CN204916215U - A automatic coiling and uncoiling device for mooring unmanned aerial vehicle aircraft - Google Patents
A automatic coiling and uncoiling device for mooring unmanned aerial vehicle aircraft Download PDFInfo
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- CN204916215U CN204916215U CN201520577471.9U CN201520577471U CN204916215U CN 204916215 U CN204916215 U CN 204916215U CN 201520577471 U CN201520577471 U CN 201520577471U CN 204916215 U CN204916215 U CN 204916215U
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- cable
- ball
- mooring
- guide wheel
- sleeve
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Abstract
The utility model discloses an automatic coiling and uncoiling device for mooring unmanned aerial vehicle aircraft, including swinging boom and cable dish, swinging boom one end connect drive arrangement, the outer ends of swinging boom has the line of a walking sleeve, the aircraft is connected through walking the line sleeve from the cable dish to the cable conductor, the line sleeve of walking include sleeve ring, the sleeve ring has the ball grooves of a plurality of installation balls, the ball is installed at the ball inslot, the ball is half -naked dew state at the opening part in ball groove. The utility model discloses in, the swinging boom passes through drive arrangement and drives rotatoryly, accomplishes receiving and releasing of in cable dish cable conductor, and the drum of rotation of arm is efficient, and is effectual moreover, and the cable conductor can be in sliding contact with the intra -annular ball of sleeve, prevents that the speed of receiving and releasing of rolling up or blocking dead phenomenon, the cable conductor that promotes moreover from appearing beating in the cable conductor.
Description
Technical field
The utility model relates to a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device.
Background technology
Mooring unmanned plane commercially occurs, also there is the take-up and pay-off device for mooring unmanned plane thereupon, the mooring unmanned plane take-up and pay-off device of current existence only can realize passive unwrapping wire along with unmanned plane during flying, and can not realize automatic takeup along with unmanned plane landing; When unmanned plane lands, take-up and pay-off device needs manual rotation's take-up to carry out take-up, works heavy, simultaneously when artificial not timely by unnecessary power cable income take-up and pay-off device time, unnecessary power cable very easily occurs that tangled up and knotted causes potential safety hazard; So need a kind of automatic lock take-up for mooring unmanned plane badly to solve the problem.
Summary of the invention
For above-mentioned prior art Problems existing, the utility model provides a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device, realizes the orderly folding and unfolding of cable, has rationally distributed, compact conformation and safe and reliable.
To achieve these goals, the technical solution adopted in the utility model is: a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device, comprise pivot arm and cable disc, described one end connecting drive device, the outboard end of pivot arm has cabling sleeve, and cable connects aircraft by cabling sleeve from cable disc.
Described cabling sleeve comprises liner ring, and liner ring has the ball grooves of multiple installation ball, and ball is arranged in ball grooves, and ball is half naked state at the opening part of ball grooves.
This device also comprises induction installation, and induction installation comprises cable guide pulley, range finding guide wheel and pressure sensor guide wheel,
Cable is through cable guide pulley, range finding guide wheel and pressure sensor guide wheel, and cable is wrapped on pressure sensor guide wheel by cable guide pulley and forms a plumbness; Cable is walked around range finding guide wheel by pressure sensor guide wheel and is passed cabling sleeve and put in order in cable disc.
Described aircraft is many rotor wing unmanned aerial vehicles aircraft, and its rotor quantity is four rotors, six rotors, eight rotors or 16 rotors.
Also comprise controller, floor power supply device and mooring electric supply installation, controller carrys out accessory drive for computing information, signal,
Cable comprises two wires, the two ends of two wires respectively with floor power supply device and mooring electric supply installation; Described mooring electric supply installation is used for the later backup power of floor power supply device power-off, needs and power for position detecting device for forced landing.
It is simple that the automatic deploying and retracting line apparatus of mooring unmanned plane during flying device of the present invention has structure, reliability is high, hovering is stable, the feature such as easy to use and with low cost, mooring mode is applied to many rotor wing unmanned aerial vehicles, solve tethered platform in stability, erection comfort feature, use the ubiquitous problems in aspect such as alerting ability, in whole device, pivot arm is by actuating device driven rotary, carry out the folding and unfolding of cable in cable disc 3, the drum efficiency that arm rotates is high, and it is effective, cable 4 can be in moving contact with the ball in liner ring 21, prevent cable from occurring clot or stuck phenomenon, and the folding and unfolding speed of the cable promoted.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is cabling sleeve and cable disc constructional drawing.
Fig. 3 is induction installation structural representation.
In figure: 1, pivot arm, 2, cabling sleeve, 3, cable disc, 4, cable, 5, induction installation, 21, liner ring, 22, ball, 51, cable guide pulley, 52, range finding guide wheel, 53, pressure sensor guide wheel.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail.
As shown in Figure 1, a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device, comprise pivot arm 1 and cable disc 3, described pivot arm 1 one end connecting drive device, actuating device can be rotated by driven rotary arm, the outboard end of pivot arm 1 has cabling sleeve 2, and cable 4 connects aircraft by cabling sleeve 2 from cable disc.
Described cabling sleeve 2 comprises liner ring 21, liner ring 21 has the ball grooves of multiple installation ball, ball 22 is arranged in ball grooves, ball 22 is half naked state at the opening part of ball grooves and is free to slide, namely ball 22 protrudes from liner ring 21 inwall, make cable 4 can be in moving contact with the ball in liner ring 21 like this, prevent cable from occurring clot or stuck phenomenon, and the folding and unfolding speed of the cable promoted.
This device also comprises induction installation 5, and induction installation comprises cable guide pulley 51, range finding guide wheel 52 and pressure sensor guide wheel 53,
Cable 4 is through cable guide pulley 51, range finding guide wheel 52 and pressure sensor guide wheel 53, and cable is wrapped on pressure sensor guide wheel by cable guide pulley and forms a plumbness; Cable is walked around range finding guide wheel by pressure sensor guide wheel and is passed cabling sleeve and put in order in cable disc.
In whole device, pivot arm 1 is by actuating device driven rotary, carry out the folding and unfolding of cable in cable disc 3, the drum efficiency that arm rotates is high, and it is effective, cable 4 can be in moving contact with the ball in liner ring 21, prevents cable from occurring clot or stuck phenomenon, and the folding and unfolding speed of the cable promoted.
Described aircraft is many rotor wing unmanned aerial vehicles aircraft, and its rotor quantity is four rotors, six rotors, eight rotors or 16 rotors.
Also comprise controller, floor power supply device and mooring electric supply installation, controller carrys out controller described in accessory drive for computing information, signal, adopts microcontroller, and Single Chip Microcomputer (SCM) system is formed, but is not limited to Single Chip Microcomputer (SCM) system.Controller employing wired mode respectively Bonding pressure sensor and photoelectric code disk also accepts the detection of unmanned plane elevation information at any time, and calculates the unwrapping wire distance required for mooring unmanned plane to specified altitude assignment according to all multi information.
Have controller in aircraft, controller has the effect of power-off protection, and when cable disconnects suddenly, controller can power-off immediately control take-up and pay-off device and carry out take-up.
Cable comprises two wires, the two ends of two wires respectively with floor power supply device and mooring electric supply installation; Described mooring electric supply installation is used for the later backup power of floor power supply device power-off, need for forced landing and power for position detecting device. a whole set of tethered platform can put into about 1 meter of cube of portable packing chest, together can be loaded in a miniature cross-country car with gen-set, have very strong manoevreability.
Four rotor wing unmanned aerial vehicle aircraft costs are lower, stable performance, easy to use, can be used for performing the multiple air taskings such as Data acquisition, coordinative command, search, measurement, communication, detection, scouting, have larger mission payload, stronger wind loading rating, outstanding gesture stability ability.Wherein mooring power and communication system no matter civilian or military in all there is very considerable application advance.
The above embodiment only represents several embodiments of invention, describes comparatively concrete and detailed, but can not be interpreted as limitation of the scope of the invention.It should be pointed out that for the person of ordinary skill of the art, without departing from the inventive concept of the premise, can also make some distortion and improvement, these all belong to scope.Therefore protection scope of the present invention should be as the criterion with described claim.
Claims (5)
1. the automatic deploying and retracting line apparatus for mooring unmanned plane during flying device, it is characterized in that, comprise pivot arm and cable disc, described pivot arm one end connecting drive device, the outboard end of pivot arm has cabling sleeve, and cable connects aircraft by cabling sleeve from cable disc.
2. a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device according to claim 1, it is characterized in that described cabling sleeve comprises liner ring, liner ring has multiple ball grooves, and ball is arranged in ball grooves, and ball is half naked state at the opening part of ball grooves.
3. a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device according to claim 1, is characterized in that, also comprise induction installation, and induction installation comprises cable guide pulley, range finding guide wheel and pressure sensor guide wheel,
Cable is through cable guide pulley, range finding guide wheel and pressure sensor guide wheel, and cable is wrapped on pressure sensor guide wheel by cable guide pulley and forms a plumbness; Cable is walked around range finding guide wheel by pressure sensor guide wheel and is passed cabling sleeve and put in order in cable disc.
4. a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device according to claim 1, is characterized in that described aircraft is many rotor wing unmanned aerial vehicles aircraft, and its rotor quantity is four rotors, six rotors, eight rotors or 16 rotors.
5. a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device according to claim 1, is characterized in that, also comprise controller, floor power supply device and mooring electric supply installation, and controller is used for computing information, signal carrys out accessory drive,
Cable comprises two wires, the two ends of two wires respectively with floor power supply device and mooring electric supply installation; Described mooring electric supply installation is used for the later backup power of floor power supply device power-off, needs and power for position detecting device for forced landing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520577471.9U CN204916215U (en) | 2015-08-04 | 2015-08-04 | A automatic coiling and uncoiling device for mooring unmanned aerial vehicle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520577471.9U CN204916215U (en) | 2015-08-04 | 2015-08-04 | A automatic coiling and uncoiling device for mooring unmanned aerial vehicle aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204916215U true CN204916215U (en) | 2015-12-30 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520577471.9U Expired - Fee Related CN204916215U (en) | 2015-08-04 | 2015-08-04 | A automatic coiling and uncoiling device for mooring unmanned aerial vehicle aircraft |
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| CN (1) | CN204916215U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2017165363A (en) * | 2016-03-18 | 2017-09-21 | 株式会社Ｉｈｉエアロスペース | Landing assist device and method |
| WO2018220607A1 (en) * | 2017-05-31 | 2018-12-06 | Elistair | Device for protecting the connection between a detachable wired drone and the wire thereof |
| CN109895991A (en) * | 2018-12-12 | 2019-06-18 | 鲁金婵 | It is a kind of can wound wire collapsible unmanned plane |
| CN113979240A (en) * | 2021-11-24 | 2022-01-28 | 中国铁道科学研究院集团有限公司铁道建筑研究所 | Cable winding and unwinding device and method |
-
2015
- 2015-08-04 CN CN201520577471.9U patent/CN204916215U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2017165363A (en) * | 2016-03-18 | 2017-09-21 | 株式会社Ｉｈｉエアロスペース | Landing assist device and method |
| WO2018220607A1 (en) * | 2017-05-31 | 2018-12-06 | Elistair | Device for protecting the connection between a detachable wired drone and the wire thereof |
| FR3066923A1 (en) * | 2017-05-31 | 2018-12-07 | Elistair | PROTECTIVE DEVICE FOR THE CONNECTION BETWEEN A DETACHABLE WIRED DRONE AND ITS WIRE. |
| US11970295B2 (en) | 2017-05-31 | 2024-04-30 | Elistair | Protective device for the connection between a detachable wired drone and the wire thereof |
| CN109895991A (en) * | 2018-12-12 | 2019-06-18 | 鲁金婵 | It is a kind of can wound wire collapsible unmanned plane |
| CN113979240A (en) * | 2021-11-24 | 2022-01-28 | 中国铁道科学研究院集团有限公司铁道建筑研究所 | Cable winding and unwinding device and method |
| CN113979240B (en) * | 2021-11-24 | 2024-01-16 | 中国铁道科学研究院集团有限公司铁道建筑研究所 | Cable winding and unwinding device and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151230 Termination date: 20160804 |