CN2875949Y - Portable load clamping and throwing device of pilotless plane - Google Patents
Portable load clamping and throwing device of pilotless plane Download PDFInfo
- Publication number
- CN2875949Y CN2875949Y CN 200620018998 CN200620018998U CN2875949Y CN 2875949 Y CN2875949 Y CN 2875949Y CN 200620018998 CN200620018998 CN 200620018998 CN 200620018998 U CN200620018998 U CN 200620018998U CN 2875949 Y CN2875949 Y CN 2875949Y
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- CN
- China
- Prior art keywords
- steering wheel
- shifting block
- support
- poke
- fixed
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- 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.)
- Expired - Fee Related
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Abstract
A portable pilot unmanned plane task clipping and positioning machine can be fitted in the positioning and clipping task load of every type of car robot, movable platform, unmanned aircrafts. The utility model comprises a rudder brackets and brackets which are positioned on the fixing board respectively. The poke block axis is positioned in the axletree hole which is on the bracket. The poke block is positioned within the long groove of the poke block axis and is fixed on the poke block axis by fixing pin while the poke fork is fixed on the poke block axis by rectangular grooves and bolts. The supporting axis which is provided with left and right lock blocks are positioned in the axletree hole under the bracket. Releasing the spring between the left and right lock and positioning the spring on the axletree, the positioning pin and the positioning axis are fixed in the corresponding hole of the bracket. The rudder is positioned on the rudder bracket and by the puller connected with the poke fork. The utility model has the characteristics of tight clipping and different task load as well as light in self weight, etc.
Description
Technical field: the utility model relates to a kind of portable unmanned aerial vehicle mission payload and clamps throwing mechanism, and it is applicable to clamping mission payloads such as being configured in various car formula robots, mobile platform, unmanned vehicle.
Background technology: in background technology, portable unmanned aerial vehicle does not have mission payload and clamps throwing mechanism, for addressing this problem, portable unmanned aerial vehicle mission payload is clamped throwing mechanism develop.
Summary of the invention: technical problem to be solved in the utility model is to provide a kind of portable unmanned aerial vehicle mission payload to clamp throwing mechanism, and its energy firm grip, reliable input and own wt are light.
The technical scheme that its technical matters that solves the utility model adopts is that it comprises steering wheel, steering wheel swing arm, steering wheel support, pull bar, locating dowel pin, latch segment, shift fork, support, shifting block, trip spring, set pin, shifting block axle, bolster, fix shaft, adapter plate;
Steering wheel support, support are separately fixed on the adapter plate, and the shifting block axle mounting is in support head bearing hole, and shifting block is installed in the elongated slot of shifting block axle and by set pin and is fixed on the shifting block axle, shift fork by rectangle keyway and screw retention on the shifting block axle; Bolster is installed in the support lower bearing hole, and left and right sides latch segment is installed in respectively on the bolster, and trip spring is between the latch segment of the left and right sides and be installed on the bolster, and four locating dowel pins and a fix shaft are separately fixed in the support respective aperture; Steering wheel is installed on the steering wheel support, and the steering wheel swing arm is fixed on the steering wheel, and connects shift fork by pull bar.
The utility model is compared the beneficial effect that is produced with background technology:
1, because the utility model has adopted the formula of revoking to clamp throwing mechanism, can guarantee the reliable grip that the mission payload of Different Weight changes like this on a large scale in, with self light weight clamping greater weight mission payload, the load-carrying capacity of raising unmanned vehicle.
2, because the utility model has adopted the axial pin type structure, reduced friction, improved kinematic accuracy, guaranteed that shifting block rotates flexibly, mission payload is reliably thrown in.
Description of drawings: Fig. 1 is a constructional drawing of the present utility model.
Fig. 2 is the left view of Fig. 1.
The specific embodiment: referring to accompanying drawing 1, accompanying drawing 2, steering wheel support 3, support 8 are separately fixed on the adapter plate 15, shifting block axle 12 is installed in the support 8 head bearing holes, shifting block 9 is installed in the elongated slot of shifting block axle 12 and by set pin 11 and is fixed on the shifting block axle 12, shift fork 7 by rectangle keyway and screw retention on shifting block axle 12.Bolster 13 is installed in the support 8 lower bearing holes, left and right sides latch segment 6 is installed in respectively on the bolster 13, trip spring 10 is between the left and right sides latch segment 6 and be installed on the bolster 13, and four locating dowel pins 5 and a fix shaft 14 are separately fixed in support 8 respective aperture.Steering wheel 1 is installed on the steering wheel support 3, and steering wheel swing arm 2 is fixed on the steering wheel 1, and connects shift fork 7 by pull bar 4.
Portable unmanned aerial vehicle mission payload clamps the throwing mechanism original position and is in loose folder state, when loading mission payload, manually revoking of mission payload is placed in two latch segments 6, and is moved upward to fix shaft 14 and contacts.Remote control starts steering wheel 1, the swing of steering wheel 1 cw, drive the swing of shifting block 9 cws by steering wheel swing arm 2, pull bar 4, shift fork 7, shifting block axle 12, run into locating dowel pin 5 location up to shifting block 9, latch segment 6 opens under the effect of power at shifting block 9, overcome the power of opening of trip spring 10, with the clamping of revoking of mission payload.When throwing in mission payload, remote control starts steering wheel 1, steering wheel 1 counter-clockwise swing, drive shifting block 9 counter-clockwise swings by steering wheel swing arm 2, pull bar 4, shift fork 7, shifting block axle 12, run into locating dowel pin 5 location up to shifting block 9, remove shifting block 9 and open the effect of power to latch segment 6, mission payload is freed the effect of latch segment 6 and the input of the load of finishing the work under the effect of weight and trip spring 10.
Claims (1)
1, a kind of portable unmanned aerial vehicle mission payload clamps throwing mechanism, it is characterized in that it comprises steering wheel (1), steering wheel swing arm (2), steering wheel support (3), pull bar (4), locating dowel pin (5), latch segment (6), shift fork (7), support (8), shifting block (9), trip spring (10), set pin (11), shifting block axle (12), bolster (13), fix shaft (14), adapter plate (15);
Steering wheel support (3), support (8) are separately fixed on the adapter plate (15), shifting block axle (12) is installed in support (8) the head bearing hole, shifting block (9) is installed in the elongated slot of shifting block axle (12) and is fixed on the shifting block axle (12) by set pin (11), and shift fork (7) passes through rectangle keyway and screw retention on shifting block axle (12); Bolster (13) is installed in support (8) the lower bearing hole, left and right sides latch segment (6) is installed in respectively on the bolster (13), trip spring (10) is positioned between the left and right sides latch segment (6) and is installed on the bolster (13), locating dowel pin (5) and fix shaft (14) are separately fixed in support (8) respective aperture, steering wheel 1 is installed on the steering wheel support (3), steering wheel swing arm (2) is fixed on the steering wheel (1), and connects shift fork (7) by pull bar (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620018998 CN2875949Y (en) | 2006-04-05 | 2006-04-05 | Portable load clamping and throwing device of pilotless plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620018998 CN2875949Y (en) | 2006-04-05 | 2006-04-05 | Portable load clamping and throwing device of pilotless plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2875949Y true CN2875949Y (en) | 2007-03-07 |
Family
ID=37819189
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620018998 Expired - Fee Related CN2875949Y (en) | 2006-04-05 | 2006-04-05 | Portable load clamping and throwing device of pilotless plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2875949Y (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102139761A (en) * | 2010-12-03 | 2011-08-03 | 中国船舶重工集团公司第七一○研究所 | Unpowered self-separated impact protection device |
| CN102183352A (en) * | 2011-02-24 | 2011-09-14 | 西北工业大学 | Releasing mechanism used for releasing experiments |
| CN103640697A (en) * | 2013-12-23 | 2014-03-19 | 景德镇陶瓷学院 | Cargo delivering device for unmanned helicopter |
| CN105217036A (en) * | 2014-06-13 | 2016-01-06 | 陕西飞机工业（集团）有限公司 | Traction air-drop parachuting unit |
| CN105667794A (en) * | 2016-03-19 | 2016-06-15 | 佛山市安尔康姆航空科技有限公司 | Bomb dropping system for unmanned aerial vehicle |
| CN106741733A (en) * | 2016-12-30 | 2017-05-31 | 哈瓦国际航空技术（深圳）有限公司 | A kind of lifebuoy carry and unmanned plane of jettisoninging by several times |
| CN109110479A (en) * | 2018-07-04 | 2019-01-01 | 牛威 | A kind of unmanned plane base station goods and materials packet switching device |
| CN109616942A (en) * | 2018-12-10 | 2019-04-12 | 国家电网有限公司 | A kind of self-propelled distribution line inspection device |
| CN110466769A (en) * | 2019-08-02 | 2019-11-19 | 辽宁力德航空科技有限公司 | A kind of unmanned plane delivery device |
| CN110844072A (en) * | 2019-11-18 | 2020-02-28 | 中国船舶重工集团公司第七0七研究所 | Airborne drop-in type detector pod system |
| CN110906809A (en) * | 2019-11-22 | 2020-03-24 | 大连理工大学 | Large-size cylinder model clamping and throwing system and method |
-
2006
- 2006-04-05 CN CN 200620018998 patent/CN2875949Y/en not_active Expired - Fee Related
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102139761A (en) * | 2010-12-03 | 2011-08-03 | 中国船舶重工集团公司第七一○研究所 | Unpowered self-separated impact protection device |
| CN102139761B (en) * | 2010-12-03 | 2013-01-09 | 中国船舶重工集团公司第七一○研究所 | Unpowered self-separated impact protection device |
| CN102183352A (en) * | 2011-02-24 | 2011-09-14 | 西北工业大学 | Releasing mechanism used for releasing experiments |
| CN102183352B (en) * | 2011-02-24 | 2012-09-05 | 西北工业大学 | Releasing mechanism used for releasing experiments |
| CN103640697A (en) * | 2013-12-23 | 2014-03-19 | 景德镇陶瓷学院 | Cargo delivering device for unmanned helicopter |
| CN105217036A (en) * | 2014-06-13 | 2016-01-06 | 陕西飞机工业（集团）有限公司 | Traction air-drop parachuting unit |
| CN105667794A (en) * | 2016-03-19 | 2016-06-15 | 佛山市安尔康姆航空科技有限公司 | Bomb dropping system for unmanned aerial vehicle |
| CN106741733B (en) * | 2016-12-30 | 2018-12-11 | 哈瓦国际航空技术（深圳）有限公司 | A kind of gradation is jettisoninged lifebuoy carry and unmanned plane |
| CN106741733A (en) * | 2016-12-30 | 2017-05-31 | 哈瓦国际航空技术（深圳）有限公司 | A kind of lifebuoy carry and unmanned plane of jettisoninging by several times |
| CN109110479A (en) * | 2018-07-04 | 2019-01-01 | 牛威 | A kind of unmanned plane base station goods and materials packet switching device |
| CN109110479B (en) * | 2018-07-04 | 2020-06-02 | 深圳市汇智通咨询有限公司 | Unmanned aerial vehicle basic station goods and materials package auto-change over device |
| CN109616942A (en) * | 2018-12-10 | 2019-04-12 | 国家电网有限公司 | A kind of self-propelled distribution line inspection device |
| CN109616942B (en) * | 2018-12-10 | 2020-04-21 | 国家电网有限公司 | Self-propelled distribution lines inspection device |
| CN110466769A (en) * | 2019-08-02 | 2019-11-19 | 辽宁力德航空科技有限公司 | A kind of unmanned plane delivery device |
| CN110844072A (en) * | 2019-11-18 | 2020-02-28 | 中国船舶重工集团公司第七0七研究所 | Airborne drop-in type detector pod system |
| CN110906809A (en) * | 2019-11-22 | 2020-03-24 | 大连理工大学 | Large-size cylinder model clamping and throwing system and method |
| CN110906809B (en) * | 2019-11-22 | 2020-09-29 | 大连理工大学 | Large-size cylinder model clamping and throwing system and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: JIANGNAN INDUSTRIES GROUP CO., LTD. Free format text: FORMER NAME: JIANGNAN MACHINERY (GROUP) CO., LTD. |
|
| CP03 | Change of name, title or address |
Address after: Bamboo town Yuhu District 411207 Hunan city of Xiangtan Province Patentee after: Jiangnan Industries Group Co., Ltd. Address before: 411207 Hunan city of Xiangtan Province bamboo Patentee before: Jiangnan Machinery (Group) Co., Ltd. |
|
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20070307 Termination date: 20140405 |