioning components, horn positioning component includes lower locating piece and upper locating piece, lower locating piece is fixedly installed in frame and its upper surface is provided with semicircular lower locating slot, upper locating piece is hinged with lower locating piece and its lower surface is provided with semicircular upper locating slot, lower locating slot and upper locating slot surround the location hole being engaged with horn outer surface, the installation end of horn is located in location hole；The upper surface of upper locating piece is provided through the briquetting of housing, and the upper surface of housing is provided with the buckle for compressing or unclamping briquetting.The utility model, the disassembling operations simple and fast of horn, time saving and energy saving, efficiency high.During carrying, horn is entirely removed, unmanned plane main body is separately packed with horn, save space, carry and storage more facilitates.
Description
Technical field
The utility model is related to unmanned plane field, and in particular to a kind of dismountable rotor wing unmanned aerial vehicle of horn.
Background technology
At present, unmanned air vehicle technique is applied to plant protection field comparative maturity, is such as sprayed using unmanned plane, broadcast
The operations such as kind, fertilising, air sampling, sampling of water quality, compared with manual work, more facilitate, and danger coefficient is small, and plant protection effect is more
It is good.The essential structure of existing unmanned plane is：Frame, battery, controller, motor and multiple rotors, each rotor is by an electricity
Machine drives, using the action of remote control or the program controlled motor of input controller when using, so that the operation of rotor is adjusted,
Realize straight trip, the divertical motion of unmanned plane.
Existing rotor wing unmanned aerial vehicle generally comprises four horns of level, and adjacent two horns are mutually perpendicular to, and horn is fixed
Around frame, motor and rotor are arranged at the end of horn, because horn is more long, it has not been convenient to carry and receive.Shen
Please number for 201420845558.5 utility model patent provide a kind of rotor wing unmanned aerial vehicle of detachable horn, including fuselage with
And the multiple horns on the fuselage；Each described horn is provided with a rotor, and each described horn includes that first connects
Extension bar, the second connecting rod；One end of the head rod is fixedly connected with the fuselage, the head rod other end with
One end of second connecting rod is detachably connected；The rotor is set on the other end of second connecting rod；And described
Two connecting rods are provided with for by the electric signal transmission on the fuselage to the rotor near one end of the head rod
The jointing holes that are electrically connected.The horn of this structure cannot be removed all, need to take up room during carrying, still not enough be facilitated.
Utility model content
The purpose of this utility model is to provide a kind of dismountable rotor wing unmanned aerial vehicle of horn, to be convenient for carrying and receive.
What the purpose of this utility model was realized in：A kind of dismountable rotor wing unmanned aerial vehicle of horn, including frame, shell
Body, many support feets, many horns, the frame are located in housing, and the horn is through housing and is installed on frame,
The sidepiece of the frame is provided with multiple horn positioning components, and the horn positioning component includes lower locating piece and upper
Locating piece, the lower locating piece is fixedly installed in frame and its upper surface is provided with semicircular lower locating slot, the upper positioning
Block is hinged with lower locating piece and its lower surface is provided with semicircular upper locating slot, the lower locating slot and upper locating slot surround with
The location hole that horn outer surface is engaged, the installation end of the horn is located in location hole；The upper surface of the upper locating piece sets
The briquetting through housing is equipped with, the upper surface of the housing is provided with the buckle for compressing or unclamping briquetting.
Further, the horn is hollow stem.
Further, the horn includes mounting rod and expansion link, and the mounting rod is connected with frame, the expansion link
It is slidably matched in one end insertion mounting rod and with mounting rod, it is axially fixed that the mounting rod is carried out with expansion link by axially position part
Position.
Further, the axially position part includes being arranged at and installs the positioning through hole of bar side wall and be arranged at outside expansion link
The annular boss of wall, outer wall and the mounting rod of the annular boss are slidably matched；The outer wall of the annular boss is provided with positioning
Groove, the bottom of the locating slot is provided with spring, and the top of the spring is fixedly connected with fixture block, the side wall of the fixture block with it is fixed
Position groove is slidably matched, and top surface is slidably matched with the inwall of mounting rod, and fixture block can extend into positioning through hole.
Further, the support feet is removably installed on horn.
Further, a pair flexible locating rings are provided with the top of the support feet, the flexible locating ring includes first
The end of semi-ring and the second semi-ring, first semi-ring and the second semi-ring is each provided with a contiguous block, passes through between two contiguous blocks
Bolt connection.
The beneficial effects of the utility model are：When using unmanned plane, the installation end of horn is inserted into location hole, pull card
Button, buckle applies downward pressure to briquetting, and, by the supreme locating piece of pressure transmission, upper locating piece and the cooperation of lower locating piece will for briquetting
Horn is compressed, and makes horn keep fixing.After the completion of use, buckle is pulled, unclamp briquetting and upper locating piece, you can easily take out
Horn.The utility model, the disassembling operations simple and fast of horn, time saving and energy saving, efficiency high.During carrying, horn is entirely removed,
Unmanned plane main body is separately packed with horn, save space, carries and storage more facilitates.
Brief description of the drawings
Fig. 1 is overall schematic cross-sectional view of the present utility model；
Fig. 2 is the front view of the utility model horn positioning component；
Fig. 3 is the sectional view of A-A in Fig. 1；
Reference：1-frame；2-housing；3-support feet；4-horn；41-mounting rod；42-expansion link；43—
Positioning through hole；44-annular boss；45-locating slot；46-spring；47-fixture block；5-lower locating piece；6-upper locating piece；
7-briquetting；8-buckle；9-upper locating slot；10-lower locating slot；11-the first semi-ring；12-the second semi-ring；13-connection
Block.
Specific embodiment
The utility model is further illustrated with reference to the accompanying drawings and examples.
A kind of as shown in Figure 1, Figure 2 and Figure 3, the dismountable rotor wing unmanned aerial vehicle of horn of the present utility model, including frame 1,
Housing 2, many support feets 3, many horns 4, the frame 1 are located in housing 2, and the horn 4 is through housing 2 and is installed on machine
Frame 1,
The sidepiece of the frame 1 is provided with multiple horn positioning components, and the horn positioning component includes the He of lower locating piece 5
Upper locating piece 6, the lower locating piece 5 is fixedly installed in frame 1 and its upper surface is provided with semicircular lower locating slot 10, described
Upper locating piece 6 is hinged with lower locating piece 5 and its lower surface is provided with semicircular upper locating slot 9, the lower locating slot 10 and upper
Locating slot 9 surrounds the location hole being engaged with the outer surface of horn 4, and the installation end of the horn 4 is located in location hole；It is described fixed
The upper surface of position block 6 is provided through the briquetting 7 of housing 2, and the upper surface of the housing 2 is provided with for compressing or unclamping pressure
The buckle 8 of block 7.
Frame 1, the material of housing 2, structure and assembling mode can use prior art, and lower locating piece 5 and upper locating piece 6 are
The positioning bore dia that cuboid, upper locating slot 9 and lower locating slot 10 are surrounded should be equal to or slightly less than the external diameter of horn 4, to protect
Card can compress horn 4.Buckle 8 is arranged at the outside of housing 2, with enough operating spaces, pulls and more facilitates.Make
When using unmanned plane, the installation end of horn 4 is inserted into location hole, pull buckle 8, buckle 8 applies downward pressure to briquetting 7, pressure
By the supreme locating piece 6 of pressure transmission, upper locating piece 6 and lower locating piece 5 coordinate and compress horn 4 block 7, make horn 4 keep fixing.
After the completion of use, buckle 8 is pulled, unclamp briquetting 7 and upper locating piece 6, you can easily take out horn 4.The utility model, horn
4 disassembling operations simple and fast, time saving and energy saving, efficiency high.During carrying, horn 4 is entirely removed, unmanned plane main body and horn 4
Separately packaging, save space, carry and storage more facilitate.
In order to mitigate the gross weight of unmanned plane, the horn 4 is hollow stem.
The horn 4 includes mounting rod 41 and expansion link 42, and the mounting rod 41 is connected with frame 1, the expansion link 42
One end insertion mounting rod 41 in and be slidably matched with mounting rod 41, the mounting rod 41 passes through axially position part with expansion link 42
Carry out axially position.When carrying and receiving, first mounting rod 41 is removed from frame 1, then expansion link 42 is pushed to mounting rod 41
It is interior, further reduce the volume of horn 4, carry and more facilitate.When using, expansion link 42 is pulled out, using axially position part
Make expansion link 42 keep fixing, then mounting rod 41 is installed in frame 1.
Axially position part can be screw, alignment pin etc., it is preferred that the axially position part includes being arranged at mounting rod 41
The positioning through hole 43 of side wall and the annular boss 44 for being arranged at the outer wall of expansion link 42, the outer wall and mounting rod of the annular boss 44
41 are slidably matched；The outer wall of the annular boss 44 is provided with locating slot 45, and the bottom of the locating slot 45 is provided with spring 46,
The top of the spring 46 is fixedly connected with fixture block 47, and side wall and the locating slot 45 of the fixture block 47 are slidably matched, top surface with peace
The inwall for filling bar 41 is slidably matched, and fixture block 47 can extend into positioning through hole 43.Positioning through hole 43 be arranged at mounting rod 41 away from
One end of frame 1, annular boss 44 is arranged at expansion link 42 near one end of frame 1, and after assembling, fixture block 47 is located at mounting rod
Inside 41, spring 46 is in compressive state, when using, pulls expansion link 42, fixture block 47 is moved to positioning through hole 43, and rotation is stretched
Contracting bar 42, makes fixture block 47 be alignd with positioning through hole 43, and now spring 46 resets, and fixture block 47 is sprung into positioning through hole 43, completes axle
To positioning.After complete, Manual press fixture block 47 makes fixture block 47 depart from positioning through hole 43, you can to shrink expansion link 42.
Support feet 3 has certain length, and is distributed in the surrounding of unmanned plane, if be arranged in frame 1, during carrying
Larger space can be taken, in order to further be easy to carry, the support feet 3 is removably installed on horn 4, during carrying
Support feet 3 is pulled down into individually packaging.
Further, the top of the support feet 3 is provided with a pair flexible locating rings, and the flexible locating ring includes first
The semi-ring 12 of semi-ring 11 and second, the end of the semi-ring 12 of first semi-ring 11 and second is each provided with a contiguous block 13, two connections
It is bolted between block 13.
Preferred embodiment of the present utility model is the foregoing is only, the utility model is not limited to, for this
For the technical staff in field, the utility model can have various modifications and variations.It is all it is of the present utility model spirit and principle
Within, any modification, equivalent substitution and improvements made etc. should be included within protection domain of the present utility model.
Claims (6)
1. a kind of dismountable rotor wing unmanned aerial vehicle of horn, including frame（1）, housing（2）, many support feets（3）, many horns
（4）, the frame（1）Positioned at housing（2）It is interior, the horn（4）Through housing（2）And it is installed on frame（1）, its feature exists
In：
The frame（1）Sidepiece be provided with multiple horn positioning components, the horn positioning component includes lower locating piece（5）With
Upper locating piece（6）, the lower locating piece（5）It is fixedly installed in frame（1）And its upper surface is provided with semicircular lower locating slot
（10）, the upper locating piece（6）With lower locating piece（5）It is hinged and its lower surface is provided with semicircular upper locating slot（9）, it is described
Lower locating slot（10）With upper locating slot（9）Surround and horn（4）The location hole that outer surface is engaged, the horn（4）Installation
End is located in location hole；The upper locating piece（6）Upper surface be provided through housing（2）Briquetting（7）, the housing（2）
Upper surface be provided with for compressing or unclamping briquetting（7）Buckle（8）.
2. the dismountable rotor wing unmanned aerial vehicle of a kind of horn according to claim 1, it is characterised in that：The horn（4）For
Hollow stem.
3. the dismountable rotor wing unmanned aerial vehicle of a kind of horn according to claim 2, it is characterised in that：The horn（4）Bag
Include mounting rod（41）And expansion link（42）, the mounting rod（41）With frame（1）It is connected, the expansion link（42）One end insertion
Mounting rod（41）In and and mounting rod（41）It is slidably matched, the mounting rod（41）With expansion link（42）Entered by axially position part
Row axially position.
4. the dismountable rotor wing unmanned aerial vehicle of a kind of horn according to claim 3, it is characterised in that：The axially position part
Including being arranged at mounting rod（41）The positioning through hole of side wall（43）Be arranged at expansion link（42）The annular boss of outer wall（44）, institute
State annular boss（44）Outer wall and mounting rod（41）It is slidably matched；The annular boss（44）Outer wall be provided with locating slot
（45）, the locating slot（45）Bottom spring is installed（46）, the spring（46）Top be fixedly connected with fixture block（47）,
The fixture block（47）Side wall and locating slot（45）It is slidably matched, top surface and mounting rod（41）Inwall be slidably matched, and fixture block
（47）Can extend into positioning through hole（43）.
5. the dismountable rotor wing unmanned aerial vehicle of a kind of horn according to claim 1,2,3 or 4, it is characterised in that：The branch
Spike（3）It is removably installed in horn（4）On.
6. the dismountable rotor wing unmanned aerial vehicle of a kind of horn according to claim 5, it is characterised in that：The support feet（3）
Top be provided with a pair flexible locating rings, the flexible locating ring includes the first semi-ring（11）With the second semi-ring（12）, it is described
First semi-ring（11）With the second semi-ring（12）End be each provided with a contiguous block（13）, two contiguous blocks（13）Between pass through bolt
Connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621388943.7U CN206255185U (en) | 2016-12-18 | 2016-12-18 | A kind of dismountable rotor wing unmanned aerial vehicle of horn |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621388943.7U CN206255185U (en) | 2016-12-18 | 2016-12-18 | A kind of dismountable rotor wing unmanned aerial vehicle of horn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206255185U true CN206255185U (en) | 2017-06-16 |
Family
ID=59029941
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621388943.7U Expired - Fee Related CN206255185U (en) | 2016-12-18 | 2016-12-18 | A kind of dismountable rotor wing unmanned aerial vehicle of horn |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206255185U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107323659A (en) * | 2017-06-22 | 2017-11-07 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being easy to store based on Internet of Things |
| CN107380397A (en) * | 2017-08-03 | 2017-11-24 | 陕西棱镜网络科技有限公司 | A kind of unmanned plane fine strain of millet fixed structure |
| CN108382587A (en) * | 2018-01-31 | 2018-08-10 | 天津翰宇昊德科技发展有限公司 | The unmanned plane horn connection structure of connection easy to disassemble |
| CN108657435A (en) * | 2018-05-30 | 2018-10-16 | 福建省复新农业科技发展有限公司 | A kind of stability it is good agricultural nobody spill medicine device |
| CN110979631A (en) * | 2019-11-19 | 2020-04-10 | 深圳市方斯精密科技有限公司 | Portable subminiature fixed wing unmanned aerial vehicle |
-
2016
- 2016-12-18 CN CN201621388943.7U patent/CN206255185U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107323659A (en) * | 2017-06-22 | 2017-11-07 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being easy to store based on Internet of Things |
| CN107380397A (en) * | 2017-08-03 | 2017-11-24 | 陕西棱镜网络科技有限公司 | A kind of unmanned plane fine strain of millet fixed structure |
| CN108382587A (en) * | 2018-01-31 | 2018-08-10 | 天津翰宇昊德科技发展有限公司 | The unmanned plane horn connection structure of connection easy to disassemble |
| CN108657435A (en) * | 2018-05-30 | 2018-10-16 | 福建省复新农业科技发展有限公司 | A kind of stability it is good agricultural nobody spill medicine device |
| CN110979631A (en) * | 2019-11-19 | 2020-04-10 | 深圳市方斯精密科技有限公司 | Portable subminiature fixed wing unmanned aerial vehicle |
| CN110979631B (en) * | 2019-11-19 | 2021-08-24 | 东莞市联德瑞智能精密有限公司 | Portable subminiature fixed wing unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170616 |