CN203318686U - Aerial photography cloud deck for aeromodelling aircraft - Google Patents
Aerial photography cloud deck for aeromodelling aircraft Download PDFInfo
- Publication number
- CN203318686U CN203318686U CN2013201938655U CN201320193865U CN203318686U CN 203318686 U CN203318686 U CN 203318686U CN 2013201938655 U CN2013201938655 U CN 2013201938655U CN 201320193865 U CN201320193865 U CN 201320193865U CN 203318686 U CN203318686 U CN 203318686U
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Abstract
The utility model discloses an aerial photography cloud deck for an aeromodelling aircraft. The aerial photography cloud deck comprises an aircraft installation part, wherein a control board installation position is arranged at the lower end of the aircraft installation part; the lower end of the control board installation position is connected with a fixing arm; a first motor is fixed at the lower part of the fixing arm; a first motor rotating shaft is connected with a moving control arm; a first shaft part and a second shaft part are fixedly connected with two sides of the moving control arm respectively; a second motor is fixedly connected with the front end of the first shaft part; and one side of a camera installation part is connected with a second motor rotating shaft, and the other side of the camera installation part is movably connected with the second shaft part. According to the aerial photography cloud deck, shooting can be performed in multiple angles, and the shooting effect is good.
Description
Technical field
The utility model relates to holder for aerial photographing, specifically a kind of aeromodelling aerocraft holder for aerial photographing.
Background technology
Aeromodelling aerocraft mainly is comprised of wing, empennage, fuselage, alighting gear and driving engine five parts.To be aeromodelling aerocraft produce the device of lift to wing when flight, and the horizontal side can keep aeromodelling aerocraft flight the time is stable.Empennage comprises tailplane and vertical tail two parts.Pitching when tailplane can keep aeromodelling aerocraft flight is stable, and direction when vertical tail keeps aeromodelling aerocraft flight is stable.Elevating rudder on tailplane can be controlled the lifting of aeromodelling aerocraft, and the yaw rudder on vertical tail can be controlled the heading of aeromodelling aerocraft.Fuselage is that the each several part of model is coupled to the trunk portion of an integral body on fuselage.Can load necessary control parts, equipment and fuel etc. in fuselage simultaneously.Driving engine is the device that aeromodelling aerocraft produces flying power.The modern Aviation model sport is divided into free flight, line manipulation, radio telecommand, emulation and the five large classes such as electronic.By the power mode, be divided into again: piston engine, jet engine, rubber-band model aircraft and motorless model glider etc.Screw propeller is to depend on blade to rotate the device that turn of engine power is converted into to propulsive force in air.During the screw propeller rotation, blade constantly pushes large quantity of air (propulsive medium) backward, produces propulsive force on blade.
At present, in some aeromodelling aerocrafts, pick up camera is housed, purpose is to utilize aeromodelling aerocraft at when flight required image of taking pictures.The strut member that pick up camera is installed on aeromodelling aerocraft is called holder for aerial photographing.The level of capable of regulating pick up camera and the angle of pitching install pick up camera on fixing The Cloud Terrace after, reach lockable adjusting mechanism after best operating attitude.The holder for aerial photographing attitude is to be realized by stepper motor, and electrical motor accepts the signal of self-controller accurately to move location.Under the effect of control signal, the pick up camera on The Cloud Terrace can be located the required image of taking pictures.Existing holder for aerial photographing is flexible not enough, can not control a plurality of angles of camera head and be taken pictures.
The utility model content
Technical matters to be solved: the utility model purpose is to provide a kind of pick up camera flexible motion aeromodelling aerocraft holder for aerial photographing that also a plurality of angles of energy are made a video recording.
Technical scheme: a kind of aeromodelling aerocraft holder for aerial photographing, comprise the aircraft fabricated section, it is characterized in that: there is a control desk installation position described aircraft fabricated section lower end, be connected with a fixed arm in lower end, control desk installation position, the first motor is fixed in the fixed arm bottom, the first machine shaft moving Control arm of taking over a job, movable Control arm both sides are connected with respectively the first axle part and the second axle part, the second motor is fixed in the first axle part front end, pick up camera fabricated section one edge joint the second machine shaft, pick up camera fabricated section another side and the second axle part loose joint.
Also be provided with shock absorption device between described aircraft fabricated section and control desk installation position.
The utility model effect is: the utility model, owing to having adopted technique scheme, is provided with the activity of electric machine control pick up camera in the aeromodelling aerocraft The Cloud Terrace, can a plurality of angles be made a video recording, and photographic effect is good.
The accompanying drawing explanation
Fig. 1 is the utility model structural representation.
In figure: number in the figure representative: aircraft fabricated section 1, shock absorption device 2, control desk installation position 3, fixed arm 4, the first motors 5, pick up camera fabricated section 6, movable Control arm 7, the first axle part 8, the second axle part 9, the second motors 10, steady arm installation portion 11.
The specific embodiment
See Fig. 1, a kind of aeromodelling aerocraft holder for aerial photographing, comprise aircraft fabricated section 1, there is a control desk installation position 3 described aircraft fabricated section 1 lower end, be connected with a fixed arm 4 in 3 lower ends, control desk installation position, the first motor 5 is fixed in fixed arm 4 bottoms, the first motor 5 rotating shafts are taken over a job and are moved Control arm 7(rotating shaft not shown in FIG.), movable Control arm 7 both sides are connected with respectively the first axle part 8 and the second axle part 9, the second motor 10 is fixed in the first axle part 8 front ends, 6 one edge joint the second motor 10 rotating shafts (rotating shaft not shown in FIG.) of pick up camera fabricated section, pick up camera fabricated section 6 another sides and the second axle part 9 loose joints.
Also be provided with shock absorption device 2 between described aircraft fabricated section 1 and control desk installation position 3.
The second axle part 9 front ends also are provided with steady arm installation portion 11, and steady arm is steady effect, reduce camera vibration.First and second motor is connected with control circuit, battery in aircraft by wire respectively.The utility model is to provide a kind of aeromodelling aerocraft holder for aerial photographing, does not comprise aircraft.
Specifically details are as follows: aircraft fabricated section 1 is to be fixed in carry-only, and shock absorption device 2 consists of a plurality of wheel shape nonrigid plastics, has elasticity.Control desk installation position 3 is used for the mounting circuit control desk, major control the first motor 5, two motors 10.The first motor 5 control activity Control arm 7 both sides move up and down, and the second motor 10 is controlled pick up camera fabricated section 6 and rotated.
The utility model only limits to absolutely not these examples.The foregoing is only the utility model embodiment preferably, only, for describing the utility model, can not be interpreted as the restriction to scope of the present utility model.It should be pointed out that all any modifications of making within spirit of the present utility model and principle, be equal to replacement and improvement etc., within all should being included in protection domain of the present utility model.
Claims (2)
1. an aeromodelling aerocraft holder for aerial photographing, comprise aircraft fabricated section (1), it is characterized in that: there is a control desk installation position (3) described aircraft fabricated section (1) lower end, be connected with a fixed arm (4) in lower end, control desk installation position (3), the first motor (5) is fixed in fixed arm (4) bottom, the first motor (5) rotating shaft moving Control arm (7) of taking over a job, movable Control arm (7) both sides are connected with respectively the first axle part (8) and the second axle part (9), the second motor (10) is fixed in the first axle part (8) front end, (6) one edge joint the second motor (10) rotating shafts of pick up camera fabricated section, pick up camera fabricated section (6) another side and the second axle part (9) loose joint.
2. a kind of aeromodelling aerocraft holder for aerial photographing according to claim 1, is characterized in that: between described aircraft fabricated section (1) and control desk installation position (3), also be provided with shock absorption device (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013201938655U CN203318686U (en) | 2013-04-17 | 2013-04-17 | Aerial photography cloud deck for aeromodelling aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013201938655U CN203318686U (en) | 2013-04-17 | 2013-04-17 | Aerial photography cloud deck for aeromodelling aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203318686U true CN203318686U (en) | 2013-12-04 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013201938655U Expired - Fee Related CN203318686U (en) | 2013-04-17 | 2013-04-17 | Aerial photography cloud deck for aeromodelling aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203318686U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104132226A (en) * | 2014-08-04 | 2014-11-05 | 昆明理工大学 | Efficient damping tripod head |
| CN104379959A (en) * | 2014-03-31 | 2015-02-25 | 深圳市大疆创新科技有限公司 | Damping device and aircraft employing same |
| CN105486349A (en) * | 2015-12-29 | 2016-04-13 | 中国科学院上海微系统与信息技术研究所 | Distribution test system of space three-dimensional multiple parameters and implementation method thereof |
| WO2017084386A1 (en) * | 2015-11-20 | 2017-05-26 | 深圳市道通智能航空技术有限公司 | Dual-arm camera mount |
| CN106742009A (en) * | 2017-03-14 | 2017-05-31 | 中交遥感载荷（北京）科技有限公司 | Unmanned plane support assembly with the adjustable camera hanger of stabilization formula |
| WO2017128782A1 (en) * | 2016-01-26 | 2017-08-03 | 深圳市道通智能航空技术有限公司 | Gimbal and unmanned aerial vehicle |
| CN111977007A (en) * | 2016-07-29 | 2020-11-24 | 深圳市大疆灵眸科技有限公司 | Cloud platform, shooting equipment and unmanned vehicles |
-
2013
- 2013-04-17 CN CN2013201938655U patent/CN203318686U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104379959A (en) * | 2014-03-31 | 2015-02-25 | 深圳市大疆创新科技有限公司 | Damping device and aircraft employing same |
| CN104132226A (en) * | 2014-08-04 | 2014-11-05 | 昆明理工大学 | Efficient damping tripod head |
| CN104132226B (en) * | 2014-08-04 | 2016-06-08 | 昆明理工大学 | A kind of damping The Cloud Terrace |
| WO2017084386A1 (en) * | 2015-11-20 | 2017-05-26 | 深圳市道通智能航空技术有限公司 | Dual-arm camera mount |
| CN105486349A (en) * | 2015-12-29 | 2016-04-13 | 中国科学院上海微系统与信息技术研究所 | Distribution test system of space three-dimensional multiple parameters and implementation method thereof |
| WO2017128782A1 (en) * | 2016-01-26 | 2017-08-03 | 深圳市道通智能航空技术有限公司 | Gimbal and unmanned aerial vehicle |
| CN111977007A (en) * | 2016-07-29 | 2020-11-24 | 深圳市大疆灵眸科技有限公司 | Cloud platform, shooting equipment and unmanned vehicles |
| CN106742009A (en) * | 2017-03-14 | 2017-05-31 | 中交遥感载荷（北京）科技有限公司 | Unmanned plane support assembly with the adjustable camera hanger of stabilization formula |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170912 Address after: Two road 516000 in Guangdong province Huizhou City Zhongkai high tech Zone No. 45 and (two) the first floor of building Patentee after: HUIZHOU DONGYANG INTELLIGENT TECHNOLOGY CO., LTD. Address before: 516000 Guangdong province Huizhou City Pingnan Zhongkai hi tech Huihuan four Village No. 28 Patentee before: Zhang Jinhai |
|
| 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: 20131204 Termination date: 20190417 |