CN204173163U - Camera pan-tilt - Google Patents

Camera pan-tilt Download PDF

Info

Publication number
CN204173163U
CN204173163U CN201420498836.4U CN201420498836U CN204173163U CN 204173163 U CN204173163 U CN 204173163U CN 201420498836 U CN201420498836 U CN 201420498836U CN 204173163 U CN204173163 U CN 204173163U
Authority
CN
China
Prior art keywords
main backstop
camera
tilt
steering wheel
camera pan
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
Application number
CN201420498836.4U
Other languages
Chinese (zh)
Inventor
李辉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
TIANJIN LEIHANG OPTOELECTRONICS TECHNOLOGY Co Ltd
Original Assignee
TIANJIN LEIHANG OPTOELECTRONICS TECHNOLOGY Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by TIANJIN LEIHANG OPTOELECTRONICS TECHNOLOGY Co Ltd filed Critical TIANJIN LEIHANG OPTOELECTRONICS TECHNOLOGY Co Ltd
Priority to CN201420498836.4U priority Critical patent/CN204173163U/en
Application granted granted Critical
Publication of CN204173163U publication Critical patent/CN204173163U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Stereoscopic And Panoramic Photography (AREA)

Abstract

Camera pan-tilt, belongs to unmanned plane camera technique field, for solving the fixing defect of existing unmanned plane pick up camera shooting angle.Camera pan-tilt of the present utility model comprises the triangle main backstop (1) be arranged on below unmanned aerial vehicle body, also comprise and be located at described main backstop (1) middle part and the center shaft (2) stretching out described main backstop (1) bottom surface, be located at the rotating mechanism (3) near described center shaft (2) lower outer, be arranged on the fixed mount (4) of described rotating mechanism (3) below, steering wheel (6) and support (9), the belt (7) be connected with described steering wheel (6), the rotating shaft (8) be connected with described belt (7).The utility model has the advantages that: pick up camera can carry out pitching operation to it again while can carrying out rotating in horizontal surface, can ensure shooting angle and image quality, lightweight, design science is reasonable, good damping effect.

Description

Camera pan-tilt
Technical field
The utility model relates to unmanned plane camera technique field, particularly relates to camera pan-tilt.
Background technology
In some field, needing the mode by taking photo by plane to take pictures to earth's surface, so just needing lower end pick up camera being arranged on aircraft, simultaneous camera also will carry out the rotation of multiple angle, improves the quality of taking pictures.
Utility model content
In order to overcome above-mentioned the deficiencies in the prior art, the purpose of this utility model is to provide camera pan-tilt.
The technical solution of the utility model is: camera pan-tilt, comprise the triangle main backstop be arranged on below unmanned aerial vehicle body, also comprise and to be located in the middle part of described main backstop and to stretch out the center shaft of described main backstop bottom surface, be located at the rotating mechanism near described center shaft lower outer, be arranged on the fixed mount below described rotating mechanism, steering wheel and support, the belt be connected with described steering wheel, the rotating shaft be connected with described belt; Described rotating shaft is connected with described support, the bottom of described fixed mount and pick up camera active link.
Three angular positions of described main backstop are separately installed with shock absorption device, and described main backstop is connected with described unmanned aerial vehicle body by described shock absorption device.
Described rotating mechanism is pivoting support.
Three limits on described main backstop are provided with the small sircle hole of equidistant arrangement.
The beneficial effects of the utility model are: when 1) rotating mechanism rotates in horizontal surface, pick up camera is driven to rotate at horizontal surface by fixed mount, be convenient to level angle shooting, steering wheel, by belt and rotating shaft, enables pick up camera carry out pitching motion, simultaneously, because steering wheel is arranged on below rotating mechanism, therefore, pick up camera can carry out pitching operation to it again while can carrying out rotating in horizontal surface, ensure that shooting angle; 2) main backstop is connected with unmanned aerial vehicle body by shock absorption device, reduces the impact that fuselage shaking brings pick up camera, ensure that the image quality of shooting; 3) small sircle hole that has main backstop arranged is conducive to alleviating the weight of main backstop, can also be convenient to signal wire (SW) simultaneously and be connected with the instrument installed in fuselage through small sircle hole.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model embodiment.
Fig. 2 is the structural representation of main backstop in the utility model embodiment.
1. main backstop, 11. shock absorption devices, 12. circular holes, 13. small sircle holes, 2. center shaft, 3. pivoting support, 4. fixed mount, 5. pick up camera, 6. steering wheel, 7. belt, 8. rotating shaft, 9. support.
Detailed description of the invention
Below in conjunction with accompanying drawing, detailed description of the invention of the present utility model is explained.
See Fig. 1, the camera pan-tilt of the utility model embodiment comprises main backstop 1, shock absorption device 11, center shaft 2, rotating mechanism 3, fixed mount 4, steering wheel 6, belt 7, rotating shaft 8, support 9.
Main backstop 1 is triangle, and three angles are provided with shock absorption device 11.Main backstop 1 is fixedly connected with unmanned aerial vehicle body by shock absorption device 11.The middle part of main backstop 1 is provided with circular hole 12, is equidistantly provided with small sircle hole 13 around circular hole 12 along three limits place.The small sircle hole 13 that has that main backstop 1 is arranged is conducive to alleviating the weight of main backstop 1, can also be convenient to signal wire (SW) simultaneously and be connected with the instrument installed in unmanned aerial vehicle body through small sircle hole 13.
Center shaft 2 one end is connected with circular hole 12, and the other end stretches out circular hole 12.
Pivoting support 3 is located at below center shaft 2, and pivoting support 3 can rotate.
Fixed mount 4 is arranged on below pivoting support 3, and meanwhile, fixed mount 4 and pick up camera 5 active link bottom it, ensure that pick up camera 5 can carry out pitching.
Steering wheel 6 and support 9 are installed in below pivoting support 3.Steering wheel 6 drives rotating shaft 8 to rotate by belt 7, thus drives pick up camera 5 luffing.
One end of rotating shaft 8 is connected with support 9 by bearing, ensure that rotating shaft 8 can rotate.
Above an embodiment of the present utility model has been described in detail, but described content being only preferred embodiment of the present utility model, can not being considered to for limiting practical range of the present utility model.All equalizations done according to the utility model application range change and improve, and all should still belong within patent covering scope of the present utility model.

Claims (4)

1. a camera pan-tilt, comprise the triangle main backstop (1) be arranged on below unmanned aerial vehicle body, it is characterized in that: also comprise and be located at described main backstop (1) middle part and the center shaft (2) stretching out described main backstop (1) bottom surface, be located at the rotating mechanism (3) near described center shaft (2) lower outer, be arranged on the fixed mount (4) of described rotating mechanism (3) below, steering wheel (6) and support (9), the belt (7) be connected with described steering wheel (6), the rotating shaft (8) be connected with described belt (7), described rotating shaft (8) is connected with described support (9), the bottom of described fixed mount (4) and pick up camera (5) active link.
2. camera pan-tilt according to claim 1, it is characterized in that: three angular positions of described main backstop (1) are separately installed with shock absorption device (11), and described main backstop (1) is connected with described unmanned aerial vehicle body by described shock absorption device (11).
3. camera pan-tilt according to claim 1, is characterized in that: described rotating mechanism (3) is pivoting support.
4. camera pan-tilt according to claim 1, is characterized in that: three limits on described main backstop (1) are provided with the small sircle hole (13) of equidistant arrangement.
CN201420498836.4U 2014-08-31 2014-08-31 Camera pan-tilt Expired - Fee Related CN204173163U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420498836.4U CN204173163U (en) 2014-08-31 2014-08-31 Camera pan-tilt

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420498836.4U CN204173163U (en) 2014-08-31 2014-08-31 Camera pan-tilt

Publications (1)

Publication Number Publication Date
CN204173163U true CN204173163U (en) 2015-02-25

Family

ID=52561992

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420498836.4U Expired - Fee Related CN204173163U (en) 2014-08-31 2014-08-31 Camera pan-tilt

Country Status (1)

Country Link
CN (1) CN204173163U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105611168A (en) * 2015-12-31 2016-05-25 南宁慧视科技有限责任公司 Multi-angle oblique aerial photographing method on rotation tripod head of unmanned aerial vehicle
CN106364687A (en) * 2016-09-26 2017-02-01 武汉天易航科技有限公司 High-precision ortho-image tripod head

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105611168A (en) * 2015-12-31 2016-05-25 南宁慧视科技有限责任公司 Multi-angle oblique aerial photographing method on rotation tripod head of unmanned aerial vehicle
CN105611168B (en) * 2015-12-31 2019-04-02 南宁慧视科技有限责任公司 A kind of method that the photography of unmanned plane rotary head multi-angle oblique is taken photo by plane
CN106364687A (en) * 2016-09-26 2017-02-01 武汉天易航科技有限公司 High-precision ortho-image tripod head

Similar Documents

Publication Publication Date Title
CN204056294U (en) A kind of collapsible four axle multi-rotor aerocrafts
CN201974620U (en) Triaxial aerial photography holder
CN204124373U (en) Unmanned plane twin shaft video cradle head structure
CN204776013U (en) Six unmanned aerial vehicle
CN101774431A (en) Spherical hanging type two freedom degree holder for unmanned device
CN205203411U (en) Carry on three -axis pan -tilt of camera
CN102849219B (en) Omni-directional damping single-freedom-degree photoelectric reconnaissance platform device
CN204527661U (en) Double end photoelectric nacelle
CN203996917U (en) A kind of unmanned vehicle
CN205916341U (en) Miniature cloud platform and have unmanned vehicles of this cloud platform
CN204173163U (en) Camera pan-tilt
CN203593169U (en) Aerial photography unmanned plane
CN206494136U (en) A kind of UAV flight's head
CN203996915U (en) Three axle Self-stabilization holders
CN206552283U (en) A kind of equipment of taking photo by plane applied to unmanned plane
CN207670655U (en) A kind of auto-folder three-axis stability augmentation camera shooting quadrotor drone
CN207670659U (en) A kind of upper and lower six rotor wing unmanned aerial vehicles of three-axis stability augmentation
CN203753417U (en) Unmanned aerial vehicle cradle head structure
CN107856825A (en) A kind of underwater robot and its method
CN207045763U (en) A kind of unmanned vehicle for carrying mobile phone
CN203819500U (en) Triaxialcradle head and aeromodeling aircraft system
CN103523241A (en) Brushless tripod head of unmanned aerial vehicle
CN203780804U (en) Shock-absorption shooting cradle head of aircraft
CN205293090U (en) Aircraft with rotatory horn multiaxis
CN207809770U (en) Smart city unmanned plane

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: 20150225

Termination date: 20150831

EXPY Termination of patent right or utility model