CN103595905A - Camera body provided with a plurality of image sensors - Google Patents
Camera body provided with a plurality of image sensors Download PDFInfo
- Publication number
- CN103595905A CN103595905A CN201310628566.4A CN201310628566A CN103595905A CN 103595905 A CN103595905 A CN 103595905A CN 201310628566 A CN201310628566 A CN 201310628566A CN 103595905 A CN103595905 A CN 103595905A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- camera lens
- bayonet socket
- integrated form
- sub
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Landscapes
- Structure And Mechanism Of Cameras (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses a camera body provided with a plurality of image sensors. A round opening serving as an integrated type lens interface is formed in a front panel of the camera body (1), N image sensors (13) are arranged inside the camera body, the N image sensors all deviate from the axis of the round opening and are arranged in the circumferential direction of the axis, the plane where the image sensors are located is perpendicular to the axis, the distances from the centers of the N image sensors to the axis are the same, the camera body is in electric connection with an integrated type lens through a contact or wire, and the camera body is provided with a display screen. N sub-lenses (4) with different focal lengths are integrated inside a lens cone of the integrated type lens, each sub-lens comprises a set of optics, and the optical axes of the N sub-lenses are aligned with the central points of the N image sensors respectively to form N imaging optical paths. The camera body provided with the plurality of image sensors is high in integration level, convenient to use, and good in portability.
Description
Technical field
The present invention relates to a kind of shooting fuselage with a plurality of imageing sensors.
Background technology
Existing main flow camera system is divided into interchangeable lenses camera and not interchangeable lens camera generally.
Not interchangeable lens camera is mainly card camera, adopt a fuselage and a camera lens, and fuselage and camera lens are fixed together completely, when using, user cannot dismantle, the problem of this pattern maximum is exactly, 1) if automatic zoom camera lens, the zoom of its camera lens need to be driven by fuselage, power consumption is exceedingly fast, the flying power of battery is poor, a general battery can only be taken tens photos or hundred multiple pictures, although very light generally, battery flying power cannot meet users' requirement.
For len changeable camera, it is mainly single anti-and micro-list (as the micro-list of nex series of Sony, the J series of Nikon, the EOS M series of Canon); This camera is all in fuselage, to have a slice imageing sensor, owing to adopting len changeable bayonet socket, thereby by camera lens group's support, to obtain excellent imaging.But the shortcoming of this camera is also apparent, because once can only access a camera lens, for professional photographer, need to be equipped with a plurality of heads that focus, when travelling or carrying out special shooting task, need to carry many pieces of camera lenses goes out simultaneously, not only weight is large, and the process of cutaway is also comparatively loaded down with trivial details: first will take off camera lens, then change another camera lens, put camera lens bonnet, change in the process of camera lens, easily cause fuselage interior to have dust to invade, and, if worked in adverse circumstances, the process of changing camera lens becomes arduous all the more.
Therefore, be necessary to design a kind of camera system of brand-new style.
Summary of the invention
Technical problem to be solved by this invention is to provide a kind of shooting fuselage with a plurality of imageing sensors, and this shooting fuselage integrated level with a plurality of imageing sensors is high, easy to use, good portability.
The technical solution of invention is as follows:
A shooting fuselage for a plurality of imageing sensors is provided with the circular open as integrated form lens interface on fuselage (1) front panel;
In described fuselage, be provided with N imageing sensor (13); 3≤N≤12, N is natural number;
A described N imageing sensor is all offset the axis setting of described circular open, and N imageing sensor is along the circumferential arrangement of axis, and imageing sensor place plane is vertical with described axis; The center of N imageing sensor is all identical with the distance of described axis;
Fuselage is electrically connected to integrated form camera lens by contact or wire;
Fuselage is provided with display screen.
N imageing sensor is positioned at same plane and arranges along the circumferential decile of axis; N sub-camera lens arranged along the circumferential decile of axial line.
N is the integer between 4-6.
In the lens barrel of described integrated form camera lens, be integrated with N the sub-camera lens (4) with different focal; In each sub-camera lens, include an arrangement of mirrors sheet; The optical axis of N sub-camera lens all with the axis parallel of integrated form camera lens; And the individual sub-lens arrangement of N is circumferential axial line;
The optical axis of N sub-camera lens is aimed at N imageing sensor central point respectively, forms N bar imaging optical path.
[for communication, and being the power supply of integrated form camera lens for the treatment of device]
Circular open is fuselage bayonet socket (11), and the rear end of integrated form camera lens is provided with the camera lens bayonet socket with described fuselage bayonet socket adaptation; On fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with mutual adaptation for locking bayonet pin (14) and the pin-and-hole (224) of integrated form camera lens.[can fix by other patterns such as bayonet socket or welding, bayonet socket is detachable camera mode, and other patterns are non-dismountable pattern, as the annexation of the camera lens of many card type digital cameras and fuselage, is prior art]
On fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with one group of fixed contact (12) and one group of round and elastic contact (211), when fuselage engages with integrated form camera lens, fixed contact (12) and round and elastic contact (211) are in contact with one another to form and are electrically connected to.
On fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with N group fixed contact (12) and N group round and elastic contact (211); N group fixed contact (12) is arranged along the circumferential decile of circular open; N group round and elastic contact (211) is along the circumferential decile layout of described axial line, and while engaging with integrated form camera lens, N group fixed contact (12) and N group round and elastic contact (211) are in contact with one another to form and are electrically connected to.
Fuselage is provided with button or the thumb wheel for display frame is switched or sub-camera lens switches.[display frame is switched, and refers to and is switched to still image or the Real-time Motion Image that different imageing sensors obtains]
Fuselage is provided with electronic viewfinder; Fuselage or integrated form camera lens are provided with focusing motor, are provided with the anti-shake system of optics on fuselage or integrated form camera lens.
N is the integer between 4-6;
In the lens barrel of described integrated form camera lens, be integrated with N the sub-camera lens (4) with different focal; In each sub-camera lens, include an arrangement of mirrors sheet; The optical axis of N sub-camera lens all with the axis parallel of integrated form camera lens; And the individual sub-lens arrangement of N is circumferential axial line;
The optical axis of N sub-camera lens is aimed at N imageing sensor central point respectively, forms N bar imaging optical path;
Circular open is fuselage bayonet socket (11), and the rear end of integrated form camera lens is provided with the camera lens bayonet socket with described fuselage bayonet socket adaptation; On fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with N group fixed contact (12) and N group round and elastic contact (211); N group fixed contact (12) is arranged along the circumferential decile of circular open; N group round and elastic contact (211) arranges along the circumferential decile of described axial line, on fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with mutual adaptation for locking bayonet pin (14) and the pin-and-hole (224) of integrated form camera lens;
While engaging with integrated form camera lens, N group fixed contact (12) and N group round and elastic contact (211) are in contact with one another to form and are electrically connected to; Fuselage is provided with button or the thumb wheel for display frame is switched or sub-camera lens switches; Fuselage is provided with electronic viewfinder; Fuselage or integrated form camera lens are provided with focusing motor, are provided with the anti-shake system of optics on fuselage or integrated form camera lens; Imageing sensor is cmos sensor, and imageing sensor is individual layer or three layers of transducer; The top of fuselage is provided with photoflash lamp and tripper (3), is integrated with automatic/hand Focusing module in fuselage, and imageing sensor is square, and display screen is provided with touch sensitive layer; Imageing sensor is of a size of 4/3 picture, 135 silent frames or APS-H picture, APS-C picture, 1/1.63 inch of picture or 1/1.7 inch of picture.
Described fuselage can be fuselage, card camera fuselage, micro-one camera/mono-electric camera body of slr camera, can be also mobile phone (as i Phone or other smart mobile phones or non intelligent mobile phone).
Beneficial effect:
The shooting fuselage with a plurality of imageing sensors of the present invention, it is a kind of camera system of brand-new original creation, be different from existing main flow camera system completely, its core idea is: a plurality of sub-camera lens being integrated with on fuselage on a plurality of imageing sensors and integrated form camera lens is adaptive, can obtain a plurality of images or a plurality of video simultaneously.Major advantage of the present invention is as follows:
1) high image quality: due to integrated a plurality of transducers, and with the integrated form camera lens of fuselage adaptation in integrated a plurality of heads that focus, as everyone knows, focusing head compares with zoom lens and has higher optical property, therefore, focus between head the zoom lens and the single anti-zoom lens that switch than traditional card camera, more easily ensure high-quality image quality, its image quality can be accomplished anti-to focus head quite with single.
2) Picture switch is convenient, by thumb wheel or menu, switches (as touch-screen) or navigation key switching, can conveniently from an imageing sensor, be switched to another imageing sensor, switches easy.
3) good portability.Fuselage is integrated a plurality of imageing sensors, and suitable integrated form camera lens is integrated a plurality of tight shots (sub-camera lenses) with it, compares a plurality of independent camera lenses, portable better.The mode of this machine one mirror is equivalent to have the function of the many mirrors of original multistage machine, compact conformation, good portability.
4) battery flying power is strong.Because the process of zoom is without driving by motor, directly switch, thereby, can save to greatest extent electric energy, while especially using electronic viewfinder, more power saving, flying power can accomplish to work as with general list is anti-phase, and therefore, this point is compared card camera and had great advantage.When switching transducer, other imageing sensor dormancy only can be activated to a transducer, power saving effect is better like this.
5) while adopting len changeable bayonet socket docking, can adopt existing multiple bayonet type, for manufacturer, without the new bayonet socket [adopting original bayonet socket] of research and development, therefore, be convenient to promotion and implementation.
Can say, this shooting fuselage with a plurality of imageing sensors integrates many U.S.s, the high image quality that existing list is anti-, have and overcome a counter poor shortcoming of portability of wearing a plurality of camera lenses of list, the portability of existing card camera, compare again card camera and there is stronger battery duration performance, and structure is novel.
In sum, it is good that the advantage of maximum of the present invention is to have taken into account high image quality, portability, handover convenience, flying power, and market prospects are good.
Accompanying drawing explanation
Fig. 1 is the general structure schematic diagram of camera system (being integrated with fuselage of the present invention and integrated form camera lens);
Fig. 2 is the structural representation (4 transducers, the situation of 1 group of contact) in fuselage front;
Fig. 3 is the outside drawing of integrated form camera lens;
Fig. 4 is the cutaway view of integrated form camera lens;
Fig. 5 is the rear end structure schematic diagram (4 transducers, the situation of 1 group of contact) of integrated form camera lens;
Fig. 6 is the structural representation (4 transducers, the situation of 4 groups of contacts) in fuselage front;
Fig. 7 is the rear end structure schematic diagram (4 transducers, the situation of 4 groups of contacts) of integrated form camera lens;
Fig. 8 is the structural representation (6 transducers, the situation of 1 group of contact) in fuselage front;
Fig. 9 is the rear end structure schematic diagram (6 transducers, the situation of 1 group of contact) of integrated form camera lens;
Figure 10 is the structural representation (3 transducers, the situation of 1 group of contact) in fuselage front;
Figure 11 is the rear end structure schematic diagram (3 transducers, the situation of 1 group of contact) of integrated form camera lens.
Label declaration: 1-fuselage, 2-integrated form camera lens, 3-tripper, 4-camera lens,
11-fuselage bayonet socket, 12-fixed contact; 13-imageing sensor; 14-bayonet pin.
211-round and elastic contact; 213-light transmission passage;
221-tread plate, 224-pin-and-hole.
Embodiment
Below with reference to the drawings and specific embodiments, the present invention is described in further details:
Embodiment 1:
As Fig. 1-5, a kind of shooting fuselage with a plurality of imageing sensors, during use, fuselage (1) and integrated form camera lens (2) adaptation; Fuselage front panel is provided with the circular open as integrated form lens interface, and described integrated form camera lens is docked on this circular open;
In described fuselage, be provided with 4 imageing sensors (13); In the lens barrel of described integrated form camera lens, be integrated with 4 sub-camera lenses (4) with different focal; In each sub-camera lens, include an arrangement of mirrors sheet;
A described N imageing sensor is all offset the axis setting of described circular open, and 4 imageing sensors are along the circumferential arrangement of axis, and imageing sensor place plane is vertical with described axis; The center of 4 imageing sensors is all identical with the distance of described axis;
The optical axis of 4 sub-camera lenses all with the axis parallel of integrated form camera lens; And 4 sub-lens arrangement axial line circumferentially;
The optical axis of 4 sub-camera lenses is aimed at 4 imageing sensor central points respectively, forms 4 imaging optical paths;
Fuselage is electrically connected to integrated form camera lens by contact; [for communication, and being the power supply of integrated form camera lens for the treatment of device], [as distortion, fuselage can also be electrically connected to integrated form camera lens by wire; While connecting by wire, can be welding, can be also on integrated form camera lens and fuselage, to be respectively provided with a socket, with the wire with plug, connects.] fuselage is provided with display screen.
4 imageing sensors are positioned at same plane and arrange along the circumferential decile of axis; 4 sub-camera lenses are arranged along the circumferential decile of axial line.--adopting this arrangement is for more attractive in appearance, if adopt asymmetrical pattern, is also fine.As long as form 4 imaging optical paths.
Circular open is fuselage bayonet socket (11), and the rear end of integrated form camera lens is provided with the camera lens bayonet socket with described fuselage bayonet socket adaptation; On fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with mutual adaptation for locking bayonet pin (14) and the pin-and-hole (224) of integrated form camera lens.[bayonet socket is detachable camera mode, as distortion, other patterns such as can also weld fixes, other patterns are non-dismountable pattern, as the annexation of the camera lens of many card type digital cameras and fuselage, being prior art] fit structure of bayonet pin-pin-and-hole is the common technology means that existing bayonet socket adopts.
On fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with one group of fixed contact (12) and one group of round and elastic contact (211), when fuselage engages with integrated form camera lens, fixed contact (12) and round and elastic contact (211) are in contact with one another to form and are electrically connected to.
Fuselage is provided with button or the thumb wheel for display frame is switched or sub-camera lens switches.[display frame is switched, and refers to and is switched to still image or the Real-time Motion Image that different imageing sensors obtains]
Fuselage is provided with electronic viewfinder.Thumb wheel, button and electronic viewfinder and display screen etc. are existing mature technology.
Embodiment 2:
All the other are with embodiment 1, and difference is, referring to Fig. 6 and Fig. 7, is respectively equipped with 4 groups of fixed contacts (12) and 4 groups of round and elastic contacts (211) on fuselage bayonet socket and camera lens bayonet socket; 4 groups of fixed contacts (12) are arranged along the circumferential decile of circular open; 4 groups of round and elastic contacts (211) are along the circumferential decile layout of described axial line, and while engaging with integrated form camera lens, 4 groups of fixed contacts (12) and N group round and elastic contact (211) are in contact with one another to form and are electrically connected to.Contact is uniformly distributed like this, and profile is also more attractive in appearance, and it is more to work as number of contacts, more reasonable by this pattern.
Embodiment 3:
All the other are with embodiment 1, and difference is, referring to Fig. 8 and Fig. 9, integrated form camera lens is integrated with 6 sub-camera lenses, is integrated with 6 imageing sensors in fuselage.
Embodiment 4:
All the other are with embodiment 1, and difference is, referring to Figure 10 and Figure 11, integrated form camera lens is integrated with 3 sub-camera lenses, is integrated with 3 imageing sensors in fuselage.
All the other it should be noted that: fuselage or integrated form camera lens are provided with focusing motor, are provided with the anti-shake system of optics on fuselage or integrated form camera lens; Imageing sensor is cmos sensor, and imageing sensor is individual layer or three layers of transducer; The top of fuselage is provided with photoflash lamp and tripper (3), is integrated with automatic/hand Focusing module in fuselage, and imageing sensor is square, and display screen is provided with touch sensitive layer; Imageing sensor is of a size of 4/3 picture, 135 silent frames or APS-H picture, APS-C picture, 1/1.63 inch of picture or 1/1.7 inch of picture.
Imageing sensor can be ccd sensor, can be also cmos sensor, can be the mosaic transducer of individual layer, can be also the transducer of three layers, (the FOVEON X3 full color image sensing chip adopting with reference to sigma company)
Can adopt socket to realize camera lens and be connected with the processor of fuselage, the electrical interface by wire connection socket and integrated form camera lens, completes data communication, and is that integrated form camera lens is powered by this socket.
Imageing sensor is ccd sensor or cmos sensor; Imageing sensor is individual layer mosaic transducer or three layers of X3 type transducer [as the FOVEON X3 full color image sensing chip of sigma company employing];
Bayonet socket can be any in F bayonet socket [nikon company adopt bayonet socket], EF bayonet socket [the anti-bayonet socket adopting of list of canon company], M bayonet socket [micro-single bayonet socket adopting of canon company], SA bayonet socket [bayonet socket that sigma company adopts], a bayonet socket (bayonet socket that sony company adopts) and E bayonet socket (bayonet socket of sony company employing).[can also be existing bayonet socket and the newly-designed bayonet socket of other types, because the type of bayonet socket is not innovative point of the present invention]
Adopt this shooting fuselage with a plurality of imageing sensors, its method of obtaining image is: light projects respectively on N imageing sensor by N sub-camera lens of integrated form camera lens, form N digital document, processor integrated in fuselage is stored at least one digital document in this N digital document in memory integrated in fuselage; Described digital document is image or video.
When described digital document is image, adopt following any mode that image is stored in memory integrated in fuselage;
Method 1: the image file that is RAW form by unprocessed form is directly stored in memory;
Method 2: after the image file of RAW form is carried out in machine processing, the image file that converts JPG form to is stored in memory;
Method 3: both the image file of RAW form was stored in memory, the image file of the JPG the form also converting of image file by RAW form being formed is stored in memory.
By thumb wheel or navigation key, select transducer and the corresponding sub-camera lens of work at present, and realtime graphic is projected in electronic viewfinder.
When starting live view function, by thumb wheel or navigation key, select transducer and the corresponding sub-camera lens of work at present, and realtime graphic is shown in real time on display screen, be convenient to focusing operation in real time.
In the time of storage, can arrange by pattern, preserve N width digital picture simultaneously, also can only preserve the current current image of choosing passage of choosing by thumb wheel or navigation key.
The story board of integrated form camera lens can arrange a plurality of different focal, as 14mm, and 24mm, 35mm, 50mm, 85mm, 100mm, 105mm, 150mm, 180mm, 200mm, 400mm etc.
Claims (10)
1. a shooting fuselage with a plurality of imageing sensors, is characterized in that, on fuselage (1) front panel, is provided with the circular open as integrated form lens interface;
In described fuselage, be provided with N imageing sensor (13); 3≤N≤12, N is natural number;
A described N imageing sensor is all offset the axis setting of described circular open, and N imageing sensor is along the circumferential arrangement of axis, and imageing sensor place plane is vertical with described axis; The center of N imageing sensor is all identical with the distance of described axis;
Fuselage is electrically connected to integrated form camera lens by contact or wire;
Fuselage is provided with display screen.
2. the shooting fuselage with a plurality of imageing sensors according to claim 1, is characterized in that, N imageing sensor is positioned at same plane and arranges along the circumferential decile of axis; N sub-camera lens arranged along the circumferential decile of axial line.
3. the shooting fuselage with a plurality of imageing sensors according to claim 1, is characterized in that, N is the integer between 4-6.
4. the shooting fuselage with a plurality of imageing sensors according to claim 1, is characterized in that, is integrated with N the sub-camera lens (4) with different focal in the lens barrel of described integrated form camera lens; In each sub-camera lens, include an arrangement of mirrors sheet; The optical axis of N sub-camera lens all with the axis parallel of integrated form camera lens; And the individual sub-lens arrangement of N is circumferential axial line;
The optical axis of N sub-camera lens is aimed at N imageing sensor central point respectively, forms N bar imaging optical path.
5. the shooting fuselage with a plurality of imageing sensors according to claim 1, is characterized in that, circular open is fuselage bayonet socket (11), and the rear end of integrated form camera lens is provided with the camera lens bayonet socket with described fuselage bayonet socket adaptation; On fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with mutual adaptation for locking bayonet pin (14) and the pin-and-hole (224) of integrated form camera lens.
6. the shooting fuselage with a plurality of imageing sensors according to claim 1, it is characterized in that, on fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with one group of fixed contact (12) and one group of round and elastic contact (211), when fuselage engages with integrated form camera lens, fixed contact (12) and round and elastic contact (211) are in contact with one another to form and are electrically connected to.
7. the shooting fuselage with a plurality of imageing sensors according to claim 1, is characterized in that, is respectively equipped with N group fixed contact (12) and N group round and elastic contact (211) on fuselage bayonet socket and camera lens bayonet socket; N group fixed contact (12) is arranged along the circumferential decile of circular open; N group round and elastic contact (211) is along the circumferential decile layout of described axial line, and while engaging with integrated form camera lens, N group fixed contact (12) and N group round and elastic contact (211) are in contact with one another to form and are electrically connected to.
8. according to the shooting fuselage with a plurality of imageing sensors described in claim 1-7 any one, it is characterized in that, fuselage is provided with button or the thumb wheel for display frame is switched or sub-camera lens switches.
9. the shooting fuselage with a plurality of imageing sensors according to claim 8, is characterized in that, fuselage is provided with electronic viewfinder; Fuselage or integrated form camera lens are provided with focusing motor, are provided with the anti-shake system of optics on fuselage or integrated form camera lens.
10. the shooting fuselage with a plurality of imageing sensors according to claim 2, is characterized in that, N is the integer between 4-6;
In the lens barrel of described integrated form camera lens, be integrated with N the sub-camera lens (4) with different focal; In each sub-camera lens, include an arrangement of mirrors sheet; The optical axis of N sub-camera lens all with the axis parallel of integrated form camera lens; And the individual sub-lens arrangement of N is circumferential axial line;
The optical axis of N sub-camera lens is aimed at N imageing sensor central point respectively, forms N bar imaging optical path;
Circular open is fuselage bayonet socket (11), and the rear end of integrated form camera lens is provided with the camera lens bayonet socket with described fuselage bayonet socket adaptation; On fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with N group fixed contact (12) and N group round and elastic contact (211); N group fixed contact (12) is arranged along the circumferential decile of circular open; N group round and elastic contact (211) arranges along the circumferential decile of described axial line, on fuselage bayonet socket and camera lens bayonet socket, be respectively equipped with mutual adaptation for locking bayonet pin (14) and the pin-and-hole (224) of integrated form camera lens;
While engaging with integrated form camera lens, N group fixed contact (12) and N group round and elastic contact (211) are in contact with one another to form and are electrically connected to; Fuselage is provided with button or the thumb wheel for display frame is switched or sub-camera lens switches; Fuselage is provided with electronic viewfinder; Fuselage or integrated form camera lens are provided with focusing motor, are provided with the anti-shake system of optics on fuselage or integrated form camera lens; Imageing sensor is cmos sensor, and imageing sensor is individual layer or three layers of transducer; The top of fuselage is provided with photoflash lamp and tripper (3), is integrated with automatic/hand Focusing module in fuselage, and imageing sensor is square, and display screen is provided with touch sensitive layer; Imageing sensor is of a size of 4/3 picture, 135 silent frames or APS-H picture, APS-C picture, 1/1.63 inch of picture or 1/1.7 inch of picture.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310628566.4A CN103595905A (en) | 2013-11-30 | 2013-11-30 | Camera body provided with a plurality of image sensors |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310628566.4A CN103595905A (en) | 2013-11-30 | 2013-11-30 | Camera body provided with a plurality of image sensors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103595905A true CN103595905A (en) | 2014-02-19 |
Family
ID=50085876
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310628566.4A Pending CN103595905A (en) | 2013-11-30 | 2013-11-30 | Camera body provided with a plurality of image sensors |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103595905A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110546949A (en) * | 2017-07-05 | 2019-12-06 | 达美尔电子有限及两合公司 | Multi-sensor camera |
| CN112637452A (en) * | 2020-12-07 | 2021-04-09 | Oppo广东移动通信有限公司 | Camera module and electronic device |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6611289B1 (en) * | 1999-01-15 | 2003-08-26 | Yanbin Yu | Digital cameras using multiple sensors with multiple lenses |
| CN201015021Y (en) * | 2007-01-22 | 2008-01-30 | 周铄 | Digital camera |
| CN201156104Y (en) * | 2007-09-13 | 2008-11-26 | 首都师范大学 | Multi-lens construction of wide array digital camera |
| CN101668115A (en) * | 2008-09-03 | 2010-03-10 | 中国科学院自动化研究所 | Multi-lens multi-resolution camera |
| CN101860760A (en) * | 2009-04-10 | 2010-10-13 | 张冬云 | Performance improvement of multi-lens multi-sensor imaging system |
| CN102131044A (en) * | 2010-01-20 | 2011-07-20 | 鸿富锦精密工业（深圳）有限公司 | Camera module |
| CN102739949A (en) * | 2011-04-01 | 2012-10-17 | 张可伦 | Control method for multi-lens camera and multi-lens device |
-
2013
- 2013-11-30 CN CN201310628566.4A patent/CN103595905A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6611289B1 (en) * | 1999-01-15 | 2003-08-26 | Yanbin Yu | Digital cameras using multiple sensors with multiple lenses |
| CN201015021Y (en) * | 2007-01-22 | 2008-01-30 | 周铄 | Digital camera |
| CN201156104Y (en) * | 2007-09-13 | 2008-11-26 | 首都师范大学 | Multi-lens construction of wide array digital camera |
| CN101668115A (en) * | 2008-09-03 | 2010-03-10 | 中国科学院自动化研究所 | Multi-lens multi-resolution camera |
| CN101860760A (en) * | 2009-04-10 | 2010-10-13 | 张冬云 | Performance improvement of multi-lens multi-sensor imaging system |
| CN102131044A (en) * | 2010-01-20 | 2011-07-20 | 鸿富锦精密工业（深圳）有限公司 | Camera module |
| CN102739949A (en) * | 2011-04-01 | 2012-10-17 | 张可伦 | Control method for multi-lens camera and multi-lens device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110546949A (en) * | 2017-07-05 | 2019-12-06 | 达美尔电子有限及两合公司 | Multi-sensor camera |
| CN112637452A (en) * | 2020-12-07 | 2021-04-09 | Oppo广东移动通信有限公司 | Camera module and electronic device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101963741B (en) | Image pickup module and portable electronic device adopting same | |
| CN103702022A (en) | Novel bayonet and integrated lens-based image obtaining method | |
| CN103592809B (en) | There is the integrated camera lens of two-part structure | |
| CN103676416B (en) | A kind of camera body with bayonet socket and single offset sensor | |
| CN103595905A (en) | Camera body provided with a plurality of image sensors | |
| CN103618849A (en) | Image shooting method based on integrated lens and multiple image sensors | |
| CN103607532A (en) | Image pick-up system with integrated type camera lens and multiple image sensors | |
| CN103716522B (en) | Image obtaining system with bayonet and integrated lens | |
| CN103595907A (en) | Image obtaining method based on lens with two integrated segments and camera body with single offset sensor | |
| CN204119330U (en) | A kind ofly be installed on the changeable optical module moving lens shaft of mobile terminal | |
| CN103607531A (en) | Integrated type camera lens | |
| CN103595906A (en) | Image obtaining system based on lens with two integrated segments and camera body with single offset sensor | |
| CN103685898B (en) | A kind of integrated form camera lens with bayonet socket | |
| CN204129417U (en) | A kind ofly be installed on the controlled optical module of mobile terminal filtered color | |
| CN204116783U (en) | A kind of optical module being installed on two kinds of imaging patterns of mobile terminal | |
| CN204116781U (en) | A kind of stabilization optical module being installed on mobile terminal | |
| CN103595908A (en) | Camera body with single offset sensor | |
| CN103685901A (en) | Image obtaining method based on novel electric control mount and integrated lens | |
| CN204116784U (en) | A kind ofly be installed on the adjustable optical module of mobile terminal sensing station | |
| CN106470302A (en) | Many camera lenses camera module and its image switching method and many lens camera systems | |
| CN204116791U (en) | A kind of optical module being installed on mobile terminal minimizing imaging time | |
| CN204129419U (en) | A kind ofly be installed on the optical module that mobile terminal has shade function | |
| CN204116782U (en) | A kind of mobile terminal that is installed on prevents over-exposed optical module | |
| CN204116790U (en) | A kind ofly be installed on the adjustable optical module of mobile terminal sensing station | |
| CN204119327U (en) | A kind ofly be installed on the changeable optical module moving lens shaft of mobile terminal |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20140219 |
|
| RJ01 | Rejection of invention patent application after publication |