CN201914468U - Net collision recovery device of unmanned aerial vehicle - Google Patents
Net collision recovery device of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN201914468U CN201914468U CN2010206790364U CN201020679036U CN201914468U CN 201914468 U CN201914468 U CN 201914468U CN 2010206790364 U CN2010206790364 U CN 2010206790364U CN 201020679036 U CN201020679036 U CN 201020679036U CN 201914468 U CN201914468 U CN 201914468U
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- net
- aerial vehicle
- unmanned aerial
- unmanned plane
- supporting rod
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Abstract
The utility model relates to a net collision recovery device of an unmanned aerial vehicle, which utilizes a pulley drive mechanism to realize an energy absorption function, and safely recoveries the unmanned aerial vehicle. The net collision recovery device of the unmanned aerial vehicle has a structure that: the bottom ends of vertical support rods are fixed on a base, and the top ends of the vertical support rods are connected with a lateral support rod; a horizontal slideway is arranged on the lateral support rod, a trolley is arranged on the horizontal slideway, and a contraction cable is connected onto the trolley; a net is arranged between the two vertical support rods, and the upper and the lower traction belts of the net are connected with the contraction cable; and one end of an oblique slideway is connected with the vertical support rods, and the other end of the oblique slideway is connected with the horizontal slideway. The net collision recovery device of the unmanned aerial vehicle can limit the unmanned aerial vehicle in the recovery field, and the unmanned aerial vehicle is safely recovered in a net collision recovery mode under the condition that conventional slide descending or parachute descending cannot be carried out, so the application scope of the unmanned aerial vehicle is widened.
Description
Technical field
The utility model relates to a kind of unmanned plane regenerative apparatus, relates in particular to a kind of unmanned plane and hits the net regenerative apparatus, realizes energy-absorbing function by pulley drive mechanism, and safety reclaims unmanned plane.
Background technology
Unmanned plane is the not manned craft of controlling by radio robot or airborne computer stored program controlled.Unmanned plane not only can be finished the task that manned aircraft is carried out, and more is applicable to the task that people's aircraft should not be carried out.
In the prior art, the mode that unmanned plane reclaims is generally: 1. land automatically.Its landing mission is identical with manned aircraft, is landed on runway by remote control equipment (RCE) or machine internal program control setup operating aircraft by the ground controlling personnel.2. parachute reclaims.Have parachute on the unmanned plane, landing period is opened automatically, or opens according to telecommand, and parachute is hanging the unmanned plane landing that slowly descends slowly and lightly.3. reclaim in the air.The program of beginning is identical with the parachute way of recycling, when unmanned plane releases a parachute when aloft descending slowly and lightly, reclaims machine tool with helicopter etc. and aloft unmanned plane is reclaimed, and carry back the field landing.
But along with the application of unmanned plane more and more widely, the landing environment of unmanned plane becomes increasingly complex, the safety that therefore conventional landing modes can't satisfy unmanned plane reclaims requirement.In addition, still do not have at present by hitting the net way of recycling and carry out the exemplary application that unmanned plane reclaims.
Summary of the invention
The utility model is at above-mentioned problems of the prior art, provide a kind of safe and effective a kind of unmanned plane to hit the net regenerative apparatus, solve in the prior art unmanned plane and reclaimed the place when limited, the problem that can't reclaim safely, and also the utility model cost is lower.
To achieve these goals, the technical solution of the utility model is as follows:
The bottom of vertical supporting rod is fixed on the base, and the top of vertical supporting rod links to each other with transverse supporting rod; Transverse supporting rod is provided with horizontal slideway, and horizontal slideway is provided with coaster, is connected with the contraction rope on the coaster; Be provided with net between two vertical supporting rods, the upper and lower traction belt of net is connected with the contraction rope; One end of inclined ramp links to each other with vertical supporting rod, and the other end of inclined ramp and horizontal slideway join.
The heading of described transverse supporting rod and unmanned plane in the same way.
Described horizontal slideway and inclined ramp intersect at the outermost end of transverse supporting rod.
The contract by distance of described contraction rope is 2 times of coaster sliding distance.
The utility model has the advantages of as follows:
The utility model can make unmanned plane limited in the recovery place, can't carry out under the situation of conventional downhill race or parachuting, realize that by hitting the net way of recycling safety of unmanned plane reclaims, widened the application of unmanned plane, simultaneously, the utility model scientific structure design is reasonable, safe and effective, cost is lower, efficiently motor-driven, and the vast market demand is arranged, and is easy to apply.
Description of drawings
Below, in conjunction with the accompanying drawings, the utility model is elaborated.
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is a construction profile scheme drawing of the present utility model.
Fig. 3 is the partial schematic diagram of Fig. 2.
Fig. 4 is the partial schematic diagram of Fig. 1.
Among the figure, 1, net, 2, transverse supporting rod, 3, horizontal slideway, 4, base, 5, vertical supporting rod, 6, inclined ramp, 7, coaster, 8, shrink rope.
The specific embodiment
Embodiment
As shown in the figure, use Fast Installation modes such as being threaded, selling connection that whole device is connected and fixed, guarantee transverse supporting rod 2 and unmanned plane during flying direction in the same way.The bottom of vertical supporting rod 5 is fixed on the base 4, and the top of vertical supporting rod 5 links to each other with transverse supporting rod 2; Transverse supporting rod 2 is provided with horizontal slideway 3, and horizontal slideway 3 is provided with coaster 7, is connected with on the coaster 7 to shrink rope 8; Be provided with net 1 between two vertical supporting rods 5, the upper and lower traction belt of net 1 is connected with contraction rope 8, and the contract by distance of shrinking rope 8 is 2 times of coaster 7 sliding distances; One end of inclined ramp 6 links to each other with vertical supporting rod 5, and the other end of inclined ramp 6 and horizontal slideway 3 intersect at the outermost end of transverse supporting rod 2.
Principle of work of the present utility model and process are as follows:
When unmanned plane bumped against net 1, net 1 travelled forward under the drive of unmanned plane, and last traction belt, slides at the drive lower edge inclined ramp 6 that shrinks rope 8 with traction belt at present to front slide obliquely upward along horizontal slideway 3.When upper and lower traction belt slided into same position, net 1 formed a pocketed structure unmanned plane is coated on wherein, thereby the net that hits of realizing unmanned plane reclaims function.
The design of running block guarantees that the contract by distance of contraction rope 8 is 2 times of coaster 7 sliding distances on the coaster 7, thereby the upper and lower traction belt that guarantees net 1 can slide into same position simultaneously, and following traction belt can not slide back again, thereby realizes auto-lock function, guarantees to hit the reliability of net regenerative apparatus.
Protection domain of the present utility model is not subjected to the restriction of specific embodiment, is as the criterion with claim.
Claims (4)
1. a unmanned plane hits the net regenerative apparatus, it is characterized in that the bottom of vertical supporting rod (5) is fixed on the base (4), and the top of vertical supporting rod (5) links to each other with transverse supporting rod (2); Transverse supporting rod (2) is provided with horizontal slideway (3), and horizontal slideway (3) is provided with coaster (7), is connected with on the coaster (7) to shrink rope (8); Be provided with net (1) between two vertical supporting rods (5), the upper and lower traction belt of net (1) is connected with contraction rope (8); One end of inclined ramp (6) links to each other with vertical supporting rod (5), and the other end of inclined ramp (6) and horizontal slideway (3) join.
2. a kind of unmanned plane according to claim 1 hits the net regenerative apparatus, and the heading that it is characterized in that described transverse supporting rod (2) and unmanned plane in the same way.
3. a kind of unmanned plane according to claim 2 hits the net regenerative apparatus, it is characterized in that described horizontal slideway (3) and inclined ramp (6) intersect at the outermost end of transverse supporting rod (2).
4. a kind of unmanned plane according to claim 1 hits the net regenerative apparatus, and the contract by distance that it is characterized in that described contraction rope (8) is 2 times of coaster (7) sliding distance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010206790364U CN201914468U (en) | 2010-12-24 | 2010-12-24 | Net collision recovery device of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010206790364U CN201914468U (en) | 2010-12-24 | 2010-12-24 | Net collision recovery device of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201914468U true CN201914468U (en) | 2011-08-03 |
Family
ID=44414276
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010206790364U Expired - Fee Related CN201914468U (en) | 2010-12-24 | 2010-12-24 | Net collision recovery device of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201914468U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102040004A (en) * | 2010-12-24 | 2011-05-04 | 沈阳航天新光集团有限公司 | Net recovery device for unmanned aerial vehicle |
| CN106945839A (en) * | 2016-01-06 | 2017-07-14 | 吕智慧 | Flight instruments and its flying method |
-
2010
- 2010-12-24 CN CN2010206790364U patent/CN201914468U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102040004A (en) * | 2010-12-24 | 2011-05-04 | 沈阳航天新光集团有限公司 | Net recovery device for unmanned aerial vehicle |
| CN102040004B (en) * | 2010-12-24 | 2013-03-06 | 沈阳航天新光集团有限公司 | Net recovery device for unmanned aerial vehicle |
| CN106945839A (en) * | 2016-01-06 | 2017-07-14 | 吕智慧 | Flight instruments and its flying method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110803 Termination date: 20131224 |