CN110745253A - Accurate landing guiding device of unmanned aerial vehicle - Google Patents
Accurate landing guiding device of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN110745253A CN110745253A CN201911053295.8A CN201911053295A CN110745253A CN 110745253 A CN110745253 A CN 110745253A CN 201911053295 A CN201911053295 A CN 201911053295A CN 110745253 A CN110745253 A CN 110745253A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- anchor
- magnet piece
- apron
- 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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- 239000004677 Nylon Substances 0.000 claims abstract description 12
- 229920001778 nylon Polymers 0.000 claims abstract description 12
- 239000000725 suspension Substances 0.000 claims abstract description 11
- 230000002457 bidirectional effect Effects 0.000 claims abstract description 7
- 238000004804 winding Methods 0.000 claims abstract description 6
- 238000009434 installation Methods 0.000 abstract description 5
- 238000013459 approach Methods 0.000 abstract description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
- B64F1/025—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables using decelerating or arresting beds
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Road Signs Or Road Markings (AREA)
Abstract
The invention discloses an accurate landing guide device of an unmanned aerial vehicle, which comprises an apron and a suspension anchor box, wherein a first magnet piece is embedded in the center of the apron, and an installation bow is fixed above the suspension anchor box; a winding shaft is rotatably arranged in the suspension anchor box and driven by a bidirectional motor, a nylon wire is wound on the winding shaft, an anchor disc is hung below the nylon wire, and the shape of the anchor disc is consistent with that of an opening below the suspension anchor box; a second magnet piece is embedded below the anchor disc, and the upper magnetic pole of the first magnet piece is opposite to the lower magnetic pole of the second magnet piece; the bidirectional motor is in signal connection with the unmanned aerial vehicle remote control system. The invention is used for landing the unmanned aerial vehicle, the unmanned aerial vehicle releases the anchor plate above the parking apron, the anchor plate approaches the parking apron and is adsorbed on the parking apron through the magnetic force, the bidirectional motor rotates reversely to tighten the nylon thread, and the unmanned aerial vehicle is pulled to land.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an accurate landing guide device for an unmanned aerial vehicle.
Background
The rotor unmanned aerial vehicle lands on the moving apron very difficultly, tests the remote control technology of an operator very much, and leads the unmanned aerial vehicle to be broken down by a little carelessness.
Disclosure of Invention
The invention provides an accurate landing guide device for a rotor unmanned aerial vehicle, which aims to improve the landing accuracy of the rotor unmanned aerial vehicle on a mobile parking apron and reduce the difficulty of landing operation.
The technical scheme adopted by the invention for solving the technical problems is as follows: an unmanned aerial vehicle accurate landing guiding device comprises an apron and a suspension anchor box, wherein a first magnet piece is embedded in the center of the apron, and an installation bow is fixedly connected above the suspension anchor box; hang anchor incasement rotation and be provided with the spool, the spool is by two-way motor drive, the winding has the nylon yarn on the spool, the nylon yarn below has hung the anchor dish, the second magnet piece has been inlayed to the anchor dish below, the last magnetic pole of first magnet piece is opposite with the lower magnetic pole of second magnet piece.
Foretell an accurate landing guider of unmanned aerial vehicle, the installation bow is used for fixing in unmanned aerial vehicle's below.
Foretell accurate landing guider of unmanned aerial vehicle, two-way motor and unmanned aerial vehicle remote control system signal connection.
Foretell accurate landing guider of unmanned aerial vehicle, the appearance of anchor disc is unanimous with the below opening appearance of hanging the anchor case.
Foretell accurate landing guider of unmanned aerial vehicle, air park four corners is provided with fixed screw.
The invention is used for landing the unmanned aerial vehicle, the unmanned aerial vehicle releases the anchor plate above the parking apron, the anchor plate approaches the parking apron and is adsorbed on the parking apron through the magnetic force, the bidirectional motor rotates reversely to tighten the nylon thread, and the unmanned aerial vehicle is pulled to land.
Drawings
The invention is further illustrated with reference to the following figures and examples.
Fig. 1 is a structural diagram of an accurate landing guidance device of an unmanned aerial vehicle according to the present invention;
fig. 2 is a top view of an apron in the precise landing guidance device for an unmanned aerial vehicle according to the present invention.
In the figure: 1. parking apron; 2. suspending an anchor box; 3. mounting a bow; 11. a first magnet piece; 12. fixing screw holes; 21. a spool; 22. a bi-directional motor; 23. nylon thread; 24. an anchor disc; 25. a second magnet piece.
Detailed Description
In order to more clearly illustrate the technical solution of the present invention, the following further description is made with reference to the accompanying drawings, and it is obvious that the following described drawings are only one embodiment of the present invention, and it is within the scope of the present invention for a person of ordinary skill in the art to obtain other embodiments based on the drawings and the embodiment without any creative effort.
An unmanned aerial vehicle accurate landing guiding device comprises an apron 1 and a suspension anchor box 2, wherein a first magnet piece 11 is embedded in the center of the apron 1, and four corners of the apron 1 are provided with fixing screw holes 12; an installation bow 3 is fixedly connected above the suspension anchor box 2, and the installation bow 3 is used for being fixed below the unmanned aerial vehicle; hang 2 internal rotations of anchor case and be provided with spool 21, spool 21 is driven by two-way motor 22, two-way motor 22 and unmanned aerial vehicle remote control system signal connection, the winding has nylon yarn 23 on the spool 21, nylon yarn 23 below has hung anchor disc 24, the appearance of anchor disc 24 is unanimous with the below opening appearance of hanging anchor case 2, second magnet piece 25 has been inlayed to anchor disc 24 below, the last magnetic pole of first magnet piece 11 is opposite with the lower magnetic pole of second magnet piece 25.
The application of the accurate landing guiding device of the unmanned aerial vehicle is used for landing of the unmanned aerial vehicle, the unmanned aerial vehicle receives signals of a remote control system, the bidirectional motor 22 works to drive the winding shaft 21 to rotate, the anchor disc 24 is released above the parking apron, the anchor disc 24 is close to the parking apron and is adsorbed on the parking apron through the magnetic action, the bidirectional motor 22 rotates reversely to tighten the nylon silk thread 23, and the unmanned aerial vehicle is pulled to land.
The above embodiments are only exemplary embodiments of the present invention, and are not intended to limit the present invention, and the scope of the present invention is defined by the claims. Various modifications and equivalents may be made by those skilled in the art within the spirit and scope of the present invention, and such modifications and equivalents should also be considered as falling within the scope of the present invention.
Claims (5)
1. An unmanned aerial vehicle accurate landing guiding device comprises an apron (1) and a suspension anchor box (2), wherein a first magnet piece (11) is embedded in the center of the apron (1), and a mounting bow (3) is fixedly connected above the suspension anchor box (2); hang anchor case (2) internal rotation and be provided with spool (21), spool (21) are driven by two-way motor (22), the winding has nylon silk thread (23) on spool (21), nylon silk thread (23) below has hung anchor disc (24), second magnet piece (25) have been inlayed to anchor disc (24) below, the last magnetic pole of first magnet piece (11) is opposite with the lower magnetic pole of second magnet piece (25).
2. An apparatus as claimed in claim 1, wherein the mounting bow (3) is adapted to be fixed under the drone.
3. An unmanned aerial vehicle precision landing guidance device of claim 1, wherein the bidirectional motor (22) is in signal connection with an unmanned aerial vehicle remote control system.
4. An unmanned aerial vehicle accurate landing guiding device according to claim 1, wherein the shape of the anchor disc (24) is consistent with the shape of the lower opening of the suspension anchor box (2).
5. The precise landing guiding device for unmanned aerial vehicle as claimed in claim 1, wherein the parking apron (1) is provided with fixing screw holes (12) at four corners.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911053295.8A CN110745253A (en) | 2019-10-31 | 2019-10-31 | Accurate landing guiding device of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911053295.8A CN110745253A (en) | 2019-10-31 | 2019-10-31 | Accurate landing guiding device of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110745253A true CN110745253A (en) | 2020-02-04 |
Family
ID=69281563
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911053295.8A Pending CN110745253A (en) | 2019-10-31 | 2019-10-31 | Accurate landing guiding device of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110745253A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3020633A1 (en) * | 2014-11-12 | 2016-05-18 | Vyzkumny utav melioraci a ochrany pudy, v.v.l. | Flight control unit for tied unmanned aerial vehicle models |
| CN105775112A (en) * | 2016-03-21 | 2016-07-20 | 安徽钰龙信息科技有限公司 | Four-shaft unmanned aerial vehicle taking-off and landing device |
| CN107406150A (en) * | 2015-02-05 | 2017-11-28 | 埃柔波提克斯有限公司 | Landing and charging system for unmanned plane |
| CN207712312U (en) * | 2017-12-05 | 2018-08-10 | 普达迪泰（天津）智能装备科技有限公司 | A kind of rotor wing unmanned aerial vehicle auxiliary landing device |
| CN211766361U (en) * | 2019-10-31 | 2020-10-27 | 绍兴文理学院元培学院 | Accurate landing guiding device of unmanned aerial vehicle |
-
2019
- 2019-10-31 CN CN201911053295.8A patent/CN110745253A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3020633A1 (en) * | 2014-11-12 | 2016-05-18 | Vyzkumny utav melioraci a ochrany pudy, v.v.l. | Flight control unit for tied unmanned aerial vehicle models |
| CN107406150A (en) * | 2015-02-05 | 2017-11-28 | 埃柔波提克斯有限公司 | Landing and charging system for unmanned plane |
| CN105775112A (en) * | 2016-03-21 | 2016-07-20 | 安徽钰龙信息科技有限公司 | Four-shaft unmanned aerial vehicle taking-off and landing device |
| CN207712312U (en) * | 2017-12-05 | 2018-08-10 | 普达迪泰（天津）智能装备科技有限公司 | A kind of rotor wing unmanned aerial vehicle auxiliary landing device |
| CN211766361U (en) * | 2019-10-31 | 2020-10-27 | 绍兴文理学院元培学院 | Accurate landing guiding device of unmanned aerial vehicle |
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