CN201380965Y - Aerial photography cloud platform on small-sized pilotless aircraft - Google Patents
Aerial photography cloud platform on small-sized pilotless aircraft Download PDFInfo
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- CN201380965Y CN201380965Y CN200920107579U CN200920107579U CN201380965Y CN 201380965 Y CN201380965 Y CN 201380965Y CN 200920107579 U CN200920107579 U CN 200920107579U CN 200920107579 U CN200920107579 U CN 200920107579U CN 201380965 Y CN201380965 Y CN 201380965Y
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Abstract
The utility model relates to an aerial photography cloud platform on a small-sized pilotless aircraft, which is characterized in that the aerial photography cloud platform comprises an outer fixed frame, a middle swing frame and an inner swing frame which are orderly sleeved, and has simple structure and light weight. The middle swing frame is asway connected on the outer fixed frame through a pair of rotating shafts, the inner swing frame is asway connected on the middle swing frame through another pair of rotating shafts, the two pairs of rotating shafts are arranged in 90 degrees, the two pairs of rotating shafts are respectively connected with a crank-link mechanism, the two crank-link mechanisms are respectively driven by a motor, and the two motors are respectively fixed on the outer fixed frame. A camera arranged on the inner swing frame can swing on two directions at the same time, thereby achieving a steady and suitable shooting angle. Therefore, the aerial photography cloud platform is suitable for onboard use of the small-sized pilotless aircraft.
Description
Technical field
The utility model relates to a kind of camera apparatus, particularly about the The Cloud Terrace of taking photo by plane on a kind of miniature self-service aircraft.
Background technology
Be accompanied by the development of aerial remote sens ing technique, often need on the miniature self-service aircraft, camera be installed, carry out aviation and take.The camera of taking photo by plane is subjected to the control of ground control system, takes the image that will choose.In order to make captured image more clear, accurate, the mutually confidential good shooting angle that remains that just requires to take photo by plane, and because aircraft in flight course, jolt, inclination is inevitable phenomenon, like this, will the shooting effect of the camera of taking photo by plane be impacted.The existing The Cloud Terrace of taking photo by plane can only carry out the adjustment of a direction mostly, and can not realize the multi-angle adjustment.
Summary of the invention
At the problems referred to above, the purpose of this utility model is the The Cloud Terrace of taking photo by plane that proposes on a kind of miniature self-service aircraft.
For achieving the above object, the utility model is taked following technical scheme: the The Cloud Terrace of taking photo by plane on a kind of miniature self-service aircraft, it is characterized in that: it comprises sheathed successively external fixation frame, middle swing frame and interior swing frame, described in swing frame by a pair of shaft swing be connected on the external fixation frame, swing frame swingingly is connected on the described middle swing frame by another countershaft in described, two pairs of described rotating shafts are 90 ° of settings, and two pairs of described rotating shafts are connected with a piston crank mechanism respectively, two described piston crank mechanisms are respectively by a motor-driven, and two described motors are separately fixed on the described external fixation frame.
A described countershaft that connects described middle swing frame and external fixation frame, wherein each rotating shaft all is that an end is fixed on the described middle swing frame, the other end is rotatably connected on the described external fixation frame.
Described another countershaft that connects described interior swing frame and middle swing frame, wherein each rotating shaft all is that an end is fixed on the described interior swing frame, the other end is rotatably connected on the described middle swing frame.
Captive joint a support on a described countershaft and another countershaft respectively, two described supports are connected respectively on the connecting rod of cooresponding described piston crank mechanism.
The crank disc of described piston crank mechanism is connected the mouth of cooresponding described motor.
The utility model is owing to take above technical scheme, it has the following advantages: 1, the utility model is owing to be provided with a kind of frame form's the The Cloud Terrace of taking photo by plane, structure is simple and direct, light, and when camera was installed on the miniature self-service aircraft by this device, camera was easy to take and adjust angle.2, the utility model adopts three layers of sheathed successively framed structure, and the external fixation frame is fixing aboard, and middle swing frame is supported on the external fixation frame and by a motor and a cover crank connecting rod mechanism by a countershaft and drives its swing; Interior swing frame is supported on the middle swing frame by another countershaft, can swing with middle swing frame, simultaneously, interior swing frame can also drive by another motor and another set of piston crank mechanism and do self swing, the swing of two countershafts is mutually 90 °, like this, the camera that is arranged on the internal fixation frame just can be done the swing of both direction simultaneously, thereby reaches steadily suitable shooting angle.Therefore the utility model is suitable for the use of miniature self-service aircraft airborne.
Description of drawings
Fig. 1 is a plan structure scheme drawing of the present utility model
The specific embodiment
Below in conjunction with drawings and Examples the utility model is described in detail.
As shown in Figure 1, the utility model comprises mainly in the external fixation frame 1, that 3, three frames of swing frame are sheathed state successively from outside to inside in the swing frame 2 and.External fixation frame 1 is fixed on aircraft and takes in the cabin.4, two rotating shaft 4 coaxial lines of difference captive joint one rotating shaft on one group of relative frame of middle swing frame 2.The other end of two rotating shafts 4 is movably connected on the external fixation frame 1 by bearing respectively.Like this, middle swing frame 2 not only can be supported on the external fixation frame 1, can also be axis swing with two rotating shafts 4, and the propulsive effort of this swing comes from first motor 5.First motor 5 is fixed on the external fixation frame 1.Connect a crank disc 6 on the output shaft of first motor 5, the eccentric connecting rod 7 that connects on the crank disc 6, the other end of connecting rod 7 is connected on the support 8, and support 8 is fixed in the contiguous rotating shaft 4, perhaps is fixed on the middle swing frame 2 that is connected with contiguous rotating shaft 4.After first motor 5 starts, drive crank disc 6 rotations, the rotation of crank disc 6 will drivening rod 7 displacements that produce horizontal directions, this displacement will be ordered about support 8 and the rotating shaft 4 that is connected left-right rotation in the bearing hole of fixed frame 1 outside, rotating shaft 4 during the rotation in the bearing hole of fixed frame 1 will cause outside swing frame 2 relative external fixation frames 1 swing.The setting of interior swing frame 3 and middle swing frame 2 are basic identical, captive joint one second rotating shaft 9 respectively on one group of relative frame of interior swing frame 3.Two second rotating shafts, 9 coaxial lines, and the axis of two second rotating shafts 9 and two rotating shafts 4 is perpendicular.The other end of two second rotating shafts 9 is movably connected on the middle swing frame 2 by bearing respectively.Same principle is fixed one second motor 10 outside on the fixed frame 1.Connect a crank disc 11 on the output shaft of second motor 10, the eccentric connecting rod 12 that connects on the crank disc 11, the other end of connecting rod 12 is connected on one second support 13, second support 13 is fixed in one the second contiguous rotating shaft 9, perhaps is fixed on the interior swing frame 3 that is connected with the second contiguous rotating shaft 9.Like this, on the swing frame 2,, can also be axle center self swing during interior swing frame 3 not only can be supported on second rotating shaft 9 with middle swing frame 2 swings.
In the inside of interior swing frame 3 the camera (not shown) of taking photo by plane is installed.
In sum, the utility model is to have utilized two drive motor and two cover crank connecting rod mechanisms, drives two swing frames respectively, and two swing frames are swung on forward and backward and left and right both direction respectively, adjusts the shooting angle of the camera of taking photo by plane with this.
Claims (7)
1, the The Cloud Terrace of taking photo by plane on the miniature self-service aircraft, it is characterized in that: it comprises sheathed successively external fixation frame, middle swing frame and interior swing frame, described in swing frame by a pair of shaft swing be connected on the external fixation frame, swing frame swingingly is connected on the described middle swing frame by another countershaft in described, two pairs of described rotating shafts are 90 ° of settings, and two pairs of described rotating shafts are connected with a piston crank mechanism respectively, two described piston crank mechanisms are respectively by a motor-driven, and two described motors are separately fixed on the described external fixation frame.
2, the The Cloud Terrace of taking photo by plane on the miniature self-service aircraft as claimed in claim 1, it is characterized in that: a described countershaft that connects described middle swing frame and external fixation frame, wherein each rotating shaft all is that an end is fixed on the described middle swing frame, and the other end is rotatably connected on the described external fixation frame.
3, the The Cloud Terrace of taking photo by plane on the miniature self-service aircraft as claimed in claim 1, it is characterized in that: described another countershaft that connects described interior swing frame and middle swing frame, wherein each rotating shaft all is that an end is fixed on the described interior swing frame, and the other end is rotatably connected on the described middle swing frame.
4, the The Cloud Terrace of taking photo by plane on the miniature self-service aircraft as claimed in claim 2, it is characterized in that: described another countershaft that connects described interior swing frame and middle swing frame, wherein each rotating shaft all is that an end is fixed on the described interior swing frame, and the other end is rotatably connected on the described middle swing frame.
5, as the The Cloud Terrace of taking photo by plane on claim 1 or 2 or the 3 or 4 described miniature self-service aircrafts, it is characterized in that: captive joint a support on a described countershaft and another countershaft respectively, two described supports are connected respectively on the connecting rod of cooresponding described piston crank mechanism.
6, as the The Cloud Terrace of taking photo by plane on claim 1 or 2 or the 3 or 4 described miniature self-service aircrafts, it is characterized in that: the crank disc of described piston crank mechanism is connected the mouth of cooresponding described motor.
7, the The Cloud Terrace of taking photo by plane on the miniature self-service aircraft as claimed in claim 5, it is characterized in that: the crank disc of described piston crank mechanism is connected the mouth of cooresponding described motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200920107579U CN201380965Y (en) | 2009-04-28 | 2009-04-28 | Aerial photography cloud platform on small-sized pilotless aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200920107579U CN201380965Y (en) | 2009-04-28 | 2009-04-28 | Aerial photography cloud platform on small-sized pilotless aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201380965Y true CN201380965Y (en) | 2010-01-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200920107579U Expired - Fee Related CN201380965Y (en) | 2009-04-28 | 2009-04-28 | Aerial photography cloud platform on small-sized pilotless aircraft |
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| CN (1) | CN201380965Y (en) |
Cited By (7)
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| CN102856840A (en) * | 2012-09-29 | 2013-01-02 | 江苏省电力公司徐州供电公司 | Auxiliary suspension device of power inspection aircraft |
| WO2013033924A1 (en) * | 2011-09-09 | 2013-03-14 | 深圳市大疆创新科技有限公司 | Dual-axis ball head for use in unmanned aerial vehicle, triple-axis ball head for use in unmanned aerial vehicle, and multi-rotor aerial vehicle |
| US8938160B2 (en) | 2011-09-09 | 2015-01-20 | SZ DJI Technology Co., Ltd | Stabilizing platform |
| CN104781600A (en) * | 2014-04-04 | 2015-07-15 | 深圳市大疆创新科技有限公司 | Cloud platform drive device and cloud platform assembly adopting drive device |
| US9277130B2 (en) | 2013-10-08 | 2016-03-01 | SZ DJI Technology Co., Ltd | Apparatus and methods for stabilization and vibration reduction |
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| CN107076350A (en) * | 2016-10-10 | 2017-08-18 | 深圳市大疆灵眸科技有限公司 | Three axle heads and three axle head filming apparatus |
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2009
- 2009-04-28 CN CN200920107579U patent/CN201380965Y/en not_active Expired - Fee Related
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| US9648240B2 (en) | 2011-09-09 | 2017-05-09 | SZ DJI Technology Co., Ltd | Stabilizing platform |
| WO2013033924A1 (en) * | 2011-09-09 | 2013-03-14 | 深圳市大疆创新科技有限公司 | Dual-axis ball head for use in unmanned aerial vehicle, triple-axis ball head for use in unmanned aerial vehicle, and multi-rotor aerial vehicle |
| US8938160B2 (en) | 2011-09-09 | 2015-01-20 | SZ DJI Technology Co., Ltd | Stabilizing platform |
| US11140322B2 (en) | 2011-09-09 | 2021-10-05 | Sz Dji Osmo Technology Co., Ltd. | Stabilizing platform |
| US10321060B2 (en) | 2011-09-09 | 2019-06-11 | Sz Dji Osmo Technology Co., Ltd. | Stabilizing platform |
| CN102856840A (en) * | 2012-09-29 | 2013-01-02 | 江苏省电力公司徐州供电公司 | Auxiliary suspension device of power inspection aircraft |
| CN102856840B (en) * | 2012-09-29 | 2016-03-23 | 江苏省电力公司徐州供电公司 | A kind of auxiliary suspension device of power inspection aircraft |
| US10747225B2 (en) | 2013-07-31 | 2020-08-18 | SZ DJI Technology Co., Ltd. | Remote control method and terminal |
| US11385645B2 (en) | 2013-07-31 | 2022-07-12 | SZ DJI Technology Co., Ltd. | Remote control method and terminal |
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| US9927812B2 (en) | 2013-07-31 | 2018-03-27 | Sz Dji Technology, Co., Ltd. | Remote control method and terminal |
| US9277130B2 (en) | 2013-10-08 | 2016-03-01 | SZ DJI Technology Co., Ltd | Apparatus and methods for stabilization and vibration reduction |
| US11962905B2 (en) | 2013-10-08 | 2024-04-16 | Sz Dji Osmo Technology Co., Ltd. | Apparatus and methods for stabilization and vibration reduction |
| US9485427B2 (en) | 2013-10-08 | 2016-11-01 | SZ DJI Technology Co., Ltd | Apparatus and methods for stabilization and vibration reduction |
| US11134196B2 (en) | 2013-10-08 | 2021-09-28 | Sz Dji Osmo Technology Co., Ltd. | Apparatus and methods for stabilization and vibration reduction |
| US10334171B2 (en) | 2013-10-08 | 2019-06-25 | Sz Dji Osmo Technology Co., Ltd. | Apparatus and methods for stabilization and vibration reduction |
| US9749544B2 (en) | 2014-04-04 | 2017-08-29 | Sz Dji Osmo Technology Co., Ltd. | Gimbal driving device and gimbal assembly using the same |
| WO2015149370A1 (en) * | 2014-04-04 | 2015-10-08 | 深圳市大疆创新科技有限公司 | Tripod head driving device and tripod head assembly using same |
| CN104781600A (en) * | 2014-04-04 | 2015-07-15 | 深圳市大疆创新科技有限公司 | Cloud platform drive device and cloud platform assembly adopting drive device |
| CN104781600B (en) * | 2014-04-04 | 2017-01-18 | 深圳市大疆创新科技有限公司 | Cloud platform drive device and cloud platform assembly adopting drive device |
| CN107076350B (en) * | 2016-10-10 | 2019-02-12 | 深圳市大疆灵眸科技有限公司 | Three axis holders and three axis holder filming apparatus |
| WO2018068173A1 (en) * | 2016-10-10 | 2018-04-19 | 深圳市大疆灵眸科技有限公司 | Three-axis pan-tilt base, and three-axis pan-tilt camera device |
| US11137667B2 (en) | 2016-10-10 | 2021-10-05 | Sz Dji Osmo Technology Co., Ltd. | Three-axis gimbal and three-axis gimbal photographing apparatus |
| US11281076B2 (en) | 2016-10-10 | 2022-03-22 | SZ DJI Technology Co., Ltd. | Three-axis gimbal and three-axis gimbal photographing apparatus |
| CN107076350A (en) * | 2016-10-10 | 2017-08-18 | 深圳市大疆灵眸科技有限公司 | Three axle heads and three axle head filming apparatus |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100113 Termination date: 20120428 |