CN203996915U - Three axle Self-stabilization holders - Google Patents
Three axle Self-stabilization holders Download PDFInfo
- Publication number
- CN203996915U CN203996915U CN201420299233.1U CN201420299233U CN203996915U CN 203996915 U CN203996915 U CN 203996915U CN 201420299233 U CN201420299233 U CN 201420299233U CN 203996915 U CN203996915 U CN 203996915U
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- CN
- China
- Prior art keywords
- motor
- output shaft
- pipe link
- stabilization
- utility
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model aims to provide a kind of three axle Self-stabilization holders that can realize airborne equipment self-stabilization.The utility model comprises the first S. A. (1), the second S. A. (2) and the 3rd S. A. (3), one end of described the first S. A. (1) is provided with the first motor (4), the other end is connected with head rod (5), the other end of described head rod (5) is fixedly installed the second motor (6), the output shaft of described the second motor (6) is fixedly connected with described the second S. A. (2), the two ends of described the second S. A. (2) are all connected with the second pipe link (7), the outer end of described second pipe link (7) is fixedly installed the 3rd motor (8) therein, on the outer end of other described second pipe link (7) and the output shaft of described the 3rd motor (8), be provided with connecting panel (9), described the 3rd S. A. (3) is arranged between two described connecting panels.The utility model can be applicable to tripod head equipment field.
Description
Technical field
The utility model relates to a kind of The Cloud Terrace, relates in particular to a kind of three axle Self-stabilization holders.
Background technology
On aircraft, tend to capture apparatus as first-class in made a video recording.Aircraft, in the process of flight, needs to take scene during the journey.In existing technology, capture apparatus is to be all fixed on aircraft exterior most time, in aircraft flight process, can only photograph a scene in direction.If obtain the scene of feature direction, need to adjust the heading of aircraft, and along with the flight angle difference of aircraft, can not catch and catch the picture needing.
Utility model content
Technical problem to be solved in the utility model is to overcome the deficiencies in the prior art, and a kind of three axle Self-stabilization holders that can realize airborne equipment self-stabilization are provided.
The technical scheme that the utility model adopts is: the utility model comprises the first S. A., the second S. A. and the 3rd S. A., one end of described the first S. A. is provided with the first motor, the other end is connected with head rod, the other end of described head rod is fixedly installed the second motor, the output shaft of described the second motor is fixedly connected with described the second S. A., the two ends of described the second S. A. are all connected with the second pipe link, the outer end of described second pipe link is fixedly installed the 3rd motor therein, on the outer end of other described second pipe link and the output shaft of described the 3rd motor, be provided with connecting panel, the described connecting panel being connected with the output shaft of described the 3rd motor is fixedly connected with the output shaft of described the 3rd motor, described in another connecting panel and described in another the second pipe link be rotationally connected, described the 3rd S. A. is arranged between two described connecting panels.
Further, the output shaft of described the first motor is fixedly connected with peripheral aircraft devices, and described the first S. A. is done the rotation of 360 ° around the output shaft of described the first motor.
Further, the output shaft of described the second motor is fixedly connected with the medium position of described the second S. A., and described the second S. A. is done the rotation of 160 ° around the output shaft of described the second motor.
Further, described the 3rd S. A. is done the rotation of 150 ° around the output shaft of described the 3rd motor.
Further, on described the 3rd S. A., be provided with equipment fixed platform.
The beneficial effects of the utility model are: the utility model comprises the first S. A., the second S. A. and the 3rd S. A., one end of described the first S. A. is provided with the first motor, the other end is connected with head rod, the other end of described head rod is fixedly installed the second motor, the output shaft of described the second motor is fixedly connected with described the second S. A., the two ends of described the second S. A. are all connected with the second pipe link, the outer end of described second pipe link is fixedly installed the 3rd motor therein, on the outer end of other described second pipe link and the output shaft of described the 3rd motor, be provided with connecting panel, the described connecting panel being connected with the output shaft of described the 3rd motor is fixedly connected with the output shaft of described the 3rd motor, described in another connecting panel and described in another the second pipe link be rotationally connected, described the 3rd S. A. is arranged between two described connecting panels, so, the utility model can be according to the flight path of aircraft, by described the first motor, the second motor and the 3rd motor, the capture apparatus that realization is arranged on the 3rd S. A. is adjusted at any angle, make airborne capture apparatus realize self-stabilization, and can arbitrarily angledly take, thereby carry out flight path adjustment without aircraft in order to take a certain angle.
Brief description of the drawings
Fig. 1 is easy structure schematic diagram of the present utility model.
Detailed description of the invention
As shown in Figure 1, the utility model comprises the first S. A. 1, the second S. A. 2 and the 3rd S. A. 3, one end of described the first S. A. 1 is provided with the first motor 4, the other end is connected with head rod 5, the other end of described head rod 5 is fixedly installed the second motor 6, the output shaft of described the second motor 6 is fixedly connected with described the second S. A. 2, the two ends of described the second S. A. 2 are all connected with the second pipe link 7, the outer end of described second pipe link 7 is fixedly installed the 3rd motor 8 therein, on the outer end of other described second pipe link 7 and the output shaft of described the 3rd motor 8, be provided with connecting panel 9, the described connecting panel 9 being connected with the output shaft of described the 3rd motor 8 is fixedly connected with the output shaft of described the 3rd motor 8, described in another, connecting panel 9 is rotationally connected with the second pipe link 7 described in another, described the 3rd S. A. 3 is arranged between two described connecting panels 9.
The output shaft of described the first motor 4 is fixedly connected with peripheral aircraft devices, and described the first S. A. 1 is done the rotation of 360 ° around the output shaft of described the first motor 4, and this makes capture apparatus carry out 360 ° of pan-shots.The output shaft of described the second motor 6 is fixedly connected with the medium position of described the second S. A. 2, described the second S. A. 2 is done the rotation of 160 ° around the output shaft of described the second motor 6, in the time that described the second S. A. 2 is positioned at horizontal direction, can respectively rotate to the left or to the right 80 °, thereby make described S. A. 3 follow synchronous rotary to the left or to the right.Described the 3rd S. A. 3 is done the rotation of 150 ° around the output shaft of described the 3rd motor 8.On described the 3rd S. A. 3, be provided with equipment fixed platform 10, determine according to its center of gravity the position of described equipment fixing 10 on described the 3rd S. A. 3.
The utility model is in the time of application, as long as capture apparatus is fixed in described equipment fixed platform 10, then aircraft is in flight course, the seat in the plane position different according to aircraft, can, by adjusting the cooperation adjustment of described the first motor 4, the second motor 6 and the 3rd motor 8, make capture apparatus be positioned at all the time level attitude.So the utility model is a kind of three axle Self-stabilization holders that can realize airborne equipment self-stabilization.
The utility model can be applicable to tripod head equipment field.
Claims (5)
1. an axle Self-stabilization holder, it is characterized in that: this The Cloud Terrace comprises the first S. A. (1), the second S. A. (2) and the 3rd S. A. (3), one end of described the first S. A. (1) is provided with the first motor (4), the other end is connected with head rod (5), the other end of described head rod (5) is fixedly installed the second motor (6), the output shaft of described the second motor (6) is fixedly connected with described the second S. A. (2), the two ends of described the second S. A. (2) are all connected with the second pipe link (7), the outer end of described second pipe link (7) is fixedly installed the 3rd motor (8) therein, on the outer end of other described second pipe link (7) and the output shaft of described the 3rd motor (8), be provided with connecting panel (9), the described connecting panel (9) being connected with the output shaft of described the 3rd motor (8) is fixedly connected with the output shaft of described the 3rd motor (8), connecting panel described in another (9) is rotationally connected with the second pipe link (7) described in another, described the 3rd S. A. (3) is arranged between two described connecting panels (9).
2. three axle Self-stabilization holders according to claim 1, it is characterized in that: the output shaft of described the first motor (4) is fixedly connected with peripheral aircraft devices, described the first S. A. (1) is done the rotation of 360 ° around the output shaft of described the first motor (4).
3. three axle Self-stabilization holders according to claim 1, it is characterized in that: the output shaft of described the second motor (6) is fixedly connected with the medium position of described the second S. A. (2), described the second S. A. (2) is done the rotation of 160 ° around the output shaft of described the second motor (6).
4. three axle Self-stabilization holders according to claim 1, is characterized in that: described the 3rd S. A. (3) is done the rotation of 150 ° around the output shaft of described the 3rd motor (8).
5. three axle Self-stabilization holders according to claim 4, is characterized in that: be provided with equipment fixed platform (10) at the medium position of described the 3rd S. A. (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420299233.1U CN203996915U (en) | 2014-06-07 | 2014-06-07 | Three axle Self-stabilization holders |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420299233.1U CN203996915U (en) | 2014-06-07 | 2014-06-07 | Three axle Self-stabilization holders |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203996915U true CN203996915U (en) | 2014-12-10 |
Family
ID=52036955
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420299233.1U Expired - Fee Related CN203996915U (en) | 2014-06-07 | 2014-06-07 | Three axle Self-stabilization holders |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203996915U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104696690A (en) * | 2015-03-18 | 2015-06-10 | 零度智控（北京）智能科技有限公司 | Onboard holder |
| CN105042299A (en) * | 2015-04-22 | 2015-11-11 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle mounted pan-tilt |
| CN105217051A (en) * | 2015-10-29 | 2016-01-06 | 中国科学院遥感与数字地球研究所 | Unmanned plane one camera multi-angled shooting bracing or strutting arrangement |
| WO2018018635A1 (en) * | 2016-07-29 | 2018-02-01 | 深圳市大疆灵眸科技有限公司 | Gimbal, photographing device, and unmanned aerial vehicle |
| US10919645B2 (en) | 2015-10-28 | 2021-02-16 | Autel Robotics Co., Ltd. | Gimbal quick assembly/disassembly apparatus and unmanned aerial vehicle having the same |
-
2014
- 2014-06-07 CN CN201420299233.1U patent/CN203996915U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104696690A (en) * | 2015-03-18 | 2015-06-10 | 零度智控（北京）智能科技有限公司 | Onboard holder |
| CN104696690B (en) * | 2015-03-18 | 2017-05-24 | 零度智控（北京）智能科技有限公司 | Onboard holder |
| CN105042299A (en) * | 2015-04-22 | 2015-11-11 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle mounted pan-tilt |
| CN105042299B (en) * | 2015-04-22 | 2017-05-31 | 零度智控（北京）智能科技有限公司 | Unmanned vehicle airborne tripod head |
| US10919645B2 (en) | 2015-10-28 | 2021-02-16 | Autel Robotics Co., Ltd. | Gimbal quick assembly/disassembly apparatus and unmanned aerial vehicle having the same |
| CN105217051A (en) * | 2015-10-29 | 2016-01-06 | 中国科学院遥感与数字地球研究所 | Unmanned plane one camera multi-angled shooting bracing or strutting arrangement |
| CN105217051B (en) * | 2015-10-29 | 2017-07-07 | 中国科学院遥感与数字地球研究所 | Unmanned plane one camera multi-angled shooting support meanss |
| WO2018018635A1 (en) * | 2016-07-29 | 2018-02-01 | 深圳市大疆灵眸科技有限公司 | Gimbal, photographing device, and unmanned aerial vehicle |
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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 |
Granted publication date: 20141210 Termination date: 20150607 |
|
| EXPY | Termination of patent right or utility model |