CN106347693B - A kind of miniature gondola of changeable type unmanned plane - Google Patents
A kind of miniature gondola of changeable type unmanned plane Download PDFInfo
- Publication number
- CN106347693B CN106347693B CN201610863408.0A CN201610863408A CN106347693B CN 106347693 B CN106347693 B CN 106347693B CN 201610863408 A CN201610863408 A CN 201610863408A CN 106347693 B CN106347693 B CN 106347693B
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- Prior art keywords
- miniature
- sensor
- unmanned plane
- gondola
- cover
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Classifications
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- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C17/00—Aircraft stabilisation not otherwise provided for
- B64C17/02—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus
- B64C17/06—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus by gyroscopic apparatus
-
- 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
Abstract
The invention discloses a kind of miniature gondolas of changeable type unmanned plane, two axis gyroscope stabilized platform and sensor group including ball cover and in ball cover, the two axis gyroscope stabilized platform includes skeleton and the orientation driving motor module and pitching driving motor module that are fixed on skeleton, azimuth axle is connected in the orientation driving motor module, pitching shafting is connected in the pitching driving motor module, control and image processing unit are also equipped on the skeleton, SD card and connection circuit, top cover is provided at the top of skeleton, connecting flange and SD card lid are respectively arranged on top cover, middle shell and rear cover are connected on the skeleton, the ball cover is equipped with front cover group, the sensor group includes the sensor stand being arranged in front cover group and the first sensor being mounted on sensor stand and second sensor；The present invention is to stablize photoelectric nacelle using the two axis gyroscope of modularized design, and multiple sensors combination can be carried according to demand.
Description
Technical field
The invention belongs to optoelectronic device technical fields in unmanned vehicle, aeronautical technology, and in particular to a kind of changeable type
Unmanned plane Miniature photoelectric hanging cabin.
Background technique
It monitors, scout on a large scale to meet different field, the various aspects mission requirements such as line walking, UAV flight is miniature at present
Gondola is the preferred high-efficient disposition for realizing such demand.Using unmanned plane to mountain area, valley, forest, river, set device et al.
Member is difficult to reach the monitoring in location, checks have the advantage flexible, easy to operate, work efficiency is high of flying, effectively reduce into
This；After various serious natural calamities, unmanned plane can be used to be monitored flying into incident area at the first time, completes electric power
The tasks such as sudden instability, Disaster Assessment, gain time, and reduce casualty loss.
The generally existing weight weight of the photoelectric nacelle of domestic development production at present, power consumption is high, configures the defects of single, it is difficult to full
The demand of sufficient small drone.
Summary of the invention
It is an object of the invention to deficiencies according to prior art, provide a kind of light-weight, compact-sized, low in energy consumption, mould
The photoelectric nacelle of block, to meet the requirement of unmanned plane.
The technical solution adopted by the present invention to solve the technical problems is: a kind of miniature gondola of changeable type unmanned plane, packet
Ball cover and two axis gyroscope stabilized platform and sensor group in ball cover are included, the two axis gyroscope stabilized platform includes skeleton
And it is fixed on orientation driving motor module and pitching driving motor module on skeleton, connect in the orientation driving motor module
It is connected to azimuth axle, pitching shafting is connected in the pitching driving motor module, control is also equipped on the skeleton
With image processing unit, SD card and couple circuit, be provided with top cover at the top of skeleton, be respectively arranged with connecting flange and SD on top cover
Ka Gai is connected with middle shell and rear cover on the skeleton, and the ball cover is equipped with front cover group, and the sensor group includes
The sensor stand being arranged in front cover group and the first sensor and second sensor that are mounted on sensor stand.
A kind of miniature gondola of changeable type unmanned plane, passes through between two axis gyroscope stabilized platform and sensor group
The direct grafting of socket is to realize the transmitting and power supply of information, then is fixed and formed by four screws.
A kind of miniature gondola of changeable type unmanned plane, front cover group is by front cover and the protection being bonded on front cover
Glass composition, the protection glass are located in front of sensor.
A kind of miniature gondola of changeable type unmanned plane, protection glass are planar wave glass or infrared glass.
A kind of miniature gondola of changeable type unmanned plane, orientation driving motor module, pitching driving motor module,
SD card and control are all made of plug-in mode with image processing unit and are fixed on skeleton.
A kind of miniature gondola of changeable type unmanned plane, control and image processing unit are by image plate, control panel
It is formed with driving plate.
A kind of miniature gondola of changeable type unmanned plane, azimuth axle realize water-stop by sealing ring.
A kind of miniature gondola of changeable type unmanned plane, pitching shafting realize water-stop by labyrinth seal.
A kind of miniature gondola of changeable type unmanned plane, sensor group pass through the sealing cord between front cover group and rear cover
Realize sealing.
A kind of miniature gondola of changeable type unmanned plane, ball cover realize that the cooperation with top cover seals by seam allowance.
The beneficial effects of the present invention are: can replace multiple sensors combination according to demand using modularized design, realize not
Congenerous；Sensor group and rear cover composition seal can realize pitching movement, and rest part is sealed with ball cover, water proof and dust proof performance
It is good；Visible light video, infrared screen can be exported in real time or object ranging is positioned, and there is gyro to increase steady function；Using interior bone
Frame structure and Integral ball cover structure have structure simple, effectively reduce the weight and volume of load, applied widely to wait spies
Point.
Detailed description of the invention
Fig. 1 is main view of the invention；
Fig. 2 is top view of the invention；
Fig. 3 is the main view inside the present invention；
Fig. 4 is the perspective view inside the present invention.
Each appended drawing reference are as follows: 101-SD card lids, 102-ball covers, 103-sealing rings, 104-azimuth axles, 105-SD
Card, 106-orientation driving motor modules, 107-skeletons, 108-pitching driving motor modules, 109-pitching shaftings, 110-
Connecting flange, 111-top covers, 112-controls and image processing unit, 113-rear covers, 114-middle shells, 201-front cover groups,
202-first sensors, 203-sensor stands, 204-second sensors.
Specific embodiment
The present invention is described in further detail below in conjunction with the accompanying drawings.
Referring to figs. 1 to 4, the invention discloses a kind of miniature gondolas of changeable type unmanned plane, including 102 He of ball cover
Two axis gyroscope stabilized platform and sensor group in ball cover 102, the two axis gyroscope stabilized platform and sensor group it
Between by the direct grafting of socket to realize the transmitting and power supply of information, then formed by four screws fixations, can be according to user demand
It is docked in various combination, when needing replacing sensor group, need to only remove 4 fixing screws, extracting sensor group can be quick
More emat sensor group.
Wherein two axis gyroscope stabilized platform includes skeleton 107 and the orientation driving motor module 106 being fixed on skeleton 107
With pitching driving motor module 108, azimuth axle 104, the pitching are connected in the orientation driving motor module 106
Pitching shafting 109 is connected in driving motor module 108, to realize the driving of two axis, orientation and pitch rotation by servo electricity
Machine drives helical gear to realize, control and image processing unit 112, SD card 105 are also equipped on the skeleton 107 and couples electricity
Road, realize control to two axis gyroscope stabilized platform, the control and image processing unit 112 by image plate, control panel with
Driving plate composition, is fixed on skeleton 107；It is provided with top cover 111 at the top of the skeleton 107, is respectively arranged on top cover 111
Connecting flange 110 and SD card lid 101, SD card 105 are located at 101 lower section of SD card lid, and the orientation driving motor module 106 is bowed
It faces upward driving motor module 108, SD card 105 and control and image processing unit 112 is independent assembly, fixed using plug-in mode
On skeleton 107, facilitate adjustment and replacement, wherein azimuth axle 104 realizes water-stop, pitching shafting 109 by sealing ring 103
Water-stop is realized by labyrinth seal；Middle shell 114 and rear cover 113, the ball cover are connected on the skeleton 107
102 are equipped with front cover group 201, and front cover group 201 and rear cover 113 are separately fixed at the front and back side of middle shell 114.
Wherein the sensor group includes being fixed on the sensor stand 203 at 201 rear of front cover group and being mounted on biography
First sensor 202 and second sensor 204 on sensor bracket 203, include two orthogonal uniaxial gyros, sensor group with
Rear cover 113, which forms seal, can realize pitching movement, and rest part is sealed with ball cover 102, have bayonet and top cover at the top of ball cover 102
111 sealings, water proof and dust proof performance is good, and sensor group realizes sealing by the sealing cord between front cover group 201 and rear cover 113；It is described
Front cover group 201 be made of front cover and the protection glass being bonded on front cover, plain protective glass is according to selected sensor wave
Duan Erding, the protection glass are located in front of sensor, are aligned with respective sensor, protection glass be planar wave glass or
Infrared glass is applicable in different-waveband, and light passing is good, undistorted, and hardness is high, is not easy to scratch；And the ball cover of traditional ball machine mostly uses
Arc non-glass ball cover, hardness and image quality are difficult to guarantee, and infrared ball cover cost is just higher thoroughly.
The present invention is a kind of two axis gyroscope stabilized platform using modularized design, and gondola can carry miniature visible image capturing
The sensors such as machine, infrared thermoviewer, miniature laser rangefinder can configure different sensor combinations according to mission requirements, such as red
Outside+visible light sensor, infrared+laser range finder, visible light+laser range finder or single-sensor etc.；Sensor is according to user
Demand, available combination are TV sensor, infrared thermal imager, TV sensor+infrared thermal imager, TV sensor+swash
Five kinds of ligh-ranging machine, infrared thermal imager+laser range finder combinations.
Gondola of the present invention is connect by connecting flange 110 with unmanned plane, can be designed according to different unmanned aerial vehicle platforms corresponding
Shock bracket；Unmanned plane provides airborne direct current+12V power supply and control signal to gondola, passes through control and image processing unit
112, the closed loop servo system of orientation driving motor module 106, pitching driving motor module 108 and gyro composition is, it can be achieved that hang
The stability contorting in cabin carries out panorama scanning and pitching scanning, realizes to suspicious object tracking, ranging, positioning etc..
The present invention can be combined in visible light camera, infrared thermoviewer and laser range finder optional two, be realized not
Same demand；And gyrocontrol function is realized, compact-sized, small in size, weight is not more than 600 grams, can fit loaded on most of small
Type unmanned plane.
Captured video and data are storable in large capacity SD card 105 during the operation of this gondola, can also be led in real time
It crosses unmanned plane transmission channel and passes control terminal back, carry out implementation data processing, can directly dismantle SD card lid 101 then after completion task
SD card 105 is taken out, subsequent processing can be carried out by obtaining work data.
When the maintenance of this gondola, removal sensor group and rear cover 113 exit ball cover 102, all skeletons from gondola
Can be adjusted and test with module, and exposed screws are few, it is beautiful reliable, can export in real time visible light video or infrared screen or
Object ranging is positioned, there is gyro to increase steady function；Using inner skeleton structure and Integral ball cover structure, have structure simple,
Effectively reduce the weight and volume of load, it is applied widely the features such as, sensor is replaceable.
The above-described embodiments merely illustrate the principles and effects of the present invention, and the embodiment that part uses, for
For those skilled in the art, without departing from the concept of the premise of the invention, can also make it is several deformation and
It improves, these are all within the scope of protection of the present invention.
Claims (10)
1. a kind of miniature gondola of changeable type unmanned plane, it is characterised in that: including ball cover (102) and be set in ball cover (102)
Two axis gyroscope stabilized platform and sensor group, the two axis gyroscope stabilized platform include skeleton (107) and are fixed on skeleton
(107) orientation driving motor module (106) and pitching driving motor module (108) on, the orientation driving motor module
(106) it is connected on azimuth axle (104), is connected with pitching shafting (109) in the pitching driving motor module (108),
It is also equipped with control and image processing unit (112), SD card (105) on the skeleton (107) and couples circuit, skeleton
(107) top is provided with top cover (111), and connecting flange (110) and SD card lid (101) are respectively arranged on top cover (111), described
Skeleton (107) on be connected with middle shell (114) and rear cover (113), the ball cover (102) is equipped with front cover group (201), institute
The sensor group stated includes the sensor stand (203) being arranged on front cover group (201) and is mounted on sensor stand (203)
On first sensor (202) and second sensor (204).
2. a kind of miniature gondola of changeable type unmanned plane according to claim 1, which is characterized in that the two axis gyroscope
The transmitting and power supply of information are realized between stabilized platform and sensor group by the direct grafting of socket, then is fixed by four screws
It forms.
3. a kind of miniature gondola of changeable type unmanned plane according to claim 1, which is characterized in that the front cover group
(201) it is made of front cover and the protection glass being bonded on front cover, the protection glass is located in front of sensor.
4. a kind of miniature gondola of changeable type unmanned plane according to claim 3, which is characterized in that the protection glass
For planar wave glass or infrared glass.
5. a kind of miniature gondola of changeable type unmanned plane according to claim 1, which is characterized in that the orientation driving
Motor module (106), pitching driving motor module (108), SD card (105) and control are all made of with image processing unit (112)
Plug-in mode is fixed on skeleton (107).
6. a kind of miniature gondola of changeable type unmanned plane according to claim 1, which is characterized in that the control and figure
As processing unit (112) are made of image plate, control panel and driving plate.
7. a kind of miniature gondola of changeable type unmanned plane according to claim 1, which is characterized in that the azimuth axle
(104) water-stop is realized by sealing ring (103).
8. a kind of miniature gondola of changeable type unmanned plane according to claim 1, which is characterized in that the pitching shafting
(109) water-stop is realized by labyrinth seal.
9. a kind of miniature gondola of changeable type unmanned plane according to claim 1, which is characterized in that the sensor group
Sealing is realized by the sealing cord between front cover group (201) and rear cover (113).
10. a kind of miniature gondola of changeable type unmanned plane according to claim 1, which is characterized in that the ball cover
(102) realize that the cooperation with top cover (111) seals by seam allowance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610863408.0A CN106347693B (en) | 2016-09-29 | 2016-09-29 | A kind of miniature gondola of changeable type unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610863408.0A CN106347693B (en) | 2016-09-29 | 2016-09-29 | A kind of miniature gondola of changeable type unmanned plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106347693A CN106347693A (en) | 2017-01-25 |
| CN106347693B true CN106347693B (en) | 2019-05-31 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610863408.0A Active CN106347693B (en) | 2016-09-29 | 2016-09-29 | A kind of miniature gondola of changeable type unmanned plane |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107831578B (en) * | 2017-11-08 | 2023-12-05 | 中船重工中南装备有限责任公司 | Multi-layer omnidirectional observation window structure |
| CN207809801U (en) * | 2017-11-08 | 2018-09-04 | 深圳市大疆创新科技有限公司 | Roll shaft assembly, camera head and the unmanned vehicle of holder |
| CN108438244A (en) * | 2018-04-27 | 2018-08-24 | 南京拓威航空科技有限公司 | A kind of airborne aerial device and the unmanned plane containing it |
| CN109139828B (en) * | 2018-10-16 | 2021-08-06 | 天津津航技术物理研究所 | Wire rope transmission mechanism of photoelectric pod |
| CN109828488A (en) * | 2018-12-27 | 2019-05-31 | 北京航天福道高技术股份有限公司 | The double optical detection tracking systems of acquisition transmission integration |
| DE202019102256U1 (en) * | 2019-04-18 | 2020-07-21 | Dürkopp Adler AG | Carrying and docking device for electronics housing modules |
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|---|---|---|---|---|
| CN101811578A (en) * | 2010-04-23 | 2010-08-25 | 福建省电力有限公司福州电业局 | Special photoelectric nacelle of power patrol unmanned helicopter |
| CN102424113A (en) * | 2012-01-13 | 2012-04-25 | 武汉华中天经光电系统有限公司 | Miniature photoelectric hanging cabin |
| CN103395496A (en) * | 2013-08-14 | 2013-11-20 | 武汉华中天经光电系统有限公司 | Triaxial orthographic nacelle of unmanned aerial vehicle |
| CN105501454A (en) * | 2016-01-20 | 2016-04-20 | 北京锁定精密科技有限公司 | Mini-sized pod |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006264567A (en) * | 2005-03-25 | 2006-10-05 | Yamaha Motor Co Ltd | Helicopter |
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2016
- 2016-09-29 CN CN201610863408.0A patent/CN106347693B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101811578A (en) * | 2010-04-23 | 2010-08-25 | 福建省电力有限公司福州电业局 | Special photoelectric nacelle of power patrol unmanned helicopter |
| CN102424113A (en) * | 2012-01-13 | 2012-04-25 | 武汉华中天经光电系统有限公司 | Miniature photoelectric hanging cabin |
| CN103395496A (en) * | 2013-08-14 | 2013-11-20 | 武汉华中天经光电系统有限公司 | Triaxial orthographic nacelle of unmanned aerial vehicle |
| CN105501454A (en) * | 2016-01-20 | 2016-04-20 | 北京锁定精密科技有限公司 | Mini-sized pod |
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| Publication number | Publication date |
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| CN106347693A (en) | 2017-01-25 |
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