CN206579854U - The universal image mechanism of unmanned plane - Google Patents

The universal image mechanism of unmanned plane Download PDF

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Publication number
CN206579854U
CN206579854U CN201720213584.XU CN201720213584U CN206579854U CN 206579854 U CN206579854 U CN 206579854U CN 201720213584 U CN201720213584 U CN 201720213584U CN 206579854 U CN206579854 U CN 206579854U
Authority
CN
China
Prior art keywords
unmanned plane
camera head
mounting base
angular adjustment
image mechanism
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
CN201720213584.XU
Other languages
Chinese (zh)
Inventor
汪云
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.)
Chongqing Hongyuanyun Zhongying Aviation Technology Co ltd
Original Assignee
Chongqing Sino Eagle Aviation 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 Chongqing Sino Eagle Aviation Technology Co Ltd filed Critical Chongqing Sino Eagle Aviation Technology Co Ltd
Priority to CN201720213584.XU priority Critical patent/CN206579854U/en
Application granted granted Critical
Publication of CN206579854U publication Critical patent/CN206579854U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of universal image mechanism of unmanned plane, including the mounting bracket being fixedly mounted on unmanned aerial vehicle body, the bottom of the mounting bracket, which is provided with mounting base for camera head, the mounting base for camera head, is provided with a spherical hollow space, and the upper and lower ends of the spherical hollow space are open respectively;The mounting bracket is provided with annular on the angular adjustment frame being located above the mounting base for camera head, the angular adjustment frame and is laid with least four angle adjusting mechanisms;With its mating spherical surfaces provided with shooting headstock in the mounting base for camera head, the angular adjustment bar for being installed on the camera for being provided with and being located at below the mounting base for camera head, the shooting headstock and being provided with and being located above the mounting base for camera head is installed on the shooting headstock;The angle adjusting mechanism includes the drive rod being engaged with the angular adjustment bar and the drive device for driving the drive rod to be stretched along its axial direction.

Description

The universal image mechanism of unmanned plane
Technical field
The utility model is related to a kind of camera device, is specifically a kind of universal image mechanism of unmanned plane.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself Not manned aircraft.It can be divided into from technical standpoint definition:Unmanned fixed-wing aircraft, unmanned VTOL machine, unmanned airship, nobody Helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..
In civilian unmanned plane field, unmanned plane largely be used to image, take pictures.Although existing unmanned plane is in certain journey The requirement of high-altitude shooting is disclosure satisfy that on degree, but the control of its camera is dumb, it is impossible to the shooting of Some features angle is completed, It is using being restricted.
The content of the invention
In view of this, the purpose of this utility model is to provide a kind of unmanned plane universal image mechanism, can realize shooting Head adjusts angle within the specific limits, and angular adjustment disclosure satisfy that the demand of various angle shots without dead angle.
To reach above-mentioned purpose, the utility model provides following technical scheme:
A kind of universal image mechanism of unmanned plane, including the mounting bracket being fixedly mounted on unmanned aerial vehicle body, the mounting bracket Bottom be provided with mounting base for camera head, be provided with a spherical hollow space in the mounting base for camera head, up and down the two of the spherical hollow space End is open respectively;The mounting bracket is provided with the angular adjustment frame being located above the mounting base for camera head, the angular adjustment Annular is laid with least four angle adjusting mechanisms on frame;
The mounting base for camera head is interior and its mating spherical surfaces is provided with to install to be provided with shooting headstock, the shooting headstock and is located at Install to be provided with camera below the mounting base for camera head, the shooting headstock and be located above the mounting base for camera head Angular adjustment bar;
The angle adjusting mechanism includes the drive rod being engaged with the angular adjustment bar and for driving the drive The drive device that lever is stretched along its axial direction.
Further, the angular adjustment frame includes four fix bars of composition square, and the angle adjusting mechanism is set For four and it is separately mounted in four fix bars.
Further, the mounting bracket includes four mounting rods, and four mounting rods are located at four fix bar compositions respectively Square diagonal position at.
Further, the lower end of four mounting rods bends inwards and is fixedly connected with the mounting base for camera head.
Further, the opening is rounded, and the ratio between the sphere diameter of the internal diameter of the opening and the spherical hollow space is more than etc. In 0.85.
Further, the drive device uses linear electric motors.
Further, the front end of the drive rod is articulated and connected to be provided with it is used for what is be engaged with the angular adjustment bar Seat is contacted, the contact seat is provided with the arc coordinated with the angular adjustment bar and contacts liner plate.
Further, the arc contact liner plate uses slip lining.
Further, the front end face of the drive rod is provided with link slot, and the link slot is stretched into the rear end of the contact seat It is interior, and be connected between the link slot and contact seat provided with rotating dog.
Further, the rotating dog is provided with the angular transducer for being used for detecting the contact seat anglec of rotation.
The beneficial effects of the utility model are:
The universal image mechanism of unmanned plane of the present utility model, by will shooting headstock be arranged on spherical hollow space in and with it is spherical Cavity mating spherical surfaces, and mounting base for camera head can be easily driven in spherical hollow space using the uniform angle adjusting mechanism of annular Interior rotation, and then the shooting angle of camera is adjusted, and in angular adjustment region, because mating spherical surfaces are rotated without dead angle, because And the shooting angle of camera is adjusted also without dead angle, it can meet and shoot at any angle.
Brief description of the drawings
In order that the purpose of this utility model, technical scheme and beneficial effect are clearer, the utility model provides as follows Accompanying drawing is illustrated:
Fig. 1 is the structural representation of the universal image mechanism embodiment of the utility model unmanned plane;
Fig. 2 is Fig. 1 A detail drawings;
Fig. 3 is the structural representation of the unmanned plane using the universal image mechanism of the present embodiment.
Embodiment
The utility model is described in further detail with specific embodiment below in conjunction with the accompanying drawings, so that those skilled in the art The utility model can be better understood from and can be practiced, but illustrated embodiment is limited not as to of the present utility model.
As shown in figure 1, being the structural representation of the universal image mechanism embodiment of the utility model unmanned plane.The present embodiment The universal image mechanism of unmanned plane, including the mounting bracket 2 being fixedly mounted on unmanned aerial vehicle body 1, the bottom of the mounting bracket 2 is provided with A spherical hollow space is provided with mounting base for camera head 3, the mounting base for camera head 3, the upper and lower ends of the spherical hollow space are opened respectively Mouthful.The mounting bracket is provided with ring on the angular adjustment frame 4 for being located at the top of mounting base for camera head 3, the angular adjustment frame 4 Shape is laid with least four angle adjusting mechanisms.It is provided with the mounting base for camera head 3 of the present embodiment with its mating spherical surfaces Image and the camera 6 for being provided with and being located at the lower section of mounting base for camera head 3, the shooting are installed on headstock 5, the shooting headstock 5 The angular adjustment bar 7 for being provided with and being located at the top of mounting base for camera head 3 is installed on headstock 5.The angular adjustment of the present embodiment Mechanism includes the drive rod 8 being engaged with the angular adjustment bar 7 and for driving the drive rod 8 to be stretched along its axial direction The drive device 9 of contracting.
Specifically, the angular adjustment frame 4 of the present embodiment includes four fix bar 4a of composition square, the angle Governor motion is set to four and is separately mounted on four fix bar 4a.The mounting bracket 2 of the present embodiment includes four Root mounting rod 2a, four mounting rod 2a are located at the square diagonal position of four fix bar 4a compositions respectively.This reality The lower end for applying four mounting rod 2a of example bends inwards and is fixedly connected with the mounting base for camera head 3.
The ratio between further, the opening of the present embodiment is rounded, and the sphere diameter of the internal diameter of the opening and the spherical hollow space More than or equal to 0.85, the cone angle of the circular cone constituted between the opening edge of the present embodiment and the centre of sphere of spherical hollow space is equal to 120 °, to ensure that camera 6 has enough angle of regulation range.
Further, the drive device 9 uses linear electric motors, and the front end of the drive rod 8 is articulated and connected provided with use with it In the contact seat 10 being engaged with the angular adjustment bar 7, the contact seat 10 is provided with to be coordinated with the angular adjustment bar 7 Arc contact liner plate 11.The arc contact liner plate 11 of the present embodiment uses slip lining, to reduce force of sliding friction.This The front end face of the drive rod 8 of embodiment is provided with link slot 12, and the link slot 12 is stretched into the rear end of the contact seat 10 It is interior, and the link slot 12 is connected with described contact between seat 10 provided with rotating dog 13, and the rotating dog 13 is provided with being used for The angular transducer 14 of the detection contact seat anglec of rotation, by setting angular transducer 14, seat 10 is contacted by detecting The anglec of rotation, you can judge the position of angular adjustment bar 7 in this direction, i.e., by detecting in orthogonal both direction The position of angular adjustment bar 7, you can the effectively position of control angle adjusting rod 7, and then control the angle position of camera 6.
The universal image mechanism of unmanned plane of the present embodiment, by will shooting headstock be arranged on spherical hollow space in and with spherical sky Chamber mating spherical surfaces, and mounting base for camera head can be easily driven in spherical hollow space using the uniform angle adjusting mechanism of annular Rotation, and then adjust the shooting angle of camera, and in angular adjustment region, because mating spherical surfaces rotation is without dead angle, thus The shooting angle of camera is adjusted also without dead angle, can be met and be shot at any angle.
Embodiment described above is only the preferred embodiment to absolutely prove the utility model and being lifted, the utility model Protection domain not limited to this.Equivalent substitute or change that those skilled in the art are made on the basis of the utility model Change, within protection domain of the present utility model.Protection domain of the present utility model is defined by claims.

Claims (10)

1. a kind of universal image mechanism of unmanned plane, it is characterised in that:Including the mounting bracket being fixedly mounted on unmanned aerial vehicle body, institute The bottom for stating mounting bracket is provided with mounting base for camera head, the mounting base for camera head provided with a spherical hollow space, the spherical hollow space Upper and lower ends be open respectively;The mounting bracket is provided with the angular adjustment frame being located above the mounting base for camera head, described Annular is laid with least four angle adjusting mechanisms on angular adjustment frame;
It is provided with the mounting base for camera head with its mating spherical surfaces provided with installation on headstock, the shooting headstock is imaged positioned at described The angle for being provided with and being located above the mounting base for camera head is installed on the camera below mounting base for camera head, the shooting headstock Adjusting rod;
The angle adjusting mechanism includes the drive rod being engaged with the angular adjustment bar and for driving the drive rod The drive device stretched along its axial direction.
2. the universal image mechanism of unmanned plane according to claim 1, it is characterised in that:The angular adjustment frame includes composition Four fix bars of square, the angle adjusting mechanism is set to four and is separately mounted in four fix bars.
3. the universal image mechanism of unmanned plane according to claim 2, it is characterised in that:The mounting bracket includes four installations Bar, four mounting rods are located at the square diagonal position of four fix bar compositions respectively.
4. the universal image mechanism of unmanned plane according to claim 3, it is characterised in that:The lower end of four mounting rods to Inner bending is simultaneously fixedly connected with the mounting base for camera head.
5. the universal image mechanism of unmanned plane according to claim 1, it is characterised in that:The opening is rounded and described The ratio between sphere diameter of the internal diameter of opening and the spherical hollow space is more than or equal to 0.85.
6. the universal image mechanism of unmanned plane according to claim 1, it is characterised in that:The drive device uses straight-line electric Machine.
7. the universal image mechanism of unmanned plane according to claim 6, it is characterised in that:Cut with scissors with it the front end of the drive rod The contact seat for being engaged with the angular adjustment bar is equipped with succession, and the contact seat is provided with and the angular adjustment The arc contact liner plate that bar coordinates.
8. the universal image mechanism of unmanned plane according to claim 7, it is characterised in that:The arc contact liner plate is using cunning Dynamic liner plate.
9. the universal image mechanism of unmanned plane according to claim 7, it is characterised in that:Set on the front end face of the drive rod There is link slot, the rear end of the contact seat is stretched into the link slot, and provided with rotation between the link slot and contact seat Ship and resell on another market connected.
10. the universal image mechanism of unmanned plane according to claim 9, it is characterised in that:The rotating dog, which is provided with, to be used for The angular transducer of the detection contact seat anglec of rotation.
CN201720213584.XU 2017-03-07 2017-03-07 The universal image mechanism of unmanned plane Expired - Fee Related CN206579854U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720213584.XU CN206579854U (en) 2017-03-07 2017-03-07 The universal image mechanism of unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720213584.XU CN206579854U (en) 2017-03-07 2017-03-07 The universal image mechanism of unmanned plane

Publications (1)

Publication Number Publication Date
CN206579854U true CN206579854U (en) 2017-10-24

Family

ID=60112895

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720213584.XU Expired - Fee Related CN206579854U (en) 2017-03-07 2017-03-07 The universal image mechanism of unmanned plane

Country Status (1)

Country Link
CN (1) CN206579854U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109899649A (en) * 2019-03-18 2019-06-18 成都泰盟软件有限公司 A kind of electric platform for teaching demonstration

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109899649A (en) * 2019-03-18 2019-06-18 成都泰盟软件有限公司 A kind of electric platform for teaching demonstration
CN109899649B (en) * 2019-03-18 2024-03-01 成都泰盟软件有限公司 Electric cradle head for teaching demonstration

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Date Code Title Description
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20210902

Address after: 408499 No. 4, Lixin Road, Dongcheng sub district office, Nanchuan District, Chongqing

Patentee after: Chongqing hongyuanyun Zhongying Aviation Technology Co.,Ltd.

Address before: No. 404-6, building 38, cloud computing Industrial Park, Banan District, Chongqing 400000

Patentee before: CHONGQING YUNZHONGYING AVIATION TECHNOLOGY Co.,Ltd.

TR01 Transfer of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20171024

CF01 Termination of patent right due to non-payment of annual fee