CN103607531A - Integrated type camera lens - Google Patents
Integrated type camera lens Download PDFInfo
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- CN103607531A CN103607531A CN201310629843.3A CN201310629843A CN103607531A CN 103607531 A CN103607531 A CN 103607531A CN 201310629843 A CN201310629843 A CN 201310629843A CN 103607531 A CN103607531 A CN 103607531A
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Abstract
The invention discloses an integrated type camera lens. According to the integrated type camera lens, N sub camera lenses (4) having different focal lengths are integrated in a lens cone, wherein 3<=N<=1, and N is a natural number; each sub camera lens comprises a set of lenses; optical axes of the N sub camera lenses are all parallel to the axial lead of the integrated type camera lens; the N sub camera lenses are arranged in the circumferential direction of the axial lead; the integrated type camera lens is electrically connected a camera body of a camera through contacts or wires. A round opening which serves as an integrated type camera lens mount is formed in a front panel of the camera body, the integrated type camera lens is arranged on the round opening in a butt joint mode, the round opening serves as a camera body bayonet (11), a camera lens bayonet which is matched with the camera body bayonet (11) is arranged at the rear end of the integrated type camera lens, a bayonet pin (14) is arranged on the camera body bayonet, a pin hole (224) is formed in the camera lens bayonet, and the bayonet pin (14) and the pin hole (224) are matched with each other and used for locking the integrated type camera lens. The integrated type camera lens is high in integration level, convenient to use, and good in portability.
Description
Technical field
The present invention relates to a kind of integrated form camera lens.
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, the camera lens that designs a kind of uniqueness is one of this novel camera system key issue to be solved.
Summary of the invention
Technical problem to be solved by this invention is to provide a kind of integrated form camera lens, and this integrated form camera lens integrated level is high, easy to use, good portability.
The technical solution of invention is as follows:
An integrated form camera lens, is integrated with N the sub-camera lens (4) with different focal in lens barrel; 3≤N≤12, N is natural number; 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;
Integrated form camera lens is electrically connected to the fuselage of camera by contact or wire.
The front panel of described fuselage is provided with the circular open as integrated form lens interface, and described integrated form camera lens is docked on this circular open; Circular open is fuselage bayonet socket (11), and the rear end of integrated form camera lens is provided with the camera lens bayonet socket adaptive with described fuselage bayonet socket (11); 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.
N is the integer between 4-6.
In described fuselage, be provided with N imageing sensor (13); 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 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]
The optical axis of N sub-camera lens is aimed at N imageing sensor central point respectively, forms N bar imaging optical path;
Fuselage is provided with display screen; [for communication, and being the power supply of integrated form camera lens for the treatment of device]
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;
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;
The front panel of described fuselage 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 N imageing sensor (13); 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;
The optical axis of N sub-camera lens is aimed at N imageing sensor central point respectively, forms N bar imaging optical path;
Fuselage is provided with display screen; [for communication, and being the power supply of integrated form camera lens for the treatment of device]
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;
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:
Integrated form camera lens of the present invention, it is a kind of camera lens of brand-new original creation, be different from existing main flow lens design 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 this integrated form camera lens 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 and switch than the zoom lens of the traditional card camera zoom lens anti-with list, more easily ensure high-quality image quality, its image quality can be accomplished anti-to focus head quite with single.
2) focal length easy switching, switches (as touch-screen) or navigation key switching conduct cooperation by fuselage thumb wheel or menu, can conveniently from a sub-camera lens, be switched to another sub-camera lens, switches easy.
3) good portability.Integrated form camera lens is integrated a plurality of tight shots (sub-camera lenses), compares a plurality of independent camera lenses, portable better.
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.In fuselage operation with matching, 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 integrated form camera lens 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, compares again card camera and has 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 with the camera system of 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 integrated form camera lens, is connected with fuselage (1), and 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 integrated form camera lens, 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 (8)
1. an integrated form camera lens, is characterized in that, is integrated with N the sub-camera lens (4) with different focal in lens barrel; 3≤N≤12, N is natural number; 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;
Integrated form camera lens is electrically connected to the fuselage of camera by contact or wire.
2. integrated form camera lens according to claim 1, is characterized in that, the front panel of described fuselage is provided with the circular open as integrated form lens interface, and described integrated form camera lens is docked on this circular open; Circular open is fuselage bayonet socket (11), and the rear end of integrated form camera lens is provided with the camera lens bayonet socket adaptive with described fuselage bayonet socket (11); 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.
3. integrated form camera lens according to claim 2, 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.
4. integrated form camera lens according to claim 2, 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.
5. integrated form camera lens according to claim 1, is characterized in that, N is the integer between 4-6.
6. according to the integrated form camera lens described in claim 1-5 any one, it is characterized in that, in described fuselage, be provided with N imageing sensor (13); 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 provided with button or the thumb wheel for display frame is switched or sub-camera lens switches.
The optical axis of N sub-camera lens is aimed at N imageing sensor central point respectively, forms N bar imaging optical path;
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;
Fuselage is provided with electronic viewfinder.
7. integrated form camera lens according to claim 6, is characterized in that, fuselage or integrated form camera lens are provided with focusing motor, is provided with the anti-shake system of optics on fuselage or integrated form camera lens.
8. integrated form camera lens according to claim 1, is characterized in that, N is the integer between 4-6;
The front panel of described fuselage 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 N imageing sensor (13); 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;
The optical axis of N sub-camera lens is aimed at N imageing sensor central point respectively, forms N bar imaging optical path;
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;
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.
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| CN201310629843.3A CN103607531A (en) | 2013-11-30 | 2013-11-30 | Integrated type camera lens |
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| CN201310629843.3A CN103607531A (en) | 2013-11-30 | 2013-11-30 | Integrated type camera lens |
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