CN203889080U - Vertical lifting holder device of unmanned aerial vehicle - Google Patents
Vertical lifting holder device of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN203889080U CN203889080U CN201420296309.5U CN201420296309U CN203889080U CN 203889080 U CN203889080 U CN 203889080U CN 201420296309 U CN201420296309 U CN 201420296309U CN 203889080 U CN203889080 U CN 203889080U
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- holder
- aerial vehicle
- unmanned aerial
- cloud terrace
- shock absorption
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Abstract
The utility model relates to a vertical lifting holder device of an unmanned aerial vehicle. The vertical lifting holder device of the unmanned aerial vehicle comprises a shock absorption device and a synchronous transmission device, a holder transmission board is linked with a shock absorption ball, an upper fixing board is linked with the holder transmission board, the upper fixing board and an unmanned aerial vehicle body are connected, and a steering engine rotates to drive a guide rail to rotate, so that the holder transmission board drives a holder to vertically lift. The shock absorption device reduces shaking of the holder when the unmanned aerial vehicle body shakes under impact of airflow. Through the vertical lifting design of the holder, the steering engine controls the holder to lift at any time, shaking of the unmanned aerial vehicle body is reduced by additional arrangement of the shock absorption device, influence on a carried precision instrument device from shaking can be reduced, the quality of information collected by the photoelectric holder can be ensured, and the operation efficiency is improved. By the design that the holder lifts vertically, the photoelectric holder is contained into the unmanned aerial vehicle body at ordinary times so as to be convenient to transport, the carried precision instrument device can also be better protected, time is shortened, rapid transportation is achieved, and the operation efficiency is improved.
Description
Technical field
The utility model relates to a kind of unmanned plane vertical lift cradle head device, uses the novel unmanned fixed-wing of newly-increased steady technology unmanned plane vertical lift cradle head device and unmanned plane during flying to carry cradle head control technical field.Relate to a kind of new equipment that utilizes, can solve the lifting at any time of photoelectricity The Cloud Terrace easy to use, reduce photoelectricity The Cloud Terrace and body resonance problem simultaneously, guarantee the high quality of photoelectricity The Cloud Terrace Information Monitoring.
Background technology
Along with the applied research of unmanned plane in 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 of low cost, high stability, applied range, has become a kind of exigence.
At present domestic unmanned plane is also in elementary development phase because the Structure Designing Problem of fuselage, cause high cost, stability not, fuselage and the bottleneck such as load equipment matching degree is low, restricting unmanned plane always and carrying out other widespread use of industrial grade.Along with the active demand of every profession and trade to industrial grade unmanned plane, a kind of low cost, the Unmanned Aircraft Systems (UAS) that stability is high, fuselage can be realized electrodeless adjusting seem particularly important.The utility model adopts the design of photoelectricity The Cloud Terrace vertical lift, not only can reduce The Cloud Terrace vibrations, guarantees the safety and stability of unmanned plane during flying, can also make the quality of photoelectricity The Cloud Terrace Information Monitoring be guaranteed, and operating efficiency is higher.The utility model can make Unmanned Aircraft Systems (UAS) 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 unmanned plane vertical lift cradle head device is provided, the security device of the low cost of use special construction design, high security, assurance remote job.
The utility model solves its technical matters and takes following technical scheme to realize:
The utility model relates to a kind of unmanned plane vertical lift cradle head device, comprise shock absorption device and synchronous transmission device, described shock absorption device includes The Cloud Terrace permanent seat and is connected with shock-absorbing ball, the link of The Cloud Terrace driver plate and shock-absorbing ball and upper mounted plate and the link of The Cloud Terrace driver plate, upper mounted plate is connected with unmanned fixed wing aircraft fuselage; Synchronous transmission device includes steering wheel and steering wheel fixer, guide rail permanent seat is connected with guide rail, optical axis permanent seat links with optical axis, steering wheel links with guide rail, by steering wheel, rotating drive rail rotates, make The Cloud Terrace driver plate drive The Cloud Terrace vertical lift, shock absorption device reduces the vibrations of The Cloud Terrace while making airframe be subject to air-flow impact endurance test shock.
The utility model compared with prior art has obvious advantage and effect.
The utility model adopts the design of The Cloud Terrace vertical lift, by steering wheel, control The Cloud Terrace lifting at any time, increase shock absorption device and reduce the vibrations that fuselage brings, such benefit is to reduce the impact that vibrations produce the precision instrument and equipment carrying, can guarantee the quality of photoelectricity The Cloud Terrace Information Monitoring, improve operating efficiency, reduce potential safety hazard.Meanwhile, make unmanned plane during flying more stable, guarantee the safety of flight.
It is convenient that The Cloud Terrace vertical lift design makes to transport, and when carrying out engineer operation task, owing to often wanting converting field, the transportation convenience of unmanned plane, directly has influence on the efficiency of operation.The design of The Cloud Terrace vertical lift, makes photoelectricity The Cloud Terrace take at ordinary times the convenient transportation of fuselage and also can protect better the precision instrument and equipment of lift-launch simultaneously, saves time, and realizes quick transition, improves operating efficiency.
The specific embodiment of the present utility model is provided in detail by following embodiment and accompanying drawing.
The specific embodiment
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. 1-2, unmanned plane vertical lift cradle head device, comprise shock absorption device and synchronous transmission device, described shock absorption device includes The Cloud Terrace permanent seat and is connected with shock-absorbing ball, the link of The Cloud Terrace driver plate and shock-absorbing ball and upper mounted plate and the link of The Cloud Terrace driver plate, upper mounted plate is connected with unmanned fixed wing aircraft fuselage; Synchronous transmission device includes steering wheel and steering wheel fixer, guide rail permanent seat is connected with guide rail, optical axis permanent seat links with optical axis, steering wheel links with guide rail, by steering wheel, rotating drive rail rotates, make The Cloud Terrace driver plate drive The Cloud Terrace vertical lift, shock absorption device reduces the vibrations of The Cloud Terrace while making airframe be subject to air-flow impact endurance test shock.
Accompanying drawing explanation
Fig. 1 is vertical lift cradle head device intraware;
Fig. 2 is vertical lift cradle head device outward appearance.
Claims (1)
1. a unmanned plane vertical lift cradle head device, comprise shock absorption device and synchronous transmission device, it is characterized in that: described shock absorption device includes The Cloud Terrace permanent seat and is connected with shock-absorbing ball, the link of The Cloud Terrace driver plate and shock-absorbing ball and upper mounted plate and the link of The Cloud Terrace driver plate, upper mounted plate is connected with unmanned fixed wing aircraft fuselage; Synchronous transmission device includes steering wheel and steering wheel fixer, guide rail permanent seat is connected with guide rail, optical axis permanent seat links with optical axis, steering wheel links with guide rail, by steering wheel, rotating drive rail rotates, make The Cloud Terrace driver plate drive The Cloud Terrace vertical lift, shock absorption device reduces the vibrations of The Cloud Terrace while making airframe be subject to air-flow impact endurance test shock.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420296309.5U CN203889080U (en) | 2014-06-05 | 2014-06-05 | Vertical lifting holder device of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420296309.5U CN203889080U (en) | 2014-06-05 | 2014-06-05 | Vertical lifting holder device of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203889080U true CN203889080U (en) | 2014-10-22 |
Family
ID=51715515
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420296309.5U Expired - Fee Related CN203889080U (en) | 2014-06-05 | 2014-06-05 | Vertical lifting holder device of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203889080U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106029502A (en) * | 2015-04-24 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
| CN106081141A (en) * | 2016-06-08 | 2016-11-09 | 朱新科 | Many rotor wing unmanned aerial vehicles |
| CN106167102A (en) * | 2016-08-31 | 2016-11-30 | 河南翱翔航空科技有限公司 | Aerial camera shock bracket |
| CN107606020A (en) * | 2017-04-24 | 2018-01-19 | 西安应用光学研究所 | A kind of composite damping structure for airborne lidar for fluorescence |
-
2014
- 2014-06-05 CN CN201420296309.5U patent/CN203889080U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106029502A (en) * | 2015-04-24 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
| WO2016169035A1 (en) * | 2015-04-24 | 2016-10-27 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
| CN106081141A (en) * | 2016-06-08 | 2016-11-09 | 朱新科 | Many rotor wing unmanned aerial vehicles |
| CN106167102A (en) * | 2016-08-31 | 2016-11-30 | 河南翱翔航空科技有限公司 | Aerial camera shock bracket |
| CN107606020A (en) * | 2017-04-24 | 2018-01-19 | 西安应用光学研究所 | A kind of composite damping structure for airborne lidar for fluorescence |
| CN107606020B (en) * | 2017-04-24 | 2019-05-31 | 西安应用光学研究所 | A kind of composite damping structure for airborne lidar for fluorescence |
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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: 20170605 |