CN203889081U - Pan-tilt damping device of electric unmanned helicopter - Google Patents
Pan-tilt damping device of electric unmanned helicopter Download PDFInfo
- Publication number
- CN203889081U CN203889081U CN201420297566.0U CN201420297566U CN203889081U CN 203889081 U CN203889081 U CN 203889081U CN 201420297566 U CN201420297566 U CN 201420297566U CN 203889081 U CN203889081 U CN 203889081U
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- shock
- cloud terrace
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- tilt
- damping
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Abstract
The utility model relates to a pan-tilt damping device of an electric unmanned helicopter. The pan-tilt damping device comprises a pan-tilt fixing device and a pan-tilt damping device body. The pan-tilt damping device body comprises a connecting device and a damping system. The damping system is formed in the mode that every three damping balls of twelve damping balls are evenly distributed at the four corners of the whole device, so that resistance in the flight process in all directions is offset well. Since vibration is reduced, the influence of the vibration on equipment can be reduced. Since the pan-tilt damping device of the unmanned helicopter has the good damping effect, videos shot in the flight process are stable and clear in picture; meanwhile, the pan-tilt damping device can effectively protect a pan-tilt.
Description
Technical field
The utility model relates to a kind of newly-increased steady technology that uses, the novel depopulated helicopter of The Cloud Terrace shock absorption device and UAV Flight Control technical field, relate to one and utilize new equipment, can solve The Cloud Terrace damping increases steady, the video of taking is steady and audible, has really solved depopulated helicopter and can shoot the effect on ground.
Background technology
Along with unmanned plane is in the applied research of every profession and trade, people all the more now unmanned plane are day by day remarkable in the effect of social production and life various aspects.Use modern new and high technology mechanical equipment, not only can increase work efficiency with quality, reduce operating cost, can also reduce the risk of personnel's operation, the protection security of the lives and property.Along with science and technology is constantly progressive, the enhancing of economic capability, the lifting of the level of consumption, the work that the alternative traditional manpower of modern conveniences is engaged in excessive risk, highly difficult, high operation intensity has become inexorable trend.The whole world for the third time industrial revolution prelude is pulled open, and develops the unmanned plane The Cloud Terrace shock absorption device of low cost, high stability, applied range, has become a kind of exigence.
At present domestic depopulated helicopter is also in elementary development phase, because damping tranquilizer design problem, cause high cost, stability not, fuselage and the bottleneck such as load equipment matching degree is low, restricting depopulated helicopter always and carrying out other widespread use of industrial grade.Along with the active demand of every profession and trade to industrial grade depopulated helicopter, a kind of low cost, the The Cloud Terrace damping stability augmentation system that stability is high seem particularly important.The utility model adopts The Cloud Terrace Aseismatic Design, not only can reduce the fugitiveness of capture video, alleviate fuselage and The Cloud Terrace shakes altogether, ensure the safety and stability of unmanned plane during flying operation, can also make unmanned plane capture video convenient, operating efficiency is higher.The utility model can make The Cloud Terrace stability augmentation system combine with sector application, realizes the unmanned plane industry level applications of real meaning.
Summary of the invention
Problem to be solved in the utility model is, overcomes the deficiencies in the prior art, and a kind of electric unmanned helicopter The Cloud Terrace shock absorption device is provided, and uses low cost, the high security of special construction design, the security device of guarantee remote job.
The utility model solves its technical matters and takes following technical scheme to realize:
The utility model relates to a kind of electric unmanned helicopter The Cloud Terrace shock absorption device, comprise fixing cradle head device and The Cloud Terrace shock absorption device, described The Cloud Terrace shock absorption device includes connecting device and shock mitigation system, for depopulated helicopter The Cloud Terrace and being connected of fuselage playing damping effect, connecting device comprises fixed main body adaptor union and fixing cradle head device, fixed main body adaptor union is four U-shaped buckles, it is to play the effect that connects fuselage and shock absorption device, fixing cradle head device is a base plate that 4mm is thick, a round platform that 2mm is dark of base plate below design, The Cloud Terrace is fixed on base plate by nut, shock mitigation system comprises two cross bars, four shock-absorbing ball adaptor unions are with a base plate, cross bar is screwed fuselage adaptor union and buffering ball adaptor union, impact absorbing connector is by shock-absorbing ball connecting bottom board, shock mitigation system is that every three of 12 shock-absorbing balls are evenly distributed on four jiaos of whole device, offset the resistance of all directions in-flight.
The utility model compared with prior art has obvious advantage and effect.
The utility model adopts The Cloud Terrace Aseismatic Design, be evenly distributed in four angles of whole shock absorption device by 12 shock-absorbing balls, each angle is evenly distributed three shock-absorbing balls, the benefit of doing is like this to realize the damping effect of four direction, the resistance that makes depopulated helicopter be subject to aerial all directions in flight course can both be offset by these shock-absorbing balls, simultaneously simple in structure, easy to assembly, the lighter weight that device itself is overall of this device, does not affect the load-carrying ability of depopulated helicopter substantially.Simultaneously because the reduction of vibrations can reduce the impact that vibrations produce the precision instrument and equipment carrying.
The Cloud Terrace Aseismatic Design makes the video of shooting have stability, leglibility, and in carrying out engineer operation task, due to the resistance of all directions in flight course, the damping effect of The Cloud Terrace is more outstanding, directly has influence on the efficiency of operation.The Cloud Terrace Aseismatic Design, reduces the vibrations of The Cloud Terrace, has directly protected The Cloud Terrace carrying equipment, makes equipment can not receive because of strenuous vibration damage.Simultaneously this design can be dual-purpose, and preliminary design is pull-down damping effect, after test and whole device is inverted to its damping of installation to increase steady effect be also good by installations, so this device has just become the structure of support type.
Detailed description of the invention of the present utility model is provided in detail by following embodiment and accompanying drawing.
Detailed description of the invention
Below in conjunction with accompanying drawing and embodiment, to provide concrete embodiment, structure, feature and function to be elaborated as follows according to the utility model:
Referring to Fig. 1-3, electric unmanned helicopter The Cloud Terrace shock absorption device, comprises fixing cradle head device and The Cloud Terrace shock absorption device, and described The Cloud Terrace shock absorption device includes connecting device and shock mitigation system, for depopulated helicopter The Cloud Terrace and being connected of fuselage playing damping effect, connecting device comprises fixed main body adaptor union and fixing cradle head device, fixed main body adaptor union is four U-shaped buckles, it is to play the effect that connects fuselage and shock absorption device, fixing cradle head device is a base plate that 4mm is thick, a round platform that 2mm is dark of base plate below design, The Cloud Terrace is fixed on base plate by nut, shock mitigation system comprises two cross bars, four shock-absorbing ball adaptor unions are with a base plate, cross bar is screwed fuselage adaptor union and buffering ball adaptor union, impact absorbing connector is by shock-absorbing ball connecting bottom board, shock mitigation system is that every three of 12 shock-absorbing balls are evenly distributed on four jiaos of whole device, offset the resistance of all directions in-flight.
Brief description of the drawings
Fig. 1 is that The Cloud Terrace shock absorption device is just being put black box;
Fig. 2 is that The Cloud Terrace shock absorption device is inverted black box;
Fig. 3 is the load module of The Cloud Terrace shock absorption device.
Claims (1)
1. an electric unmanned helicopter The Cloud Terrace shock absorption device, comprise fixing cradle head device and The Cloud Terrace shock absorption device, it is characterized in that: described The Cloud Terrace shock absorption device includes connecting device and shock mitigation system, for depopulated helicopter The Cloud Terrace and being connected of fuselage playing damping effect, connecting device comprises fixed main body adaptor union and fixing cradle head device, fixed main body adaptor union is four U-shaped buckles, it is to play the effect that connects fuselage and shock absorption device, fixing cradle head device is a base plate that 4mm is thick, a round platform that 2mm is dark of base plate below design, The Cloud Terrace is fixed on base plate by nut, shock mitigation system comprises two cross bars, four shock-absorbing ball adaptor unions are with a base plate, cross bar is screwed fuselage adaptor union and buffering ball adaptor union, impact absorbing connector is by shock-absorbing ball connecting bottom board, shock mitigation system is that every three of 12 shock-absorbing balls are evenly distributed on four jiaos of whole device, offset the resistance of all directions in-flight.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420297566.0U CN203889081U (en) | 2014-06-06 | 2014-06-06 | Pan-tilt damping device of electric unmanned helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420297566.0U CN203889081U (en) | 2014-06-06 | 2014-06-06 | Pan-tilt damping device of electric unmanned helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203889081U true CN203889081U (en) | 2014-10-22 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420297566.0U Expired - Fee Related CN203889081U (en) | 2014-06-06 | 2014-06-06 | Pan-tilt damping device of electric unmanned helicopter |
Country Status (1)
| Country | Link |
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| CN (1) | CN203889081U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539871A (en) * | 2016-01-19 | 2016-05-04 | 无锡觅睿恪科技有限公司 | Pan-tilt anti-vibration device for unmanned aerial vehicle |
| WO2016095837A1 (en) * | 2014-12-18 | 2016-06-23 | 优利科技有限公司 | Aircraft system |
| CN107640310A (en) * | 2017-10-09 | 2018-01-30 | 北京沃氏航空科技有限公司 | Unmanned plane damping push and pull system and unmanned plane |
| CN107985617A (en) * | 2017-10-27 | 2018-05-04 | 成都云瞰科技有限公司 | A kind of double light photoelectric nacelles |
| CN110143288A (en) * | 2019-04-29 | 2019-08-20 | 一飞智控(天津)科技有限公司 | IMU damping device |
-
2014
- 2014-06-06 CN CN201420297566.0U patent/CN203889081U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016095837A1 (en) * | 2014-12-18 | 2016-06-23 | 优利科技有限公司 | Aircraft system |
| CN105539871A (en) * | 2016-01-19 | 2016-05-04 | 无锡觅睿恪科技有限公司 | Pan-tilt anti-vibration device for unmanned aerial vehicle |
| CN107640310A (en) * | 2017-10-09 | 2018-01-30 | 北京沃氏航空科技有限公司 | Unmanned plane damping push and pull system and unmanned plane |
| CN107985617A (en) * | 2017-10-27 | 2018-05-04 | 成都云瞰科技有限公司 | A kind of double light photoelectric nacelles |
| CN110143288A (en) * | 2019-04-29 | 2019-08-20 | 一飞智控(天津)科技有限公司 | IMU damping device |
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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: 20141022 Termination date: 20170606 |