CN104443413A - Unmanned aerial vehicle withdrawing equipment - Google Patents
Unmanned aerial vehicle withdrawing equipment Download PDFInfo
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- CN104443413A CN104443413A CN201310417636.1A CN201310417636A CN104443413A CN 104443413 A CN104443413 A CN 104443413A CN 201310417636 A CN201310417636 A CN 201310417636A CN 104443413 A CN104443413 A CN 104443413A
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- aerial vehicle
- unmanned aerial
- unmanned plane
- withdrawing equipment
- hook
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Abstract
The invention discloses unmanned aerial vehicle withdrawing equipment, and relates to improvement on unmanned aerial vehicle withdrawing equipment. The unmanned aerial vehicle withdrawing equipment comprises an unmanned aerial vehicle and two walking vehicles, and is characterized in that telescopic rods are arranged on the upper sides of the two walking vehicles, and the upper ends of the two telescopic rods are connected with each other by a connecting rod; a hook is arranged at the bottom of the unmanned aerial vehicle via a steel wire rope. The unmanned aerial vehicle withdrawing equipment has the advantages that the unmanned aerial vehicle withdrawing equipment is simple in structure and free of constraints of external conditions and is safe and reliable.
Description
Technical field
the present invention relates to a kind of improvement of unmanned aerial vehicle reclaiming scrap.
Background technology
small-sized pilotless aircraft can carry shooting instrument, when being subject to the disasters such as earthquake, does relief observation.By small-sized pilotless aircraft, can realize being difficult to people the region low-latitude flying that enters, and monitor.But taking off and landing substantially the same with there being people's aircraft of small-sized pilotless aircraft, needs longer dragging track.
because satisfactory track is less, therefore, unmanned aerial vehicle at present also cannot free flight, especially occurs near area in disaster, does not well take off especially, place of landing.This is also the biggest obstacle of small-sized pilotless aircraft on using.
at present, for the situation that small-sized pilotless aircraft takes off, the unmanned aerial vehicle that many builds are less uses the method for catapult-assisted take-off, therefore, without the need to larger place of taking off.But the landing of unmanned aerial vehicle but still needs very large place.
usually, in order to reclaim robot airplane in less place, needing to discharge parachute, miniature self-service is driven an airplane abrupts deceleration, robot airplane reclaims by the net that then employing one is vertical.
at present, there is one on the market, utilize the net perpendicular to ground to carry out reclaiming the method for unmanned aerial vehicle, this regenerative apparatus is comparatively easily arranged, but, time it lands, need to use the cushions such as balloon, and, in net and unmanned aerial vehicle contact process, due to the constructional feature of unmanned plane, wing and fuselage joint are easily damaged.
in addition, owing to adopting net to reclaim unmanned plane, need unmanned plane level to pour in net, this just needs netting gear to have enough areas; In order to this adds the recovery difficult of unmanned plane virtually.And if increase the area of net, at strong wind weather, net and unmanned plane, all by large wind effect, make the recovery difficult of unmanned plane increase substantially, very easily cause damage to unmanned plane.
Summary of the invention
the present invention is exactly for the problems referred to above, provides a kind of structure simple, safe and reliable, not by the unmanned aerial vehicle reclaiming scrap of external condition restriction.
for realizing above-mentioned purpose of the present invention, the present invention adopts following technical scheme, the present invention includes unmanned plane and two moving trolleys, it is characterized in that: be provided with expansion link above two moving trolleys, and the upper end of two expansion links is connected by connecting rod; Bottom described unmanned plane, steel rope is provided with hook.
described hook is set to W shape, and the top mid point that steel rope is linked up with W shape is connected.
beneficial effect of the present invention: when the present invention uses, by moving trolley, moves to correct position, is then fixed on expansion link by the two ends of connecting rod; Lift telescopic bar is to proper height, and when unmanned plane flies over, the hook on steel rope can hook connecting rod, unmanned plane is moved in a circle, and the speed of unmanned plane reduces along with the carrying out of circular movement, finally becomes and swings on connecting rod, finally stop again, hang on connecting rod; Unmanned plane can be reclaimed.
the present invention is easy to use, is not afraid of large wind effect; And, can different terrain be adapted to.The ground error that causes of injustice can be made up, strong adaptability by the two expansion links different length that stretches.
Accompanying drawing explanation
fig. 1 is structural representation of the present invention.
in accompanying drawing, q is hook, k is expansion link, r is steel rope, p is unmanned plane, j is connecting rod.
Detailed description of the invention
the present invention includes unmanned plane p and two moving trolleys, be provided with expansion link k above two moving trolleys, the upper end of two expansion link k is connected by connecting rod j; Bottom described unmanned plane p, steel rope r is provided with hook q.
described hook q is set to W shape, and steel rope r is connected with the top mid point of W shape hook q.
when the present invention uses, by moving trolley, move to correct position, then the two ends of connecting rod j are fixed on expansion link k; Lift telescopic bar k is to proper height, and when unmanned plane p flies over, the hook q on steel rope r can hook connecting rod j, unmanned plane p is moved in a circle, and the speed of unmanned plane p reduces along with the carrying out of circular movement, finally becomes and swings on connecting rod j, finally stop again, hang on connecting rod j; Unmanned plane p can be reclaimed.
the present invention is easy to use, is not afraid of large wind effect; And, can different terrain be adapted to.The ground error that causes of injustice can be made up, strong adaptability by the two expansion link k different length that stretches.
Claims (2)
1. unmanned aerial vehicle reclaiming scrap, comprises unmanned plane and two moving trolleys, it is characterized in that: be provided with expansion link above two moving trolleys, and the upper end of two expansion links is connected by connecting rod; Bottom described unmanned plane, steel rope is provided with hook.
2. unmanned aerial vehicle reclaiming scrap according to claim 1, is characterized in that, described hook is set to W shape, and the top mid point that steel rope is linked up with W shape is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310417636.1A CN104443413A (en) | 2013-09-14 | 2013-09-14 | Unmanned aerial vehicle withdrawing equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310417636.1A CN104443413A (en) | 2013-09-14 | 2013-09-14 | Unmanned aerial vehicle withdrawing equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104443413A true CN104443413A (en) | 2015-03-25 |
Family
ID=52890325
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310417636.1A Pending CN104443413A (en) | 2013-09-14 | 2013-09-14 | Unmanned aerial vehicle withdrawing equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104443413A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081147A (en) * | 2016-08-23 | 2016-11-09 | 成都翼高九天科技有限公司 | A kind of SUAV indoor retracting device |
| CN106672256A (en) * | 2016-12-15 | 2017-05-17 | 南京航空航天大学 | Cord-hook recovery device based on rubber string damping rope |
| CN107284662A (en) * | 2016-04-11 | 2017-10-24 | 周良勇 | A kind of multi-rotor unmanned aerial vehicle suspension bracket |
| CN107697303A (en) * | 2017-09-27 | 2018-02-16 | 北京航空航天大学 | A kind of unmanned plane space base retracting device and method based on the stable target system of aviation pull-type |
| CN109906186A (en) * | 2016-09-21 | 2019-06-18 | 兹普澜国际股份有限公司 | Automation recovery system for UAV |
| CN111077903A (en) * | 2019-12-12 | 2020-04-28 | 南京航空航天大学 | High-fault-tolerance skyhook recovery method based on window decision |
-
2013
- 2013-09-14 CN CN201310417636.1A patent/CN104443413A/en active Pending
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107284662A (en) * | 2016-04-11 | 2017-10-24 | 周良勇 | A kind of multi-rotor unmanned aerial vehicle suspension bracket |
| CN106081147A (en) * | 2016-08-23 | 2016-11-09 | 成都翼高九天科技有限公司 | A kind of SUAV indoor retracting device |
| CN106081147B (en) * | 2016-08-23 | 2019-03-26 | 成都翼高九天科技有限公司 | Recyclable device in a kind of small drone room |
| CN109906186A (en) * | 2016-09-21 | 2019-06-18 | 兹普澜国际股份有限公司 | Automation recovery system for UAV |
| CN109906186B (en) * | 2016-09-21 | 2022-09-06 | 兹普澜国际股份有限公司 | Automated recovery system for unmanned aerial vehicle |
| CN106672256A (en) * | 2016-12-15 | 2017-05-17 | 南京航空航天大学 | Cord-hook recovery device based on rubber string damping rope |
| CN106672256B (en) * | 2016-12-15 | 2018-04-03 | 南京航空航天大学 | A kind of rope hook retracting device based on elastic damping rope |
| CN107697303A (en) * | 2017-09-27 | 2018-02-16 | 北京航空航天大学 | A kind of unmanned plane space base retracting device and method based on the stable target system of aviation pull-type |
| CN111077903A (en) * | 2019-12-12 | 2020-04-28 | 南京航空航天大学 | High-fault-tolerance skyhook recovery method based on window decision |
| CN111077903B (en) * | 2019-12-12 | 2021-11-16 | 南京航空航天大学 | High-fault-tolerance skyhook recovery method based on window decision |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150325 |