CN107226195A - A kind of unmanned plane wing registration locking device - Google Patents
A kind of unmanned plane wing registration locking device Download PDFInfo
- Publication number
- CN107226195A CN107226195A CN201710294188.9A CN201710294188A CN107226195A CN 107226195 A CN107226195 A CN 107226195A CN 201710294188 A CN201710294188 A CN 201710294188A CN 107226195 A CN107226195 A CN 107226195A
- Authority
- CN
- China
- Prior art keywords
- wing
- fixing axle
- pin
- hole
- locking device
- 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.)
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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
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Automatic Assembly (AREA)
Abstract
The invention discloses a kind of unmanned plane wing registration locking device, including body, body Corner Strapped is provided with fixing axle, movable sleeve is connected to rotary shaft in fixing axle, wing is fixed with the outside of rotary shaft, inboard is provided with iron plate, and the position of body both sides correspondence iron plate is provided with flat thin magnet.The present invention passes through pull-up handle when in use, hexagonal pin departs from positioning hole, hexagonal pin can under the action of the spring be moved down and plugged together again in positioning hole, realize the accurate lock of wing, when need not use, pull-up handle, close wing, rotary shaft is driven to be rotated in fixing axle, the iron plate of inboard can be adsorbed on flat thin magnet in the presence of magnetic force, put down handle, further lock wing, prevent that wing is opened in carrying process, cause fractureing for propeller, the locking device structure is simple, and avoid the perforate on wing and body by adding fixing axle and rotation shaft structure, housing construction intensity is impacted so as to avoid.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, specially a kind of unmanned plane wing registration locking device.
Background technology
Unmanned plane is the not manned vehicle manipulated by radio robot or airborne computer stored program controlled,
Unmanned plane is simple in construction, use cost is low, can not only complete the task of manned aircraft execution, be more suitable for manned aircraft not
Preferably performing for task, burst thing is emergent, early warning play the role of it is very big.Simultaneously with the progress of science, more civilian nothings
Man-machine to be developed, a large amount of unmanned planes are used to take photo by plane field, unmanned plane image have high-resolution, large scale, small area,
The advantage of high Up-to-date state, is particularly suitable for obtaining the regional aerial images of banding, and unmanned plane photographed to take photo by plane provide it is easy to operate,
It is easy to the remote sensing platform of transition, landing of taking off is limited smaller by place, can be risen on playground, highway or other openr ground
Drop, its stability, security are good, and transition etc. is very easy to, therefore proposes higher requirement to the portability of unmanned plane.
Current unmanned plane uses wing folding structure mostly, so as to reduce the volume of unmanned plane, is convenient for carrying, existing
Used in more conventional folding wing and fixed pin removal is installed on fuselage, by the pin and wing of pin removal
Pin-and-hole coordinate and realize the locking to folded wing, need to pin removal to ensure the cooperation of pin removal pin and wing pin-and-hole
Finished with fuselage assembling, wing and fuselage assembling, the perforate of wing pin-and-hole processing etc., to ensure the precision of pin and pin-and-hole
Coordinate, such difficulty of processing is big, and unmanned plane structural strength can be impacted with perforate on wing in itself in body, so that shadow
Ring the degree of accuracy of the device of pin locking, but also the overall aesthetics of unmanned plane can be destroyed, be this it is proposed that it is a kind of nobody
Machine wing registration locking device is used to solve the above problems.
The content of the invention
It is an object of the invention to provide a kind of unmanned plane wing registration locking device, to solve above-mentioned background technology
The problem of middle proposition.
To achieve the above object, the present invention provides following technical scheme：A kind of unmanned plane wing registration locking device,
Including body, the body Corner Strapped is provided with movable sleeve in fixing axle, the fixing axle and is connected to outside rotary shaft, the rotary shaft
Side is fixed with wing, and the inboard is provided with iron plate, and the position of the body both sides correspondence iron plate is provided with flat thin magnet；
The fixing axle upper end, which is movably equipped with to be provided with to run through in pin hole, the pin hole on the left of shaft-cup, the shaft-cup, is provided with six
Angle pin, the hexagonal pin is provided with upper limit plate and lower limiting board, institute in be connected axle and rotary shaft, and fixing axle
State upper limit plate and lower limiting board and the hexagonal being equipped with hexagonal dowel contact between through hole, and upper limit plate and lower limiting board
Pin is provided with top on limited block, the limited block and is fixedly connected with lower spring end, and the spring upper end is fixedly connected with upper limit
The lower top surface of plate；
Locating piece is provided with the rotary shaft, the locating piece is provided with activity grafting six in some positioning holes, the positioning hole
The bottom of angle pin, and rotary shaft upper end is provided with fixture block, fixing axle lower end correspondence position is provided with neck.
It is preferred that, the shaft-cup lower end is provided with external screw thread, and the inner side of the fixing axle upper end is provided with internal thread.
It is preferred that, hexagonal pin top on the outside of the shaft-cup is provided with handle, and the handle is provided with draw ring, and handle
Cross-sectional area is more than the size of pin hole, and the pin hole is located at shaft-cup left side/position.
It is preferred that, the upper limit plate and lower limiting board are collar plate shape structure, and both diameters are identical with fixing axle internal diameter, and
Correspond to and be fixed in fixing axle up and down respectively, the through hole is regular hexagon structure, the hole size is more than the horizontal stroke of hexagonal pin
Sectional area.
It is preferred that, the limited block is cyclic structure, and is fixedly mounted on the side of hexagonal pin, the horizontal stroke of the limited block
Sectional area is more than through hole, and limited block top is more than the depth of positioning hole to the distance of top surface under upper limit plate.
It is preferred that, the locating piece is that the positioning hole on cylindrical structure, and locating piece is regular hexagon structure, described fixed
The position size in hole and the cross section size of hexagonal pin are consistent, and the quantity of the positioning hole is four, and four positioning holes are closed
It is symmetrical in the locating piece top center of circle.
It is preferred that, the bayonet slot ring is on the medial surface positioned at fixing axle lower end, and its section is U-shape structure, the card
Block is surround on the lateral surface of rotary shaft upper end, and its shape and neck are consistent, and fixture block width is less than the width of neck.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention when in use by the draw ring on pull-up handle,
Hexagonal pin departs from positioning hole, opens wing to the position needed, puts down handle, hexagonal pin can be downward under the action of the spring
It is mobile, so that the bottom of hexagonal pin is plugged together in positioning hole again, the accurate lock of wing is realized, while limited block can be with
The distance that limitation hexagonal pin is moved down, convenient regulation is not being needed in use, same pull-up handle, hexagonal pin departs from
Positioning hole, closes wing, drives rotary shaft to be rotated in fixing axle, the iron plate of inboard can be adsorbed in the presence of magnetic force
On flat thin magnet, while putting down handle, wing is further locked, prevents that wing is opened in carrying process, causes the folding of propeller
Disconnected, the locking device structure is simple, and avoids the perforate on wing and body by adding fixing axle and rotation shaft structure,
Housing construction intensity is impacted so as to avoid.
Brief description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is fixing axle of the present invention and rotation shaft structure schematic diagram；
Fig. 3 is positioning plate structure schematic diagram of the present invention；
Fig. 4 is interface arrangment schematic diagram of the present invention.
In figure：1 body, 2 fixing axles, 3 wings, 4 iron plates, 5 flat thin magnets, 6 internal threads, 7 rotary shafts, 8 shaft-cups, 9 handles, 10
Pin hole, 11 upper limit plates, 12 lower limiting boards, 13 hexagonal pins, 14 springs, 15 limited blocks, 16 through holes, 17 necks, 18 fixture blocks,
19 locating pieces, 20 positioning holes, 21 external screw threads.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Fig. 1-4 are referred to, the present invention provides a kind of technical scheme：A kind of unmanned plane wing registration locking device, bag
Body 1 is included, the Corner Strapped of body 1 is provided with movable sleeve in fixing axle 2, fixing axle 2 and is connected to rotary shaft 7, and the fixation of the outside of rotary shaft 7 is set
There is wing 3, rotary shaft 7 can be rotated in fixing axle 2, so as to drive the rotation adjusting position of wing 3, the upper end of fixing axle 2 is lived
Dynamic to be provided with shaft-cup 8, the left side of shaft-cup 8 is provided with pin hole 10, and the lower end of shaft-cup 8 is provided with external screw thread 21, and the inner side of the upper end of fixing axle 2 is provided with
Internal thread 6, the dismounting and installation of shaft-cup 8 can be realized by the helicitic texture on shaft-cup 8 and fixing axle 2, be easy to maintenance, shaft-cup
The top of hexagonal pin 13 in 8 outsides is provided with handle 9, and handle 9 is provided with draw ring, and the cross-sectional area of handle 9 is more than pin hole 10
Size, pin hole 10 is located at 1/4 position of the left side of shaft-cup 8, and the active card of handle 9 is in the upper end of shaft-cup 8, pin hole 10 through setting
There is hexagonal pin 13, hexagonal pin 13 is in be connected axle 2 and rotary shaft 7, and fixing axle 2 provided with upper limit plate 11 with
Limiting plate 12, upper limit plate 11 and lower limiting board 12 are equipped with through hole 16 with the contact position of hexagonal pin 13, and upper limit plate 11 is with
Limiting plate 12 is collar plate shape structure, and both diameters are identical with the internal diameter of fixing axle 2, and corresponds to be fixed in fixing axle 2 up and down respectively,
Through hole 16 is regular hexagon structure, and the size of through hole 16 is more than the cross-sectional area of hexagonal pin 13, and upper limit plate 11 and lower limit
Hexagonal pin 13 between the plate 12 of position is provided with top on limited block 15, limited block 15 and is fixedly connected with the lower end of spring 14, spring 14
Upper end is fixedly connected with the lower top surface of upper limit plate 11, and limited block 15 is cyclic structure, and is fixedly mounted on the side of hexagonal pin 13
On face, the cross-sectional area of the limited block 15 is more than through hole 16, and the distance of the top of limited block 15 to 11 times top surfaces of upper limit plate is big
In the depth of positioning hole 20.
Locating piece 19 is provided with rotary shaft 7, locating piece 19 is provided with activity grafting six in some positioning holes 20, positioning hole 20
The bottom of angle pin 13, locating piece 19 is that the positioning hole 20 on cylindrical structure, and locating piece 19 is regular hexagon structure, positioning
The size in hole 20 and the cross section size of hexagonal pin 13 are consistent, and the quantity of the positioning hole 20 is four, and four positioning
Hole 20 is symmetrical on the top center of circle of locating piece 19, so that ensure the engaging of hexagonal pin 13 and each positioning hole 20, and
The upper end of rotary shaft 7 is provided with fixture block 18, and the lower end correspondence position of fixing axle 2 is provided with neck 17, and neck 17 is around under fixing axle 2
On the medial surface at end, and its section be U-shape structure, fixture block 18 around positioned at the upper end of rotary shaft 7 lateral surface on, and its shape and
Neck 17 is consistent, and the width of fixture block 18 is less than the width of neck 17.
The inner side of wing 3 is provided with iron plate 4, and the position of the both sides of body 1 correspondence iron plate 4 is provided with flat thin magnet 5, and unmanned plane need not
In use, wing is adsorbed on the both sides of body 1 by flat thin magnet 5 and the structure of iron plate 4.
Operation principle：Structure of the present invention is when in use by the draw ring on pull-up handle 9, and hexagonal pin 13 departs from positioning hole
20, wing 3 is opened to the position needed, puts down handle 9, hexagonal pin 13 can be moved down under action from the spring 14, so that
The bottom of hexagonal pin 13 is plugged together in positioning hole 20 again, the accurate lock of wing 3 is realized, while limited block 15 can be limited
The distance that hexagonal pin 13 processed is moved down, convenient regulation is not being needed in use, same pull-up handle 9, hexagonal pin 13 takes off
From positioning hole 20, wing 3 is closed, drives rotary shaft 7 to be rotated in fixing axle 2, work of the meeting of iron plate 4 on the inside of wing 3 in magnetic force
With lower absorption on flat thin magnet 5, while putting down handle 9, further locking wing 3, prevents that wing 3 is opened in carrying process,
Cause fractureing for propeller.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of changes, modification can be carried out to these embodiments, replace without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (7)
1. a kind of unmanned plane wing registration locking device, including body（1）, the body（1）Corner Strapped is provided with fixation
Axle（2）, the fixing axle（2）Interior movable sleeve is connected to rotary shaft（7）, the rotary shaft（7）Outside is fixed with wing（3）, its
It is characterised by：The wing（3）Inner side is provided with iron plate（4）, the body（1）Both sides correspondence iron plate（4）Position be provided with magnetic
Iron plate（5）；
The fixing axle（2）Upper end is movably equipped with shaft-cup（8）, the shaft-cup（8）Left side is provided with pin hole（10）, the pin hole
（10）It is interior to run through provided with hexagonal pin（13）, the hexagonal pin（13）Through the axle that is connected（2）And rotary shaft（7）, and it is solid
Dead axle（2）It is interior to be provided with upper limit plate（11）And lower limiting board（12）, the upper limit plate（11）And lower limiting board（12）With hexagonal
Pin（13）Contact position is equipped with through hole（16）, and upper limit plate（11）And lower limiting board（12）Between hexagonal pin（13）On
Provided with limited block（15）, the limited block（15）Upper top is fixedly connected with spring（14）Lower end, the spring（14）Upper end is fixed
Connect upper limit plate（11）Lower top surface；
The rotary shaft（7）It is interior to be provided with locating piece（19）, the locating piece（19）It is provided with some positioning holes（20）, the positioning
Hole（20）Interior activity grafting hexagonal pin（13）Bottom, and rotary shaft（7）Upper end is provided with fixture block（18）, the fixing axle（2）
Lower end correspondence position is provided with neck（17）.
2. a kind of unmanned plane wing registration locking device according to claim 1, it is characterised in that：The shaft-cup
（8）Lower end is provided with external screw thread（21）, the fixing axle（2）The inner side of upper end is provided with internal thread（6）.
3. a kind of unmanned plane wing registration locking device according to claim 1, it is characterised in that：The shaft-cup
（8）The hexagonal pin in outside（13）Top is provided with handle（9）, the handle（9）It is provided with draw ring, and handle（9）Cross section
Product is more than pin hole（10）Size, the pin hole（10）Positioned at shaft-cup（8）At the position of left side 1/4.
4. a kind of unmanned plane wing registration locking device according to claim 1, it is characterised in that：The upper limit
Plate（11）And lower limiting board（12）For collar plate shape structure, both diameters and fixing axle（2）Internal diameter is identical, and corresponds to up and down respectively solid
It is scheduled on fixing axle（2）It is interior, the through hole（16）For regular hexagon structure, the through hole（16）Size is more than hexagonal pin（13）Horizontal stroke
Sectional area.
5. a kind of unmanned plane wing registration locking device according to claim 1, it is characterised in that：The limited block
（15）For cyclic structure, and it is fixedly mounted on hexagonal pin（13）Side on, the limited block（15）Cross-sectional area be more than it is logical
Hole（16）, and limited block（15）Top is to upper limit plate（11）The distance of lower top surface is more than positioning hole（20）Depth.
6. a kind of unmanned plane wing registration locking device according to claim 1, it is characterised in that：The locating piece
（19）For cylindrical structure, and locating piece（19）On positioning hole（20）For regular hexagon structure, the positioning hole（20）It is big
Small and hexagonal pin（13）Cross section size be consistent, the positioning hole（20）Quantity be four, and four positioning holes
（20）On locating piece（19）The top center of circle is symmetrical.
7. a kind of unmanned plane wing registration locking device according to claim 1, it is characterised in that：The neck
（17）Around positioned at fixing axle（2）On the medial surface of lower end, and its section is U-shape structure, the fixture block（18）Turn around being located at
Moving axis（7）On the lateral surface of upper end, and its shape and neck（17）It is consistent, fixture block（18）Width is less than neck（17）Width
Degree.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710294188.9A CN107226195B (en) | 2017-04-28 | 2017-04-28 | A kind of unmanned plane wing registration locking device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710294188.9A CN107226195B (en) | 2017-04-28 | 2017-04-28 | A kind of unmanned plane wing registration locking device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107226195A true CN107226195A (en) | 2017-10-03 |
| CN107226195B CN107226195B (en) | 2019-10-01 |
Family
ID=59934632
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710294188.9A Expired - Fee Related CN107226195B (en) | 2017-04-28 | 2017-04-28 | A kind of unmanned plane wing registration locking device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107226195B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108031129A (en) * | 2017-12-18 | 2018-05-15 | 深圳市中航电科技有限公司 | Easy-to-mount fuselage docks connected structure with wing |
| CN108394547A (en) * | 2018-01-24 | 2018-08-14 | 倪惠芳 | A kind of multi-direction lockable mechanism of unmanned plane wing |
| CN110758035A (en) * | 2019-11-08 | 2020-02-07 | 杭州师范大学钱江学院 | Road-air dual-purpose unmanned aerial vehicle with stair climbing function and operation method thereof |
| CN113697119A (en) * | 2021-10-03 | 2021-11-26 | 广东技术师范大学 | Unmanned aerial vehicle inspection equipment for power transmission line |
| CN114701645A (en) * | 2022-04-02 | 2022-07-05 | 深圳市昱晟通讯设备有限公司 | Multi-rotor unmanned aerial vehicle |
| CN115384763A (en) * | 2022-08-29 | 2022-11-25 | 北京卫通新科测控技术有限公司 | Unmanned aerial vehicle and unmanned aerial vehicle system with infrared thermal imaging function |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150321755A1 (en) * | 2014-04-28 | 2015-11-12 | Arch Aerial, Llc | Collapsible multi-rotor uav |
| CN204956909U (en) * | 2015-07-09 | 2016-01-13 | 武汉高德无人机科技有限公司 | Portable unmanned aerial vehicle |
| CN105711812A (en) * | 2016-03-11 | 2016-06-29 | 胡建令 | Folding wing unmanned aerial vehicle for municipal garden |
| CN205675222U (en) * | 2016-02-22 | 2016-11-09 | 深圳市大疆创新科技有限公司 | Frame and use the unmanned plane of this frame |
| CN206068130U (en) * | 2016-09-08 | 2017-04-05 | 深圳创动科技有限公司 | Aircraft and its folding rotor arm |
-
2017
- 2017-04-28 CN CN201710294188.9A patent/CN107226195B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150321755A1 (en) * | 2014-04-28 | 2015-11-12 | Arch Aerial, Llc | Collapsible multi-rotor uav |
| CN204956909U (en) * | 2015-07-09 | 2016-01-13 | 武汉高德无人机科技有限公司 | Portable unmanned aerial vehicle |
| CN205675222U (en) * | 2016-02-22 | 2016-11-09 | 深圳市大疆创新科技有限公司 | Frame and use the unmanned plane of this frame |
| CN105711812A (en) * | 2016-03-11 | 2016-06-29 | 胡建令 | Folding wing unmanned aerial vehicle for municipal garden |
| CN206068130U (en) * | 2016-09-08 | 2017-04-05 | 深圳创动科技有限公司 | Aircraft and its folding rotor arm |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108031129A (en) * | 2017-12-18 | 2018-05-15 | 深圳市中航电科技有限公司 | Easy-to-mount fuselage docks connected structure with wing |
| CN108031129B (en) * | 2017-12-18 | 2024-01-02 | 深圳市中航电科技有限公司 | Butt joint grafting structure of fuselage and wing convenient to dismouting |
| CN108394547A (en) * | 2018-01-24 | 2018-08-14 | 倪惠芳 | A kind of multi-direction lockable mechanism of unmanned plane wing |
| CN110758035A (en) * | 2019-11-08 | 2020-02-07 | 杭州师范大学钱江学院 | Road-air dual-purpose unmanned aerial vehicle with stair climbing function and operation method thereof |
| CN110758035B (en) * | 2019-11-08 | 2020-10-27 | 杭州师范大学钱江学院 | Road-air dual-purpose unmanned aerial vehicle with stair climbing function and operation method thereof |
| CN113697119A (en) * | 2021-10-03 | 2021-11-26 | 广东技术师范大学 | Unmanned aerial vehicle inspection equipment for power transmission line |
| CN114701645A (en) * | 2022-04-02 | 2022-07-05 | 深圳市昱晟通讯设备有限公司 | Multi-rotor unmanned aerial vehicle |
| CN115384763A (en) * | 2022-08-29 | 2022-11-25 | 北京卫通新科测控技术有限公司 | Unmanned aerial vehicle and unmanned aerial vehicle system with infrared thermal imaging function |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107226195B (en) | 2019-10-01 |
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Effective date of registration: 20190904 Address after: 312500 Taoyuan Xincun 21-101, Juzhen, Dashi, Juzhen, Xinchang County, Shaoxing City, Zhejiang Province Applicant after: Xinchang Yixulong Machinery Technology Co., Ltd. Address before: Room 607, Building 9, Tiantai Financial Plaza, 333 Macau Road, Jiaozhou City, Qingdao City, Shandong Province Applicant before: Qingdao Gaozhi High-New Tech Co., Ltd. |
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Granted publication date: 20191001 Termination date: 20210428 |