CN202961882U - Aeromodelling aircraft aerial photo triaxial tripod head with photographic device - Google Patents
Aeromodelling aircraft aerial photo triaxial tripod head with photographic device Download PDFInfo
- Publication number
- CN202961882U CN202961882U CN 201220675024 CN201220675024U CN202961882U CN 202961882 U CN202961882 U CN 202961882U CN 201220675024 CN201220675024 CN 201220675024 CN 201220675024 U CN201220675024 U CN 201220675024U CN 202961882 U CN202961882 U CN 202961882U
- Authority
- CN
- China
- Prior art keywords
- driven pulley
- servomotor
- boom
- video camera
- arm
- 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
Links
- 230000009916 joint effect Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 6
- 238000009434 installation Methods 0.000 abstract description 2
- 230000001141 propulsive effect Effects 0.000 description 3
- 239000000446 fuel Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Images
Landscapes
- Accessories Of Cameras (AREA)
Abstract
The utility model discloses an aeromodelling aircraft aerial photo triaxial tripod head with a photographic device. The aeromodelling aircraft aerial photo triaxial tripod head with the photographic device comprises aircraft installing parts, three rack arms and three foot stools, wherein one ends of the three rack arms are connected together, and the other ends of the three rack arms are respectively and fixedly connected with the three foot stools. A spindle of the aircraft installing parts is installed in a bearing of the connection portion of the three rack arms and is fixedly connected with a first driven wheel, a first servo motor is fixed in a first rack arm, a photographic device frame is further installed below the three rack arms, and the photographic device frame comprises a fixing part, and a movable control arm and an installation arm for a video camera. According to the aeromodelling aircraft aerial photo triaxial tripod head with the photographic device, photos can be taken in a plurality of angles, and an effect of taking the photos is good.
Description
Technical field
The utility model relates to aeromodelling aerocraft, specifically a kind of aeromodelling aerocraft that carries camera head three axle The Cloud Terraces of taking photo by plane.
Background technology
Aeromodelling aerocraft is general the same with manned aircraft, mainly is comprised of wing, empennage, fuselage, undercarriage and 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 the direction when vertical tail keeps aeromodelling aerocraft flight is stable.Elevator on tailplane can be controlled the lifting of aeromodelling aerocraft, and the rudder on vertical tail can be controlled the heading of aeromodelling aerocraft.Fuselage is that the each several part with 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.The device that undercarriage takes off, lands and park for aeromodelling aerocraft.Anterior undercarriage, each undercarriage of two sides, back is front bikini, and anterior two sides is a undercarriage respectively, and one of back undercarriage is rear bikini.Engine is the device that aeromodelling aerocraft produces flying power.The modern Aviation model sport is divided into free flight, line manipulation, wireless remotecontrol, emulation and the five large classes such as electronic.Be divided into again by the power mode: piston engine, jet engine, rubber-band model aircraft and motorless model glider etc.Screw is to depend on blade to rotate the device that engine rotation power is converted into propulsive force in air.During the screw rotation, blade constantly pushes large quantity of air (propulsive medium) backward, produces propulsive force on blade.
The aeromodelling aerocraft frame comprises undercarriage, and at present, in some undercarriages, with camera head, purpose is to utilize aeromodelling aerocraft to take the photograph according to required image when flight.Yet existing camera head is dumb, can not control a plurality of angles of camera head and take the photograph photograph.
The utility model content
Technical problem to be solved: the utility model purpose is to provide a kind of camera head flexible motion and the aeromodelling aerocraft of can a plurality of angles making a video recording is taken photo by plane three axle The Cloud Terraces.
technical scheme: a kind of aeromodelling aerocraft that carries camera head three axle The Cloud Terraces of taking photo by plane, comprise the aircraft installed part, three support arms are the first boom, the second boom, the 3rd boom, three foot-supporting frames, one end of three support arms connects, the other end of three support arms is affixed foot rest respectively, it is characterized in that: the rotating shaft of described aircraft installed part is installed in the bearing of three support arm connecting portions, affixed the first driven pulley of the rotating shaft of aircraft installed part, be fixed with the first servomotor in the first boom, between the wheel output shaft of the first servomotor and the first driven pulley, the first driving-belt is installed,
The camera head frame also is installed below three support arms, and the camera head frame comprises a fixture, movable control arm and video camera hold-down arm;
Affixed the second boom in fixture upper end, fixture lower end loose joint activity control arm, the second driven pulley is located in the middle of movable control arm, is connected with the second servomotor on fixture, between the wheel output shaft of the second servomotor and the second driven pulley, the second driving-belt is installed; The second driven pulley rotating shaft rear end is provided with the first locator;
Movable control arm two ends are affixed with the first axle spare front end and the second axle spare front end respectively, video camera hold-down arm two ends respectively with the first axle spare rear end and the second axle spare rear end loose joint, be fixed with the 3rd servomotor in the first axle spare, video camera hold-down arm one end is provided with the 3rd driven pulley, between the wheel output shaft of the 3rd servomotor and the 3rd driven pulley, the 3rd driving-belt is installed.
Be provided with the video camera installed part in the middle of described video camera hold-down arm; The second axle spare rear end is provided with the second locator.
The utility model effect is: the utility model is owing to having adopted technique scheme, be provided with servomotor and control the activity of camera head frame in aeromodelling aerocraft three axle The Cloud Terraces, can a plurality of angles take the photograph photograph, the utility model is provided with locator, steady when making its shooting, location.Photographic effect is good.
Description of drawings
Fig. 1 is one of the utility model structural representation.
Fig. 2 is two of the utility model structural representation.
Fig. 3 is three of the utility model structural representation.
In figure: number in the figure representative: aircraft installed part 1, the three boom 2, wheel output shaft 7, the first driving-belts 8 of foot rest 3, the first driven pulley 4, the first boom 5, the first servomotor 6, the first servomotors.Camera head frame 9, fixture 10, movable control arm 11, video camera hold-down arm 12, the second boom 13, the second driven pulley 14, the second servomotors 15, the second locator 16, the second driving-belt 18, the first locators 17, the first axle spare 19, the second axle spare 20, the three servomotors 21, the 3rd driven pulley 22, wheel output shaft 23, the three driving-belts 24 of the 3rd servomotor, video camera installed part 25.
The specific embodiment
See Fig. 1-3, a kind of aeromodelling aerocraft that carries camera head three axle The Cloud Terraces of taking photo by plane comprise aircraft installed part 1, three support arms are the first boom 5, the second boom 13, the 3rd boom 2, one end of three foot-supporting frame 3, three support arms connects, and the other end of three support arms is affixed foot rest 3 respectively.The rotating shaft of described aircraft installed part 1 is installed in the bearing of three support arm connecting portions, affixed the first driven pulley 4 of the rotating shaft of aircraft installed part 1, be fixed with in the first boom 5 between the wheel output shaft 7 of the first servomotor 6, the first servomotors and the first driven pulley 4 the first driving-belt 8 is installed.Wheel output shaft refers in rotating shaft with wheel (driving wheel).
Camera head frame 9 also is installed below three support arms, and camera head frame 9 comprises that a fixture 10(sees Fig. 2,3), movable control arm 11 and video camera hold-down arm 12;
Affixed the second boom 13 in fixture 10 upper ends, fixture 10 lower end loose joint activity control arms 11, the second driven pulley 14 is located in the middle of movable control arm 11, be connected with the second servomotor 15(on fixture 10 and see Fig. 1), between the wheel output shaft of the second servomotor (because the visual angle relation does not draw) and the second driven pulley 14, the second driving-belt 18 is installed; The second driven pulley 14 rotating shaft rear ends are provided with the first locator 17(and see Fig. 1).
Be provided with video camera installed part 25 in the middle of described video camera hold-down arm 12; The second axle spare 20 rear ends are provided with the second locator 16(and see Fig. 3), be steady effect, reduce camera vibration.First, second and third servomotor and first and second locator are connected with control circuit, battery in aircraft by wire respectively.The utility model is to provide a kind of aeromodelling aerocraft that carries camera head three axle The Cloud Terraces of taking photo by plane, and does not comprise aircraft.
Specifically details are as follows: three support arms are divided into the first boom 5, the second boom 13, the 3rd boom 2, one end of three support arms connects, and forms described three support arm connecting portions, and a bearing is arranged in connecting portion, the rotating shaft of described aircraft installed part is installed in bearing, bearing not shown in FIG., rotating shaft.The other end of three support arms is affixed foot rest 3 respectively, and foot rest 3 has three, forms tripod structure.During assembling, aircraft installation piece installing 1 is fixed on aircraft, after aircraft takeoff, can control the first servomotor 6 work, the first servomotor drives the first driven pulley 4 and rotates, like this, the rotation thereupon of boom and foot rest and camera head frame 9 is convenient to multi-faceted the taking the photograph of video camera and is shone and the location.
If inoperation boom and foot rest rotate, single camera head frame 9 also has two rotating functions, one, the second servomotor 15 drives the second driven pulley 14 and rotates, movable control arm 11 two ends can form miter angle and move up and down, the second driven pulley 14 rotating shaft rear ends are provided with the first locator 17, are steady effects, reduce camera vibration.Its two, the three servomotor 21 drives the 3rd driven pulley 22 and rotates, and video camera hold-down arm 12 can 360 degree rotations.Video camera (video camera does not draw) is installed on video camera installed part 25.
The utility model only limits to absolutely not these examples.The above is only the utility model embodiment preferably, only is used for describing the utility model, can not be interpreted as the restriction to scope of the present utility model.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 (1)
1. the aeromodelling aerocraft that can carry camera head three axle The Cloud Terraces of taking photo by plane, comprise aircraft installed part (1), three support arms are the first boom (5), the second boom (13), the 3rd boom (2), three foot-supporting frames (3), one end of three support arms connects, the other end of three support arms is affixed foot rest (3) respectively, it is characterized in that: the rotating shaft of described aircraft installed part (1) is installed in the bearing of three support arm connecting portions, affixed the first driven pulley of the rotating shaft of aircraft installed part (1) (4), be fixed with the first servomotor (6) in the first boom (5), between the wheel output shaft of the first servomotor (7) and the first driven pulley (4), the first driving-belt (8) is installed,
Camera head frame (9) also is installed below three support arms, and camera head frame (9) comprises a fixture (10), movable control arm (11) and video camera hold-down arm (12);
Affixed the second boom in fixture (10) upper end (13), fixture (10) lower end loose joint activity control arm (11), the second driven pulley (14) is located in the middle of movable control arm (11), be connected with the second servomotor (15) on fixture (10), between the wheel output shaft of the second servomotor and the second driven pulley (14), the second driving-belt (18) be installed; The second driven pulley (14) rotating shaft rear end is provided with the first locator (17);
Movable control arm (11) two ends are affixed with the first axle spare (19) front end and the second axle spare (20) front end respectively, video camera hold-down arm (12) two ends respectively with the first axle spare (19) rear end and the second axle spare (20) rear end loose joint, be fixed with the 3rd servomotor (21) in the first axle spare (19), video camera hold-down arm (12) one ends are provided with the 3rd driven pulley (22), between the wheel output shaft of the 3rd servomotor (23) and the 3rd driven pulley (22), the 3rd driving-belt (24) are installed;
Be provided with video camera installed part (25) in the middle of described video camera hold-down arm (12); The second axle spare (20) rear end is provided with the second locator (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220675024 CN202961882U (en) | 2012-12-10 | 2012-12-10 | Aeromodelling aircraft aerial photo triaxial tripod head with photographic device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220675024 CN202961882U (en) | 2012-12-10 | 2012-12-10 | Aeromodelling aircraft aerial photo triaxial tripod head with photographic device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202961882U true CN202961882U (en) | 2013-06-05 |
Family
ID=48503013
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220675024 Expired - Fee Related CN202961882U (en) | 2012-12-10 | 2012-12-10 | Aeromodelling aircraft aerial photo triaxial tripod head with photographic device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202961882U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN112124608A (en) * | 2020-08-24 | 2020-12-25 | 温州大学 | A aircraft cloud platform of making a video recording for taking photo by plane |
-
2012
- 2012-12-10 CN CN 201220675024 patent/CN202961882U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN112124608A (en) * | 2020-08-24 | 2020-12-25 | 温州大学 | A aircraft cloud platform of making a video recording for taking photo by plane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203318686U (en) | Aerial photography cloud deck for aeromodelling aircraft | |
| CN107150803A (en) | Mixed layout unmanned plane and its control method | |
| CN111731475B (en) | Vertical take-off and landing tilting composite wing aircraft | |
| CN203666995U (en) | Three-shaft aerial shooting holder | |
| CN104260873B (en) | A kind of delta-wing aircraft | |
| CN204264452U (en) | Electric single-rotor ducted unmanned aerial vehicle | |
| CN206826927U (en) | Mixed layout unmanned plane | |
| CN204173155U (en) | A kind of delta-wing aircraft | |
| CN105346715A (en) | Vertical take-off and landing unmanned plane | |
| CN202961882U (en) | Aeromodelling aircraft aerial photo triaxial tripod head with photographic device | |
| CN207580162U (en) | A kind of visible ray and thermal imaging quadrotor unmanned plane | |
| CN212797308U (en) | Five-axis hybrid power tilting vertical take-off and landing fixed wing | |
| CN204750561U (en) | Four rotor crafts of area propulsion and steering control duct | |
| CN209870739U (en) | Anti-vibration high-freedom bird-like flapping wing aircraft | |
| CN202666408U (en) | Six-arm model aerial propeller | |
| CN207346096U (en) | Vertical take-off and landing fixed wing aircraft with rear-mounted propeller | |
| CN206885351U (en) | A kind of takeoff and landing system | |
| CN104229130A (en) | Four-rotor wing unmanned aerial vehicle with pneumatic structure | |
| CN210618464U (en) | Fixed wing unmanned aerial vehicle's VTOL coupling assembling and fixed wing unmanned aerial vehicle | |
| CN203816222U (en) | Model airplane spiral frame | |
| CN204056295U (en) | Pneumatic structure four rotor unmanned aircraft | |
| CN209852575U (en) | A compound wing UAV | |
| CN209467320U (en) | A kind of all-wing aircraft unmanned plane that can be vertically moved up or down | |
| CN201535852U (en) | Aerial photography camera support | |
| CN204996125U (en) | A motor for model aeroplane and model ship aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: HUIZHOU DONGYANG PLASTIC MODEL CO., LTD. Free format text: FORMER OWNER: ZHANG JINHAI Effective date: 20150821 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20150821 Address after: 516000 Guangdong province Huizhou City Pingnan Zhongkai high tech area Huihuan Village No. 28 building four Patentee after: HUIZHOU DONGYANG PLASTIC MODEL CO., LTD. Address before: 516000 No. 11 Goose Road South, Huicheng District, Guangdong, Huizhou Patentee before: Zhang Jinhai |
|
| C56 | Change in the name or address of the patentee | ||
| CP03 | Change of name, title or address |
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 high tech area Huihuan Village No. 28 building four Patentee before: HUIZHOU DONGYANG PLASTIC MODEL CO., LTD. |
|
| 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: 20130605 Termination date: 20191210 |