CN207360597U - A kind of double camera rotating disc type oblique photograph device for aircraft - Google Patents
A kind of double camera rotating disc type oblique photograph device for aircraft Download PDFInfo
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- CN207360597U CN207360597U CN201720809677.9U CN201720809677U CN207360597U CN 207360597 U CN207360597 U CN 207360597U CN 201720809677 U CN201720809677 U CN 201720809677U CN 207360597 U CN207360597 U CN 207360597U
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- camera
- turntable
- rotating disc
- disc type
- eyeglass
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- 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 15
- 230000000694 effects Effects 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 description 7
- 238000000034 method Methods 0.000 description 4
- 238000000926 separation method Methods 0.000 description 4
- 230000007812 deficiency Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 235000007926 Craterellus fallax Nutrition 0.000 description 1
- 240000007175 Datura inoxia Species 0.000 description 1
- 208000004350 Strabismus Diseases 0.000 description 1
- 230000009286 beneficial effect 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
- 230000005611 electricity Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- DETAHNVSLBCZAA-ARJGXJLFSA-N photo product Chemical compound C[C@@H]([C@]12O)[C@@H](OC(C)=O)[C@@]3(OC(C)=O)C(C)(C)C3[C@@H]2C2[C@]3(COC(C)=O)C[C@]4(O)[C@H]1C2[C@@]3(C)C4=O DETAHNVSLBCZAA-ARJGXJLFSA-N 0.000 description 1
- 238000012805 post-processing Methods 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
-
- 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
- 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
- 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)
- Signal Processing (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Optics & Photonics (AREA)
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
- Stereoscopic And Panoramic Photography (AREA)
Abstract
The utility model provides a kind of double camera rotating disc type oblique photograph device for aircraft, including:First camera, second camera, rotating disc type angle adjusting mechanism, the power part for driving disc formula angle adjusting mechanism;First camera is installed on aircraft, and second camera is installed on aircraft;Rotating disc type angle adjusting mechanism includes the different eyeglass of some space angles, the turntable by power part driving, connecting portion, and eyeglass is arranged on turntable by connecting portion;Turntable is rotatably installed on aircraft, and power part is installed on aircraft;By rotating turntable, switching face first camera, the eyeglass of second camera, so as to change first camera, the shooting direction of second camera.The utility model device is simply light, and shooting effect is good;Camera is fixed, and the eyeglass by switching different angle changes the shooting direction of camera, reduces failure risk, and reliability is high.
Description
Technical field
It the utility model is related to a kind of double camera rotating disc type oblique photograph device for aircraft.
Background technology
With the development of unmanned air vehicle technique, its application field is also gradually expanding, unmanned plane oblique photograph technology be
The novel photographic e measurement technology to grow up on the basis of this.Unlike traditional photogrammetric technology:Oblique photograph
Camera is usually formed by facing camera lens and multiple strabismus camera lenses, carry on unmanned plane, while from it is vertical, the different angle such as tilt
Take pictures to ground object.The image that angle shot obtains perpendicular to the ground is known as positive, camera lens towards with ground into a clamp
The image that angle shooting obtains is known as inclined tab.Image data is obtained as material using oblique photograph technology, can be automated and add
True orthophoto (TDOM), digital surface model (DSM) are obtained after work processing, realizes the three-dimensional modeling of real scene, it is quick to go back
Former true present situation, provides the geography information of more horn of plenty to the user.
Since oblique photograph technology compensate for the deficiency of traditional orthography, before the several years be applied to urban construction,
The fields such as geological prospecting, however in recent years due to oblique photograph post-processing technology rapid progress and unmanned air vehicle technique it is continuous
Development, unmanned plane oblique photograph present the trend being skyrocketed through in the application of multiple industries.Have more moneys not on the market at present
The inclined camera product of same type.
The aviation oblique photograph device used at present generally uses multiple built-in cameras, such as Chinese patent
201310404384.9 disclose a kind of small-sized unmanned aerial vehicle onboard regards three-dimensional air remote sensing device and system more, including:Nobody
Machine;The fixed frame being arranged on unmanned plane, is provided with first camera, second camera and third camera on fixed frame;First camera,
The long side of second camera and third camera is each perpendicular to heading setting;First camera and third camera favour horizontal plane
45 ° of settings, second camera are set perpendicular to photography direction.By putting for different angle, multiple angle shots are realized, to obtain
The panoramic picture on ground.In order to reduce main screw lift and cost, generally use rotates built-in camera and realizes multi-angled shooting, to subtract
Few built-in camera quantity.Since the volume and weight of built-in camera itself is larger, when rotation, can cause complete machine vibrations also larger, together
When also increase the consumption of electricity, be 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.
Utility model content
In view of the deficiencies of the prior art, the utility model provides a kind of double camera rotating disc type inclination for aircraft and takes the photograph
Image device, realizes from the earthward shooting of any direction in the air, enriches the application range of product, its is simple in structure, reliably
Property it is high, effectively mitigate the weight of aviation oblique photograph device, more adapt to aeroplane photography.
To achieve these goals, the utility model provides a kind of double camera rotating disc type oblique photograph for aircraft
Device, it includes:First camera, second camera, rotating disc type angle adjusting mechanism, for driving disc formula angle adjusting mechanism
Power part;First camera is installed on aircraft, and second camera is installed on aircraft;Rotating disc type angle adjusting mechanism includes
The different eyeglass of some space angles, the turntable by power part driving, connecting portion, eyeglass are arranged on turntable by connecting portion
On;Turntable is rotatably installed on aircraft, and power part is installed on aircraft;By rotating turntable, switching face the
The eyeglass of one camera, second camera, so as to change first camera, the shooting direction of second camera.
In the utility model, by setting the different eyeglass of some space angles before camera lens, different angle is obtained
Incident light source, in the case where camera is fixed, the eyeglass different by switching space angle, obtains the light source of different angle,
Complete the shooting of multi-angle.
Double camera is set in the utility model, reduces the shooting time of target location, increases the faying surface of shooting photo
Product, it is possible to reduce the requirement for Duplication of taking photo by plane, increases the interval in course line, work efficiency is improved, so as to be more suitable for aeroplane photography.
In the utility model, using the direction of one of camera lens as front.
Another embodiment according to the present utility model, eyeglass number are six.By setting six eyeglasses to realize
From the earthward shooting of six direction in the air;Wherein, six space angles correspond to respectively left front, lower-left, it is left back, right before, bottom right,
Six direction behind the right side.
Another embodiment according to the present utility model, six eyeglasses include three groups of equal numbers of lens sets, its
In every group of eyeglass include the different eyeglass of two spaces angle.
Another embodiment according to the present utility model, first camera, second camera are oppositely arranged on the two of turntable
Side;Three groups of lens sets are disposed on turntable.Wherein, left front eyeglass and right front lens are oppositely arranged on the both sides of turntable;It is left
Rear lens and right rear lens are oppositely arranged on the both sides of turntable;Lower-left eyeglass and bottom right eyeglass are oppositely arranged on the both sides of turntable,
The designated position that can make to need eyeglass to be used to switch to straight-on camera by adjusting turntable.
Another embodiment according to the present utility model, connecting portion are connecting rod, and eyeglass is turned by connecting rod connection
Disk, connecting rod are evenly distributed on turntable, and the angular separation between adjacent connecting rod is 60 °;Eyeglass it is consistent with connecting rod number and
It is correspondingly arranged, connecting rod one end connection eyeglass, other end connection turntable;Connecting rod is radially arranged on turntable.
Another embodiment according to the present utility model, first camera, second camera are disposed side by side on the same of turntable
Side;Three groups of lens sets are uniformly arranged on turntable.Wherein, left front eyeglass and left back eyeglass are oppositely arranged on the homonymy of turntable;It is right
Front lens and right rear lens are oppositely arranged on the homonymy of turntable;Lower-left eyeglass and bottom right eyeglass are oppositely arranged on the homonymy of turntable,
The designated position that can make to need eyeglass to be used to switch to straight-on camera by adjusting turntable.
Another embodiment according to the present utility model, connecting portion are contiguous block, and eyeglass is turned by contiguous block connection
Disk, contiguous block are evenly distributed on turntable, and the angular separation between adjacent connections is 120 °.In the utility model, camera shooting
When, while there is one group of two eyeglass to be located at operating position, wherein operating position, refer to eyeglass and camera carry out with the use of when eyeglass
The position at place, ensures that first camera, second camera can be carried out at the same time shooting, and the angle in eyeglass space is different, first camera,
The photo of second camera shooting is different, greatly improves work efficiency.
Another embodiment according to the present utility model, power part are steering engine, and steering engine is by driving axis connection to turn
Disk.Steering engine drives drive rod driving disc to rotate, and then realizes the switching of eyeglass;In whole shooting process, due to rotating turntable
And eyeglass, its light weight of rotatable parts, vibrations during rotation are small, influence also small, whole transmission process to the shooting effect of complete machine
The only movement of one degree of freedom, drive mechanism is simple, and positioning accuracy is high.
Another embodiment according to the present utility model, camera are horizontal camera, and horizontal camera here refers to light
Axis is less than or equal to 75 ° with horizontal plane angulation.
Another embodiment according to the present utility model, rotating disc type oblique photograph device further include pedestal, pedestal peace
On aircraft, first camera, second camera, power part are fixedly mounted on pedestal dress, and turntable is rotatably installed in base
On seat.First camera, second camera, power part are corresponded in pedestal and is equipped with support base, it is removably connected and aircraft, its
In be additionally provided with other parts, such as control mechanism in Aerial photography.
The shooting process of the utility model:When reaching target location, first jiao is carried out by first camera, second camera
The shooting of degree state, after completing the angle shot, drives turntable to rotate, switches to the eyeglass of other different conditions by steering engine,
Carry out the shooting of other angles;Multiple rotary turntable, completes the multi-angled shooting of target location.
The utility model is beneficial in that:Multi-angled shooting is realized by rotating eyeglass, and two built-in cameras are realized
The shooting effect of six built-in cameras.Layout vertical compared to conventional bevel camera is set, the effective weight for mitigating whole device,
Be conducive to aeroplane photography;Simultaneously because rotating eyeglass, its light weight, vibrations during rotation are small, and the shooting effect of complete machine is influenced
Also it is small.Built-in camera position is fixed, it is electrically connected without movement, reduces failure risk, and reliability is high.Only one degree of freedom
Movement, drive mechanism is simple, and positioning accuracy 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, work efficiency is improved, so as to more adapt to aeroplane photography.
The utility model 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 signal of double camera rotating disc type oblique photograph device for aircraft of embodiment 1
Figure;
Fig. 2 is a kind of schematic diagram of double camera rotating disc type oblique photograph device for aircraft of embodiment 1, it shows
Downward shooting state;
Fig. 3 is a kind of overall structure signal of double camera rotating disc type oblique photograph device for aircraft of embodiment 2
Figure;
Fig. 4 is a kind of schematic diagram of double camera rotating disc type oblique photograph device for aircraft of embodiment 2, it shows
Downward shooting state.
Embodiment
Embodiment 1
A kind of double camera rotating disc type oblique photograph device for aircraft is present embodiments provided, as shown in Figs. 1-2, bag
Include:Pedestal and the first camera 1 being arranged on pedestal, second camera 2, rotating disc type angle adjusting mechanism 3, steering engine 4.
Wherein, first camera 1, second camera 2 are horizontal camera, it is installed on pedestal.
Rotating disc type angle adjusting mechanism 3 includes the different eyeglass 31 of six space angles, is driven by steering engine 4 turntable 32,
Connecting rod 33, eyeglass 31 is consistent with 33 number of connecting rod and is correspondingly arranged, and 31 number of eyeglass is 6, the number of connecting rod 33
For 6, it is evenly distributed on turntable 32, and the angular separation between adjacent connecting rod 33 is 60 °;Turntable 32 is rotatably installed in
On pedestal, 33 one end of connecting rod connection eyeglass 31, other end connection turntable 32;Six connecting rods 33 are radially arranged on turntable
On 32;First camera 1, second camera 2 are oppositely arranged on the both sides of turntable 32.
Steering engine 4 connects turntable 32 by drive shaft 41;4 driving disc 32 of steering engine rotates, switching face first camera 1, the
The eyeglass 31 of two cameras 2, so as to change first camera 1, the shooting direction of second camera 2.
In the present embodiment, drive turntable 32 to horizontally rotate by steering engine 4, control 32 rotational angle of turntable, make on turntable 32
Eyeglass face first camera 1 and second camera 2, realize that the light of six direction is reflected into first camera 1 and second respectively
Camera 2, 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.
As shown in Fig. 2, the state shot downwards for the present embodiment, at this time, eyeglass 311 correspond to first camera, bottom right is shot
The photo in direction, eyeglass 312 correspond to second camera, shoot the photo of lower left.
Embodiment 2
A kind of double camera rotating disc type oblique photograph device for aircraft is present embodiments provided, as shown in Figure 3-4, bag
Include:Pedestal and the first camera 5 being arranged on pedestal, second camera 6, rotating disc type angle adjusting mechanism 7, steering engine 8.
Wherein, first camera 5, second camera 6 are horizontal camera, it is installed on pedestal.
Rotating disc type angle adjusting mechanism 7 includes the different eyeglass 71 of six space angles, turntable 72, contiguous block 73, connection
Block 73 is equipped with connecting rod 731, and eyeglass 71 is consistent with 731 number of connecting rod and is correspondingly arranged, and 71 number of eyeglass is 6, connection
The number of bar 73 is also 6;73 number of contiguous block is three, it is evenly distributed on turntable 72, between adjacent contiguous block 73
Angular separation is 120 °;First camera 5, second camera 6 are oppositely arranged on the both sides of turntable 72.
Steering engine 8 connects turntable 72 by drive shaft 81;Steering engine 8 connects turntable 72 by drive shaft 81;By rotating turntable
72, switching face first camera 5, the eyeglass 71 of second camera 6, so as to change first camera 5, the shooting direction of second camera 6.
In the present embodiment, steering engine 8 drives lens slewing disc 72 to horizontally rotate, and controls 72 rotational angle of turntable, makes on turntable 72
Eyeglass face first camera 5 and second camera 6, realize that the light of six direction is reflected into first camera 5 and second respectively
Camera 6, 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.
As shown in figure 4, the state shot downwards for the present embodiment, at this time, eyeglass 711 correspond to first camera, bottom right is shot
The photo in direction, eyeglass 712 correspond to second camera, shoot the photo of lower left.
Although the utility model is disclosed above with preferred embodiment, the model of the utility model implementation is not limited to
Enclose.Any those of ordinary skill in the art, in the invention scope for not departing from the utility model, improve when can make a little,
I.e. every equal improvement done according to the utility model, should be the scope of the utility model and is covered.
Claims (10)
- A kind of 1. double camera rotating disc type oblique photograph device for aircraft, it is characterised in that including:First camera, second Camera, rotating disc type angle adjusting mechanism, the power part for driving the rotating disc type angle adjusting mechanism;The first camera On the aircraft, the second camera is installed on the aircraft;The rotating disc type angle adjusting mechanism includes The different eyeglass of some space angles, the turntable driven by the power part, connecting portion, the eyeglass pass through the connecting portion It is arranged on the turntable;The turntable is rotatably installed on the aircraft, and the power part is installed on the boat On pocket;By rotating the turntable, switch first camera, the eyeglass of the second camera described in face, so as to change described The shooting direction of first camera, the second camera.
- 2. rotating disc type oblique photograph device as claimed in claim 1, it is characterised in that the eyeglass number is six.
- 3. rotating disc type oblique photograph device as claimed in claim 2, it is characterised in that six eyeglasses are divided into three numbers Equal lens set.
- 4. rotating disc type oblique photograph device as claimed in claim 3, it is characterised in that the first camera, second phase Machine is oppositely arranged on the both sides of the turntable;Lens set described in three groups is disposed on the turntable.
- 5. rotating disc type oblique photograph device as claimed in claim 4, it is characterised in that the connecting portion is connecting rod, described Eyeglass connects the turntable by the connecting rod, and the connecting rod is evenly distributed on the turntable, the adjacent connecting rod Between spacing be 60 °.
- 6. rotating disc type oblique photograph device as claimed in claim 3, it is characterised in that the first camera, second phase Machine is disposed side by side on the homonymy of the turntable;Lens set described in three groups is uniformly arranged on the turntable.
- 7. rotating disc type oblique photograph device as claimed in claim 6, it is characterised in that the connecting portion is contiguous block, described Eyeglass connects the turntable by contiguous block, and the contiguous block is evenly distributed on the turntable, between the adjacent connector Spacing be 120 °.
- 8. rotating disc type oblique photograph device as claimed in claim 1, it is characterised in that the power part is steering engine, described Steering engine is by driving turntable described in axis connection.
- 9. rotating disc type oblique photograph device as claimed in claim 1, it is characterised in that the camera is horizontal camera.
- 10. the rotating disc type oblique photograph device as described in one of claim 1-9, it is characterised in that the rotating disc type is tilted and taken the photograph Image device further includes pedestal, and the pedestal is installed on the aircraft, the first camera, the second camera, described dynamic Power component is fixedly mounted on the pedestal, and the turntable is rotatably installed on the pedestal.
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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CN207360597U true CN207360597U (en) | 2018-05-15 |
Family
ID=60196799
Family Applications (40)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710542036.6A Pending CN107340671A (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for airborne vehicle |
CN201710542315.2A Pending CN107390450A (en) | 2017-04-25 | 2017-07-05 | A kind of reflection type inclined camera of polyphaser for airborne vehicle |
CN201710541954.7A Pending CN107367263A (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph device 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 |
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 |
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 |
CN201710542705.XA Pending CN107576312A (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph method at 12 visual angles 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 |
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 |
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 |
CN201710542197.5A Pending CN107340672A (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens 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 |
CN201710541936.9A Pending CN107367886A (en) | 2017-04-25 | 2017-07-05 | A kind of rotary single-lens oblique photograph device 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 |
CN201720809656.7U Expired - Fee Related CN207752284U (en) | 2017-04-25 | 2017-07-05 | A kind of one camera turntable 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 |
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 |
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 |
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 |
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 |
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 |
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 |
CN201710542628.8A Pending CN107390454A (en) | 2017-04-25 | 2017-07-05 | A kind of shaft type lens supports for camera multi-angled shooting |
CN201710542703.0A Pending CN107390469A (en) | 2017-04-25 | 2017-07-05 | A kind of polyphaser camera 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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CN201720809493.2U Expired - Fee Related CN207764534U (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for aircraft |
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 |
CN201720809475.4U Expired - Fee Related 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 |
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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CN201710542643.2A Pending CN107560602A (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for airborne vehicle |
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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 |
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 |
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 |
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Publication number | Priority date | Publication date | Assignee | Title |
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CN107380471A (en) * | 2017-04-25 | 2017-11-24 | 广州市红鹏直升机遥感科技有限公司 | A kind of double camera rotating disc type oblique photograph device for airborne vehicle |
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