CN207181918U - A kind of single-lens single-axis tilt camera for airborne vehicle - Google Patents
A kind of single-lens single-axis tilt camera for airborne vehicle Download PDFInfo
- Publication number
- CN207181918U CN207181918U CN201720809528.2U CN201720809528U CN207181918U CN 207181918 U CN207181918 U CN 207181918U CN 201720809528 U CN201720809528 U CN 201720809528U CN 207181918 U CN207181918 U CN 207181918U
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- camera
- reflective mirror
- power part
- connector
- axis tilt
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- 230000007246 mechanism Effects 0.000 claims abstract description 49
- 230000003287 optical effect Effects 0.000 claims abstract description 12
- 230000003028 elevating effect Effects 0.000 claims abstract description 7
- 230000008859 change Effects 0.000 claims abstract description 6
- 230000007935 neutral effect Effects 0.000 claims description 4
- 238000000034 method Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 6
- 230000008569 process Effects 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 230000001965 increasing effect Effects 0.000 description 3
- 230000000903 blocking effect Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000000116 mitigating effect Effects 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 230000003044 adaptive effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000035800 maturation Effects 0.000 description 1
Classifications
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- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B17/00—Details of cameras or camera bodies; Accessories therefor
- G03B17/02—Bodies
- G03B17/17—Bodies with reflectors arranged in beam forming the photographic image, e.g. for reducing dimensions of camera
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B37/00—Panoramic or wide-screen photography; Photographing extended surfaces, e.g. for surveying; Photographing internal surfaces, e.g. of pipe
- G03B37/04—Panoramic or wide-screen photography; Photographing extended surfaces, e.g. for surveying; Photographing internal surfaces, e.g. of pipe with cameras or projectors providing touching or overlapping fields of view
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C11/00—Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
- G01C11/02—Picture taking arrangements specially adapted for photogrammetry or photographic surveying, e.g. controlling overlapping of pictures
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C11/00—Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
- G02B7/18—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
- G02B7/182—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
- G02B7/1821—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors for rotating or oscillating mirrors
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
- G02B7/18—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
- G02B7/182—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
- G02B7/198—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors with means for adjusting the mirror relative to its support
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/50—Constructional details
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/50—Constructional details
- H04N23/55—Optical parts specially adapted for electronic image sensors; Mounting thereof
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Multimedia (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Optics & Photonics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Signal Processing (AREA)
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
- Stereoscopic And Panoramic Photography (AREA)
Abstract
The utility model provides a kind of single-lens single-axis tilt camera for airborne vehicle, and it includes:Eyeglass mechanism, supporting mechanism, camera;Eyeglass mechanism includes reflective mirror, reflector bracket and the first power part, and reflective mirror and the first power part are arranged on reflector bracket, the output axis connection of reflective mirror and the first power part;Supporting mechanism includes the second power part and connector, and the output shaft of the second power part is fixedly connected with connector;Camera is arranged at the rear of eyeglass mechanism, and reflective mirror is arranged on the optical axis of camera;Camera and eyeglass mechanism are respectively fixedly connected with to be connected on aircraft in the both ends of connector, supporting mechanism;Reflective mirror is driven to do elevating movement by the first power part;Second power part band follower link is swung, and connector drives reflective mirror and camera to swing;So as to change the shooting direction of camera.The optical axis that the utility model changes camera by reflective mirror realizes multi-angled shooting, and weight of equipment is light, and reliability is high, easy to operate.
Description
Technical field
It the utility model is related to a kind of single-lens single-axis tilt camera for airborne vehicle.
Background technology
Maturation and extensive use with aviation flight technology, increasing user begin to use airborne vehicle as aviation
The carrier of photography.Airborne vehicle can carry out controllable flight in endoatmosphere, and height is carried out by carrying picture pick-up device in flying platform
Sky photography.A usual picture pick-up device can only be shot from a direction, needed from the different directions such as vertical, inclination
When gathering imaging material, a simple picture pick-up device just can not accomplish the task satisfactorily.
Oblique photograph technology is the new and high technology that international survey field grew up in recent years, and it had been overturned in the past just
The limitation that projection picture can only be shot from vertical angle, can be from five different angle acquisition images such as vertical, inclinations, by user
Introduce the true world directly perceived for meeting human eye vision.
The main method used at present is that multiple built-in cameras are installed in aeroplane photography device, passes through the pendulum of different angle
Put, realize multiple angle shots, to obtain the panoramic image on ground.In order to reduce main screw lift and cost, generally use rotates
Built-in camera realizes multi-angled shooting, to reduce built-in camera quantity.
The major defect of above-mentioned technical proposal has:
The 1st, multiple cameras are installed in airborne vehicle, to realize the shooting of full angular, it usually needs downward, forward and backward, left,
The camera of right five directions shooting, it is necessary to five built-in cameras are installed on an airborne vehicle, and the angle photographed has
Limit.Because the volume and weight of camera is larger, the weight that airborne vehicle is capable of carrying equipment also has certain limitation.And airborne vehicle
Weight increase, to maintain the balance of airborne vehicle and stability, it is necessary to consume more energy, is unfavorable for the flight of airborne vehicle.
2nd, multi-angled shooting is realized using rotation built-in camera, because the volume and weight of built-in camera itself is larger, turned
It can cause complete machine vibrations also larger when dynamic, while also increase the consumption of electricity, be unfavorable for aeroplane photography.
3rd, camera rotation period is grown, and under the requirement of certain Duplication, shooting efficiency and quality can decline.
Utility model content
In view of the shortcomings of the prior art, the purpose of this utility model is to provide a kind of single-lens single shaft for airborne vehicle and inclined
Oblique camera, its built-in camera and camera angle automatically switch, and simultaneously effective mitigation aviation easy to operation, which tilts, takes the photograph
The weight of image device, is adaptive to aeroplane photography.
To achieve these goals, the utility model provides a kind of single-lens single-axis tilt photography dress for airborne vehicle
Put, it includes:Eyeglass mechanism, supporting mechanism, camera;
Eyeglass mechanism includes reflective mirror, reflector bracket and the first power part, reflective mirror and the installation of the first power part
On reflector bracket, the output axis connection of reflective mirror and the first power part;
Supporting mechanism includes the second power part and connector, and the output shaft and connector of the second power part, which are fixed, to be connected
Connect;
Camera is arranged at the rear of eyeglass mechanism, and reflective mirror is arranged on the optical axis of camera;
Camera and eyeglass mechanism are respectively fixedly connected with to be connected on aircraft in the both ends of connector, supporting mechanism;Pass through
First power part drives reflective mirror to do elevating movement;Second power part band follower link is swung, and connector drives reflective mirror
Swung with camera;So as to change the shooting direction of camera.
In the utility model, by camera front end increase an eyeglass mechanism, reflective mirror do elevating movement realize camera to
Under just, to it is front lower, to the back lower place to shooting, the elevating movement of reflective mirror driven by the first power part.
In the utility model, support and connect camera and reflective mirror by supporting mechanism, camera and reflective mirror simultaneously with
Supporting mechanism is swung in the horizontal direction, realize to left down, to the right to shooting, supporting mechanism to swing by second dynamic
Power part drives.
The utility model is by increasing reflective mirror, reflector bracket, the first power part, the second power part, connector
It is the shooting that multiple different angles can be achieved using a camera etc. simple equipment, shooting angle is various, and weight of equipment is light,
It is electrically connected without motion, and failure risk is small, and reliability is high, shakes during rotation small, the shooting effect of complete machine is influenceed small.
According to another embodiment of the utility model, connector is neutral straight, the reclinate bar in both ends, second
The output shaft of power part is connected to connector neutral straight position.Connector is support member main in supporting mechanism, is
The sight for avoiding blocking camera and reflective mirror influences shooting, and connector is located at the upper end of camera and reflective mirror and connected with airborne vehicle
Connect, connector is a bar with certain rigidity and intensity, for supporting camera and reflective mirror, maintains camera and reflective mirror in height
Stabilization and normal work at empty position.
According to another embodiment of the utility model, camera is horizontal camera.Camera is laterally disposed, and reflective mirror is in phase
The front end of machine camera, the optical axis of camera camera are projected on reflective mirror, and the angle by adjusting reflective mirror realizes camera not
With the scene shooting in angle.
According to another embodiment of the utility model, number of cameras is one, and camera is fixedly connected with connector.Even
Fitting middle is connected on airborne vehicle, one end connection camera at both ends, plays a part of support and firm camera.
According to another embodiment of the utility model, reflective mirror number is one, and the angle of reflective mirror passes through first
The driving of power part is changeable.
According to another embodiment of the utility model, reflector bracket is bow, reflector bracket one end with it is anti-
Light microscopic is flexibly connected, and the reflector bracket other end is fixedly connected with the first power part, reflector bracket middle position and company
Fitting is fixedly connected.
According to another embodiment of the utility model, the output shaft of reflective mirror one end and the first power part, which is fixed, to be connected
Connect, the other end of reflective mirror is rockably mounted on reflector bracket.Reflective mirror needs to change different angles in shooting process
Degree, it is necessary to which power part is driven, therefore one end of reflective mirror is fixedly connected with the output shaft of the first power part, reflective
Mirror is swung with the motion of output shaft, while the other end needs to keep energy freely activity, therefore the other end is swingably installed
On reflector bracket.
According to another embodiment of the utility model, the output shaft of the first power part is defeated with the second power part
Shaft is orthogonal.Locus is a three-dimensional structure, and reflective mirror passes through the rotation in two mutually perpendicular directions, you can is realized
Projected at any angle in three dimensions.
According to another embodiment of the utility model, the angle of the optical axis of reflector bracket plane and camera in 0 °-
90 °, reflector bracket need to only meet that the minute surface of reflective mirror can be achieved to clap on the optical axis of camera horizontally or diagonally to set
Take the photograph.
According to another embodiment of the utility model, camera and eyeglass mechanism are connected with supporting mechanism, support machine
Structure connects airborne vehicle.Supporting mechanism is fixedly connected with photograph and eyeglass mechanism, will be whole as one with photograph and eyeglass mechanism
Body is connected on airborne vehicle, and airborne vehicle carries photograph and eyeglass mechanism realizes different angle oblique photograph on high-altitude.
Shooting process of the present utility model is, for example, comprising the following steps:
1st, the first power part rotates the shooting that reflective mirror carries out forward downward, be rotated further by a reflective mirror carry out to
The shooting of underface, it is rotated further the shooting once carried out to the back lower place;
2nd, the second power part rotates once (such as 90 °) to the left or to the right, and the first power part rotates three times, complete successively
Into lower section to the left, to underface, the shooting in the direction such as to the right.
In above-mentioned steps, the first power part, the second power part rotation order can be suitable according to different shooting direction
Sequence is adjusted, and is not limited to said sequence process.
Compared with prior art, the utility model possesses following beneficial effect:
1st, the shooting of camera different angle is realized by the rotation of reflective mirror, reflective mirror is in light weight, shake during rotation it is small, no
Influence the shooting effect of camera.
2nd, the equipment for adding reflective mirror, reflector bracket, the first power part, the second power part, connector etc., is adopted
It is the shooting for realizing different angle with a camera, increased weight of equipment is light, does not influence the flight of airborne vehicle.
3rd, built-in camera is fixed with respect to reflective mirror, and it is electrically connected without motion, and failure risk is small, and reliability is high, is used
It is simple to operate with implementing.
The utility model is described in further detail below in conjunction with the accompanying drawings.
Brief description of the drawings
Fig. 1 is the overall structure diagram of the single-lens single-axis tilt camera of embodiment 1;
Fig. 2 is the camera forward downward shooting schematic diagram of embodiment 1;
Fig. 3 is the camera schematic diagram of lower section shooting to the left of embodiment 1;
Fig. 4 is that the camera of embodiment 1 shoots schematic diagram to underface;
Fig. 5 is that the camera of embodiment 1 shoots schematic diagram to the right;
Fig. 6 is that the camera of embodiment 1 shoots schematic diagram to the back lower place;
Embodiment
Embodiment 1
As shown in figs 1 to 6, a kind of single-lens single-axis tilt camera for airborne vehicle is present embodiments provided, its
Including the first power part 1, the second power part 2, connector 3, reflective mirror 4, camera 5 and reflector bracket 6.
Eyeglass mechanism includes the first power part 1, reflective mirror 4, reflector bracket 6, and eyeglass mechanism is mainly used to realize instead
The fixation of light microscopic 4 and angular adjustment, reflector bracket 6 is used to install and fixed counter-mirror 4, and the first power part 1 is used to drive
Reflective mirror 4 is swung;
Supporting mechanism includes the second power part 2, connector 3, and supporting mechanism is used for connecting and supporting reflective mirror 4 and camera
5.Connector 3 is neutral straight, the reclinate bar in both ends, and the output shaft of the second power part 2 is connected to the centre of connector 3
Straight position.Connector 3 is support member main in supporting mechanism, and camera 5 and eyeglass mechanism are respectively fixedly connected with connection
The both ends of part 3.Shooting is influenceed to avoid blocking the sight of camera 5 and reflective mirror 4, and connector 3 is located at camera 5 and reflective mirror 4
Upper end and it is connected with airborne vehicle, connector 3 is a bar with certain rigidity and intensity, for supporting camera 5 and reflective mirror
4, camera 5 and reflective mirror 4 are maintained in the stabilization and normal work of high-altitude opening position.
The drive connection part 3 of second power part 2 rotates, and connector 3 drives reflective mirror 4 and camera 5 to rotate.
Camera 5 is used for shooting and gathering image data.
In the present embodiment, camera 5 is horizontal camera, and camera 5 is laterally put, reflective mirror 4 in the front end of the camera of camera 5,
The optical axis of the camera of camera 5 is projected on reflective mirror 4, and the angle by adjusting reflective mirror 4 realizes the scape in the different angle of camera 5
As shooting.
Reflective mirror 4 is made reflective by the driving of the first power part 1 and second 2 two orthogonal directions of power part
Mirror 4 switches different space angles.Locus is three-dimensional structure, reflective mirror 4 by the rotation in two mutually perpendicular directions,
It can be achieved to project at any angle in three dimensions.
In the present embodiment, one end of reflective mirror 4 is fixedly connected with the output shaft of the first power part 1, reflective mirror 4 it is another
End is rockably mounted on reflector bracket 6.Reflector bracket 6 is bow, and the one end of reflector bracket 6 is lived with reflective mirror 4
Dynamic connection, the other end of reflector bracket 6 are fixedly connected with the first power part 1, the middle position of reflector bracket 6 and connector
3 are fixedly connected.Reflective mirror 4 is needed to change different angles in shooting process, it is necessary to which power part is driven, therefore reflective
One end of mirror 4 is fixedly connected with the output shaft of the first power part 1, and reflective mirror 4 is swung with the motion of output shaft, while separately
One end needs to keep energy freely activity, therefore the other end is rockably mounted on reflector bracket 6.First power part 4 is defeated
Shaft only does elevating movement, and control reflective mirror 4 does elevating movement, realize under just, to it is front lower, to the back lower place to shooting.
In the present embodiment, camera 5 and eyeglass mechanism are connected with supporting mechanism, supporting mechanism connection airborne vehicle.Support machine
Structure is fixedly connected with photograph and eyeglass mechanism, will be integrally connected to photograph and eyeglass mechanism as one on airborne vehicle, boat
Pocket carries photograph and eyeglass mechanism realizes different angle oblique photograph on high-altitude.
Camera 5 and eyeglass mechanism are respectively fixedly connected with puts in the both ends of connector 3, the drive connection part 3 of the second power part 2
When dynamic, connector 3 drives camera 5 and eyeglass mechanism to swing, make reflective mirror 4 change the optical axis of camera 5 to it is front lower, under just,
To the back lower place to shooting become to left down, under just, the shooting in inferior direction to the right.
In the present embodiment, the angle of the optical axis of the plane of reflector bracket 6 and camera is in 0 ° of -90 ° of any angle, reflective mirror branch
Frame 6 need to only meet that shooting can be achieved in the minute surface of reflective mirror on the optical axis of camera horizontally or diagonally to set.
The shooting process of the present embodiment is, for example, comprising the following steps:
1st, the first power part 1 rotates a shooting that reflective mirror 4 carries out forward downward, is rotated further by a reflective mirror 4 and enters
Shooting of the row to underface, is rotated further the shooting once carried out to the back lower place;
2nd, the second power part 2 rotates once (such as 90 °) to the left or to the right, and the first power part 1 rotates three times, successively
Complete lower section to the left, to underface, the shooting in the direction such as to the right.
In above-mentioned steps, the first power part 1, the second power part 2 rotation order can be according to different shooting direction
Order is adjusted, and is not limited to said sequence process.
The present embodiment uses a camera 5 and a reflective mirror 4, carries some driving parts and support connection member, real
The multi-angle oblique photography of existing camera.The multi-angled shooting of camera is realized by the rotation of reflective mirror, using minimum camera number
Amount, the effective weight for mitigating oblique photograph device, is advantageous to aeroplane photography;Simultaneously because rotating reflective mirror, its light weight, turn
Vibrations when dynamic are small, and the shooting effect influence on complete machine is also small, and built-in camera is fixed with respect to reflective mirror, and it is electrically connected without fortune
It is dynamic, reduce failure risk, reliability is high, and photograph distortion is small, and modeling accuracy is high.It can have wider in aviation oblique photograph field
General application.
Although the utility model is disclosed above with preferred embodiment, the model of the utility model implementation is not limited to
Enclose.Any one of ordinary skill in the art, do not departing from invention scope of the present utility model, when a little improvement can be made,
I.e. every equal improvement done according to the utility model, should be the scope of the utility model and is covered.
Claims (10)
1. a kind of single-lens single-axis tilt camera for airborne vehicle, it is characterised in that the single-lens single-axis tilt is taken the photograph
Image device includes:Eyeglass mechanism, supporting mechanism, camera;
The eyeglass mechanism includes reflective mirror, reflector bracket and the first power part, the reflective mirror and first power
Part is arranged on the reflector bracket, the output axis connection of the reflective mirror and first power part;
The supporting mechanism includes the second power part and connector, the output shaft and the connector of second power part
It is fixedly connected;
The camera is arranged at the rear of the eyeglass mechanism, and the reflective mirror is arranged on the optical axis of the camera;
The camera and the eyeglass mechanism are respectively fixedly connected with is connected to boat in the both ends of the connector, the supporting mechanism
On pocket;
The reflective mirror is driven to do elevating movement by first power part;Second power part drives the connection
Part is swung, and the connector drives the reflective mirror and the camera to swing;So as to change the shooting direction of the camera.
2. single-lens single-axis tilt camera as claimed in claim 1, it is characterised in that the connector is middle flat
Directly, the reclinate bar in both ends, the output shaft of second power part are connected to the connector neutral straight position.
3. single-lens single-axis tilt camera as claimed in claim 1, it is characterised in that the camera is horizontal camera.
4. single-lens single-axis tilt camera as claimed in claim 1, it is characterised in that the number of cameras is one,
The camera is fixedly connected with the connector.
5. single-lens single-axis tilt camera as claimed in claim 1, it is characterised in that the reflective mirror number is one
It is individual.
6. single-lens single-axis tilt camera as claimed in claim 1, it is characterised in that the reflector bracket is arc
Bar, described reflector bracket one end are flexibly connected with the reflective mirror, the reflector bracket other end and first power
Part is fixedly connected, and the reflector bracket middle position is fixedly connected with the connector.
7. single-lens single-axis tilt camera as claimed in claim 1, it is characterised in that described reflective mirror one end with it is described
The output shaft of first power part is fixedly connected, and the other end of the reflective mirror is rockably mounted to the reflector bracket
On.
8. single-lens single-axis tilt camera as claimed in claim 1, it is characterised in that first power part it is defeated
The output shaft of shaft and second power part is orthogonal.
9. single-lens single-axis tilt camera as claimed in claim 1, it is characterised in that the reflector bracket plane with
The angle of the optical axis of the camera is in 0 ° -90 °.
10. single-lens single-axis tilt camera as claimed in claim 1, it is characterised in that the camera and the eyeglass
Mechanism is connected with the supporting mechanism, and the supporting mechanism connects airborne vehicle.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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CN201710277859 | 2017-04-25 | ||
CN2017102778590 | 2017-04-25 |
Publications (1)
Publication Number | Publication Date |
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CN207181918U true CN207181918U (en) | 2018-04-03 |
Family
ID=60196799
Family Applications (40)
Application Number | Title | Priority Date | Filing Date |
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CN201710542051.0A Pending CN107561831A (en) | 2017-04-25 | 2017-07-05 | The implementation method that a kind of one camera multi-angle oblique for airborne vehicle is photographed |
CN201720809561.5U Expired - Fee Related CN207742455U (en) | 2017-04-25 | 2017-07-05 | A kind of reflective single-lens bi-axial tilt camera for aircraft |
CN201710541937.3A Pending CN107340670A (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens single-axis tilt camera for airborne vehicle |
CN201720809528.2U Expired - Fee Related CN207181918U (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens single-axis tilt camera for airborne vehicle |
CN201710542576.4A Pending CN107390453A (en) | 2017-04-25 | 2017-07-05 | A kind of reflective single-lens bi-axial tilt camera for airborne vehicle |
CN201710541954.7A Pending CN107367263A (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph device for airborne vehicle |
CN201710542200.3A Pending CN107367265A (en) | 2017-04-25 | 2017-07-05 | A kind of reflective single-lens rotating disk oblique photograph device for airborne vehicle |
CN201710542703.0A Pending CN107390469A (en) | 2017-04-25 | 2017-07-05 | A kind of polyphaser camera for airborne vehicle |
CN201710541936.9A Pending CN107367886A (en) | 2017-04-25 | 2017-07-05 | A kind of rotary single-lens oblique photograph device for airborne vehicle |
CN201710542723.8A Pending CN107449401A (en) | 2017-04-25 | 2017-07-05 | The implementation method that a kind of multi-angle oblique for airborne vehicle is photographed |
CN201720809656.7U Expired - Fee Related CN207752284U (en) | 2017-04-25 | 2017-07-05 | A kind of one camera turntable oblique photograph device for aircraft |
CN201710542741.6A Pending CN107643649A (en) | 2017-04-25 | 2017-07-05 | A kind of implementation method of nine visual angle oblique photographs for airborne vehicle |
CN201710542558.6A Pending CN107390452A (en) | 2017-04-25 | 2017-07-05 | A kind of reflective twin-lens bi-axial tilt camera for airborne vehicle |
CN201720809495.1U Expired - Fee Related CN207366911U (en) | 2017-04-25 | 2017-07-05 | A kind of reflective twin-lens bi-axial tilt camera for aircraft |
CN201710542352.3A Pending CN107560601A (en) | 2017-04-25 | 2017-07-05 | A kind of implementation method of the visual angle oblique photograph of one camera five for airborne vehicle |
CN201710542641.3A Pending CN107364585A (en) | 2017-04-25 | 2017-07-05 | A kind of double camera oblique photograph device for airborne vehicle |
CN201720809659.0U Expired - Fee Related CN207181922U (en) | 2017-04-25 | 2017-07-05 | A kind of rotating disc type lens supports for camera multi-angled shooting |
CN201720809538.6U Expired - Fee Related CN207113871U (en) | 2017-04-25 | 2017-07-05 | A kind of reflective single-lens rotating disk oblique photograph device for airborne vehicle |
CN201720809493.2U Expired - Fee Related CN207764534U (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for aircraft |
CN201710542628.8A Pending CN107390454A (en) | 2017-04-25 | 2017-07-05 | A kind of shaft type lens supports for camera multi-angled shooting |
CN201720809677.9U Expired - Fee Related CN207360597U (en) | 2017-04-25 | 2017-07-05 | A kind of double camera rotating disc type oblique photograph device for aircraft |
CN201710542329.4A Pending CN107390451A (en) | 2017-04-25 | 2017-07-05 | A kind of rotating disc type lens supports for camera multi-angled shooting |
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CN201710542329.4A Pending CN107390451A (en) | 2017-04-25 | 2017-07-05 | A kind of rotating disc type lens supports for camera multi-angled shooting |
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CN201710542197.5A Pending CN107340672A (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens oblique photograph device for airborne vehicle |
CN201710542705.XA Pending CN107576312A (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph method at 12 visual angles for airborne vehicle |
CN201720809537.1U Expired - Fee Related CN207113869U (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph device for airborne vehicle |
CN201710542036.6A Pending CN107340671A (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for airborne vehicle |
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CN201720809565.3U Expired - Fee Related CN207181919U (en) | 2017-04-25 | 2017-07-05 | A kind of rotary single-lens oblique photograph device for airborne vehicle |
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CN201710542577.9A Pending CN107499525A (en) | 2017-04-25 | 2017-07-05 | A kind of opposed double camera rotating disc type oblique photograph device for airborne vehicle |
CN201710551944.1A Pending CN107367887A (en) | 2017-04-25 | 2017-07-05 | A kind of one camera rotating disk oblique photograph device for airborne vehicle |
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Publication number | Priority date | Publication date | Assignee | Title |
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CN107340670A (en) * | 2017-04-25 | 2017-11-10 | 广州市红鹏直升机遥感科技有限公司 | A kind of single-lens single-axis tilt camera for airborne vehicle |
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