CN107985617A - A kind of double light photoelectric nacelles - Google Patents
A kind of double light photoelectric nacelles Download PDFInfo
- Publication number
- CN107985617A CN107985617A CN201711021738.6A CN201711021738A CN107985617A CN 107985617 A CN107985617 A CN 107985617A CN 201711021738 A CN201711021738 A CN 201711021738A CN 107985617 A CN107985617 A CN 107985617A
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- CN
- China
- Prior art keywords
- motor
- gondola
- ball
- damping
- axis
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
The invention discloses a kind of double light photoelectric nacelles, including ball-type gondola, first motor mount, gondola principal arm, second motor mount, 3rd motor mount, control module and damping holder, zoom movement and camera device are installed in the ball-type gondola, ball-type gondola both sides are installed on first motor mount, first motor is installed on the first motor mount, second motor mount installs the second motor, the output shaft of second motor is connected with the first motor mount, the gondola principal arm both ends are provided with the second motor mount and the 3rd motor mount, control module is installed on 3rd motor mount, control module both sides are provided with damping holder.Gondola is arranged to ball-type by the present invention, reduces the volume and weight of gondola, and controls rotation of the gondola on X-axis, Y-axis and Z axis by three motors, and then controls the rotation of zoom movement and camera device, so that the collection of multi-angle shooting information can be realized.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, and in particular to a kind of double light photoelectric nacelles.
Background technology
The application of unmanned plane is more and more extensive, and having benefited from it can be visited by the infra-red radiation ripple sent to object itself
Survey, and then obtain the information of object exactly, be widely used in public security monitoring, dangerous situation rescue etc..Because of existing unmanned plane all
It is to fix a holder in fuselage bottom, camera device is fixed on holder, which can only be directed at a direction and carry out letter
Breath collection, and when needing to be acquired other angles, complete information typically by the flight attitude of adjustment unmanned plane and adopt
Collection acts, it is this be in a manner of adjusting UAV Attitude and carry out information gathering, it is cumbersome, and adjust unmanned plane in real time
Flight attitude also easily influences the state of flight and flying speed of unmanned plane.
The content of the invention
It is an object of the invention to provide a kind of double light photoelectric nacelles, the gondola by the rotation along X-axis, Y-axis and Z axis,
The collection of multi-angle shooting information can be achieved.
The purpose of the present invention is what is be achieved through the following technical solutions：
A kind of double light photoelectric nacelles, including ball-type gondola, the first motor mount, gondola principal arm, the second motor mount,
3rd motor mount, the first motor, the second motor, the 3rd motor, control module and damping holder, the interior peace of the ball-type gondola
Equipped with zoom movement and camera device, the first motor mount is U-shaped structure, including be fixedly connected sequentially left support abutment, left branch
Arm, mounting base, right support arm and right support abutment, are provided with bearing on left support abutment, the first motor, left support abutment and the right side are provided with right support abutment
Bearing is installed on ball-type gondola both sides, and the first motor is connected with ball-type gondola, the output shaft and mounting base of second motor
It is fixedly connected, the second motor is installed on the second motor mount, and the second motor mount is connected with the bottom of gondola principal arm, is hung
3rd motor mount is installed on the top of cabin principal arm, the 3rd motor be installed on the 3rd motor mount and with gondola principal arm
Connecting, control module is installed at the top of the 3rd motor mount, the both sides of control module are mounted on damping holder,
Space coordinates are established, using the first motor output shaft as X-axis, using the second motor output shaft as Y-axis, with the 3rd motor
Output shaft is Z axis, and the first motor control ball-type gondola is rotated around X-axis, and then controls the pitching visual angle of camera device；Second motor
Control ball-type gondola is rotated around Y-axis, and then controls the vertical visual angle of camera device；3rd motor control ball-type gondola revolves about the z axis
Turn, and then control the horizontal view angle of camera device.
Further, the ball-type gondola includes front casing, rear casing and central plate, and front casing connects combination with rear casing
For a spherical, central plate is installed among spherical along the diameter of spherical, zoom movement and the camera device installation
On the central plate.
Further, the damping holder includes holder and two shock-damping structures on holder, the damping
Structure includes hangers, damping upper plate, damping lower plate and shock-absorbing ball, and shock-absorbing ball is installed between damping upper plate and damping lower plate, is hung
Ear is connected with damping lower plate, and damping upper plate is connected with holder.
The invention has the advantages that：
(1) gondola is set to ball shape structure, alleviates the weight of gondola, reduce the volume of gondola；
(2) rotation of the gondola on X-axis, Y-axis and Z axis is controlled by three motors, and then controls zoom movement and shooting
The rotation of device, so that the collection of multi-angle shooting information can be realized；
(3) by setting damping holder, reduce the vibrations that unmanned plane is brought in flight course to camera device, improve
The quality of shooting picture；
(4) it is simple in structure, small, easy to operate.
Brief description of the drawings
Fig. 1 is the structure diagram of the present invention；
Fig. 2 is the structure diagram of ball-type gondola of the present invention；
Fig. 3 is the internal structure schematic diagram of ball-type gondola of the present invention；
Fig. 4 is the structure diagram of the first motor mount of the invention；
Fig. 5 is the structure diagram of gondola principal arm of the present invention；
Fig. 6 is the structure diagram of damping holder of the present invention.
Marked in figure：1st, ball-type gondola；2nd, the first motor mount；3rd, the first motor；4th, the second motor mount；5th,
Two motors；6th, gondola principal arm；7th, the 3rd motor mount；8th, the 3rd motor；9th, control module；10th, damping holder；11st, it is preceding outer
Shell；12nd, rear casing；13rd, central plate；21st, left support abutment；22nd, left support arm；23rd, mounting base；24th, right support arm；25th, right support abutment；131、
First fixing piece；132nd, the second fixing piece；101st, holder；102nd, shock-damping structure；1021st, damping lower plate；1022nd, shock-absorbing ball；
1023rd, damping upper plate；1024th, hangers；A, 10 times of zoom movements；B, infrared eye.
Embodiment
As shown in Fig. 1~Fig. 6, double light photoelectric nacelles provided in this embodiment include ball-type gondola 1, the first motor mount
2nd, the first motor 3, the second motor mount 4, the second motor 5, gondola principal arm 6, the 3rd motor mount 7, the 3rd motor 8, control
10,10 times of molding block 9, damping holder zoom movement A and infrared eye B, as shown in Fig. 2, before the ball-type gondola 1 includes
Shell 11, rear casing 12 and central plate 13, front casing 11 and the connection of rear casing 12 are combined as a spherical, and central plate 13 is along ball
The diameter of body is installed among spherical, and 10 times of zoom movements are installed with by the first fixing piece 131 on central plate 13
A, is also installed with infrared eye B by the second fixing piece 132；By the way that gondola is arranged to spherical, can including
Zoom movement A and infrared eye B is installed in portion, and can reduce the weight and volume of gondola.The electricity of ball-type gondola 1 and first
Machine 3 connects, and the first motor 3 is installed on the first motor mount 2, as shown in figure 4, first motor mount 2 is U-shaped knot
Structure, it includes left support abutment 21, left support arm 22, mounting base 23, right support arm 24 and the right support abutment 25 being fixedly connected sequentially；Left support abutment 21
On bearing is installed, the first motor 3 is installed, left support abutment 21 and right support abutment 25 are separately mounted to ball-type gondola 1 on right support abutment 25
Both sides, the output shaft of the first motor 3 is fixedly connected with central plate 13, realizes that control ball-type gondola 1 does elevating movement, so that real
Now control the pitch angle of infrared eye B.Roll axis is installed, roll axis is defeated for the second motor 5 in the mounting base 23
Shaft, the second motor 5 control ball-type gondola 1 do roll motion, further control the rotation of infrared eye B；Second motor 5
On the second motor mount 4, the second motor mount 4 is installed on the bottom of gondola principal arm 6, the top of gondola principal arm 6
3rd motor mount 7 is installed, the 3rd motor 8 is installed on the 3rd motor mount 7；The output shaft of 3rd motor 8 is with hanging
Cabin principal arm 6 connects, and realizes that control ball-type gondola 1 rotates, and then control the rotation of infrared eye B.The 3rd motor peace
The top of dress seat 7 is installed with control module 9, and control module 9 is used to receive remote control signal and send control signal
To corresponding motor, remote control gondola is realized.The both sides of the control module 9 are provided with damping holder 10, as shown in fig. 6,
The damping holder 10 includes holder 101 and shock-damping structure 102, and the shock-damping structure 102 includes damping upper plate 1023, shock-absorbing ball
1022nd, damping lower plate 1021 and hangers 1024, shock-absorbing ball 1022 are installed between damping upper plate 1023 and damping lower plate 1021, institute
State holder 101 to be fixedly connected with damping upper plate 1023, damping lower plate 1021 is connected by hangers 1024 with unmanned plane, the damping
Holder 10 reduces the vibrations that unmanned plane is brought in flight course to infrared eye B, improves the quality of shooting picture.
Space coordinates are established, using 3 output shaft of the first motor as X-axis, using 5 output shaft of the second motor as Y-axis, with the 3rd electricity
8 output shaft of machine is Z axis, and the first motor 3 control ball-type gondola 1 is rotated around X-axis, and then controls the pitching of infrared eye B to regard
Angle；Second motor 5 control ball-type gondola 1 is rotated around Y-axis, and then controls the vertical visual angle of infrared eye B；3rd motor 8
Control ball-type gondola 1 rotates about the z axis, and then controls the horizontal view angle of infrared eye B.
The above is only the preferred embodiment of the present invention, but protection scope of the present invention is not limited thereto, any
The transformation and replacement that are carried out based on technical solution provided by the present invention and inventive concept should all cover the protection model in the present invention
In enclosing.
Claims (3)
- A kind of 1. double light photoelectric nacelles, it is characterised in that：Including ball-type gondola, the first motor mount, gondola principal arm, the second electricity Machine mounting base, the 3rd motor mount, the first motor, the second motor, the 3rd motor, control module and damping holder, the ball Zoom movement and camera device be installed, the first motor mount is U-shaped structure, including the left side being fixedly connected sequentially in type gondola Bearing, left support arm, mounting base, right support arm and right support abutment, are provided with bearing on left support abutment, the first motor are provided with right support abutment, Left support abutment and right support abutment are installed on ball-type gondola both sides, and the first motor is connected with ball-type gondola, the output of second motor Axis is fixedly connected with mounting base, and the second motor is installed on the second motor mount, the second motor mount and gondola principal arm Bottom connects, and the 3rd motor mount is provided with the top of gondola principal arm, and the 3rd motor is installed on the 3rd motor mount And be connected with gondola principal arm, control module is installed, the both sides of control module are mounted on subtracting at the top of the 3rd motor mount Shake holder；Space coordinates are established, using the first motor output shaft as X-axis, using the second motor output shaft as Y-axis, are exported with the 3rd motor Axis is Z axis, and the first motor control ball-type gondola is rotated around X-axis, and then controls the pitching visual angle of camera device；Second motor controls Ball-type gondola is rotated around Y-axis, and then controls the vertical visual angle of camera device；3rd motor control ball-type gondola rotates about the z axis, into And control the horizontal view angle of camera device.
- 2. double light photoelectric nacelles according to claim 1, it is characterised in that：The ball-type gondola includes front casing, rear outer Shell and central plate, front casing and rear casing, which connect, is combined as a spherical, and central plate is along the diameter of spherical installed in spherical Among body, zoom movement and the camera device installation is on the central plate.
- 3. double light photoelectric nacelles according to claim 1, it is characterised in that：The damping holder includes holder and installation Two shock-damping structures on holder, the shock-damping structure include hangers, damping upper plate, damping lower plate and shock-absorbing ball, shock-absorbing ball Between damping upper plate and damping lower plate, hangers is connected with damping lower plate, and damping upper plate is connected with holder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711021738.6A CN107985617A (en) | 2017-10-27 | 2017-10-27 | A kind of double light photoelectric nacelles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711021738.6A CN107985617A (en) | 2017-10-27 | 2017-10-27 | A kind of double light photoelectric nacelles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107985617A true CN107985617A (en) | 2018-05-04 |
Family
ID=62030586
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711021738.6A Pending CN107985617A (en) | 2017-10-27 | 2017-10-27 | A kind of double light photoelectric nacelles |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107985617A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2801866A1 (en) * | 1999-12-06 | 2001-06-08 | Jean Eyer | Mounting for camera suspended from fixed balloon includes universal joints with magnetic damping to keep camera frame vertical |
| CN203889081U (en) * | 2014-06-06 | 2014-10-22 | 中孚航空科技（天津）有限公司 | Pan-tilt damping device of electric unmanned helicopter |
| CN204674844U (en) * | 2015-05-15 | 2015-09-30 | 深圳市大疆创新科技有限公司 | Vibration damper plate and there is the unmanned vehicle of this vibration damper plate |
| CN205418138U (en) * | 2016-03-18 | 2016-08-03 | 江苏数字鹰科技发展有限公司 | Triaxial optoelectronic pod |
| CN106439418A (en) * | 2016-11-21 | 2017-02-22 | 天津中翔腾航科技股份有限公司 | High-pixel optical zooming imaging holder |
| CN206494136U (en) * | 2016-10-27 | 2017-09-15 | 江苏云端智能科技有限公司 | A kind of UAV flight's head |
-
2017
- 2017-10-27 CN CN201711021738.6A patent/CN107985617A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2801866A1 (en) * | 1999-12-06 | 2001-06-08 | Jean Eyer | Mounting for camera suspended from fixed balloon includes universal joints with magnetic damping to keep camera frame vertical |
| CN203889081U (en) * | 2014-06-06 | 2014-10-22 | 中孚航空科技（天津）有限公司 | Pan-tilt damping device of electric unmanned helicopter |
| CN204674844U (en) * | 2015-05-15 | 2015-09-30 | 深圳市大疆创新科技有限公司 | Vibration damper plate and there is the unmanned vehicle of this vibration damper plate |
| CN205418138U (en) * | 2016-03-18 | 2016-08-03 | 江苏数字鹰科技发展有限公司 | Triaxial optoelectronic pod |
| CN206494136U (en) * | 2016-10-27 | 2017-09-15 | 江苏云端智能科技有限公司 | A kind of UAV flight's head |
| CN106439418A (en) * | 2016-11-21 | 2017-02-22 | 天津中翔腾航科技股份有限公司 | High-pixel optical zooming imaging holder |
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180504 |
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| RJ01 | Rejection of invention patent application after publication |