CN205499365U - Magnetism is inhaled and is separated locking -type unmanned aerial vehicle horn stop gear - Google Patents
Magnetism is inhaled and is separated locking -type unmanned aerial vehicle horn stop gear Download PDFInfo
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- CN205499365U CN205499365U CN201620136085.0U CN201620136085U CN205499365U CN 205499365 U CN205499365 U CN 205499365U CN 201620136085 U CN201620136085 U CN 201620136085U CN 205499365 U CN205499365 U CN 205499365U
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- spacing magnet
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Abstract
The utility model discloses a magnetism is inhaled and is separated locking -type unmanned aerial vehicle horn stop gear is opened by rotatory mounting, horn that spacing magnet, rotatory mounting magnet, horn draw spacing magnet in, the fixing base is formed, and the fixing base is fixed and is covered on unmanned aerial vehicle's organism, and the fixing base horn is fixed on the fixing base through rotating the mounting, its characterized in that: rotatory mounting magnet is fixed on rotatory mounting to rotatory along with rotatory mounting, the horn is opened spacing magnet, horn and is drawn in spacing magnet in and fix respectively correspond the position on the fixing base, and the horn rotation is during to operating condition, and the absorption firmly of spacing magnet is opened together with the horn to rotatory mounting magnet, makes the horn not have and rocks, and the horn rotation is during to folded state, and rotatory mounting magnet draws in the absorption firmly of spacing magnet in together with the horn, makes the horn not have and rocks. The utility model discloses make the unmanned aerial vehicle horn more reliable and more stable under operating condition or folded state, the security is higher.
Description
Technical field
This utility model belongs to aircraft field, relates to a kind of magnetic unlocking type unmanned plane horn position-limit mechanism.
Background technology
The unmanned plane using collapsible horn at present is generally spacing by machinery button bit, the smoothness folded in view of horn, general reserved certain gap between horn and rotating shaft, this still suffers from 2 °~5 ° rock when causing horn in working order with rounding state, unmanned vehicle vibration in running can be aggravated, run shakiness, and there is potential safety hazard.And horn rocks under rounding state, fragile horn and wing in transportation.
Utility model content
The purpose of this utility model is to overcome existing unmanned vehicle in normal work, the problem of the fuselage caused because of the horn shakiness vibrations existed, damage with wing because horn rocks the horn caused with in transportation, a kind of magnetic unlocking type unmanned plane horn position-limit mechanism is provided, when horn rotates to duty, rotary mount Magnet and horn are opened spacing Magnet and are attached together firmly, make horn without rocking, when horn rotates to rounding state, rotary mount Magnet and horn draw spacing Magnet in and are attached together firmly, make horn without rocking.
The technical solution of the utility model is as follows:
A kind of magnetic unlocking type unmanned plane horn position-limit mechanism, by rotary mount, horn opens spacing Magnet, rotary mount Magnet, horn draws spacing Magnet in, fixing seat composition, fixing seat is fixed on the organism top case of unmanned plane, fixing base arm is fixed on fixing seat by rotary mount, it is characterized in that: rotary mount Magnet is fixed on rotary mount, and rotate with rotary mount, horn opens spacing Magnet, horn draws spacing Magnet in and is separately fixed at correspondence position on fixing seat, when horn rotates to duty, rotary mount Magnet and horn are opened spacing Magnet and are attached together firmly, make horn without rocking, when horn rotates to rounding state, rotary mount Magnet and horn draw spacing Magnet in and are attached together firmly, make horn without rocking.
When four horns of the present utility model are in working order with rounding state, horn all can open spacing Magnet by the rotary mount Magnet on rotary mount with corresponding horn or the horn spacing Magnet of gathering is attached together firmly, making horn in working order or more reliable and more stable under rounding state, safety is higher.
Accompanying drawing explanation
Fig. 1 is horn scheme of installation of the present utility model.
Fig. 2 is structural representation of the present utility model.
Fig. 3 is the schematic diagram being arranged on unmanned plane under horn open mode of the present utility model.
Fig. 4 is the schematic diagram being arranged on unmanned plane under horn rounding state of the present utility model.
Detailed description of the invention
In conjunction with accompanying drawing, this utility model is further described.
nullSuch as Fig. 1、Shown in Fig. 2,This utility model is by rotary mount 2、Horn opens spacing Magnet 3、Rotary mount Magnet 4、Horn draws spacing Magnet 5 in、Fixing seat 7 forms,Fixing seat 7 is fixed on the organism top case 1 of unmanned plane,Fixing base arm 6 is fixed on fixing seat 7 by rotary mount 2,It is characterized in that: rotary mount Magnet 4 is fixed on rotary mount 2,And rotate with rotary mount 2,Horn opens spacing Magnet 3、Horn draws spacing Magnet 5 in and is separately fixed at correspondence position on fixing seat 7,When horn 6 rotates to duty,Rotary mount Magnet 4 and horn are opened spacing Magnet 3 and are attached together firmly,Make horn without rocking,When horn 6 rotates to rounding state,Rotary mount Magnet 4 and horn draw spacing Magnet 5 in and are attached together firmly,Make horn without rocking.
As shown in Figure 3, Figure 4, unmanned plane is mounted with four horns, when four horns are in working order with rounding state, horn all can open spacing Magnet 3 by the rotary mount Magnet 4 on horn rotary mount 2 with corresponding horn or the horn spacing Magnet 5 of gathering is attached together firmly, making horn more reliable and more stable with under rounding state in working order, safety is higher.
Claims (1)
1. a magnetic unlocking type unmanned plane horn position-limit mechanism, is opened spacing Magnet by rotary mount (2), horn
(3), rotary mount Magnet (4), horn draw spacing Magnet (5), fixing seat (7) composition, fixing seat (7) in
Being fixed on the organism top case (1) of unmanned plane, fixing base arm (6) is fixed on fixing by rotary mount (2)
On seat (7), it is characterised in that: rotary mount Magnet (4) is fixed on rotary mount (2), and with rotation
Turning fixture (2) to rotate together, horn opens spacing Magnet (3), horn draws spacing Magnet (5) in and is separately fixed at
The upper correspondence position of fixing seat (7), when horn (6) rotates to duty, rotary mount Magnet (4) and horn
Open spacing Magnet (3) to be attached together firmly, when horn (6) rotates to rounding state, rotary mount Magnet
(4) draw spacing Magnet (5) in horn to be attached together firmly.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620136085.0U CN205499365U (en) | 2016-02-23 | 2016-02-23 | Magnetism is inhaled and is separated locking -type unmanned aerial vehicle horn stop gear |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620136085.0U CN205499365U (en) | 2016-02-23 | 2016-02-23 | Magnetism is inhaled and is separated locking -type unmanned aerial vehicle horn stop gear |
Publications (1)
Publication Number | Publication Date |
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CN205499365U true CN205499365U (en) | 2016-08-24 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201620136085.0U Active CN205499365U (en) | 2016-02-23 | 2016-02-23 | Magnetism is inhaled and is separated locking -type unmanned aerial vehicle horn stop gear |
Country Status (1)
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CN (1) | CN205499365U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017185621A1 (en) * | 2016-04-28 | 2017-11-02 | 乐视控股(北京)有限公司 | Foldable unmanned aerial vehicle and use method thereof |
CN109421913A (en) * | 2017-08-30 | 2019-03-05 | 深圳市道通智能航空技术有限公司 | Folding rack and unmanned plane |
CN109421914A (en) * | 2017-08-30 | 2019-03-05 | 深圳市道通智能航空技术有限公司 | Folding rack and unmanned plane |
-
2016
- 2016-02-23 CN CN201620136085.0U patent/CN205499365U/en active Active
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2017185621A1 (en) * | 2016-04-28 | 2017-11-02 | 乐视控股(北京)有限公司 | Foldable unmanned aerial vehicle and use method thereof |
CN109421913A (en) * | 2017-08-30 | 2019-03-05 | 深圳市道通智能航空技术有限公司 | Folding rack and unmanned plane |
CN109421914A (en) * | 2017-08-30 | 2019-03-05 | 深圳市道通智能航空技术有限公司 | Folding rack and unmanned plane |
WO2019041875A1 (en) * | 2017-08-30 | 2019-03-07 | 深圳市道通智能航空技术有限公司 | Foldable frame and unmanned aerial vehicle |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CP03 | Change of name, title or address | ||
CP03 | Change of name, title or address |
Address after: 518066 Room 201, building A, No. 1, Qian Wan Road, Qianhai Shenzhen Hong Kong cooperation zone, Shenzhen, Guangdong (Shenzhen Qianhai business secretary Co., Ltd.) Patentee after: Puzhou Technology (Shenzhen) Co.,Ltd. Address before: 518000 Room 201, building A, 1 front Bay Road, Shenzhen Qianhai cooperation zone, Shenzhen, Guangdong Patentee before: PRODRONE TECHNOLOGY (SHENZHEN) Co.,Ltd. |