CN105711821B - A kind of SUAV landing pintle mechanism - Google Patents
A kind of SUAV landing pintle mechanism Download PDFInfo
- Publication number
- CN105711821B CN105711821B CN201610063068.3A CN201610063068A CN105711821B CN 105711821 B CN105711821 B CN 105711821B CN 201610063068 A CN201610063068 A CN 201610063068A CN 105711821 B CN105711821 B CN 105711821B
- Authority
- CN
- China
- Prior art keywords
- connecting rod
- axis hole
- end axis
- unmanned plane
- pintle
- 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
- B64C25/00—Alighting gear
- B64C25/68—Arrester hooks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
Abstract
The present invention provides a kind of SUAV landing pintle mechanism, including unmanned plane tail boom, pintle bar, fourth link, third connecting rod, second connecting rod, first connecting rod, worm type of reduction gearing, bearing pin, pass through above part, form link-type pintle jack, it is simple and convenient, dead point is formed when putting down, it is reliable in impact force action lower stress, fold and place when packing up, reduce space-consuming；And driven using servomotor, on the basis of the unmanned plane confined space and load-carrying, avoid the hydraulic system of complexity.
Description
Technical field
The present invention provides a kind of SUAV landing pintle mechanism, belongs to SUAV landing pintle designing technique neck
Domain.
Background technology
With the progress and expanding economy of science and technology, unmanned air vehicle technique is more and more come into the sight of the public, especially
In military field, Shipborne UAV is increasingly paid close attention to by various countries, and the landing pintle design of Shipborne UAV is also more next to be protruded；
Civil area, due to the limitation in the place of landing, catapult-assisted take-off and block landing and be increasingly taken seriously, design one will weaken pair
The requirement in place, two will can save power, reduce the high request to unmanned plane load-carrying and space.
The content of the invention
In view of the above-mentioned problems, the present invention provides a kind of SUAV landing pintle mechanism, its is simple and reliable, convenient easy
OK.
To achieve the above object, the technology path that uses of the present invention for：A kind of SUAV landing pintle mechanism, including
Unmanned plane tail boom, pintle bar, fourth link, third connecting rod, second connecting rod, first connecting rod, worm type of reduction gearing, bearing pin, its
It is characterised by：Described unmanned plane tail boom is a part for unmanned plane main body, and the upper end axis hole of pintle bar passes through bearing pin and nobody
Tail beam is rotatablely connected, and one end axis hole of fourth link is rotatablely connected by the intermediate shaft hole of bearing pin and pintle bar, fourth link
Other end axis hole be rotatablely connected by one end axis hole of bearing pin and third connecting rod, the other end axis hole of third connecting rod passes through bearing pin
It is rotatablely connected with the tail end axis hole of unmanned plane tail boom, the connection of the forked end axis hole and fourth link and third connecting rod of second connecting rod
Place is rotatedly connected, it is ensured that second connecting rod can drive fourth link and third connecting rod to link, and the other end axis hole of second connecting rod passes through
One end axis hole of bearing pin and first connecting rod is rotatedly connected, and the other end axis hole of first connecting rod is fixedly connected on worm type of reduction gearing
Worm-gear output shaft on, worm type of reduction gearing is fixedly mounted on unmanned plane tail boom.
The present invention uses above technical scheme, has advantages below：Link-type pintle jack, it is simple and convenient, put down
When form dead point, it is reliable in impact force action lower stress, when packing up fold place, reduce space-consuming；Driven using servomotor
It is dynamic, on the basis of the unmanned plane confined space and load-carrying, avoid the hydraulic system of complexity.
Brief description of the drawings
Fig. 1 is the measurements of the chest, waist and hips model schematic of the present invention.
Drawing reference numeral：1- unmanned plane tail booms；2- pintle bars；3- fourth links；4- third connecting rods；5- second connecting rods；6-
One connecting rod；7-- worm type of reduction gearings；8- bearing pins.
Embodiment
With reference to specific embodiment, the invention will be further described, the illustrative examples and explanation invented herein
For explaining the present invention, but it is not as a limitation of the invention.
As shown in figure 1, a kind of SUAV landing pintle mechanism, including unmanned plane tail boom 1, pintle bar 2, fourth link
3rd, third connecting rod 4, second connecting rod 5, first connecting rod 6, worm type of reduction gearing 7, bearing pin 8, it is characterised in that：Described unmanned plane
Tail boom 1 is a part for unmanned plane main body, and the upper end axis hole of pintle bar 2 is rotatablely connected by bearing pin 8 and unmanned plane tail boom 1, the
One end axis hole of double leval jib 3 is rotatablely connected by the intermediate shaft hole of bearing pin 8 and pintle bar 2, and the other end axis hole of fourth link 3 leads to
One end axis hole for crossing bearing pin 8 and third connecting rod 4 is rotatablely connected, and the other end axis hole of third connecting rod 4 passes through bearing pin 8 and unmanned tail
The tail end axis hole rotation connection of beam 1, forked end axis hole and the junction of fourth link 3 and third connecting rod 4 of second connecting rod 5 rotate
It is connected, it is ensured that second connecting rod 5 can drive fourth link 3 and third connecting rod 4 to link, and the other end axis hole of second connecting rod 5 passes through pin
One end axis hole of axle 8 and first connecting rod 6 is rotatedly connected, and the other end axis hole of first connecting rod 6 is fixedly connected on worm and gear deceleration
On the worm-gear output shaft of device 7, worm type of reduction gearing 7 is fixedly mounted on unmanned plane tail boom 1.
The present invention concrete operating principle be：When unmanned plane lands, worm type of reduction gearing 7 starts, and drives first connecting rod 6
To lower swing, by the linkage of second connecting rod 5 and third connecting rod 4 and fourth link 3, put down pintle bar 2, when third connecting rod 4
Stop the action of worm type of reduction gearing 7 when conllinear with fourth link 3, at this moment pintle bar 2 prepares to catch on check cable landing；Work as drop
Complete after work(, worm type of reduction gearing 7 reversely starts, and makes the folding and retraction of pintle bar 2, Automatic-falling again by the linkage of connecting rod
Check cable, execution process.
Claims (1)
1. a kind of SUAV landing pintle mechanism, including unmanned plane tail boom（1）, pintle bar（2）, fourth link（3）, the 3rd
Connecting rod（4）, second connecting rod（5）, first connecting rod（6）, worm type of reduction gearing（7）, bearing pin（8）, it is characterised in that：Described nothing
Man-machine tail boom（1）For a part for unmanned plane main body, pintle bar（2）Upper end axis hole pass through bearing pin（8）With unmanned plane tail boom（1）
Rotation connection, fourth link（3）One end axis hole pass through bearing pin（8）With pintle bar（2）Intermediate shaft hole rotation connection, the 4th connect
Bar（3）Other end axis hole pass through bearing pin（8）With third connecting rod（4）The rotation connection of one end axis hole, third connecting rod（4）It is another
End axis hole passes through bearing pin（8）With unmanned plane tail boom（1）Tail end axis hole rotation connection, second connecting rod（5）Forked end axis hole with
Fourth link（3）And third connecting rod（4）Junction be rotatedly connected, it is ensured that second connecting rod（5）Fourth link can be driven（3）With
Three connecting rods（4）Linkage, second connecting rod（5）Other end axis hole pass through bearing pin（8）With first connecting rod（6）One end axis hole rotate phase
Even, first connecting rod（6）Other end axis hole be fixedly connected on worm type of reduction gearing（7）Worm-gear output shaft on, worm and gear
Decelerator（7）It is fixedly mounted on unmanned plane tail boom（1）On.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610063068.3A CN105711821B (en) | 2016-01-30 | 2016-01-30 | A kind of SUAV landing pintle mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610063068.3A CN105711821B (en) | 2016-01-30 | 2016-01-30 | A kind of SUAV landing pintle mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105711821A CN105711821A (en) | 2016-06-29 |
| CN105711821B true CN105711821B (en) | 2018-01-02 |
Family
ID=56155378
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610063068.3A Active CN105711821B (en) | 2016-01-30 | 2016-01-30 | A kind of SUAV landing pintle mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105711821B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113148124B (en) * | 2021-05-19 | 2021-12-21 | 宜宾职业技术学院 | Unmanned aerial vehicle sliding landing arresting mechanism |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2428684A (en) * | 1945-03-28 | 1947-10-07 | Ryan Aeronautical Co | Arresting hook retracting mechanism |
| CN203727645U (en) * | 2014-03-20 | 2014-07-23 | 鲁京 | Hook locking mechanism of unmanned aerial vehicle |
| CN104176246A (en) * | 2014-09-17 | 2014-12-03 | 江西洪都航空工业集团有限责任公司 | Arresting hook retracting and releasing mechanism |
| CN204297115U (en) * | 2014-06-09 | 2015-04-29 | 李岗 | A kind of aircraft short field take-off help-fly lock |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0439199U (en) * | 1990-07-31 | 1992-04-02 |
-
2016
- 2016-01-30 CN CN201610063068.3A patent/CN105711821B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2428684A (en) * | 1945-03-28 | 1947-10-07 | Ryan Aeronautical Co | Arresting hook retracting mechanism |
| CN203727645U (en) * | 2014-03-20 | 2014-07-23 | 鲁京 | Hook locking mechanism of unmanned aerial vehicle |
| CN204297115U (en) * | 2014-06-09 | 2015-04-29 | 李岗 | A kind of aircraft short field take-off help-fly lock |
| CN104176246A (en) * | 2014-09-17 | 2014-12-03 | 江西洪都航空工业集团有限责任公司 | Arresting hook retracting and releasing mechanism |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105711821A (en) | 2016-06-29 |
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Legal Events
| Date | Code | Title | Description |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20170803 Address after: 510640 Guangdong City, Tianhe District Province, No. five, road, public education building, unit 371-1, unit 2401 Applicant after: Guangdong Gaohang Intellectual Property Operation Co., Ltd. Address before: Hebei Street West Harbor area, 066004 Hebei city of Qinhuangdao province No. 438 School of mechanical engineering Yanshan University Applicant before: Feng Shengbing |
|
| TA01 | Transfer of patent application right | ||
| CB03 | Change of inventor or designer information |
Inventor after: He Chen Inventor after: Yang Hongzhen Inventor after: Lu Xiaofan Inventor after: Wang Yunye Inventor after: Wang Yanbo Inventor after: Jin Lanju Inventor after: Shi Junxiao Inventor after: Wang Zhen Inventor after: Fang Xiaofeng Inventor before: The inventor has waived the right to be mentioned |
|
| TA01 | Transfer of patent application right |
Effective date of registration: 20171206 Address after: 310000 Huanglong Road, 8, Hangzhou, Zhejiang Province, room 641 Applicant after: Information communication branch office of Guo Wang Zhejiang Electric Power Company Applicant after: State Grid Zhejiang Electric Power Company Applicant after: State Grid Corporation of China Address before: 510640 Guangdong City, Tianhe District Province, No. five, road, public education building, unit 371-1, unit 2401 Applicant before: Guangdong Gaohang Intellectual Property Operation Co., Ltd. |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |