CN203753417U - Unmanned aerial vehicle cradle head structure - Google Patents

Unmanned aerial vehicle cradle head structure Download PDF

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Publication number
CN203753417U
CN203753417U CN201320809102.9U CN201320809102U CN203753417U CN 203753417 U CN203753417 U CN 203753417U CN 201320809102 U CN201320809102 U CN 201320809102U CN 203753417 U CN203753417 U CN 203753417U
Authority
CN
China
Prior art keywords
camera
pedestal
aerial vehicle
unmanned aerial
hole clipping
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
CN201320809102.9U
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Chinese (zh)
Inventor
任路坦
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.)
Zhenghai Ningbo City Peace Endurance Unmanned Plane Technology Service Co Ltd
Original Assignee
Zhenghai Ningbo City Peace Endurance Unmanned Plane Technology Service 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 Zhenghai Ningbo City Peace Endurance Unmanned Plane Technology Service Co Ltd filed Critical Zhenghai Ningbo City Peace Endurance Unmanned Plane Technology Service Co Ltd
Priority to CN201320809102.9U priority Critical patent/CN203753417U/en
Application granted granted Critical
Publication of CN203753417U publication Critical patent/CN203753417U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to an unmanned aerial vehicle cradle head structure, which comprises a first mounting plate, a second mounting plate and a base, wherein the first mounting plate is rotationally connected with the side wall of the base; a steering engine which can be used for driving the base to rotate is arranged on the second mounting plate; a clamping hole for mounting a camera or video camera is formed in the base; an output shaft of the steering engine and the first mounting plate are connected to two opposite side walls of the base respectively. Compared with the prior art, the unmanned aerial vehicle cradle head structure is simple, reasonable, light in weight and low in power consumption.

Description

Unmanned aerial vehicle cradle head structure
Technical field
The utility model relates to a kind of stable The Cloud Terrace for taking photo by plane, and relates in particular to a kind of unmanned aerial vehicle cradle head structure.
Background technology
Unmanned aerial vehicle has that volume is little, lightweight, expense is low, flexible operation and safe feature, can be widely used in taking photo by plane, monitors, the field such as search and rescue, resource exploration.Because unmanned aerial vehicle itself exists high-frequency vibration and low-frequency jitter, The Cloud Terrace be need to configure and pick up camera, photographic camera are used for carrying to realize steady shot, pick up camera or the photographic camera of the middle use of taking photo by plane are arranged on The Cloud Terrace, and The Cloud Terrace is suspended on the belly of aircraft.Aerial camera or photographic camera are subject to the control of ground control system, take the image that will choose, in order to make captured image more clear, accurate, just require aerial camera or photographic camera will remain a good shooting angle.But unmanned aerial vehicle, in flight course, can inevitably occur jolting, the phenomenon such as inclination, like this, will impact the shooting effect of aerial camera or photographic camera.Existing holder for aerial photographing can only carry out the adjustment of a direction mostly, and can not realize multi-angle adjustment.
In order to obtain steadily suitable shooting angle, the patent No. is that the Chinese utility model " holder for aerial photographing on small-sized pilotless aircraft " (Granted publication number is CN201380965Y) of ZL200920107579.6 discloses the holder for aerial photographing on a kind of small-sized pilotless aircraft, comprise sheathed successively outer fixed frame, middle swing frame and interior swing frame, middle swing frame by a pair of shaft swing be connected on outer fixed frame, described interior swing frame is swingingly connected on described middle swing frame by another countershaft, two pairs of described rotating shafts are 90 ° of settings, and two countershafts are connected with a piston crank mechanism respectively, described in two, piston crank mechanism is driven by a motor respectively, two motors are separately fixed on outer fixed frame.The camera of this utility model holder for aerial photographing is arranged on interior swing frame, thereby can do the swing of both direction simultaneously, to reach steadily suitable shooting angle.But the camera in this utility model swings too flexible, wayward its shooting angle in the process of taking photo by plane, and the cradle head structure of this utility model need to configure two cover drive motor, its complex structure, weight is large, has increased the integrally-built cost of The Cloud Terrace and weight.
Separately having application number is that the Chinese invention patent application " three-degree-of-freedom aerial photographic head with stable inertia " (application notification number is CN101734377A) of 200910258080.X discloses a kind of three-degree-of-freedom aerial photographic head with stable inertia, it comprises stabilizing device, three parts of driving device and camera head, on The Cloud Terrace support, connect horizontal rotating frame, on horizontal rotating frame, connect mechanical gyro and form stabilizing device, stabilizing device is connected with camera head by driving device, can realize being synchronized with the movement of gyro and camera vertical direction, rely on the stability of gyro to realize the steady shot of camera.Holder for aerial photographing disclosed by the invention can be eliminated because aircraft high and low frequency shakes the impact that Aerial Images is caused, and the problem that tilts of the picture that tilts to cause due to body itself, can shoot very clear, stable image.But holder for aerial photographing structure of the present invention is too complicated, and cost is higher.
Utility model content
Technical problem to be solved in the utility model is that a kind of unmanned aerial vehicle cradle head structure simple in structure is separately provided.
Another technical matters to be solved in the utility model is to provide a kind of unmanned aerial vehicle cradle head structure that can steadily take a picture or make a video recording.
The utility model solves the problems of the technologies described above adopted technical scheme: comprise the first adapter plate, the second adapter plate and pedestal, described the first adapter plate and pedestal sidewall are rotationally connected, the steering wheel that can drive pedestal to rotate is installed on described the second adapter plate, on described pedestal, offer the hole clipping that photographic camera or pick up camera are installed, the output shaft of described steering wheel and the first adapter plate are connected on two opposed sidewalls of pedestal.
For photographic camera or pick up camera being more firmly placed in the hole clipping on pedestal, described pedestal comprises the first base station and second base station of arranging up and down, and described the first base station and the second base station be corresponding the first hole clipping that limits photographic camera or pick up camera fuselage position and the second hole clipping that limits photographic camera or camera lens position of offering respectively.In the time that photographic camera or pick up camera are installed, fuselage is stuck in the first hole clipping, and camera lens is stuck in the second hole clipping.
In order to strengthen the fixation of this The Cloud Terrace to photographic camera or pick up camera, the diameter of described the second hole clipping is than the large 0.05mm of the diameter of the first hole clipping.When photographic camera or pick up camera are installed, fuselage is stuck in the first hole clipping, and camera lens is just in time stuck in the second hole clipping.
In order further to fix the position of photographic camera or pick up camera fuselage, described pedestal periphery is upwards extended with baffle plate, and this baffle plate is arranged around the first hole clipping.The fuselage of photographic camera or pick up camera is placed in the space between baffle plate and can not rotates.In order effectively to prevent that fuselage from rotating, the number of baffle plate is preferably three, and these three baffle plates are all rectangular plate, between baffle plate, form the accommodation space of a rectangle, after the fuselage of photographic camera or pick up camera is stuck in the first hole clipping, baffle plate has further stoped the rotation of fuselage, has guaranteed the stationarity of its photograph or shooting.
For the ease of photographic camera or pick up camera are disassembled from The Cloud Terrace, the inwall of described the first hole clipping forms the first dismounting groove, corresponding, the inwall of described the second hole clipping forms the second dismounting groove.The first dismounting groove and the second dismounting groove can be realized respectively the dismounting to photographic camera or pick up camera fuselage and camera lens, and do not affect the limit effect of these two hole clippings to fuselage or camera lens.Specifically, in the time of dismounting, the first dismounting groove and the second dismounting groove can stretch in hole clipping for finger.
Described baffle plate, the first adapter plate and the second adapter plate one of at least offer respectively through hole, are specifically preferably on baffle plate and the first adapter plate and offer through hole simultaneously.These through holes offer the weight that not only can alleviate whole unmanned aerial vehicle cradle head structure, can save again material, thereby save cost.
One as steering wheel and pedestal connection mode is preferred, described steering wheel is fastenedly connected by a steering wheel and pedestal, described steering wheel two ends are fastenedly connected with pedestal sidewall respectively, described steering wheel middle part is provided with an installation portion, and the output shaft of described steering wheel inserts the Kong Houyu pedestal being opened on this installation portion and is fastenedly connected.This The Cloud Terrace is in the time of work, and steering wheel can drive pedestal to rotate relative to the first adapter plate, thereby regulates the shooting angle of photographic camera or pick up camera.
Compared with prior art, the utility model has the advantage of: this unmanned aerial vehicle cradle head structure has been divided into this three part of the first adapter plate, pedestal and the second adapter plate, wherein the first adapter plate is fixed on the fuselage of unmanned aerial vehicle and is rotationally connected with pedestal, the second adapter plate is for steering wheel is installed, and pedestal is in order to settle photographic camera or pick up camera.Pedestal in this unmanned aerial vehicle cradle head structure is divided into two base stations of arranging up and down, and the diameter of the hole clipping on each base station matches with the fuselage of photographic camera or pick up camera and the external diameter of camera lens, more guarantee the firm effect of pedestal to photographic camera or pick up camera, make in unmanned aerial vehicle operational process, photographic camera or pick up camera are taken pictures more reposefully or are made a video recording.In addition, this unmanned aerial vehicle cradle head structure is simple, low in energy consumption and safe and reliable.
Brief description of the drawings
Fig. 1 is the utility model example structure schematic diagram;
Fig. 2 is the structural representation of the utility model embodiment pedestal.
Detailed description of the invention
Below in conjunction with accompanying drawing, embodiment is described in further detail the utility model.
The unmanned aerial vehicle cradle head structure of the present embodiment as depicted in figs. 1 and 2, comprise the first adapter plate 2, the second adapter plate 3 and pedestal 1, on pedestal 1, offer the hole clipping that photographic camera or pick up camera are installed, the steering wheel 4 that can drive pedestal 1 to rotate is installed on the second adapter plate 3, steering wheel 4 can directly be fixed on the second adapter plate 3, in the present embodiment, on the second adapter plate 3, offer mounting hole, steering wheel 4 is through after mounting hole, the connecting portion of steering wheel 4 both sides is fixedly connected with the second adapter plate 3 with screw, and the output shaft of steering wheel 4 is fixedly connected with the sidewall of pedestal 1, simultaneously, the first adapter plate 2 is connected on the sidewall with the opposed pedestal 1 of steering wheel 4, the bottom of the first adapter plate 2 is rotationally connected by a rotating shaft and pedestal 1.
After steering wheel 4 is arranged on the second adapter plate 3, the output shaft of steering wheel 4 can directly be fixed on the sidewall of pedestal 1, and in this enforcement, steering wheel 4 is fastenedly connected by a steering wheel 9 and the sidewall of pedestal 1, and steering wheel 9 two ends are connected with screw fastening with pedestal 1 sidewall respectively; Steering wheel 9 middle parts are provided with an installation portion 91, on installation portion 91, offer through hole, and the output shaft of steering wheel 4 inserts after this through hole, then are fastenedly connected with the sidewall of screw and pedestal 1.
First adapter plate 2 of the present embodiment is fixedly connected with the fuselage of unmanned aerial vehicle respectively with the second adapter plate 3, concrete available screw is fixedly connected with, sticky etc., in this enforcement, the first adapter plate 2 and the second adapter plate 3 fasten with glue respectively on the fuselage of unmanned aerial vehicle.
For photographic camera or pick up camera being more firmly placed in the hole clipping on pedestal 1, pedestal 1 comprise first base station 7 of arranging up and down and the second base station 8, the first base stations 7 and the second base station 8 respectively correspondence offer the first hole clipping 71 and the second hole clipping 81.In the time that photographic camera or pick up camera are installed, the fuselage of photographic camera or pick up camera is stuck in the first hole clipping 71, and camera lens is stuck in the second hole clipping 81.In order to strengthen the fixation of this unmanned aerial vehicle The Cloud Terrace to photographic camera or pick up camera fuselage, the diameter of the first hole clipping 71 is according to the large 0.05mm of external diameter of camera or pick up camera fuselage, and the diameter of the second hole clipping 81 is than the large 0.05mm of the diameter of the first hole clipping 71 simultaneously.In the time that photographic camera or pick up camera are installed, camera lens is just in time stuck in the second hole clipping 81, and the fuselage of photographic camera or pick up camera is just in time stuck in the first hole clipping 71.
In order further to fix the position of photographic camera or pick up camera fuselage, pedestal 1 periphery is upwards extended with baffle plate 6, and baffle plate 6 arranges around the first hole clipping 71, and the fuselage of photographic camera or pick up camera is placed in the space of 6, baffle plate and can not rotates.In order effectively to prevent that fuselage from rotating, the number of baffle plate 6 is preferably three, and these three baffle plates 6 are all rectangular plate, between adjacent baffle plate 6, be the angle of 90 °, between baffle plate 6, form the accommodation space of a rectangle, the fuselage of photographic camera or pick up camera is stuck in after the first hole clipping interior 71, and baffle plate 6 has further stoped the rotation of the fuselage of photographic camera or pick up camera, thereby has guaranteed the stationarity of taking a picture or making a video recording.
For the ease of photographic camera or pick up camera are disassembled from The Cloud Terrace, the inwall of the first hole clipping 71 forms the first dismounting groove 72, corresponding, the inwall of the second hole clipping 81 forms the second dismounting groove 82.Thereby the fuselage that the first dismounting groove 72 and the second dismounting groove 82 can supply finger to insert to be realized respectively photographic camera or pick up camera and the dismounting of camera lens, and do not affect this fuselage of two hole clippings to photographic camera or pick up camera or limit effect of camera lens.
In the time of concrete use, the first adapter plate 2 and the second adapter plate 3 are bonded on unmanned aerial vehicle fuselage, thereby The Cloud Terrace is fixed on unmanned aerial vehicle fuselage, as can be seen here, for The Cloud Terrace is more firmly fixed on unmanned aerial vehicle fuselage, need to alleviate the weight of The Cloud Terrace itself, in baffle plate 6, the first adapter plate 2 and the second adapter plate 3, one of at least offer through hole 5, in the present embodiment, on the first adapter plate 2 and baffle plate 6, offer through hole 5 simultaneously.Offering of through hole 5 not only can alleviate the weight of The Cloud Terrace entirety but also can save material.

Claims (7)

1. a unmanned aerial vehicle cradle head structure, it is characterized in that: comprise the first adapter plate (2), the second adapter plate (3) and pedestal (1), described the first adapter plate (2) is rotationally connected with pedestal (1) sidewall, the steering wheel (4) that can drive pedestal (1) to rotate is installed on described the second adapter plate (3), on described pedestal (1), offer the hole clipping that photographic camera or pick up camera are installed, the output shaft of described steering wheel (4) and the first adapter plate (2) are connected on two opposed sidewalls of pedestal (1).
2. unmanned aerial vehicle cradle head structure according to claim 1, it is characterized in that: described pedestal (1) comprises the first base station (7) and second base station (8) of arranging up and down, described the first base station (7) and the second base station (8) be corresponding the first hole clipping (71) that limits photographic camera or pick up camera fuselage position and the second hole clipping (81) that limits photographic camera or camera lens position of offering respectively.
3. unmanned aerial vehicle cradle head structure according to claim 2, is characterized in that: the diameter of described the second hole clipping (81) is than the large 0.05mm of diameter of the first hole clipping (71).
4. unmanned aerial vehicle cradle head structure according to claim 2, is characterized in that: described pedestal (1) periphery is upwards extended with baffle plate (6), and this baffle plate (6) is arranged around the first hole clipping (71).
5. unmanned aerial vehicle cradle head structure according to claim 4, it is characterized in that: the inwall of described the first hole clipping (71) forms the first dismounting groove (72), corresponding, the inwall of described the second hole clipping (81) forms the second dismounting groove (82).
6. unmanned aerial vehicle cradle head structure according to claim 5, is characterized in that: described baffle plate (6), the first adapter plate (2) and the second adapter plate (3) one of at least offer through hole (5).
7. according to the unmanned aerial vehicle cradle head structure described in any one in claim 1 to 6, it is characterized in that: described steering wheel (4) is fastenedly connected by a steering wheel (9) and pedestal (1), described steering wheel (9) two ends are fastenedly connected with pedestal (1) sidewall respectively, described steering wheel (9) middle part is provided with an installation portion (91), and the output shaft of described steering wheel (4) inserts the Kong Houyu pedestal (1) being opened on this installation portion (91) and is fastenedly connected.
CN201320809102.9U 2013-12-10 2013-12-10 Unmanned aerial vehicle cradle head structure Expired - Fee Related CN203753417U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320809102.9U CN203753417U (en) 2013-12-10 2013-12-10 Unmanned aerial vehicle cradle head structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320809102.9U CN203753417U (en) 2013-12-10 2013-12-10 Unmanned aerial vehicle cradle head structure

Publications (1)

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CN203753417U true CN203753417U (en) 2014-08-06

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104977693A (en) * 2015-07-12 2015-10-14 安徽捷迅光电技术有限公司 Adjustable imaging mechanism based on transmission platform
CN105202330A (en) * 2015-07-12 2015-12-30 安徽捷迅光电技术有限公司 Modularized comprehensive visual platform
CN105573022A (en) * 2016-01-29 2016-05-11 北京臻迪机器人有限公司 Platform camera for aircraft and aircraft using same
CN108622430A (en) * 2017-05-03 2018-10-09 李秀荣 A kind of unmanned plane

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104977693A (en) * 2015-07-12 2015-10-14 安徽捷迅光电技术有限公司 Adjustable imaging mechanism based on transmission platform
CN105202330A (en) * 2015-07-12 2015-12-30 安徽捷迅光电技术有限公司 Modularized comprehensive visual platform
CN105573022A (en) * 2016-01-29 2016-05-11 北京臻迪机器人有限公司 Platform camera for aircraft and aircraft using same
CN105573022B (en) * 2016-01-29 2018-08-31 北京臻迪机器人有限公司 A kind of holder camera of aircraft and use its aircraft
CN108622430A (en) * 2017-05-03 2018-10-09 李秀荣 A kind of unmanned plane
CN108622430B (en) * 2017-05-03 2020-08-28 黑龙江新综科技有限公司 Unmanned aerial vehicle

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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: 20140806

Termination date: 20161210

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