CN208750323U - A kind of unmanned plane electric platform mechanism - Google Patents
A kind of unmanned plane electric platform mechanism Download PDFInfo
- Publication number
- CN208750323U CN208750323U CN201821435468.3U CN201821435468U CN208750323U CN 208750323 U CN208750323 U CN 208750323U CN 201821435468 U CN201821435468 U CN 201821435468U CN 208750323 U CN208750323 U CN 208750323U
- Authority
- CN
- China
- Prior art keywords
- fixed frame
- camera
- camera fixed
- unmanned plane
- sustaining portion
- 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
Landscapes
- Accessories Of Cameras (AREA)
Abstract
The utility model discloses a kind of unmanned plane electric platform mechanisms, including support base, rolling control motor, pitching control motor, camera, camera fixing device, camera tripod, sensor, control circuit board and route；Support base is reinforced, and control circuit board is installed at rear portion, is docked by mounting hole with the installation of unmanned machine frame；Rolling controls motor and is mounted among support base in pit by screw, then docks camera tripod；Camera tripod divides three parts: carriage mounting, left sustaining portion and right sustaining portion, and left sustaining portion installs pitching control motor, and right sustaining portion then installs bearing and rotates smoothness for camera；This holder not only convenient disassembly, but also there is stronger axial anti-overload ability.
Description
Technical field
The utility model belongs to vehicle technology field, and in particular to a kind of unmanned plane electric platform mechanism.
Background technique
Unmanned plane is all widely used in every field at present, wherein the unmanned planes such as take photo by plane, investigate need to carry
Video camera is observed and is imaged to the target detected, due to unmanned plane in flight course the vibration of itself, in atmosphere not
The effect of steady air flow and UAV Attitude, will lead to video camera and is under a more unstable environment and work, and return
Picture tremble unclear, need to use clouds terrace system at this time, for installing, fixing the support device of picture pick-up device, automatic leveling
Holder makes video camera be in a metastable working environment, to be accurately realized the observation and camera shooting to target.
But the prior art has the following problems: existing holder disassembly is inconvenient, and anti-overload ability is excessively weak, Wu Fashi
The mode of taking off such as penetrate with ejection, cylinder.
Utility model content
The technical problem to be solved by the present invention is to provide a kind of unmanned plane electric platform mechanism, this is novel to be can solve
Above-mentioned technical problem, the technical solution of the utility model are as follows:
A kind of unmanned plane electric platform mechanism, including mounting seat, rolling control motor, carriage mounting, Left-side support
Portion, camera fixed frame bearing, camera fixed frame, camera fixed frame gland, pitching control motor, right sustaining portion, circuit board and
IMU sensor；
The mounting seat leading flank is equipped with motor slot, and rolling control motor one end is fixed in motor slot, another
End is fixed with carriage mounting；The left sustaining portion and right sustaining portion are both secured to carriage mounting surface and are located at described
The opposite two sides of carriage mounting；The left sustaining portion front is equipped with mounting hole, and the camera fixed frame bearing is fixed on peace
It fills on hole；Camera fixed frame left side is equipped with projecting shaft, and the projecting shaft is fixed on camera fixed frame bearing, the camera
Fixed frame right side is equipped with installation base, and described pitching control motor one end is fixed with right sustaining portion, and the other end and installation are convex
Platform connects；The pitch axis of the pitching control motor passes through installation base and is fixed on installation base；The camera fixed frame
It is bolted between gland upper and lower side and camera fixed frame；The circuit board is fixed on mounting seat trailing flank, institute
It states IMU sensor and is affixed on camera fixed frame upper surface, connected between the IMU sensor and circuit board by wire circuit.
As the further improvement of this programme, camera fixed frame trailing flank is in Openworks shape.
As the further improvement of this programme, the thickness of the rolling control motor is greater than the depth of motor slot.
As the further improvement of this programme, the right sustaining portion is equipped with wire casing and string holes.
As the further improvement of this programme, through-hole is equipped in the middle part of the mounting seat.
As the further improvement of this programme, the mounting seat is equipped with acrylic translucent cover.
By adopting the above technical scheme, since a kind of unmanned plane electric platform mechanism provided by the utility model passes through setting branch
Support collet, right sustaining portion and left sustaining portion make it form holder camera support, and structure is simple, and convenient disassembly is used in
The unmanned plane that ejection, floodlight tube mode are taken off, may be arranged at unmanned head, directly docks with fuselage frame, have stronger axial direction anti-
Overload capacity.
Detailed description of the invention
Fig. 1 is unmanned plane electric platform mechanism isometric front view in the present embodiment；
Fig. 2 is unmanned plane electric platform mechanism reverse side perspective view in the present embodiment；
Fig. 3 is unmanned plane electric platform mechanism perspective view of the explosion in the present embodiment.
In figure, 1- mounting seat, 2- rolling controls motor, 3- carriage mounting, 4- left sustaining portion, 5- camera fixed frame
Bearing, 6- camera fixed frame, 7- camera, 8- camera fixed frame gland, 9- pitching control motor, 10- right sustaining portion, 11- control
Circuit board processed, 61- installation base.
Specific embodiment
Specific embodiment of the present utility model is described further with reference to the accompanying drawing.It should be noted that
The explanation of these embodiments is used to help to understand the utility model, but does not constitute the restriction to the utility model.This
Outside, technical characteristic involved in the various embodiments of the present invention described below is as long as they do not conflict with each other
It can be combined with each other.
As shown in Figure 1 to Figure 3, a kind of unmanned plane electric platform mechanism, including mounting seat 1, rolling control motor 2, branch
Support collet 3, left sustaining portion 4, camera fixed frame bearing 5, camera fixed frame 6, camera fixed frame gland 8, pitch control electricity
Machine 9, right sustaining portion 10, circuit board 11 and IMU sensor；
1 leading flank of mounting seat is equipped with motor slot, and the rolling control 2 one end of motor is fixed in motor slot, separately
One end and carriage mounting 3 are fixed；The left sustaining portion 4 is both secured to 3 surface of carriage mounting simultaneously with right sustaining portion 10
The two sides opposite positioned at support frame as described above collet 3；4 front of left sustaining portion is equipped with mounting hole, the camera fixed frame axis
5 are held to be fixed on mounting hole；6 left side of camera fixed frame is equipped with projecting shaft, and the projecting shaft is fixed on camera fixed frame
Bearing 5,6 right side of camera fixed frame are equipped with installation base 61, described 9 one end of pitching control motor and right sustaining portion 10
Fixed, the other end connects with installation base；The pitch axis of the pitching control motor 9 passes through installation base 61 and is fixed on installation
On boss 61；It is bolted between 8 upper and lower side of camera fixed frame gland and camera fixed frame 6；The circuit board
11 are fixed on 1 trailing flank of mounting seat, and the IMU sensor is affixed on 6 upper surface of camera fixed frame, the IMU sensor with
It is connected between circuit board 11 by wire circuit.
1 shape of mounting seat is determined by unmanned plane shape, selects cup dolly, diameter 130mm, base electrical machinery groove depth herein
19.5mm, diameter 24mm, for installing rolling control motor 2, to keep holder roll attitude to adjust；Lead among mounting seat 1
Hole is used for cabling.
Rolling controls motor 2, considers holder circuit question, selects 4108 mesoporous hollow shaft motor of JD-POWER；Rolling control
Motor 2 processed is fixed in mounting seat 1, and carriage mounting 3 is mounted on rolling control motor 2, controls motor 2 by rolling
Holder rolling movement is realized in adjustment.
The selection of pitching control motor 9 is with rolling control motor 2 with model motor；It is fixed on right sustaining portion 10, camera
Fixed frame 6 is mounted on pitching control motor 9, and the pitching movement of camera is realized by the adjustment of pitching control motor 9.
Carriage mounting 3, left sustaining portion 4 and right sustaining portion 10 form holder camera support, easy to disassemble.
Hole is dug through at the intermediate position of carriage mounting 3, is used for holder cabling.
Left sustaining portion 4 is mounted on 3 right side of carriage mounting by corresponding mounting hole, installs camera fixed frame axis thereon
5 are held, camera fixed frame bearing 5 and 6 right side shaft diameter 8mm of camera fixed frame cooperate, and are used to support camera fixed frame pitch rotation.
Right sustaining portion 10 is mounted on 3 left side of carriage mounting by corresponding mounting hole, installs pitching control motor thereon
9；Corresponding wire casing is dug on right sustaining portion 10 and hole is used for cabling, and does loss of weight processing, guarantees that holder position of centre of gravity is in rolling
Shaft position.
Camera 7 is mounted between camera fixed frame gland 8 and camera fixed frame 7, and camera 7 selects honey ant moving camera.
Camera fixed frame 6 is used for fixed camera 7, and shape is depending on camera shape, back hollow out loss of weight, and right side is stretched out
Axis cooperates with camera fixed frame bearing 5, and left side installation base connects with pitching control motor 9, makes camera fixed frame 6 can be with bowing
Control motor 9 is faced upward to move；The installation base in left side does wire casing processing, is used for sensor and phase machine circuit cabling.
Camera fixed frame gland 8 is docked to together by mounting hole and camera fixed frame 6 with bolt, compresses camera 7.
IMU sensor is parallel to pitch axis according to bottom edge, and side is parallel to wobble shaft and is affixed on 6 upper surface of camera fixed frame.
Control circuit board 11 selects BaseCam SimpleBGC 3.55, is fixed on base back surface, receives IMU sensing
The posture information of device controls motor 2 to rolling and pitching control motor 9 is adjusted, and realizes the posture balancing of holder camera, protects
Camera is held to work in a stable environment.
To guarantee unmanned plane protection holder, acrylic translucent cover can also be installed in holder mounting seat 1.
The embodiments of the present invention is explained in detail in conjunction with attached drawing above, but the utility model is not limited to be retouched
The embodiment stated.For a person skilled in the art, right in the case where not departing from the utility model principle and spirit
These embodiments carry out a variety of change, modification, replacement and modification, still fall in the protection scope of the utility model.
Claims (6)
1. a kind of unmanned plane electric platform mechanism, it is characterised in that: including mounting seat (1), rolling control motor (2), support
Frame collet (3), camera fixed frame bearing (5), camera fixed frame (6), camera fixed frame gland (8), is bowed at left sustaining portion (4)
Face upward control motor (9), right sustaining portion (10), circuit board (11) and IMU sensor；
Mounting seat (1) leading flank is equipped with motor slot, and rolling control motor (2) one end is fixed in motor slot, separately
One end and carriage mounting (3) are fixed；The left sustaining portion (4) and right sustaining portion (10) are both secured to carriage mounting
(3) surface and two sides opposite positioned at support frame as described above collet (3)；Left sustaining portion (4) front is equipped with mounting hole, described
Camera fixed frame bearing (5) is fixed on mounting hole；Camera fixed frame (6) left side is equipped with projecting shaft, the projecting shaft
It is fixed on camera fixed frame bearing (5), camera fixed frame (6) right side is equipped with installation base (61), the pitch control
Motor (9) one end and right sustaining portion (10) are fixed, and the other end connects with installation base；Pitching control motor (9) bow
Axis is faced upward across installation base (61) and is fixed on installation base (61)；Camera fixed frame gland (8) upper and lower side and camera
Fixed frame is bolted between (6)；The circuit board (11) is fixed on mounting seat (1) trailing flank, and the IMU is passed
Sensor is affixed on camera fixed frame (6) upper surface, is connect between the IMU sensor and circuit board (11) by wire circuit.
2. a kind of unmanned plane electric platform mechanism according to claim 1, it is characterised in that: the camera fixed frame (6)
Trailing flank is in Openworks shape.
3. a kind of unmanned plane electric platform mechanism according to claim 1, it is characterised in that: the rolling controls motor
(2) thickness is greater than the depth of motor slot.
4. a kind of unmanned plane electric platform mechanism according to claim 1, it is characterised in that: the right sustaining portion (10)
It is equipped with wire casing and string holes.
5. a kind of unmanned plane electric platform mechanism according to claim 1, it is characterised in that: in the mounting seat (1)
Portion is equipped with through-hole.
6. a kind of unmanned plane electric platform mechanism according to claim 5, it is characterised in that: on the mounting seat (1)
Equipped with acrylic translucent cover.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821435468.3U CN208750323U (en) | 2018-09-03 | 2018-09-03 | A kind of unmanned plane electric platform mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821435468.3U CN208750323U (en) | 2018-09-03 | 2018-09-03 | A kind of unmanned plane electric platform mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208750323U true CN208750323U (en) | 2019-04-16 |
Family
ID=66082991
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821435468.3U Expired - Fee Related CN208750323U (en) | 2018-09-03 | 2018-09-03 | A kind of unmanned plane electric platform mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208750323U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110896684A (en) * | 2018-05-31 | 2020-03-20 | 深圳市大疆创新科技有限公司 | Camera structure, cloud platform and unmanned aerial vehicle |
-
2018
- 2018-09-03 CN CN201821435468.3U patent/CN208750323U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110896684A (en) * | 2018-05-31 | 2020-03-20 | 深圳市大疆创新科技有限公司 | Camera structure, cloud platform and unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11140322B2 (en) | Stabilizing platform | |
| AU2011376582B2 (en) | Dual-axis platform for use in an unmanned aerial vehicle, Tri-axis platform for use in an unmanned aerial vehicle, and multi-rotor aerial vehicle | |
| US10805540B2 (en) | Quadcopter with pitched propeller configuration | |
| KR101617808B1 (en) | Installation for helicam gimbal having a function of controlling center of camera | |
| KR20170065235A (en) | Small camera gimbal | |
| CN208750323U (en) | A kind of unmanned plane electric platform mechanism | |
| CN107867395B (en) | Host structure assembly and remote control mobile device using same | |
| CN110823188A (en) | Full-automatic topographic map surveying and mapping device and surveying and mapping method | |
| CN206202711U (en) | A kind of head and unmanned plane | |
| CN110325438A (en) | Unmanned plane | |
| KR20200036195A (en) | Drone | |
| KR101549380B1 (en) | Apparatus for fixing the aerial camera | |
| CN108995820B (en) | Cloud platform, have shooting device and unmanned aerial vehicle of this cloud platform | |
| CN203753417U (en) | Unmanned aerial vehicle cradle head structure | |
| CN107690606B (en) | Cloud platform, shooting equipment and unmanned vehicles | |
| CN203780804U (en) | Shock-absorption shooting cradle head of aircraft | |
| CN206272712U (en) | Image module and unmanned plane | |
| CN214138993U (en) | Unmanned aerial vehicle's mounting bracket of making a video recording for survey and drawing | |
| CN210526875U (en) | Camera automatic balancing device arranged on unmanned aerial vehicle | |
| CN207496957U (en) | A kind of cradle head device and unmanned plane | |
| CN215514164U (en) | Hollow cup triaxial self-stabilizing holder and unmanned aerial vehicle | |
| CN104075084B (en) | Load-carrying body | |
| WO2021013672A1 (en) | System and method for lifting an object | |
| CN201535852U (en) | Aerial photography camera support | |
| CN212354412U (en) | Aerial sweeping camera device with deviation rectifying function |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190416 Termination date: 20190903 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |