CN203439269U - A special aerial photography holder for multiaxial aircrafts - Google Patents
A special aerial photography holder for multiaxial aircrafts Download PDFInfo
- Publication number
- CN203439269U CN203439269U CN201320261237.6U CN201320261237U CN203439269U CN 203439269 U CN203439269 U CN 203439269U CN 201320261237 U CN201320261237 U CN 201320261237U CN 203439269 U CN203439269 U CN 203439269U
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- China
- Prior art keywords
- camera stand
- camera frame
- camera
- turning wheel
- guide rail
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Abstract
The utility model discloses a special aerial photography holder for multiaxial aircrafts. The special aerial photography holder comprises a rotating shaft; a top plate is disposed below the rotating shaft, two support stands and a camera stand support are arranged under the top plate; an inclined bracket is fixedly arranged on the outer side of the camera stand support; the inner side of the camera stand support is connected with a camera stand through a transverse rolling shaft turning wheel; the camera stand is connected with the camera stand support through the transverse rolling shaft turning wheel; a semi-circular guide rail is disposed on the front end of the camera stand; the guide rail is hung below the top plate through an upper group of guide wheels and a lower group of guide wheels; the guide rail can be driven to slide between the two groups of guide wheels by the transverse rolling shaft turning wheel; the camera stand is connected with a camera base through a pitch shaft turning wheel; and the transverse rolling shaft turning wheel is perpendicular to the pitch shaft turning wheel. The special aerial photography holder overcomes the deficiency of the conventional technology. With the semi-circular guide rail at the front end of the camera stand, the camera stand has a front support part and a rear support part, namely the transverse rolling shaft turning wheel and the front end semi-circular guide rail, so that the stability of rotation of the camera stand is improved and the imaging quality is improved.
Description
Technical field
The utility model relates to a kind of equipment of taking photo by plane, the special-purpose holder for aerial photographing of especially a kind of Multi-axis aircraft.
Background technology
Along with the raising that making video needs, take photo by plane more and more general.In the process of taking photo by plane, camera is placed on The Cloud Terrace and takes.Because camera need to convert shooting angle when taking, so The Cloud Terrace need to be designed to rotate the structure of inclination.But the existing poor shortcoming of The Cloud Terrace ubiquity rotational stability that can rotate inclination, has affected the visibility of camera imaging.
Utility model content
The technical problems to be solved in the utility model is to provide the special-purpose holder for aerial photographing of a kind of Multi-axis aircraft, can solve the deficiencies in the prior art, by setting, is suspended on the guide rail on top board, has improved stability when camera frame rotates, and has improved image quality.
For solving the problems of the technologies described above, technical solution adopted in the utility model is as follows.
The special-purpose holder for aerial photographing of a kind of Multi-axis aircraft, structure comprises S. A., S. A. below is provided with top board, top board below is provided with two bracing frames and a camera frame pillar, camera frame pillar outside is fixedly installed tilted supporter, camera frame pillar inner side is connected with camera frame, described camera frame is connected with described camera frame pillar by roll axle runner, camera frame top is provided with half round guide, guide rail is suspended on described top board below by upper and lower two groups of guide wheels, and guide rail can slide under the drive of roll axle runner in the middle of two groups of guide wheels; Described camera frame is connected with camera pedestal by pitch axis runner, and roll axle runner is mutually vertical with pitch axis runner.
As a kind of optimal technical scheme of the present utility model, the center of circle of the center of circle of described half round guide and described roll axle runner is concentric design.
As a kind of optimal technical scheme of the present utility model, described guide wheel has four, and described guide wheel is according to the axis symmetric design of described S. A..
As a kind of optimal technical scheme of the present utility model, the scope of the included angle A between support frame as described above and top board is 60 °～80 °.
As a kind of optimal technical scheme of the present utility model, between described S. A. and described top board, be provided with bumper.
As a kind of optimal technical scheme of the present utility model, the material of holder for aerial photographing is carbon fiber.
Adopt the beneficial effect that technique scheme is brought to be: on camera frame of the present utility model, be provided with guide rail, guide rail can slide under guide wheel spacing, that has avoided that camera frame produces when rotating radially rocks, and has improved the visibility of camera imaging.The center of circle of the center of circle of guide rail and roll axle runner is concentric design, has improved smoothness when guide rail slides.Guide wheel is according to the axis symmetric design of described S. A., and the bearing force left and right that makes to be applied on guide rail is average.Angle between bracing frame and top board is designed to 60 °～80 °, can not affect under the prerequisite of shooting, improves the stability of strutting system of holder for aerial photographing.The bumper arranging between S. A. and top board can effectively cushion the vibration producing in flight course.Whole holder for aerial photographing adopts carbon fibre material to make, and lightweight, intensity is high, can bear a heavy burden for aircraft reduces.
Accompanying drawing explanation
Fig. 1 is the front view of a specific embodiment of the utility model.
Fig. 2 is the right elevation of a specific embodiment of the utility model.
In figure: 1, S. A.; 2, top board; 3, bracing frame; 4, camera frame pillar; 5, tilted supporter; 6, camera frame; 7, roll wheel runner; 8, half round guide; 9, guide wheel; 10, pitch axis runner; 11, camera pedestal; 12, bumper.
The specific embodiment
Referring to accompanying drawing, the utility model structure comprises S. A. 1, S. A. 1 below is provided with top board 2, top board 2 belows are provided with two bracing frames 3 and a camera frame pillar 4, camera frame pillar 4 outsides are fixedly installed tilted supporter 5, camera frame pillar 4 inner sides are connected with camera frame 6, described camera frame 6 is connected with described camera frame pillar 4 by the first runner 7, camera frame 6 tops are provided with half round guide 8, half round guide 8 is suspended on described top board 2 belows by upper and lower two groups of guide wheels 9, half round guide 8 can slide under the drive of roll wheel runner 7 in the middle of two groups of guide wheels 9, described camera frame 6 is connected with camera pedestal 11 by facing upward the axle runner 10 of bowing, and roll wheel runner 7 is mutually vertical with pitch axis runner 10.The center of circle of the center of circle of described half round guide 8 and described roll wheel runner 7 is concentric design.Described guide wheel 9 has four, and described guide wheel 9 is according to the axis symmetric design of described S. A. 1.Included angle A between support frame as described above 3 and top board 2 is 70 °.Between described S. A. 1 and described top board 2, be provided with bumper 12.The material of holder for aerial photographing is carbon fiber.
Referring to accompanying drawing, principle of work of the present utility model is: camera is fixed in camera pedestal 11, and camera pedestal 11 can, under the drive of horizontal roller wheel shaft 7 and pitch axis runner 10, be carried out the random rotation of four direction all around.
On camera frame 6 of the present utility model, being provided with half round guide 8, half round guides 8 can slide under guide wheel 9 spacing, and that has avoided that camera frame 6 produces when rotating radially rocks, and has improved the visibility of camera imaging.The center of circle of the center of circle of half round guide 8 and horizontal roller wheel shaft 7 is concentric design, has improved smoothness when half round guide 8 slides.Guide wheel 9 is according to the axis symmetric design of described S. A. 1, and the bearing force left and right that makes to be applied on half round guide 8 is average.Angle between bracing frame 3 and top board 2 is designed to 70 °, can not affect under the prerequisite of shooting, improves the stability of strutting system of holder for aerial photographing.The bumper 12 arranging between S. A. 1 and top board 2 can effectively cushion the vibration producing in flight course.Whole holder for aerial photographing adopts carbon fibre material to make, and lightweight, intensity is high, can bear a heavy burden for aircraft reduces.
Foregoing description only proposes as the enforceable technical scheme of the utility model, not as the Single restriction condition to its technical scheme itself.
Claims (4)
1. the special-purpose holder for aerial photographing of a Multi-axis aircraft, structure comprises S. A. (1), S. A. (1) below is provided with top board (2), top board (2) below is provided with two bracing frames (3) and a camera frame pillar (4), camera frame pillar (4) outside is fixedly installed tilted supporter (5), camera frame pillar (4) inner side is connected with camera frame (6), it is characterized in that: described camera frame (6) is connected with described camera frame pillar (4) by roll axle runner (7), camera frame (6) front end is provided with half round guide (8), half round guide (8) is suspended on described top board (2) below by upper and lower two groups of guide wheels (9), half round guide (8) can slide under the drive of roll axle runner (7) in the middle of two groups of guide wheels (9), described camera frame (6) is connected with camera pedestal (11) by pitch axis (10), and roll axle runner (7) is mutually vertical with pitch axis runner (10).
2. the special-purpose holder for aerial photographing of Multi-axis aircraft according to claim 1, is characterized in that: described camera frame front end increase by half round guide (8) and with the center of circle of described roll axle runner (7) be concentric design.
3. the special-purpose holder for aerial photographing of Multi-axis aircraft according to claim 1, is characterized in that: described guide wheel (9) has four, and described guide wheel (9) is according to the axis symmetric design of described S. A. (1).
4. the special-purpose holder for aerial photographing of Multi-axis aircraft according to claim 1, is characterized in that: the material of holder for aerial photographing is aviation aluminium and carbon fiber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320261237.6U CN203439269U (en) | 2013-05-15 | 2013-05-15 | A special aerial photography holder for multiaxial aircrafts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320261237.6U CN203439269U (en) | 2013-05-15 | 2013-05-15 | A special aerial photography holder for multiaxial aircrafts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203439269U true CN203439269U (en) | 2014-02-19 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320261237.6U Expired - Fee Related CN203439269U (en) | 2013-05-15 | 2013-05-15 | A special aerial photography holder for multiaxial aircrafts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203439269U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104176265A (en) * | 2014-07-09 | 2014-12-03 | 中国人民解放军理工大学 | Overturnable bracket system for panoramic camera of unmanned aerial vehicle |
| CN104991572A (en) * | 2015-06-02 | 2015-10-21 | 中国科学院上海技术物理研究所 | Variable-angle hyperspectral imaging system based on posture stability and control method of said system |
| CN105323485A (en) * | 2015-11-16 | 2016-02-10 | 广州供电局有限公司 | Single-camera oblique image acquisition device and method |
| CN106275478A (en) * | 2016-09-08 | 2017-01-04 | 四川建筑职业技术学院 | A kind of slide rail type three-axis stabilization The Cloud Terrace |
| CN106687376A (en) * | 2016-09-09 | 2017-05-17 | 深圳市大疆创新科技有限公司 | Load component and UAV equipped with load component |
-
2013
- 2013-05-15 CN CN201320261237.6U patent/CN203439269U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104176265A (en) * | 2014-07-09 | 2014-12-03 | 中国人民解放军理工大学 | Overturnable bracket system for panoramic camera of unmanned aerial vehicle |
| CN104176265B (en) * | 2014-07-09 | 2016-05-11 | 中国人民解放军理工大学 | The reversible supporting frame system that a kind of unmanned plane panorama camera uses |
| CN104991572A (en) * | 2015-06-02 | 2015-10-21 | 中国科学院上海技术物理研究所 | Variable-angle hyperspectral imaging system based on posture stability and control method of said system |
| CN105323485A (en) * | 2015-11-16 | 2016-02-10 | 广州供电局有限公司 | Single-camera oblique image acquisition device and method |
| CN105323485B (en) * | 2015-11-16 | 2018-10-23 | 广州供电局有限公司 | One camera Oblique images capture device and acquisition method |
| CN106275478A (en) * | 2016-09-08 | 2017-01-04 | 四川建筑职业技术学院 | A kind of slide rail type three-axis stabilization The Cloud Terrace |
| CN106687376A (en) * | 2016-09-09 | 2017-05-17 | 深圳市大疆创新科技有限公司 | Load component and UAV equipped with load component |
| CN106687376B (en) * | 2016-09-09 | 2020-03-20 | 深圳市大疆创新科技有限公司 | Load assembly and unmanned aerial vehicle mounted with same |
| US11155344B2 (en) | 2016-09-09 | 2021-10-26 | SZ DJI Technology Co., Ltd. | Load assembly 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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140219 Termination date: 20170515 |