CN204452950U - Convertible The Cloud Terrace accommodation device - Google Patents
Convertible The Cloud Terrace accommodation device Download PDFInfo
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- CN204452950U CN204452950U CN201520045599.0U CN201520045599U CN204452950U CN 204452950 U CN204452950 U CN 204452950U CN 201520045599 U CN201520045599 U CN 201520045599U CN 204452950 U CN204452950 U CN 204452950U
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- cantilever
- cloud terrace
- servomotor
- fuselage
- function device
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Abstract
The utility model discloses a kind of convertible The Cloud Terrace accommodation device, be arranged on fuselage base plate, comprise function device, the first cantilever that the second cantilever be connected with function device, end are connected with the second cantilever, drive the servomotor of the first cantilever, The Cloud Terrace supporting plate for fixing servomotor; Servomotor comprises left side servomotor and right side servomotor, and the transmission shaft of left side servomotor is connected with rotating shaft, and the transmission shaft of right side servomotor is connected in this rotating shaft, and the top of rotating shaft and the first cantilever is fixed; Described fuselage base plate is provided with hole, and the first cantilever passes from hole after transmission shaft rotates, and makes function device carry in the outside of fuselage.The utility model has the advantages that: The Cloud Terrace and function device can be stretched out freely fuselage in unmanned plane during flying process by this device and be received into fuselage; Be received into fuselage interior, the effect of protection The Cloud Terrace and function device can be played, windage of flying can be reduced simultaneously.
Description
Technical field
The utility model relates to aircraft The Cloud Terrace class field, particularly relates to a kind of convertible The Cloud Terrace accommodation device for the protection of aircraft The Cloud Terrace.
Background technology
The mounting base of the The Cloud Terrace of existing carry on unmanned plane is fixed, the function device of The Cloud Terrace and The Cloud Terrace carry is in the outside of unmanned plane all the time, cannot be accommodated into fuselage, under special circumstances, can not defencive function equipment, and larger windage is caused for the flight of unmanned plane; Also have some can be received into the cradle head device of fuselage, but its design is complicated, takies fuselage interior larger space.
Utility model content
The purpose of this utility model is to avoid the deficiencies in the prior art part, and provides a kind of convertible The Cloud Terrace accommodation device for the protection of aircraft The Cloud Terrace.
For realizing above object, the utility model takes following technical scheme: convertible The Cloud Terrace accommodation device, be arranged on fuselage base plate, comprise function device, the first cantilever that the second cantilever be connected with function device, end are connected with the second cantilever, drive the servomotor of the first cantilever, The Cloud Terrace supporting plate for fixing servomotor; Servomotor comprises left side servomotor and right side servomotor, and the transmission shaft of left side servomotor is connected with rotating shaft, and the transmission shaft of right side servomotor is connected in this rotating shaft, and the top of rotating shaft and the first cantilever is fixed; Described fuselage base plate is provided with hole, and the first cantilever passes from hole after transmission shaft rotates, and makes function device carry in the outside of fuselage.
The setting of left side servomotor, right side servomotor, transmission shaft and rotating shaft, orders about the transmission shaft rotating in same direction of biography two servomotor, thus jointly realizes stretching, extension and the storage of the first cantilever, make it stress equalization and tilt-stable; First cantilever and the second cantilever are used for turn over function equipment.
Described fuselage base plate is provided with the pillar connecting shock-absorbing ball, and described The Cloud Terrace supporting plate is fixed on fuselage base plate by pillar, and shock-absorbing ball is between The Cloud Terrace supporting plate and fuselage base plate.Pillar is used for fixing The Cloud Terrace supporting plate, and shock-absorbing ball is for alleviating the impulsive force of The Cloud Terrace supporting plate, thus protection The Cloud Terrace.
Compared with prior art, tool has the following advantages the utility model: The Cloud Terrace and function device can be stretched out freely fuselage in unmanned plane during flying process by this device and be received into fuselage; Be received into fuselage interior, the effect of protection The Cloud Terrace and function device can be played, windage of flying can be reduced simultaneously.
Accompanying drawing explanation
Fig. 1 is the utility model embodiment The Cloud Terrace and the function device schematic diagram at external fuselage;
Fig. 2 is the utility model embodiment The Cloud Terrace storage first step action schematic diagram;
Fig. 3 is the utility model embodiment The Cloud Terrace storage second step action schematic diagram.
Reference numeral implication in figure:
1, fuselage; 2, The Cloud Terrace supporting plate; 3, function device; 4, the second cantilever; 5, the first cantilever; 6, shock-absorbing ball; 7, hole; 8, left side servomotor; 9, right side servomotor; 10, rotating shaft.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, content of the present utility model is described in further details.
Embodiment
Consult Fig. 1 to Fig. 3, for the convertible The Cloud Terrace accommodation device of one, be arranged on fuselage base plate, comprise function device 3, the first cantilever 5 that the second cantilever 4 be connected with function device 3, end are connected with the second cantilever 4, drive the servomotor of the first cantilever 5, the The Cloud Terrace supporting plate 2 for fixing servomotor; Servomotor comprises left side servomotor 8 and right side servomotor 9, and the transmission shaft of left side servomotor 8 is connected with rotating shaft 10, and the transmission shaft of right side servomotor 9 is connected in this rotating shaft 10, and the top of rotating shaft 10 and the first cantilever 5 is fixed; Fuselage base plate is provided with hole 7, and the first cantilever 5 passes from hole 7 after transmission shaft rotates, and makes function device 3 carry in the outside of fuselage 1.
The setting of left side servomotor 8, right side servomotor 9, transmission shaft and rotating shaft 10, orders about the transmission shaft rotating in same direction of biography two servomotor, thus jointly realizes stretching, extension and the storage of the first cantilever 5, make it stress equalization and tilt-stable; First cantilever 5 and the second cantilever 4 are for turn over function equipment 3.
Fuselage base plate is provided with the pillar connecting shock-absorbing ball 6, and The Cloud Terrace supporting plate 2 is fixed on fuselage base plate by pillar, and shock-absorbing ball 6 is between The Cloud Terrace supporting plate 2 and fuselage base plate.Pillar is used for fixing The Cloud Terrace supporting plate 2, and shock-absorbing ball 6 is for alleviating the impulsive force of The Cloud Terrace supporting plate 2, thus protection The Cloud Terrace.
When function device 3 and The Cloud Terrace are received into fuselage 1 by needs, first the second cantilever 4 is rotated to assigned address, then control left side servomotor 8, right side servomotor 9 synchronous axial system, drive the first cantilever 5 to overturn, thus The Cloud Terrace and function device 3 are received into fuselage 1 inner.
Above-listed detailed description is illustrating for the utility model possible embodiments, and this embodiment is also not used to limit the scope of the claims of the present utility model, does not allly depart from the equivalence that the utility model does and implements or change, and all should be contained in the scope of the claims of this case.
Claims (2)
1. convertible The Cloud Terrace accommodation device, be arranged on fuselage base plate, it is characterized in that: comprise function device, the first cantilever that the second cantilever be connected with function device, end are connected with the second cantilever, drive the servomotor of the first cantilever, The Cloud Terrace supporting plate for fixing servomotor; Servomotor comprises left side servomotor and right side servomotor, and the transmission shaft of left side servomotor is connected with rotating shaft, and the transmission shaft of right side servomotor is connected in this rotating shaft, and the top of rotating shaft and the first cantilever is fixed; Described fuselage base plate is provided with hole, and the first cantilever passes from hole after transmission shaft rotates, and makes function device carry in the outside of fuselage.
2. convertible The Cloud Terrace accommodation device according to claim 1, is characterized in that: described fuselage base plate is provided with the pillar connecting shock-absorbing ball, and described The Cloud Terrace supporting plate is fixed on fuselage base plate by pillar, and shock-absorbing ball is between The Cloud Terrace supporting plate and fuselage base plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520045599.0U CN204452950U (en) | 2015-01-22 | 2015-01-22 | Convertible The Cloud Terrace accommodation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520045599.0U CN204452950U (en) | 2015-01-22 | 2015-01-22 | Convertible The Cloud Terrace accommodation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204452950U true CN204452950U (en) | 2015-07-08 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520045599.0U Active CN204452950U (en) | 2015-01-22 | 2015-01-22 | Convertible The Cloud Terrace accommodation device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204452950U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105083577A (en) * | 2015-08-05 | 2015-11-25 | 北京韦加航通科技有限责任公司 | Holder steering lifting system for narrow load cabin of unmanned aerial vehicle and unmanned aerial vehicle |
| WO2017132990A1 (en) * | 2016-02-05 | 2017-08-10 | Autel Robotics Co.,Ltd | Multirotor aircraft |
| CN107249982A (en) * | 2016-01-26 | 2017-10-13 | 深圳市大疆创新科技有限公司 | Shock-damping structure and head assembly, the unmanned plane using the shock-damping structure |
| WO2018082058A1 (en) * | 2016-11-04 | 2018-05-11 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN108240533A (en) * | 2016-12-26 | 2018-07-03 | 中山日高精密工业有限公司 | Multi-functional special cantilever pan tilt structure |
| CN109159905A (en) * | 2018-10-31 | 2019-01-08 | 上海歌尔泰克机器人有限公司 | A kind of holder and the unmanned plane with the holder |
| WO2020062170A1 (en) * | 2018-09-29 | 2020-04-02 | 深圳市大疆创新科技有限公司 | Storage box and gimbal assembly having same |
| CN113022853A (en) * | 2021-03-27 | 2021-06-25 | 孙鹏 | Mobile 5G communication signal test platform and use method thereof |
-
2015
- 2015-01-22 CN CN201520045599.0U patent/CN204452950U/en active Active
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105083577A (en) * | 2015-08-05 | 2015-11-25 | 北京韦加航通科技有限责任公司 | Holder steering lifting system for narrow load cabin of unmanned aerial vehicle and unmanned aerial vehicle |
| CN107249982A (en) * | 2016-01-26 | 2017-10-13 | 深圳市大疆创新科技有限公司 | Shock-damping structure and head assembly, the unmanned plane using the shock-damping structure |
| US11999505B2 (en) | 2016-01-26 | 2024-06-04 | SZ DJI Technology Co., Ltd. | Unmanned vehicle |
| EP3409592A4 (en) * | 2016-01-26 | 2019-01-09 | SZ DJI Technology Co., Ltd. | Shock-absorbing structure, pan-tilt assembly using same, and unmanned aerial vehicle |
| CN107249982B (en) * | 2016-01-26 | 2019-08-02 | 深圳市大疆创新科技有限公司 | Shock-damping structure and head assembly, the unmanned plane for using the shock-damping structure |
| US10919646B2 (en) | 2016-01-26 | 2021-02-16 | SZ DJI Technology Co., Ltd. | Unmanned vehicle |
| WO2017132990A1 (en) * | 2016-02-05 | 2017-08-10 | Autel Robotics Co.,Ltd | Multirotor aircraft |
| CN108290641B (en) * | 2016-11-04 | 2021-12-17 | 深圳市道通智能航空技术股份有限公司 | Unmanned aerial vehicle |
| WO2018082058A1 (en) * | 2016-11-04 | 2018-05-11 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN108290641A (en) * | 2016-11-04 | 2018-07-17 | 深圳市道通智能航空技术有限公司 | A kind of unmanned plane |
| CN108240533A (en) * | 2016-12-26 | 2018-07-03 | 中山日高精密工业有限公司 | Multi-functional special cantilever pan tilt structure |
| WO2020062170A1 (en) * | 2018-09-29 | 2020-04-02 | 深圳市大疆创新科技有限公司 | Storage box and gimbal assembly having same |
| CN109159905A (en) * | 2018-10-31 | 2019-01-08 | 上海歌尔泰克机器人有限公司 | A kind of holder and the unmanned plane with the holder |
| CN113022853A (en) * | 2021-03-27 | 2021-06-25 | 孙鹏 | Mobile 5G communication signal test platform and use method thereof |
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| GR01 | Patent grant |