CN205158139U - A flight attitude control ware for mooring gyroplane - Google Patents
A flight attitude control ware for mooring gyroplane Download PDFInfo
- Publication number
- CN205158139U CN205158139U CN201520978156.7U CN201520978156U CN205158139U CN 205158139 U CN205158139 U CN 205158139U CN 201520978156 U CN201520978156 U CN 201520978156U CN 205158139 U CN205158139 U CN 205158139U
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- module
- mooring
- pulling force
- giro
- pedestal
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Abstract
The utility model discloses a flight attitude control ware for mooring gyroplane, include the ground base and be used for the aerial base continuous with the staying gyroplane, be equipped with control module and a plurality of pulling force module on the base of ground, the pulling force mould splits do not passes through the stay cord and links to each other with aerial base, just be equipped with force sensor on the stay cord, pulling force module, force sensor link to each other with control module respectively. The utility model discloses can realize the altitude control to the different positions of aerial base through the stay cord to realize the flight attitude control of staying gyroplane, have simple to operate, simple structure, convenient to use, low cost's advantage.
Description
Technical field
The utility model relates to aircraft, is specifically related to a kind of Attitude Controller for mooring giro.
Background technology
Current, electronic unmanned plane, because battery electric quantity problem, exists and uses obstacle.Mooring giro to be energized communication by a main cables and ground, can 24 Small Time Lags leave a blank in advantage, more and more come into one's own.For maintenance mooring giro, how to keep mooring giro more and more important relative to the position stability of car or ship.
Utility model content
The technical problems to be solved in the utility model is to provide a kind of Attitude Controller for mooring giro, this Attitude Controller being used for mooring giro can by the Altitude control of stay cord realization to aerial pedestal diverse location, the flight attitude realizing mooring giro controls, and has advantage easy for installation, that structure is simple, easy to use, with low cost.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is:
A kind of Attitude Controller for mooring giro, comprise ground pedestal and the aerial pedestal for being connected with mooring giro, described ground pedestal is provided with control module and multiple pulling force module, described pulling force module is connected with aerial pedestal respectively by stay cord, and described stay cord is provided with pulling force sensor, described pulling force module, pulling force sensor are connected with control module respectively.
Described pulling force module comprises the motor be individually fixed on the pedestal of ground, gear drive box, cylinder and pulley, described motor is connected with control module, the output shaft of described motor is connected with the main shaft of cylinder by gear drive box, and described stay cord one end is connected with aerial pedestal, the other end is set around on cylinder through pulley.
Described control module comprises control chip, driving circuit and power module, described pulling force sensor is connected with the input end of control chip, the output terminal of described control chip is connected with motor by driving circuit, and described power module is connected with control chip, driving circuit respectively.
Described control module comprises radiocommunication module, and described radiocommunication module is connected with control chip, power module respectively.
Described aerial pedestal is provided with the stationary pipes for placing mooring giro main push-towing rope rope, and described stationary pipes is arranged along vertical direction.
Reinforced company's extension bar is provided with between described aerial pedestal and stationary pipes.
The utility model has following advantage: the utility model comprises ground pedestal and the aerial pedestal for being connected with mooring giro, ground pedestal is provided with control module and multiple pulling force module, pulling force module is connected with aerial pedestal respectively by stay cord, and stay cord is provided with pulling force sensor, pulling force module, pulling force sensor is connected with control module respectively, by the pulling force module traction stay cord of diverse location, can realize by the Altitude control of stay cord realization to aerial pedestal diverse location, the flight attitude realizing mooring giro controls, have easy for installation, structure is simple, easy to use, advantage with low cost.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation of the utility model embodiment.
Fig. 2 is the partial enlargement structural representation of region A in Fig. 1.
Marginal data: 1, ground pedestal; 2, aerial pedestal; 21, stationary pipes; 22, reinforced company's extension bar; 3, control module; 4, pulling force module; 41, motor; 42, gear drive box; 43, cylinder; 44, pulley; 5, stay cord; 6, pulling force sensor.
Embodiment
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described in detail, to make advantage of the present utility model and feature can be easier to be readily appreciated by one skilled in the art, thus more explicit defining is made to protection domain of the present utility model.
As depicted in figs. 1 and 2, the Attitude Controller for mooring giro of the present embodiment, comprise ground pedestal 1 and the aerial pedestal 2 for being connected with mooring giro, ground pedestal 1 is provided with control module 3 and four pulling force modules 4, pulling force module 4 is connected with aerial pedestal 2 respectively by stay cord 5, and stay cord 5 is provided with pulling force sensor 6, pulling force module 4, pulling force sensor 6 are connected with control module 3 respectively.In addition, three pulling force modules 4 or more pulling force module 4 can also be adopted as required.
In the present embodiment, pulling force module 4 comprises the motor 41 be individually fixed on ground pedestal 1, gear drive box 42, cylinder 43 and pulley 44, motor 41 is connected with control module 3, the output shaft of motor 41 is connected with the main shaft of cylinder 43 by gear drive box 42, and stay cord 5 one end is connected with aerial pedestal 2, the other end is set around on cylinder 43 through pulley 44.
In the present embodiment, control module 3 comprises control chip, driving circuit and power module, pulling force sensor 6 is connected with the input end of control chip, and the output terminal of control chip is connected with motor 41 by driving circuit, and power module is connected with control chip, driving circuit respectively.In the present embodiment, control chip adopts ARM9 control chip, and ARM9 control chip is used for controlling the rotating of four motors 41, thus realizes the folding and unfolding to stay cord 5.
In the present embodiment, control module 3 comprises radiocommunication module, radiocommunication module is connected with control chip, power module respectively, control module 3 can realize carrying out radio communication with the flight control system of mooring giro by radiocommunication module, be convenient to mooring giro flight control system to be communicated with control chip by radiocommunication module and obtain the pulling force of each stay cord 5, and the rotating speed of corresponding screw propeller is adjusted according to the numerical value of pulling force, keep the attitude relative to surface installation, the final relative flight attitude stabilization keeping mooring giro.
In the present embodiment, aerial pedestal 2 is provided with the stationary pipes 21 for placing mooring giro main push-towing rope rope, and stationary pipes 21 is arranged along vertical direction.Have power lead and signal wire in main push-towing rope rope, power lead provides electric power for giro work, and the data of giro collection are transferred to ground by signal wire.Main push-towing rope rope is connected with the cable car of giro, by the artificial lay and recover wire of cable car.
In the present embodiment, between aerial pedestal 2 and stationary pipes 21, be provided with reinforced company's extension bar 22, the mechanical property of aerial pedestal 2 can be strengthened, make aerial pedestal 2 more solid and reliable.
The foregoing is only preferred implementation of the present utility model, protection domain of the present utility model is not limited in above-mentioned embodiment, and every technical scheme belonging to the utility model principle all belongs to protection domain of the present utility model.For a person skilled in the art, some improvements and modifications of carrying out under the prerequisite not departing from principle of the present utility model, these improvements and modifications also should be considered as protection domain of the present utility model.
Claims (6)
1. the Attitude Controller for mooring giro, it is characterized in that: comprise ground pedestal (1) and the aerial pedestal (2) for being connected with mooring giro, described ground pedestal (1) is provided with control module (3) and multiple pulling force module (4), described pulling force module (4) is connected with aerial pedestal (2) respectively by stay cord (5), and described stay cord (5) is provided with pulling force sensor (6), described pulling force module (4), pulling force sensor (6) are connected with control module (3) respectively.
2. the Attitude Controller for mooring giro according to claim 1, it is characterized in that: described pulling force module (4) comprises the motor (41) be individually fixed on ground pedestal (1), gear drive box (42), cylinder (43) and pulley (44), described motor (41) is connected with control module (3), the output shaft of described motor (41) is connected with the main shaft of cylinder (43) by gear drive box (42), described stay cord (5) one end is connected with aerial pedestal (2), the other end is set around on cylinder (43) through pulley (44).
3. the Attitude Controller for mooring giro according to claim 2, it is characterized in that: described control module (3) comprises control chip, driving circuit and power module, described pulling force sensor (6) is connected with the input end of control chip, the output terminal of described control chip is connected with motor (41) by driving circuit, and described power module is connected with control chip, driving circuit respectively.
4. the Attitude Controller for mooring giro according to claim 3, is characterized in that: described control module (3) comprises radiocommunication module, and described radiocommunication module is connected with control chip, power module respectively.
5. according to the Attitude Controller for mooring giro in Claims 1 to 4 described in any one, it is characterized in that: described aerial pedestal (2) is provided with the stationary pipes (21) for placing mooring giro main push-towing rope rope, and described stationary pipes (21) is arranged along vertical direction.
6. the Attitude Controller for mooring giro according to claim 5, is characterized in that: be provided with reinforced company's extension bar (22) between described aerial pedestal (2) and stationary pipes (21).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520978156.7U CN205158139U (en) | 2015-11-27 | 2015-11-27 | A flight attitude control ware for mooring gyroplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520978156.7U CN205158139U (en) | 2015-11-27 | 2015-11-27 | A flight attitude control ware for mooring gyroplane |
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| Publication Number | Publication Date |
|---|---|
| CN205158139U true CN205158139U (en) | 2016-04-13 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520978156.7U Active CN205158139U (en) | 2015-11-27 | 2015-11-27 | A flight attitude control ware for mooring gyroplane |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108255190A (en) * | 2016-12-28 | 2018-07-06 | 北京卓翼智能科技有限公司 | Precision landing method based on multisensor and it is tethered at unmanned plane using this method |
| CN113060282A (en) * | 2021-03-24 | 2021-07-02 | 安徽中青检验认证服务有限公司 | Atmospheric environment detection device and method based on laser monitoring |
-
2015
- 2015-11-27 CN CN201520978156.7U patent/CN205158139U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108255190A (en) * | 2016-12-28 | 2018-07-06 | 北京卓翼智能科技有限公司 | Precision landing method based on multisensor and it is tethered at unmanned plane using this method |
| CN108255190B (en) * | 2016-12-28 | 2023-06-16 | 北京卓翼智能科技有限公司 | Accurate landing method based on multiple sensors and tethered unmanned aerial vehicle using same |
| CN113060282A (en) * | 2021-03-24 | 2021-07-02 | 安徽中青检验认证服务有限公司 | Atmospheric environment detection device and method based on laser monitoring |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A flight attitude control ware for mooring gyroplane Effective date of registration: 20170113 Granted publication date: 20160413 Pledgee: Bank of Communications Ltd Anhui branch Pledgor: HEFEI SIWILL INTELLIGENT CO., LTD. Registration number: 2017340000005 |
|
| PLDC | Enforcement, change and cancellation of contracts on pledge of patent right or utility model | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20171219 Granted publication date: 20160413 Pledgee: Bank of Communications Ltd Anhui branch Pledgor: HEFEI SIWILL INTELLIGENT CO., LTD. Registration number: 2017340000005 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A flight attitude control ware for mooring gyroplane Effective date of registration: 20171225 Granted publication date: 20160413 Pledgee: Bank of Communications Ltd Anhui branch Pledgor: HEFEI SIWILL INTELLIGENT CO., LTD. Registration number: 2017340000442 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right |