CN107364585A - A kind of double camera oblique photograph device for airborne vehicle - Google Patents
A kind of double camera oblique photograph device for airborne vehicle Download PDFInfo
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- CN107364585A CN107364585A CN201710542641.3A CN201710542641A CN107364585A CN 107364585 A CN107364585 A CN 107364585A CN 201710542641 A CN201710542641 A CN 201710542641A CN 107364585 A CN107364585 A CN 107364585A
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- camera
- eyeglass
- lens set
- oblique photograph
- photograph device
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- 230000007246 mechanism Effects 0.000 claims abstract description 27
- 230000008859 change Effects 0.000 claims abstract description 7
- 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 claims description 19
- 230000033228 biological regulation Effects 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 4
- 238000013507 mapping Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
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- VMXUWOKSQNHOCA-UKTHLTGXSA-N ranitidine Chemical compound [O-][N+](=O)\C=C(/NC)NCCSCC1=CC=C(CN(C)C)O1 VMXUWOKSQNHOCA-UKTHLTGXSA-N 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
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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
-
- 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
- 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
-
- 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 invention provides a kind of double camera oblique photograph device for airborne vehicle, including：First camera, second camera, eyeglass mechanism, the power part for driving eyeglass mechanism；First camera is installed on aircraft, and second camera is installed on aircraft；Eyeglass mechanism includes the first lens set, the second lens set, the eyeglass adjusting part for adjusting the first lens set and the second lens set state；First lens set corresponds to first camera setting, and the second lens set corresponds to second camera setting；First lens set, the second lens set comprise at least an eyeglass；Power part is installed on aircraft；Pass through eyeglass adjusting part, state, the state of the second lens set eyeglass of the first lens set of adjustment, so as to change first camera, the shooting direction of second camera.Apparatus of the present invention are simply light, and shooting effect is good；Camera is fixed, and changes the shooting direction of camera by adjusting lens set, reduces failure risk, and reliability is high.
Description
Technical field
The present invention relates to a kind of double camera oblique photograph device for airborne vehicle.
Background technology
Airborne inclined photography is the high-new technology of taking photo by plane that international survey field grew up in recent years, and it passes through same
More different sensors of camera angle are carried on one flying platform, to gather the aerial image of atural object difference side.It is airborne to incline
Tiltedly the vertical photography pattern that tradition is taken photo by plane has been overturned in photography, and the multi-angle oblique image that it is gathered meets the true of human eye vision
The world directly perceived, spatial information is more rich, complete, friendly, is with a wide range of applications.It is but existing airborne inclined in the world
Generally there is the shortcomings that complex designing, instrument maximizes, involved great expense, operating cost is high in camera chain, and single, close
40 degree of oblique photograph angle design can not adapt to Surveying and Mapping Industry image very well primarily to meet the purpose of landscape covering
The needs of mapping.In recent years, the Technology of low altitude remote sensing based on unmanned plane, unmanned airship has obtained faster development, high performance CCD
The resolution ratio of camera is up to tens million of grades of pixels, using being mounted on unmanned flight's platform, camera angle design and overall cloth
Rational multiple CCD (appliance coupler part, the Charge Coupled Device) cameras of office carry out low latitudes photography can not only be from
The applications such as right Disaster Assessment, military information collection, emergency command, city management provide inexpensive, real-time high definition and tilt image
Data, moreover it is possible to meet Surveying and Mapping Industry mapping and the needs of other three-dimensional spatial informations processing.
The aviation oblique photograph device used at present generally uses multiple built-in cameras, real by putting for different angle
Existing multiple angle shots, to obtain the panoramic picture on ground.Or in order to reduce main screw lift and cost, using phase built in rotation
Machine realizes multi-angled shooting.In order to reduce main screw lift and cost, generally use rotates built-in camera and realizes multi-angled shooting, with
Reduce built-in camera quantity.Complete machine vibrations can be caused also larger because the volume and weight of built-in camera itself is larger, during rotation,
The consumption of electricity is also increased simultaneously, is unfavorable for aeroplane photography.
The defects of above-mentioned technical proposal, is：
1st, installation weight is larger, and complete machine vibrations are obvious；
2nd, camera rotational structure is complicated, and precision is low, poor reliability；
3rd, camera rotation period is grown, and under the requirement of certain Duplication, shooting efficiency and quality can decline.
The content of the invention
In view of the shortcomings of the prior art, it is real the invention provides a kind of double camera oblique photograph device for airborne vehicle
Show from the earthward shooting of any direction in the air, enriched the application of product, its is simple in construction, and reliability is high, effectively
Ground mitigates the weight of aviation oblique photograph device, more adapts to aeroplane photography.
To achieve these goals, the invention provides a kind of double camera oblique photograph device for airborne vehicle, it is wrapped
Include：First camera, second camera, eyeglass mechanism, the power part for driving eyeglass mechanism；
First camera is installed on aircraft, and second camera is installed on aircraft；
Eyeglass mechanism includes the first lens set, the second lens set, for adjusting the first lens set and the second lens set state
Eyeglass adjusting part；First lens set corresponds to first camera setting, and the second lens set corresponds to second camera setting；First eyeglass
Group, the second lens set comprise at least an eyeglass；
Power part is installed on aircraft；
By eyeglass adjusting part, the state of the first lens set of face first camera, the of face second camera are adjusted
The state of two lens set eyeglasses, so as to change first camera, the shooting direction of second camera.
In the present invention, the incident light source of different angle is obtained by first camera, second camera, in the situation that camera is fixed
Under, the first lens set, the state of the second lens set are adjusted by eyeglass adjusting part, obtain the light source of different angle, changes the
The shooting direction of one camera, second camera, complete multi-angled shooting.
The present invention sets double camera, reduces the shooting time of target location, increases the overlapping area of shooting photo, can be with
The requirement for Duplication of taking photo by plane is reduced, increases the interval in course line, operating efficiency is improved, so as to be more suitable for aeroplane photography.
According to another embodiment of the present invention, the first lens set includes first rotating shaft and is arranged in first rotating shaft
The first swing type eyeglass, the second lens set includes the second rotating shaft and the second swing type eyeglass for being arranged in the second rotating shaft.Pendulum
Dynamic formula eyeglass, it can be rotated a certain angle along certain line for crossing center of eyeglass；For example, the first swing type eyeglass is located at
The front of one camera, first rotating shaft drive the first swing type eyeglass to be swung, and first camera is completed forward, downwards, rearward
To shooting；Second swing type eyeglass is located at the front of second camera, and the second rotating shaft is set perpendicular to first rotating shaft, passes through second
Rotating shaft drives the second swing type eyeglass to be swung, and second camera completes shooting to the left, downwards, to the right.
First phase is rotatably arranged according to another embodiment of the present invention, the first lens set according to the present invention
Machine front, the second lens set are rotatably arranged in the front of second camera.For example, first camera and the first mirror being correspondingly arranged
Piece group shoot forward, downwards, rearwardly direction, the eyeglass number in the first lens set is multiple, passes through the side such as rotating disk or slide rail
Formula switches to eyeglass forward, downwards, backward in the front of first camera, completes to specify the shooting of angle corresponding to eyeglass；
Accordingly, second camera and the second lens set being correspondingly arranged shoot direction to the left, downwards, to the right, pass through a swing type
Eyeglass or multiple fixed eyeglasses are completed to specify the switching between eyeglass, complete shooting to the left, downwards, to the right.
Another embodiment, first rotating shaft connection eyeglass adjusting part, the second rotating shaft connection eyeglass adjusting part.
Eyeglass adjusting part includes but is not limited to rotating disk, runing rest, slide rail eyeglass adjusting part.
According to another embodiment of the present invention, the first lens set includes three fixed eyeglasses, the second lens set
Including three fixed eyeglasses.Fixed eyeglass, the eyeglass that space angle is fixed.For example, in the first lens set, the second lens set
Eyeglass space angle it is different, six space angles correspond to respectively left front, lower-left, it is left back, right before, bottom right, it is right after six
Direction.
According to another embodiment of the present invention, eyeglass adjusting part is rotary or parallel-moving type eyeglass regulation group
Part.Eyeglass adjusting part includes but is not limited to rotating disk, runing rest, slide rail eyeglass adjusting part.
According to another embodiment of the present invention, first camera, second camera are oppositely arranged on the two of eyeglass mechanism
Side.For example, using rotating disc type eyeglass adjusting part, first camera, second camera are oppositely arranged on the both sides of rotating disk；First eyeglass
Group, the second lens set are disposed on the rotating disk, wherein, left front eyeglass and right front lens are oppositely arranged on the two of rotating disk
Side；Left back eyeglass and right rear lens are oppositely arranged on the both sides of rotating disk；Lower-left eyeglass and bottom right eyeglass are oppositely arranged on rotating disk
Both sides, the eyeglass needed to use by adjusting rotating disk to make switch to the specified location of straight-on camera.
According to another embodiment of the present invention, first camera, second camera are arranged on the homonymy of eyeglass mechanism.Example
Such as, linearly it is distributed in using slide rail type eyeglass adjusting part, the first lens set, the second lens set edge on slide rail, it is preferred that left front
Eyeglass and left back eyeglass are oppositely arranged on the homonymy of slide rail；Right front lens and right rear lens are oppositely arranged on the homonymy of slide rail；It is left
Lower eyeglass and bottom right eyeglass are oppositely arranged on the homonymy of slide rail, and the eyeglass needed to use by adjusting sliding block to make switches to face
The specified location of camera.
According to another embodiment of the present invention, first camera and second camera are horizontal camera.Here sleeping
Formula camera refers to that optical axis is less than or equal to 75 ° with horizontal plane angulation.
According to another embodiment of the present invention, oblique photograph device also includes pedestal, first camera, the second phase
Machine, eyeglass mechanism and power part are arranged on pedestal..First camera, second camera, eyeglass mechanism, power are corresponded in pedestal
Part is provided with support base, and it is removably connected and airborne vehicle, wherein being additionally provided with other parts, such as control machine in Aerial photography
Structure etc..
According to another embodiment of the present invention, power part includes but is not limited to motor, cylinder, gear etc..
The shooting process of the present invention：When airborne vehicle reaches target location, target is carried out by first camera, second camera
The shooting in position first angle direction；After the shooting for completing the angle position, the first lens set, second are changed by power part
The position of eyeglass, carries out the shooting of second angle in the state of lens set or the first lens set, the second lens set；Power part is more
Secondary action, complete the multi-angled shooting of target location.
The present invention is advantageous in that：First lens set, the state of the second lens set or the are changed by power part
The position of eyeglass in one lens set, the second lens set, realizes multi-angled shooting, and two built-in cameras realize six built-in cameras
Shooting effect.Layout vertical compared to conventional bevel camera is set, and the effective weight for mitigating whole device, is advantageous to aviation and is taken the photograph
Shadow；Camera is fixed simultaneously, eyeglass mechanism kinematic, its light weight, and vibrations during rotation are small, and the shooting effect of complete machine is influenceed
It is small.Built-in camera position is fixed, and it is electrically connected without motion, reduces failure risk, and reliability is high.Only one degree of freedom
Motion, drive mechanism is simple, and positioning precision is high.The photo of built-in camera shooting is overlapped, it is possible to reduce Duplication of taking photo by plane will
Ask, increase the interval in course line, improve operating efficiency, so as to more adapt to aeroplane photography.
The present invention is described in further detail below in conjunction with the accompanying drawings.
Brief description of the drawings
Fig. 1 is a kind of overall structure diagram of double camera oblique photograph device for airborne vehicle of embodiment 1, and it is aobvious
Swing type eyeglass is shown；
Fig. 2 is a kind of overall structure diagram of double camera oblique photograph device for airborne vehicle of embodiment 2, and it is aobvious
Rotating disc type Lens assembly is shown；
Fig. 3 is a kind of overall structure diagram of double camera oblique photograph device for airborne vehicle of embodiment 3, and it is aobvious
Rotating disc type Lens assembly is shown；
Fig. 4 is a kind of overall structure diagram of double camera oblique photograph device for airborne vehicle of embodiment 4, and it is aobvious
Sliding Lens assembly is shown.
Embodiment
Embodiment 1
A kind of double camera oblique photograph device for airborne vehicle is present embodiments provided, as shown in figure 1, including：Pedestal
And it is arranged on first camera 11, second camera 12, eyeglass mechanism 13 and steering wheel 14 on pedestal.
Wherein, eyeglass mechanism 13 include first rotating shaft (not shown), the first swing type eyeglass 132, the second rotating shaft 133,
Second swing type eyeglass 134, support 135, the corresponding first camera 11 of the first swing type eyeglass 132 are set, the second swing type eyeglass
134 corresponding second cameras 12 are set, the first swing type eyeglass 132, the second swing type eyeglass 134 it is swingable be connected to support
135, support 135 is arranged on pedestal；Rotate the first swing type eyeglass 134 and the second swing type eyeglass 134 can obtain respectively to
It is left, to the right, forward, backward, the shooting visual angle in downward five directions.
First camera 11 and second camera 12 are horizontal camera；The camera lens axis of first camera 11 and second camera 12
Camera lens axis be mutually perpendicular to, and be generally aligned in the same plane；First rotating shaft (not shown) is vertical with the second rotating shaft 133, and
It is generally aligned in the same plane.
The number of steering wheel 14 is 2, drives the first swing type eyeglass 132, the second swing type eyeglass 134 to carry out certain model respectively
The swing enclosed, by adjust the first swing type eyeglass 132 of face first camera 11, face second camera 12 the second swing type
Eyeglass 134, so as to change first camera 11, the shooting direction of second camera 12.
Embodiment 2
A kind of double camera oblique photograph device for airborne vehicle is present embodiments provided, as shown in Fig. 2 including：Pedestal
And it is arranged on first camera 21, second camera 22, eyeglass mechanism 23 and steering wheel 24 on pedestal.
Wherein, eyeglass mechanism 23 includes the first lens set, the second lens set, for adjusting the first lens set and the second mirror
The rotating disk 231 of piece group state, connecting rod 232；First lens set corresponds to first camera 21 and set, corresponding second phase of the second lens set
Machine 22 is set；First lens set includes three fixed eyeglasses, the second lens set includes three fixed eyeglasses, six eyeglasses point
Do not correspond to left front, lower-left, it is left back, right before, bottom right, it is right after six direction.
Rotating disk 231 is provided with connecting rod 232, and the number of connecting rod 232 is consistent with the number of eyeglass and is correspondingly arranged, connection
The number of bar is 6, and it is evenly distributed on rotating disk 231, and the angular separation between adjacent connecting rod 232 is 60 °；Rotating disk 231
It is rotatably installed on pedestal, the one end of connecting rod 234 connection eyeglass, other end connection rotating disk 231；Six connecting rods 232 are in
It is radial to be arranged on rotating disk.
First camera 21, second camera 22 are horizontal camera, and first camera 21, second camera 22 are oppositely arranged on rotating disk
231 both sides, on pedestal.
Steering wheel 24 is by the drive connection rotating disk 231 of drive shaft 241, in the first lens set for switching face first camera 21
Eyeglass, face second camera 22 the second lens set in eyeglass, so as to change the shooting side of first camera 21, second camera 22
To.
In the present embodiment, drive rotating disk 231 to horizontally rotate by steering wheel 24, control the rotational angle of rotating disk 231, make rotating disk
Eyeglass face first camera 21 and second camera 22 on 231, realize that the light of six direction is reflected into first camera respectively
21 and second camera 22, obtain respectively left front, lower-left, it is left back, right before, bottom right, it is right after six direction photo, realize multi-angle
Shooting.
Embodiment 3
A kind of double camera oblique photograph device for airborne vehicle is present embodiments provided, as shown in figure 3, including：Pedestal
And it is arranged on first camera 31, second camera 32, eyeglass mechanism 33 and steering wheel 34 on pedestal.
Wherein, eyeglass mechanism 33 includes the first lens set, the second lens set, for adjusting the first lens set and the second mirror
The rotating disk 331 of piece group state；First lens set corresponds to first camera 31 and set, and the second lens set corresponds to second camera 32 and set；
First lens set includes three fixed eyeglasses, the second lens set includes three fixed eyeglasses.Six eyeglasses correspond to a left side respectively
Before, lower-left, it is left back, right before, bottom right, it is right after six direction.
Rotating disk 331 is provided with contiguous block 332, and contiguous block 332 is provided with connecting rod 333, the number and eyeglass of connecting rod 333
Number it is consistent and be correspondingly arranged, the number of connecting rod 333 is 6, and the number of contiguous block 332 is three, and it, which is evenly distributed on, turns
On disk 331, the angular separation between adjacent contiguous block 332 is 120 °；Rotating disk 331 is rotatably installed on pedestal.
First camera 31, second camera 32 are horizontal camera, and first camera 31, second camera 32 are disposed side by side on rotating disk
331 homonymy, on pedestal.
Steering wheel 34 is by the drive connection rotating disk 331 of drive shaft 341, in the first lens set for switching face first camera 31
Eyeglass, face second camera 32 the second lens set in eyeglass, so as to change the shooting side of first camera 31, second camera 32
To.
Embodiment 4
A kind of double camera oblique photograph device for airborne vehicle is present embodiments provided, as shown in figure 4, including：Pedestal
And it is arranged on first camera 41 on pedestal, second camera 42, sliding angle adjusting mechanism 43.
Wherein, sliding angle adjusting mechanism 43 includes the different eyeglass 431 of six space angles, slide rail 432, by power
The sliding block 433 of part driving；Slide rail 432 is located on pedestal, and sliding block 433 is slippingly arranged on slide rail 432, and eyeglass 431 is logical
Connecting rod 434 is crossed to be arranged on sliding block 433；Power part is arranged on pedestal, and power part is steering wheel；Pass through sliding slider
433, switching face first camera 41, the eyeglass 431 of second camera 42, so as to change the bat of first camera 41, second camera 42
Take the photograph direction.
The number of eyeglass 431 is six, and the number of connecting rod 434 is also six, and it is evenly distributed on sliding block 433, phase
Spacing between adjacent connecting rod 434 is consistent.Six eyeglasses 431 are divided for the first lens set, the second lens set, the 3rd lens set,
First lens set includes the eyeglass 431 of left front, left back both direction, the second lens set include it is right before, the mirror in latter two right direction
Piece 431；3rd lens set includes lower-left, the eyeglass 431 of bottom right both direction.
First camera 41, second camera 42 are disposed side by side on the homonymy of sliding angle adjusting mechanism 43, first camera 41,
Second camera 42 is horizontal camera.
Steering wheel and its transmission parts drive the eyeglass 431 being arranged on sliding block 433 to slide, control slide block 433 slide away from
From making eyeglass 431 on sliding block 433 distinguish face first camera 41 and second camera 42, realize the light difference of six direction
Be reflected into first camera 41 and second camera 42, obtain respectively left front, lower-left, it is left back, right before, bottom right, it is right after six direction
Photo, realize the shooting of multi-angle.
Although the present invention is disclosed above with preferred embodiment, the scope that the present invention is implemented is not limited to.Any
The those of ordinary skill in field, it is when a little improvement can be made, i.e., every according to this hair in the invention scope for not departing from the present invention
Bright done equal improvement, should be the scope of the present invention and is covered.
Claims (10)
1. a kind of double camera oblique photograph device for airborne vehicle, it is characterised in that the oblique photograph device includes：First
Camera, second camera, eyeglass mechanism, the power part for driving the eyeglass mechanism；
The first camera is arranged on the airborne vehicle, and the second camera is arranged on the airborne vehicle；
The eyeglass mechanism includes the first lens set, the second lens set, for adjusting first lens set and second mirror
The eyeglass adjusting part of piece group state；First lens set corresponds to the first camera and set, and second lens set is corresponding
The second camera is set；First lens set, second lens set comprise at least an eyeglass；
The power part is arranged on the airborne vehicle；
By the eyeglass adjusting part, the state of the first lens set of first camera described in face is adjusted, second described in face
The state of second lens set eyeglass of camera, so as to change the first camera, the shooting direction of the second camera.
2. oblique photograph device as claimed in claim 1, it is characterised in that first lens set includes first rotating shaft and set
Put the first swing type eyeglass in the first rotating shaft, second lens set includes the second rotating shaft and is arranged on described second
The second swing type eyeglass in rotating shaft.
3. oblique photograph device as claimed in claim 2, it is characterised in that the first swing type eyeglass rotatably arranged with
In front of the first camera, the second swing type eyeglass be rotatably arranged in the front of the second camera.
4. oblique photograph device as claimed in claim 3, it is characterised in that the first rotating shaft connects the eyeglass regulation group
Part, second rotating shaft connect the eyeglass adjusting part.
5. oblique photograph device as claimed in claim 1, it is characterised in that first lens set includes three fixed mirrors
Piece, second lens set include three fixed eyeglasses.
6. oblique photograph device as claimed in claim 5, it is characterised in that the eyeglass adjusting part is adjusted for rotary eyeglass
Save component.
7. oblique photograph device as claimed in claim 6, it is characterised in that the first camera, the second camera are relative
It is arranged on the both sides of the eyeglass mechanism.
8. oblique photograph device as claimed in claim 6, it is characterised in that the first camera, the second camera are side by side
It is arranged on the homonymy of the eyeglass mechanism.
9. oblique photograph device as claimed in claim 1, it is characterised in that the first camera and the second camera are
Horizontal camera.
10. a kind of oblique photograph device as described in one of claim 1-9, it is characterised in that the oblique photograph device is also
Including pedestal, the first camera, the second camera, the eyeglass mechanism and the power part are installed in the base
On seat.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710277859 | 2017-04-25 | ||
| CN2017102778590 | 2017-04-25 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107364585A true CN107364585A (en) | 2017-11-21 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| 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 |
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| CN201720809656.7U Expired - Fee Related CN207752284U (en) | 2017-04-25 | 2017-07-05 | A kind of one camera turntable oblique photograph device for aircraft |
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| CN201720809536.7U Expired - Fee Related CN207360596U (en) | 2017-04-25 | 2017-07-05 | A kind of opposed double camera rotating disc type oblique photograph device for aircraft |
| 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 |
| 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 |
| 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 |
| CN201720809623.2U Expired - Fee Related CN207181920U (en) | 2017-04-25 | 2017-07-05 | A kind of one 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 |
| CN201710542703.0A Pending CN107390469A (en) | 2017-04-25 | 2017-07-05 | A kind of polyphaser camera for airborne vehicle |
| CN201710542256.9A Pending CN107367266A (en) | 2017-04-25 | 2017-07-05 | A kind of fixed one camera oblique photograph device for airborne vehicle |
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| 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 |
| 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 |
| CN201710542197.5A Pending CN107340672A (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens oblique photograph device for airborne vehicle |
| CN201710541954.7A Pending CN107367263A (en) | 2017-04-25 | 2017-07-05 | A kind of 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 |
| CN201710542329.4A Pending CN107390451A (en) | 2017-04-25 | 2017-07-05 | A kind of rotating disc type lens supports for camera multi-angled shooting |
| 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 |
| CN201710541936.9A Pending CN107367886A (en) | 2017-04-25 | 2017-07-05 | A kind of rotary single-lens oblique photograph device for airborne vehicle |
| CN201720809492.8U Expired - Fee Related CN207113870U (en) | 2017-04-25 | 2017-07-05 | A kind of fixed one camera 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 |
| 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 |
| CN201720809537.1U Expired - Fee Related CN207113869U (en) | 2017-04-25 | 2017-07-05 | A kind of 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 |
| 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 |
| 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 |
| 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 |
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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 |
| CN201710542705.XA Pending CN107576312A (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph method at 12 visual angles for airborne vehicle |
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| CN201720809656.7U Expired - Fee Related CN207752284U (en) | 2017-04-25 | 2017-07-05 | A kind of one camera turntable oblique photograph device for aircraft |
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| CN201710542643.2A Pending CN107560602A (en) | 2017-04-25 | 2017-07-05 | A kind of one camera 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 Expired - Fee Related CN207360596U (en) | 2017-04-25 | 2017-07-05 | A kind of opposed double camera rotating disc type oblique photograph device for aircraft |
| 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 |
| 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 |
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| CN201720809623.2U Expired - Fee Related CN207181920U (en) | 2017-04-25 | 2017-07-05 | A kind of one 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 |
| CN201710542703.0A Pending CN107390469A (en) | 2017-04-25 | 2017-07-05 | A kind of polyphaser camera for airborne vehicle |
| CN201710542256.9A Pending CN107367266A (en) | 2017-04-25 | 2017-07-05 | A kind of fixed one camera oblique photograph device for airborne vehicle |
| 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 |
| 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 |
| CN201710542197.5A Pending CN107340672A (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens oblique photograph device for airborne vehicle |
| CN201710541954.7A Pending CN107367263A (en) | 2017-04-25 | 2017-07-05 | A kind of 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 |
| CN201710542329.4A Pending CN107390451A (en) | 2017-04-25 | 2017-07-05 | A kind of rotating disc type lens supports for camera multi-angled shooting |
| 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 |
| CN201710541936.9A Pending CN107367886A (en) | 2017-04-25 | 2017-07-05 | A kind of rotary single-lens oblique photograph device for airborne vehicle |
| CN201720809492.8U Expired - Fee Related CN207113870U (en) | 2017-04-25 | 2017-07-05 | A kind of fixed one camera 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 |
| 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 |
| CN201720809537.1U Expired - Fee Related CN207113869U (en) | 2017-04-25 | 2017-07-05 | A kind of 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 |
| 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 |
| 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 |
| 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 |
| CN201720809625.1U Expired - Fee Related CN207181921U (en) | 2017-04-25 | 2017-07-05 | A kind of shaft type lens supports for camera multi-angled shooting |
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| CN201720809475.4U Expired - Fee Related CN207106926U (en) | 2017-04-25 | 2017-07-05 | A kind of double camera oblique photograph device for airborne vehicle |
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