CN209351613U - A kind of concealed three axis holder of O-E Payload for UAV - Google Patents
A kind of concealed three axis holder of O-E Payload for UAV Download PDFInfo
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- CN209351613U CN209351613U CN201821788723.2U CN201821788723U CN209351613U CN 209351613 U CN209351613 U CN 209351613U CN 201821788723 U CN201821788723 U CN 201821788723U CN 209351613 U CN209351613 U CN 209351613U
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- driving motor
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- axis driving
- payload
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Abstract
The utility model discloses a kind of concealed three axis holders of O-E Payload for UAV, including head assembly and O-E Payload component, the O-E Payload component includes: package casing, camera, roll axis driving motor and end cap, the roll axis driving motor is connected to camera right end, and is fixed on motor supporting base;The head assembly includes: pitch axis driving motor, pitching axis connection horn, course axis driving motor and holder damping, the pitch axis driving motor is mounted on the rear side of camera, and pitching axis connection horn is connect with course axis driving motor and pitch axis driving motor respectively.The utility model changes structure design, has symmetry in structure, supports more stable;Camera roll axial rearward end is motor, and front end is the support of bearing, increases camera stability and structural reliability;Changing Eulerian angles sequence in gesture stability is camera-roll axis-pitch axis-course axis, reduces posture diverging.
Description
Technical field
The utility model relates to industrial intelligent equipment related fields, specifically a kind of O-E Payload for UAV it is concealed
Three axis holders.
Background technique
With further increasing for social productive forces, industrial unmanned plane, as it is a kind of it is dynamic, controllable, can carry
At the equipment of task, in recent years by the favor of every profession and trade.
The three-axis stability augmentation gondola roll spindle motor of traditional unmanned plane is external, causes the asymmetry of structure, reality in rotation process
Space needed for border is larger, simultaneously as the asymmetry and aerodynamic configuration of structure are bad, is also easy to produce increasing flight resistance;Adjustment is axial
Sequentially, there are problems that Euler's critical angle, i.e., course axis easily occur and coupled with roll axis, holder generates shake and exciting, causes
Attitude parameter diverging.
Utility model content
It is above-mentioned to solve the purpose of this utility model is to provide a kind of concealed three axis holder of O-E Payload for UAV
The problem of being proposed in background technique.
To achieve the above object, the utility model provides the following technical solutions:
A kind of concealed three axis holder of O-E Payload for UAV, including head assembly and O-E Payload component, the light
Electric load component includes: package casing, camera, roll axis driving motor and end cap, and the roll axis driving motor is connected to phase
Machine right end, and be fixed on motor supporting base, camera is arranged in package casing;
The head assembly includes: pitch axis driving motor, pitching axis connection horn, course axis driving motor and holder
Damping, the pitch axis driving motor are mounted on the rear side of camera, and pitching axis connection horn drives electricity with course axis respectively
Machine is connected with pitch axis driving motor.
As a further solution of the present invention: the left end of the camera is camera lens, camera lens pad is set on camera lens
Piece and camera lens roll sleeve.
As a further solution of the present invention: the left end of the camera also sets up roll axis rolling bearing and bearing branch
Seat is supportted, roll axis rolling bearing is mounted on bearing support block.
As a further solution of the present invention: the holder damping includes equipment connecting plate and rubber shock-absorbing
Ball, course axis driving motor are mounted on equipment connecting plate.
Compared with prior art, the utility model has the beneficial effects that
1, change structure design, holder camera is directly connected with roll spindle motor, then by connector and pitch axis and
Course axis connection has symmetry in structure, supports more stable;
2, camera roll axial rearward end is motor, and front end is the support of bearing, increases camera stability and structural reliability;
3, adjustment holder axial arrangement distribution, roll axis is hidden in equipment, shape is without protrusion, and aerodynamic configuration is more preferably;
4, changing Eulerian angles sequence in gesture stability is camera-roll axis-pitch axis-course axis, reduces posture diverging.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model.
Fig. 2 is the schematic view of the front view of Fig. 1.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Please refer to Fig. 1~2, in the utility model embodiment, a kind of concealed three axis holder of O-E Payload for UAV, packet
Head assembly and O-E Payload component are included, the O-E Payload component includes: package casing 1, camera 6, roll axis driving motor 7
With end cap 13, the roll axis driving motor 7 is connected to 6 right end of camera, and is fixed on motor supporting base 8, and the setting of camera 6 exists
In package casing 1, the left end of camera 6 is camera lens, and camera lens gasket 2 and camera lens roll sleeve 3 is arranged on camera lens, camera 6
Left end also sets up roll axis rolling bearing 5 and bearing support block 4, and roll axis rolling bearing 5 is mounted on bearing support block 4, this
The roll axial rearward end of sample camera 6 is motor, and front end is the support of bearing, to increase camera stability and structural reliability;
The head assembly include: pitch axis driving motor 9, pitching axis connection horn 10, course axis driving motor 11 with
And holder damping 12, holder damping 12 include equipment connecting plate 15 and rubber shock-absorbing ball 14, the pitch axis driving
Motor 9 is mounted on the rear side of camera 6, pitching axis connection horn 10 respectively with course axis driving motor 11 and pitch axis driving motor
9 connections, course axis driving motor 11 is mounted on equipment connecting plate 15, and in this way in gesture stability, changing Eulerian angles sequence is
Camera-roll axis-pitch axis-course axis solves the problems, such as course axis and the coupling of roll axis, effectively controls posture diverging.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (4)
1. a kind of concealed three axis holder of O-E Payload for UAV, including head assembly and O-E Payload component, the photoelectricity
Load components include: package casing (1), camera (6), roll axis driving motor (7) and end cap (13), it is characterised in that: described
Roll axis driving motor (7) is connected to camera (6) right end, and is fixed on motor supporting base (8), and camera (6) setting is encapsulating
In shell (1);
The head assembly includes: pitch axis driving motor (9), pitching axis connection horn (10), course axis driving motor (11)
And holder damping (12), the pitch axis driving motor (9) are mounted on the rear side of camera (6), pitching axis connection horn
(10) it is connect respectively with course axis driving motor (11) and pitch axis driving motor (9).
2. a kind of concealed three axis holder of O-E Payload for UAV according to claim 1, it is characterised in that: the phase
The left end of machine (6) is camera lens, and camera lens gasket (2) and camera lens roll sleeve (3) is arranged on camera lens.
3. a kind of concealed three axis holder of O-E Payload for UAV according to claim 1 or 2, it is characterised in that: institute
The left end for stating camera (6) also sets up roll axis rolling bearing (5) and bearing support block (4), and roll axis rolling bearing (5) is mounted on
On bearing support block (4).
4. a kind of concealed three axis holder of O-E Payload for UAV according to claim 1, it is characterised in that: the cloud
Platform damping (12) includes equipment connecting plate (15) and rubber shock-absorbing ball (14), and course axis driving motor (11) is mounted on equipment
On connecting plate (15).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201821788723.2U CN209351613U (en) | 2018-11-01 | 2018-11-01 | A kind of concealed three axis holder of O-E Payload for UAV |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201821788723.2U CN209351613U (en) | 2018-11-01 | 2018-11-01 | A kind of concealed three axis holder of O-E Payload for UAV |
Publications (1)
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CN209351613U true CN209351613U (en) | 2019-09-06 |
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CN201821788723.2U Active CN209351613U (en) | 2018-11-01 | 2018-11-01 | A kind of concealed three axis holder of O-E Payload for UAV |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021134644A1 (en) * | 2019-12-31 | 2021-07-08 | 深圳市大疆创新科技有限公司 | Gimbal control method and gimbal |
CN114112297A (en) * | 2021-11-12 | 2022-03-01 | 中国船舶科学研究中心 | Vision-based on-board sea wave observation device and method |
WO2022213384A1 (en) * | 2021-04-09 | 2022-10-13 | 深圳市大疆创新科技有限公司 | Lens module, aircraft, handheld gimbal, and camera |
-
2018
- 2018-11-01 CN CN201821788723.2U patent/CN209351613U/en active Active
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021134644A1 (en) * | 2019-12-31 | 2021-07-08 | 深圳市大疆创新科技有限公司 | Gimbal control method and gimbal |
WO2022213384A1 (en) * | 2021-04-09 | 2022-10-13 | 深圳市大疆创新科技有限公司 | Lens module, aircraft, handheld gimbal, and camera |
CN114112297A (en) * | 2021-11-12 | 2022-03-01 | 中国船舶科学研究中心 | Vision-based on-board sea wave observation device and method |
CN114112297B (en) * | 2021-11-12 | 2023-08-18 | 中国船舶科学研究中心 | Vision-based on-ship sea wave observation device and method |
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Legal Events
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CP03 | Change of name, title or address |
Address after: Floor 12, plant 1, No.128, Shangnan East Road, Huangpu Community, Xinqiao street, Bao'an District, Shenzhen City, Guangdong Province Patentee after: Shenzhen Shunwei Communication Technology Co., Ltd Address before: 518000 Third Floor of Hengchangrong High-tech Industrial Park, 128 Shangnan East Road, Hongtian Village, Shajing Street, Baoan District, Shenzhen City, Guangdong Province Patentee before: Shenzhen doctoral Intelligent Technology Co., Ltd. |
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CP03 | Change of name, title or address |