CN205872506U - Unmanned aerial vehicle's nacelle - Google Patents
Unmanned aerial vehicle's nacelle Download PDFInfo
- Publication number
- CN205872506U CN205872506U CN201620847934.3U CN201620847934U CN205872506U CN 205872506 U CN205872506 U CN 205872506U CN 201620847934 U CN201620847934 U CN 201620847934U CN 205872506 U CN205872506 U CN 205872506U
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- support
- motor
- plane
- gondola
- module
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Abstract
The utility model discloses an unmanned aerial vehicle's nacelle, include: the picture passes rain -proof shell for the setting is on unmanned aerial vehicle's organism, and wherein, the picture passes rain -proof shell and is equipped with first motor, first support, its one end sets up on first motor to rotate through the first support of first electric machine control, second support, one of which end hinge connect the setting on the other end of first motor is kept away from to first support, the module of taking photo by plane, the articulated setting on the other end of first support is kept away from to the second support, the module of wherein taking photo by plane is equipped with the camera for shooting picture or video, wherein, the one end that the second support is close to first support is equipped with the second motor, and the second motor is articulated with the other end of first support to rotate through second electric machine control second support. In this way, the utility model discloses can let unmanned aerial vehicle stable shooting or observe around situation under complicated condition, can work under the rainy day environment, can clap the infrared thermal imaging, also can take the image of clarity night, and anti -shake be effectual.
Description
Technical field
This utility model relates to unmanned air vehicle technique field, more particularly, it relates to the gondola of a kind of unmanned plane.
Background technology
Unmanned plane is the most manned aircraft of the programme-control manipulation utilizing radio robot with providing for oneself.It is generally used for height
Empty shooting, to realize detecting landforms, looking down the purposes such as ground.Unmanned plane on existing market uses airborne tripod head also or airborne
The mode of photoelectric nacelle can realize the shoot function of unmanned plane.But due to current technical deficiency, exist existing unmanned
When machine is taken pictures more overcritical to environment, the stabilization weak effect and cause performing round-the-clock without thermal imaging system when flight shooting
The shortcoming of task.
Utility model content
This utility model provides the gondola of a kind of unmanned plane, mainly solves unmanned plane in prior art anti-when flight shooting
The problem trembling weak effect.
For solving above-mentioned technical problem, the technical scheme that this utility model uses is: provide hanging of a kind of unmanned plane
Cabin, including: figure passes rainproof shell, and for being arranged on the body of unmanned plane, wherein, figure passes rainproof shell and is provided with the first motor；First
Support, its one end is arranged on the first motor, to control the first holder pivots by the first motor；Second support, its one end is cut with scissors
Connect and be arranged on first support other end away from the first motor；Taking photo by plane module, hinged second support that is arranged on is away from first
On the other end of frame, module of wherein taking photo by plane is provided with photographic head, is used for shooting picture or video；Wherein, the second support is near first
One end of support is provided with the second motor, and the other end of the second motor and the first support is hinged, to control second by the second motor
Holder pivots.
Wherein, module of taking photo by plane is provided with the 3rd motor, and the other end of the 3rd motor and the second support is hinged, with by the 3rd electricity
Machine controls module rotation of taking photo by plane.
Wherein, figure is provided with shock-absorbing ball and fixed support in passing rainproof shell, and shock-absorbing ball is arranged on fixed support, fixed support
For being arranged on the body of unmanned plane.
Wherein, the second support includes swingle and is arranged on the connecting rod at swingle two ends, and the second motor is arranged on rotation
In bar, module clip of taking photo by plane is located between connecting rod.
Wherein, module symmetry of taking photo by plane is provided with the first side and the second side, the 3rd motor be separately positioned on the first side and
On second side, connecting rod is provided with clamp cap, and clamp cap is hinged with the 3rd motor.
Wherein, module of taking photo by plane is provided with the 3rd side, and the 3rd side is arranged at intervals with photographic head and infrared lamp.
Wherein, photographic head includes visible image capturing head and infrared thermal imaging camera.
Wherein, the rainproof shell of figure biography is cylindrical.
Wherein, the first L-shaped shape of support, the second U-shaped shape of support.
Wherein, module of taking photo by plane shape spherical in shape.
This utility model, owing to have employed technique scheme, has the advantage that
1, unmanned plane can shoot the carrying out that complex condition is stable or observe ambient conditions；
2, unmanned plane can clap infrared thermal imaging, and night can also photograph to be affected clearly；
3, during unmanned plane shooting, image shake is the least, and shooting effect is good.
Accompanying drawing explanation
Fig. 1 is the structural representation of this utility model unmanned plane；
Fig. 2 is the perspective view of the gondola of this utility model unmanned plane；
Fig. 3 is the partial structurtes schematic diagram of the gondola of unmanned plane in Fig. 2；
Fig. 4 is the structural representation of the second support of the gondola of unmanned plane in Fig. 2；
The structural representation of the module of taking photo by plane of the gondola of unmanned plane in Fig. 5 Fig. 2；
Fig. 6 is the stereochemical structure sectional view of the gondola of unmanned plane in Fig. 2.
Description of reference numerals: 1, figure passes rainproof shell, the 2, second support, 3, module of taking photo by plane, 4, unmanned plane, the 11, first support,
12, the first motor, 13, contiguous block, 14, fixed support, 15, figure pass, 16, cradle head control plate, 17, vibration-proof motor mounting seat,
18, shock-absorbing ball, the 21, second motor, 22, swingle, 23, connecting rod, 24, clamp cap, the 31, first side, the 32, second side,
33, the 3rd side, the 34, the 3rd motor, 35, visible image capturing head, 36, infrared thermal imaging camera, 37, infrared lamp, 41, machine
Body, 42, spike.
Detailed description of the invention
With embodiment, this utility model is described in detail below in conjunction with the accompanying drawings.
It is the structural representation of this utility model unmanned plane with reference to Fig. 1, Fig. 1.This unmanned plane 4 includes body 41, is arranged on
Propping up spike 42, the horn being arranged on body 41 and being arranged on the propeller of the horn other end, horn and spiral shell on the downside of body 41
Rotation oar is for controlling the flight of unmanned plane.
In the present embodiment, the quantity of horn is 4, and horn is uniformly arranged on the body 41 of unmanned plane 4.Should be understood that
This utility model does not limit the quantity of horn as 4, in other embodiments, the quantity of horn can also is that 1,2,3
Individual or more, depending on specifically needing according to practical situation.
With further reference to shown in Fig. 2-Fig. 6, Fig. 2 is the perspective view of the gondola of this utility model unmanned plane, Fig. 3
Being the partial structurtes schematic diagram of the gondola of unmanned plane in Fig. 2, Fig. 4 is that the structure of the second support of the gondola of unmanned plane in Fig. 2 is shown
Being intended to, Fig. 5 is the structural representation of the module of taking photo by plane of the gondola of unmanned plane in Fig. 2, and Fig. 6 is the vertical of the gondola of unmanned plane in Fig. 2
Body structure sectional view.The gondola of this unmanned plane includes that figure passes rainproof shell the 1, first support the 11, second support 2 and module 3 of taking photo by plane.
Figure passes rainproof shell 1 and is used for being arranged on the body 41 of unmanned plane 4, and wherein, figure passes rainproof shell 1 and is provided with the first motor
12.Figure is provided with shock-absorbing ball 18 and fixed support 14 in passing rainproof shell 1, and shock-absorbing ball 18 is arranged on fixed support 14, fixed support
14 for being arranged on the body 41 of unmanned plane 4.Wherein, the rainproof shell 1 of figure biography is cylindrical.
In the present embodiment, figure is additionally provided with figure and passes 15, vibration-proof motor mounting seat 17 and shock-absorbing ball 18 in passing rainproof shell 1,
Wherein, figure passes 15 is image transmitter.Preferably, vibration-proof motor mounting seat 17 is arranged on shock-absorbing ball 18, and shock-absorbing ball 18 is pacified
Being contained on fixed support 14, the first motor 12 is arranged in vibration-proof motor mounting seat 17.During running status, from unmanned plane 4
Vibrations pass on fixed support 14 after the shock-absorbing ball 18 that is installed on fixed support 14 absorb, prevent vibrations to be transmitted to prevent
In vibration motor mounting seat 17 so that the vibrations of unmanned plane 14 do not interfere with the gondola of vibration-proof motor mounting seat less than 17, carry
High stabilization ability.
Further, the first motor 12 output shaft connects contiguous block 13, and this contiguous block 13 is connected with the first support 11.Its
In, contiguous block 13 has the function of slide rail, so that the first support 11 can adjust first in the enterprising line slip of contiguous block 13
Frame 11 is with the position of contiguous block 13, thus adjusts the center of gravity of gondola.
One end of first support 11 is arranged on the first motor 12, to control 11 turns of the first support by the first motor 12
Dynamic.Further, the first L-shaped shape of support.Specifically, the first motor 12 controls the direction of the first support 11 rotation is " boat
To ", this course is the direction that the photographic head on gondola is observed to the left or to the right.
One end of second support 2 is hinged to be arranged on first support 11 other end away from the first motor 12, and wherein second
The U-shaped shape of support 2.Wherein the second support 2 is provided with the second motor 21, the second motor 21 and first near one end of the first support 11
The other end of support 14 is hinged, rotates controlling the second support 2 by the second motor 21.Further, the second support 2 includes rotation
Bull stick 22 and the connecting rod 23 being arranged on swingle 22 two ends, the second motor 21 is arranged in swingle 22, specifically, the second electricity
Machine 21 is arranged on the centre position of swingle 22.Wherein, connecting rod 23 is provided with clamp cap 24.
In the present embodiment, it is " roll " that the second motor 21 controls the direction of the second support 2 rotation, and this roll is on gondola
Photographic head to clockwise or counterclockwise direction observe direction.
Module of taking photo by plane 3 is hinged to be arranged on second support 2 other end away from the first support 11, wherein, module of taking photo by plane 3 in
Ball shape, module of taking photo by plane 3 is provided with photographic head, is used for shooting picture or video.Further, module of taking photo by plane 3 is folded in connecting rod
Between 23.Module of taking photo by plane 3 is provided with the 3rd motor 34, and the 3rd motor 34 is hinged with the other end of the second support 2, with by the 3rd electricity
Machine 34 controls module 3 of taking photo by plane and rotates.Preferably, module of taking photo by plane 3 is arranged with the first side 31 and the second side 32, the 3rd motor
34 are separately positioned on the first side 31 and the second side 32, and further, the 3rd motor 34 is hinged with clamp cap 24.More enter one
Step ground, module of taking photo by plane 3 is provided with the 3rd side 33, the 3rd side 33 is arranged at intervals with photographic head and infrared lamp 37.Photographic head bag
Include visible image capturing 35 and infrared thermal imaging camera 36.In the present embodiment, infrared lamp 37 and infrared thermal imaging camera
The setting of 36, make use of the penetration power of infrared light 37 by force and by day can the characteristic of good imaging with night so that this reality
Can also photograph image clearly with novel at night, shooting effect is good.
Specifically, the 3rd motor 34 control to take photo by plane direction that module 3 rotates is for " pitching ", and this pitching is the shooting on gondola
The direction that head is observed up or down.
In the present embodiment, the photographic head on gondola can be carried out on " course ", " roll " and " pitching " three directions in the past
Motion, to reach the optimum efficiency of shooting.
This unmanned plane, owing to have employed technique scheme, has the advantage jolted overcoming aircraft self.When unmanned
When jolting on machine " pitching " direction, the 3rd motor 34 of the double photoelectric nacelle of airborne stabilization rotates, and drives module of taking photo by plane to rotate, rotates
That jolts in direction and unmanned plane pitch orientation is in opposite direction, and angle is identical, so that the double photoelectric nacelle shooting of airborne stabilization
Head pitch orientation upper angle is constant.In like manner, unmanned plane can also overcome jolting in " roll " direction and " course " direction.Specifically
Ground, during unmanned plane during flying, " pitching ", " roll " and " course " three directions all can change always, and this change is by mould of taking photo by plane
Gyroscope in block and figure pass the gyroscope collection in rainproof shell 1, then are analyzed by the cradle head control plate 16 in the first support 1
And command first motor the 12, second motor 21 and the 3rd motor 34 to rotate, keep stablizing of the photographic head shooting direction on gondola.
This utility model in the specific implementation, before and after the shell of module of taking photo by plane 3 is divided into the first side 31 and the second side 32
Two sides, the gap between two sides uses marine glue waterproof.3rd motor 34 is closely coupled with the hole of two sides and makes
Using marine glue filling chink, the water that module of taking photo by plane 3 is possible to prevent all directions to splash and comes immerses.Figure passes rainproof shell 1 top and uses
Carbon fiber board covers, and bottom the first support 11 is covered by thin carbon fiber board, and inside is trough, and this master drawing passes rainproof shell 1 to be prevented
Rain or the water preventing the direction being less than 60 degree with vertical angle from being sprayed immerse and electrically cause damage.
Module of taking photo by plane 3 is provided with visible image capturing 35 and infrared thermal imaging camera 36.When equipment uses, photographic head leads to
Electricity, signal is passed in 15 by the incoming figure of holding wire and passes to the external world with wireless form again.Infrared lamp 37 launches infrared radiation source outward
The brightness on boundary improves to realize the shooting of visible image capturing 35 pairs dim environment at night.
To sum up, the gondola of unmanned plane disclosed in the utility model can allow unmanned plane in the stable shooting of complex condition
Or observation ambient conditions, can work under rainy day environment, infrared thermal imaging can be clapped, night can also photograph shadow clearly
Picture, and image shake is the least, shooting effect is good.
The foregoing is only embodiment of the present utility model, not thereby limit the scope of the claims of the present utility model, all
It is the equivalent structure utilizing this utility model description and accompanying drawing content to be made or equivalence flow process conversion, or directly or indirectly uses
In the technical field that other are relevant, the most in like manner it is included in scope of patent protection of the present utility model.
Claims (10)
1. the gondola of a unmanned plane, it is characterised in that including:
Figure passes rainproof shell, and for being arranged on the body of described unmanned plane, wherein, described figure passes rainproof shell and is provided with the first motor；
First support, its one end is arranged on described first motor, to be turned by described first motor described first support of control
Dynamic；
Second support, its one end is hinged to be arranged on described first support other end away from described first motor；
Take photo by plane module, hinged be arranged on described second support other end away from described first support, wherein said mould of taking photo by plane
Block is provided with photographic head, is used for shooting picture or video；
Wherein, described second support is provided with the second motor near one end of described first support, described second motor and described the
The other end of one support is hinged, to control described second holder pivots by described second motor.
Gondola the most according to claim 1, it is characterised in that described in module of taking photo by plane be provided with the 3rd motor, described 3rd electricity
Machine is hinged with the other end of described second support, to be rotated by module of taking photo by plane described in described 3rd motor control.
Gondola the most according to claim 2, it is characterised in that described figure is provided with shock-absorbing ball and props up with fixing in passing rainproof shell
Frame, described shock-absorbing ball is arranged on described fixed support, and described fixed support is for being arranged on the body of described unmanned plane.
Gondola the most according to claim 2, it is characterised in that described second support includes swingle and is arranged on described rotation
The connecting rod at bull stick two ends, described second motor is arranged in described swingle, described in module clip of taking photo by plane be located at described connecting rod
Between.
Gondola the most according to claim 4, it is characterised in that described in module symmetry of taking photo by plane be provided with the first side and the second side
Face, described 3rd motor is separately positioned on described first side and described second side, and described connecting rod is provided with clamp cap, institute
State clamp cap hinged with described 3rd motor.
Gondola the most according to claim 5, it is characterised in that described in module of taking photo by plane be provided with the 3rd side, described 3rd side
Photographic head and infrared lamp it is arranged at intervals with on face.
Gondola the most according to claim 6, it is characterised in that described photographic head includes that visible image capturing head becomes with infra-red heat
As photographic head.
Gondola the most according to claim 1, it is characterised in that it is cylindrical that described figure passes rainproof shell.
Gondola the most according to claim 1, it is characterised in that the described first L-shaped shape of support, described second support is U
Type shape.
Gondola the most according to claim 1, it is characterised in that described in take photo by plane module shape spherical in shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620847934.3U CN205872506U (en) | 2016-08-04 | 2016-08-04 | Unmanned aerial vehicle's nacelle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620847934.3U CN205872506U (en) | 2016-08-04 | 2016-08-04 | Unmanned aerial vehicle's nacelle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205872506U true CN205872506U (en) | 2017-01-11 |
Family
ID=57701972
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620847934.3U Expired - Fee Related CN205872506U (en) | 2016-08-04 | 2016-08-04 | Unmanned aerial vehicle's nacelle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205872506U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110294137A (en) * | 2019-07-15 | 2019-10-01 | 深圳市科卫泰实业发展有限公司 | A kind of overall package structure convenient for the fast quick-detach of fixed-wing gondola |
| CN111717406A (en) * | 2020-06-17 | 2020-09-29 | 中国人民解放军陆军工程大学 | Unmanned aerial vehicle image acquisition system |
| CN111824442A (en) * | 2020-08-18 | 2020-10-27 | 广东北研航空遥感科技有限公司 | Multifunctional unmanned aerial vehicle |
| CN111891370A (en) * | 2019-05-06 | 2020-11-06 | 广州成至智能机器科技有限公司 | Unmanned aerial vehicle shooting device |
| CN112804433A (en) * | 2017-10-31 | 2021-05-14 | 深圳市大疆创新科技有限公司 | Cloud platform camera, cloud platform device and unmanned vehicles |
| CN113867377A (en) * | 2021-09-29 | 2021-12-31 | 重庆大学 | ROS-based vision quad-rotor unmanned aerial vehicle and development system thereof |
-
2016
- 2016-08-04 CN CN201620847934.3U patent/CN205872506U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112804433A (en) * | 2017-10-31 | 2021-05-14 | 深圳市大疆创新科技有限公司 | Cloud platform camera, cloud platform device and unmanned vehicles |
| CN111891370A (en) * | 2019-05-06 | 2020-11-06 | 广州成至智能机器科技有限公司 | Unmanned aerial vehicle shooting device |
| CN110294137A (en) * | 2019-07-15 | 2019-10-01 | 深圳市科卫泰实业发展有限公司 | A kind of overall package structure convenient for the fast quick-detach of fixed-wing gondola |
| CN110294137B (en) * | 2019-07-15 | 2024-02-23 | 深圳市科卫泰实业发展有限公司 | Integral packaging structure convenient for quick disassembly of fixed wing nacelle |
| CN111717406A (en) * | 2020-06-17 | 2020-09-29 | 中国人民解放军陆军工程大学 | Unmanned aerial vehicle image acquisition system |
| CN111717406B (en) * | 2020-06-17 | 2021-10-01 | 中国人民解放军陆军工程大学 | Unmanned aerial vehicle image acquisition system |
| CN111824442A (en) * | 2020-08-18 | 2020-10-27 | 广东北研航空遥感科技有限公司 | Multifunctional unmanned aerial vehicle |
| CN113867377A (en) * | 2021-09-29 | 2021-12-31 | 重庆大学 | ROS-based vision quad-rotor unmanned aerial vehicle and development system thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170111 Termination date: 20180804 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |