CN207181919U - A kind of rotary single-lens oblique photograph device for airborne vehicle - Google Patents
A kind of rotary single-lens oblique photograph device for airborne vehicle Download PDFInfo
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- CN207181919U CN207181919U CN201720809565.3U CN201720809565U CN207181919U CN 207181919 U CN207181919 U CN 207181919U CN 201720809565 U CN201720809565 U CN 201720809565U CN 207181919 U CN207181919 U CN 207181919U
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- 230000003287 optical effect Effects 0.000 claims abstract description 11
- 230000007935 neutral effect Effects 0.000 claims description 5
- 238000009434 installation Methods 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract description 8
- 238000010586 diagram Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 5
- 230000000903 blocking effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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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
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- 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
- 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
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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
- G01C11/02—Picture taking arrangements specially adapted for photogrammetry or photographic surveying, e.g. controlling overlapping of pictures
-
- 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
-
- 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 rotary single-lens oblique photograph device for airborne vehicle, and it includes:Eyeglass mechanism, supporting mechanism, camera;Eyeglass mechanism includes rotary turnplate, the first power part and some reflective mirrors, reflective mirror and is installed in rotary turnplate, and reflective mirror is installed in rotary turnplate in different angle;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;First power part drives rotary turnplate rotation, drives the reflective mirror of different angle to be moved to camera front end;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 utility model realizes the oblique photograph in camera different angle by the optical axis of the reflective mirror change camera in different spaces angle, and its device is simple, in light weight, does not influence shooting effect, easy to operation.
Description
Technical field
It the utility model is related to a kind of rotary single-lens oblique photograph device for airborne vehicle.
Background technology
Oblique photograph automation modeling technology is the height that international remote sensing in recent years develops rapidly with survey field
New technology.Currently, lot of domestic and foreign surveying and mapping unit and widely used this technology of relevant enterprise produce three-dimensional modeling data, and
Progressively substitute traditional-handwork modeling, turn into the important way of new threedimensional model production.
More rich geography information can be provided the user based on the large scene outdoor scene threedimensional model for tilting image, it is more friendly
Consumer's Experience, at home and abroad welcome extensively.But technology slower development, the Difficulty, it is largely determined by acquisition and tilts
The filming apparatus of image.
Chinese patent 201510018429.8 discloses one kind, discloses a kind of 5 camera lens oblique photograph aerial surveying cameras, it includes
Support and be fixed on lower on support depending on, left view, the right side regard, 5 forward sight, backsight inclination camera lenses.
Chinese patent 201520440596.7 discloses a kind of unmanned plane oblique photograph device, including positive camera, just
Camera side is provided with support, and support is provided with rotatable rotating mechanism, inclined camera is fixed with rotating mechanism.
Chinese patent 201511027220.4 discloses the side that a kind of unmanned plane rotary head multi-angle oblique photography is taken photo by plane
Method.Single camera is arranged on rotary head by it, and when unmanned plane, which reaches, takes pictures, cradle head control plate passes through shutter line traffic control
Camera is taken pictures, and after receiving camera feedback signal, cradle head control plate is rotated by motor control head, and is taken pictures again, until complete
Into the photograph collection of three angles.After aircraft landing, head is manually rotated by 90 ° installation, flies one again along course line before
Sortie, you can complete the data acquisition of five angles.
The defects of aforesaid way, is:
1st, the oblique photograph device of 5 cameras is carried, main screw lift can be heavier, it is necessary to which being carried using large aircraft is made
With this limitation can cause use cost small compared with high, less efficient and application;
2nd, one camera oblique photograph collection all using certain driving part and pedestal enable camera tilt and rotate from
And oblique photograph is realized, because camera weight is heavier, when driving camera is tilted or rotated or certain vibrations are produced, influence phase
Machine shooting effect, image is modeled and handled to the later stage and produces certain difficulty.
3rd, the multi-angle oblique camera that head carries, because the control head rotation of its cradle head control plate is taken pictures, and
And need aircraft landing manually to be rotated after completing three angles, its complex operation, control is difficult, it is difficult to be promoted with extensively
General application.
4th, camera rotation period is grown, and under the requirement of certain Duplication, shooting efficiency and quality can decline.
Therefore, how to provide one kind can wing drop photography and lighter in weight, do not influence the inclination of camera shooting effect
Camera, which becomes industry, to be needed to solve the problems, such as.
Utility model content
In view of the shortcomings of the prior art, the purpose of this utility model is to provide a kind of for the rotary single-lens of airborne vehicle
Oblique photograph device, it uses a camera, and oblique photograph is realized using the different direction of illumination of reflective mirror, lighter in weight, no
Camera shooting effect is influenceed, it is easy to operation.
To achieve these goals, the utility model provides a kind of rotary single-lens oblique photograph device, and it includes:
Eyeglass mechanism, supporting mechanism, camera;
Eyeglass mechanism includes rotary turnplate, the first power part and some reflective mirrors, and the driving rotation of the first power part turns
Disk, reflective mirror are installed in rotary turnplate, and reflective mirror is installed in rotary turnplate in different angle;
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;
First power part drives rotary turnplate rotation, before rotary turnplate drives the reflective mirror of different angle to be moved to camera
End;Second power part band follower link is swung, and connector drives reflective mirror and camera to swing;So as to change the shooting side of camera
To.
The utility model drives rotary turnplate to rotate by the first power part, makes reflective in three different spaces angles
Mirror is moved to the front end of camera, and the oblique photograph of camera, three angles are realized by the optical axis of the angulation change camera of reflective mirror
After the completion of shooting, the rotation for leading to rear connectors drives camera and reflective mirror rotation position together, completes the bat of the other three angle
Take the photograph, whole process realizes the shooting of forward downward, the back lower place, underface, five lower left, lower right directions, meets three
Tie up the demand of solid modelling.
The utility model is by increasing reflective mirror, rotary turnplate, the first power part, the second power part, connector etc.
Simple equipment, it is the shooting that multiple different angles can be achieved using a camera, shooting angle is various, and weight of equipment is light, boat
The electrical connection of pocket is without motion, and failure risk is small, and reliability is high, shakes during rotation small, and the shooting effect of complete machine is influenceed
It is small.
According to another embodiment of the utility model, reflective mirror number is three, and reflective mirror passes through connecting rod and rotation
Rotating disk is fixedly connected.
According to another embodiment of the utility model, three reflective mirror setting angles are fixed, and make the light of camera respectively
Axle points to front lower place, the back lower place, underface.
According to another embodiment of the utility model, reflective mirror is arranged on the edge or outside of rotary turnplate.
It is horizontal positioned according to another embodiment of the utility model, rotary turnplate.
According to another embodiment of the utility model, the first power part is arranged on the top or bottom of rotary turnplate
Portion, the output shaft of the first power part are fixedly connected with rotary turnplate.
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.
According to another embodiment of the utility model, number of cameras is one, and camera is fixedly connected with connector.
According to another embodiment of the utility model, camera is horizontal camera.
According to another embodiment of the utility model, camera and eyeglass mechanism are connected with supporting mechanism, support machine
Structure connects airborne vehicle.
Shooting process of the present utility model is, it may for example comprise following steps:
1st, drive the first power part to drive rotary turnplate rotation, the reflective mirror of three different angles is rotated to phase successively
The front end of machine is shot, complete forward downward, to underface, to the photography in the angle of the back lower place three;
2nd, drive the second power part band follower link to swing to the left or to the right, after position is stable, is shot, led to again
The driving rotary turnplate rotation of the first power part is crossed, the reflective mirror of three different angles is rotated to the front end progress of camera successively
Shooting, complete to the left lower section, to underface, the photography in three angles 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, drive reflective mirror to rotate by rotary turnplate, change the optical axis of camera by reflective mirror, so as to change camera
Shooting direction, it shakes small and need not install multiple cameras when rotating, and easy to operate, whole device is in light weight, does not influence to navigate
The flight of pocket.
2nd, camera is fixed with respect to mirror position, and the shooting in five directions disclosure satisfy that the needs of three-dimensional modeling, angle of oscillation
Degree is few, angle stabilization, does not influence the shooting effect of camera, and photograph distortion is small, and modeling accuracy is high.
3rd, during tilt, it is electrically connected without motion, and failure risk is small, and reliability is high.
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 rotary single-lens oblique photograph device 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 rotary single-lens oblique photograph device for airborne vehicle is present embodiments provided,
It includes:First power part 1, the second power part 2, connector 3, reflective mirror 4, camera 5, rotary turnplate 6.
Eyeglass mechanism includes the first power part 1, reflective mirror 4, rotary turnplate 6, and the number of wherein reflective mirror 4 has three,
Three reflective mirrors 4 are installed in rotary turnplate 6, and reflective mirror 4 is installed in rotary turnplate 6 in different space angles.
In the present embodiment, three setting angles of reflective mirror 4 are fixed, make respectively camera optical axis point to front lower place, the back lower place,
Underface.
Rotary turnplate 6 is located at the front end of camera 5, and eyeglass mechanism rotates the reflective mirror 4 that three different spaces angles are installed
And the front end of camera 5 is aligned, the optical axis of camera 5 is projected on reflective mirror 4.First power part 1 is rotary turnplate 6
The power drive of rotation is provided.
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, camera 5 and eyeglass mechanism are respectively fixedly connected with and connected on aircraft in the both ends of connector 3, supporting mechanism.
Connector 3 is neutral straight, the reclinate bar in both ends, and the output shaft of the second power part 2 is connected to connector 3
Neutral straight position.Connector 3 is main support member in supporting mechanism, to avoid blocking regarding for camera 5 and reflective mirror 4
Line influences shooting, and connector 3 is located at the upper end of camera 5 and eyeglass mechanism and is connected with airborne vehicle, and connector 3 is one with one
Determine the bar of rigidity and intensity, for supporting camera 5 and rotary turnplate 6, maintain camera 5 and rotary turnplate 6 in high-altitude opening position
Stable and normal work.
The drive connection part 3 of second power part 2 is swung, and connector 3 drives rotary turnplate 6 and camera 5 to swing.
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, and reflective mirror 4 is located on the optical axis of camera 5.
Rotary turnplate 6 rotates under the driving of the first power part 1, drives the reflective mirror 4 of different spaces angle to revolve successively
The front end of camera 5 is gone to, the optical axis of the camera of camera 5 passes through the reflection of reflective mirror 4, changes shooting direction.
Preferably, rotary turnplate 6 is horizontal positioned, and the first power part 1 is arranged on the top of rotary turnplate 6, the first power
The output shaft of part 1 is fixedly connected with rotary turnplate 6.Connector 3 is connected to the top of the first power part 1.
Preferably, to avoid rotary turnplate 6 from blocking the sight of camera 5 and reflective mirror 4, reflective mirror 4 is arranged on rotary turnplate 6
Edge or outside.
In the present embodiment, the number of camera 5 is one, and camera 5 is fixedly connected with connector 3.The middle of connector 3 connects
In on airborne vehicle, one end connection camera 5 at both ends, one end connection rotary turnplate 6, plays support and firm camera 5 and rotation turns
The effect of disk 6.
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.
The shooting process of the present embodiment is, for example, comprising the following steps:
1st, drive the first power part 1 to drive rotary turnplate rotation, the reflective mirror 4 of three different angles is rotated to successively
The front end of camera 5 is shot, complete forward downward, to underface, to the photography in the angle of the back lower place three;
2nd, the second power part 2 of driving rotates to the left or to the right with follower link 3, after position is stable, is shot, again
Drive the first power part 1 to rotate, the reflective mirror of three different angles is rotated to the front end of camera 5 successively and shot, it is complete
Into to the left lower section, to underface, the photography in three angles 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 three reflective mirrors 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 different angle of reflective mirror, using minimum phase
Machine quantity, the effective weight for mitigating oblique photograph device, is advantageous to aeroplane photography;Simultaneously because rotate reflective mirror, its quality
Gently, vibrations during rotation 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 motion, failure risk is small, and reliability is high, and photograph distortion is small, and modeling accuracy is high.It can have in aviation oblique photograph field
Widely 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 rotary single-lens oblique photograph device for airborne vehicle, it is characterised in that described rotary single-lens to incline
Oblique camera includes:Eyeglass mechanism, supporting mechanism, camera;
The eyeglass mechanism includes rotary turnplate, the first power part and some reflective mirrors, and first power part drives institute
Rotary turnplate is stated, some reflective mirrors are installed in the rotary turnplate, and the reflective mirror is in the rotary turnplate
Different angle is installed;
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;
First power part drives the rotary turnplate rotation, and the rotary turnplate drives the reflective mirror of the different angle
It is moved to the camera front end;Second power part drives the connector to swing, and the connector drives described reflective
Mirror and the camera are swung;So as to change the shooting direction of the camera.
2. rotary single-lens oblique photograph device as claimed in claim 1, it is characterised in that the reflective mirror number is three
Individual, the reflective mirror is fixedly connected by connecting rod with the rotary turnplate.
3. rotary single-lens oblique photograph device as claimed in claim 2, it is characterised in that three reflective mirrors installation
Angle is fixed, and the optical axis of the camera is pointed to front lower place, the back lower place, underface respectively.
4. rotary single-lens oblique photograph device as claimed in claim 2, it is characterised in that the reflective mirror is arranged on institute
State the edge or outside of rotary turnplate.
5. rotary single-lens oblique photograph device as claimed in claim 1, it is characterised in that the rotary turnplate level is put
Put.
6. rotary single-lens oblique photograph device as claimed in claim 1, it is characterised in that the first power part peace
Mounted in the top of the rotary turnplate or bottom, the output shaft of first power part is fixedly connected with the rotary turnplate.
7. rotary single-lens oblique photograph device 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.
8. rotary single-lens oblique photograph device as claimed in claim 1, it is characterised in that the number of cameras is one
Platform, the camera are fixedly connected with the connector.
9. rotary single-lens oblique photograph device as claimed in claim 1, it is characterised in that the camera is horizontal phase
Machine.
10. rotary single-lens oblique photograph device as claimed in claim 1, it is characterised in that the camera and the mirror
Piece 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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CN207181919U true CN207181919U (en) | 2018-04-03 |
Family
ID=60196799
Family Applications (40)
Application Number | Title | Priority Date | Filing Date |
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CN201720809625.1U Active CN207181921U (en) | 2017-04-25 | 2017-07-05 | A kind of shaft 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 |
CN201720809565.3U Active CN207181919U (en) | 2017-04-25 | 2017-07-05 | A kind of rotary single-lens 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 |
CN201720809659.0U Active CN207181922U (en) | 2017-04-25 | 2017-07-05 | A kind of rotating disc type lens supports for camera multi-angled shooting |
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 |
CN201710542705.XA Pending CN107576312A (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph method at 12 visual angles for airborne vehicle |
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 |
CN201720809495.1U Active CN207366911U (en) | 2017-04-25 | 2017-07-05 | A kind of reflective twin-lens bi-axial tilt camera 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 |
CN201720809492.8U Active CN207113870U (en) | 2017-04-25 | 2017-07-05 | A kind of fixed one camera oblique photograph device for airborne vehicle |
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 |
CN201710542218.3A Pending CN107380471A (en) | 2017-04-25 | 2017-07-05 | A kind of double camera rotating disc type 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 |
CN201720809475.4U Active CN207106926U (en) | 2017-04-25 | 2017-07-05 | A kind of double camera 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 |
CN201710542576.4A Pending CN107390453A (en) | 2017-04-25 | 2017-07-05 | A kind of reflective single-lens bi-axial tilt camera for airborne vehicle |
CN201710542197.5A Pending CN107340672A (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens oblique photograph device for airborne vehicle |
CN201720809537.1U Active CN207113869U (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph device for airborne vehicle |
CN201710542722.3A Pending CN107329363A (en) | 2017-04-25 | 2017-07-05 | A kind of method of six visual angle oblique photographs of double camera for airborne vehicle |
CN201710541954.7A Pending CN107367263A (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph device for airborne vehicle |
CN201710542560.3A Pending CN107685871A (en) | 2017-04-25 | 2017-07-05 | A kind of block form double camera rotating disc type 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 |
CN201720809536.7U Active CN207360596U (en) | 2017-04-25 | 2017-07-05 | A kind of opposed double camera rotating disc type oblique photograph device for aircraft |
CN201710541936.9A Pending CN107367886A (en) | 2017-04-25 | 2017-07-05 | A kind of rotary single-lens oblique photograph device for airborne vehicle |
CN201710541937.3A Pending CN107340670A (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens single-axis tilt camera 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 |
CN201710542329.4A Pending CN107390451A (en) | 2017-04-25 | 2017-07-05 | A kind of rotating disc type lens supports for camera multi-angled shooting |
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 |
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CN107367886A (en) * | 2017-04-25 | 2017-11-21 | 广州市红鹏直升机遥感科技有限公司 | A kind of rotary single-lens oblique photograph device for airborne vehicle |
CN109188851A (en) * | 2018-09-19 | 2019-01-11 | 白荣超 | The spaceborne imaging system of large format |
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