CN103676416B - A kind of camera body with bayonet socket and single offset sensor - Google Patents
A kind of camera body with bayonet socket and single offset sensor Download PDFInfo
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- CN103676416B CN103676416B CN201410000131.XA CN201410000131A CN103676416B CN 103676416 B CN103676416 B CN 103676416B CN 201410000131 A CN201410000131 A CN 201410000131A CN 103676416 B CN103676416 B CN 103676416B
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Abstract
The invention discloses a kind of camera body with Novel bayonet and single offset sensor, fuselage front panel is provided with the fuselage bayonet socket (5) for docking with camera lens; (1) camera lens described in is integrated form camera lens, and integrated form camera lens is docked on this fuselage bayonet socket (5); 1 imageing sensor (13) is provided with in described fuselage; The axis that described imageing sensor offsets described fuselage bayonet socket (5) is arranged, imageing sensor place plane and described axes normal; (2) camera lens described in is integrated form camera lens (2), is integrated with N number of sub-camera lens (4) with different focal in the lens barrel of described integrated form camera lens; Adopt the novel bayonet socket based on fore shaft change and telescopic catch mechanism.This camera body integrated level with Novel bayonet and single offset sensor is high, easy to use, after integrated form bayonet socket adaptation, can take into account the remarkable optical property of multiple tight shot and the portability of a machine (fuselage) mirror (camera lens).
Description
Technical field
The present invention relates to a kind of camera body with bayonet socket and single offset sensor.
Background technology
Existing main flow camera system is divided into interchangeable lenses camera and not interchangeable lens camera generally.
Not interchangeable lens camera mainly card camera, namely a fuselage and a camera lens is adopted, and fuselage and camera lens are fixed together completely, cannot dismantle when user uses, the maximum problem of this pattern is exactly, 1) if automatic zoom camera lens, the zoom of its camera lens needs to be driven by fuselage, power consumption is exceedingly fast, the flying power of battery is poor, general one piece of battery can only take tens photos or hundred multiple pictures, although very light generally, battery durable ability cannot meet the requirement of users.
For len changeable camera, mainly single anti-and micro-list (as the micro-list of nex series of Sony, the J series of Nikon, the E0SM series of Canon); See Fig. 1, this camera is all have a slice imageing sensor in fuselage, owing to adopting len changeable bayonet socket, thus by the support of camera lens group to obtain excellent imaging.But the shortcoming of this camera is also apparent, because a camera lens once can only be accessed, for professional photographer, need to be equipped with and multiplely focus head, travelling or when performing special shooting task, need to carry many pieces of camera lenses to go 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 rugged surroundings, the process of changing camera lens becomes difficult all the more.
Therefore, be necessary the camera system designing a kind of brand-new style, and the design of fuselage is one of core of the camera system of this brand-new style.
Summary of the invention
Technical matters to be solved by this invention is to provide a kind of camera body with bayonet socket and single offset sensor, this camera body integrated level with bayonet socket and single offset sensor is high, easy to use, after integrated form bayonet socket adaptation, the remarkable optical property of multiple tight shot and the portability of a machine (fuselage) mirror (camera lens) can be taken into account.
The technical solution of invention is as follows:
Have a camera body for bayonet socket and single offset sensor, fuselage front panel is provided with the fuselage bayonet socket (5) for docking with camera lens;
(1) 1 imageing sensor (13) is provided with in the fuselage described in; Described imageing sensor offset described fuselage bayonet socket (5) axis arrange [described skew can be the skew in any direction, as relative to 0 ° of the bayonet socket center of circle, 45 °, 90 °, 180 ° (as shown in Figure 3)], imageing sensor place plane and described axes normal;
(2) camera lens described in is integrated form camera lens (2), and integrated form camera lens is docked on this fuselage bayonet socket (5); N number of sub-camera lens (4) with different focal is integrated with in the lens barrel of described integrated form camera lens; 3≤N≤12, N is natural number; An arrangement of mirrors sheet is included in each sub-camera lens;
The optical axis of N number of sub-camera lens all with the axis parallel of integrated form camera lens; And N number of sub-lens arrangement is in the circumference of axial line;
(3) one group of stationary contact (12) is provided with in fuselage bayonet socket, camera lens rear end has one group of round and elastic contact (17), the camera lens bayonet socket of integrated form camera lens rear end is installed on after on fuselage bayonet socket (5), described stationary contact (12) and round and elastic contact (17) correspondence contacts, and completes docking of camera lens and fuselage;
Fuselage bayonet socket is columnar structured, and the inwall of fuselage bayonet socket is provided with the snap ring (51) that has M breach (52); 2≤M≤9, M is integer;
Each indentation, there is provided with a telescopic catch mechanism; Telescopic catch mechanism described in each comprises dynamic catch (9), the servo-actuated orienting lug (15) of dynamic catch both sides setting, 2 guideposts (14) and 2 extension springs (11); 2 guiding storehouses are respectively provided with in the snap ring of each breach both sides; 2 described guideposts are separately positioned in these 2 guiding storehouses; 2 extension springs are set on 2 guideposts, and 2 servo-actuated orienting lugs are set on 2 guideposts and are also connected with 2 extension springs respectively; The rear end of dynamic catch is the teat of circular arc or ellipse arc; [namely teat is outline is elliptic arc or circular arc]
The outer ring of fuselage bayonet socket is provided with the fore shaft change (6) for driving described telescopic catch mechanism; The inwall of fore shaft change is provided with M projection; [projection is circular arc or ellipse arc]; The M sheet quiet catch (18) suitable with described breach is provided with outside the bayonet socket of the rear end of camera lens;
M projection, a M breach, the quiet catch of M sheet and M dynamic catch is circumferential spaced set;
Along with fore shaft change is rotated, when the top of the teat of catch dynamic described in bump contact, the leading portion of dynamic catch reaches maximum position to seal described breach (52), [now the quiet catch of camera lens is locked in inside snap ring and projection, realize the locking of camera lens, now camera lens can rotate relative to fuselage, to switch sub-camera lens]
When projection does not contact with the teat of described dynamic catch, dynamic catch retracts to maximum position to abdicate described breach (52) under the effect of extension spring (11); [now breach is opened, and the quiet catch on camera lens can free in and out, and is convenient to load onto or take off camera lens];
After integrated form camera lens and fuselage complete and dock, the optical axis of a sub-camera lens in N number of sub-camera lens is aimed at image sensor center point, forms imaging optical path.
Fuselage is provided with display screen.
A shank is provided with at fuselage bayonet socket, camera lens bayonet socket is provided with for circumference locking integrated form camera lens N number of pin-and-hole [shank (21) and pin-and-hole (20) are the common components in existing slr camera opening, in addition, fuselage is also provided with for driving the camera lens of this bayonet pin to lock/discharge button].
Fuselage is provided with electronic viewfinder or optical finder, and fuselage or integrated form camera lens are provided with focusing motor, and fuselage or integrated form camera lens are provided with optical anti-vibration system.
N is the integer between 4-6.
Fore shaft change is provided with axial slide block (7), is provided with the guiding stop chute (8) of circular arc in camera lens bayonet socket, and slide block external part is arranged in guiding stop chute.(such fore shaft change can not unrestrictedly rotate, and can only rotate to an angle)
The torsion spring resetted for fore shaft change is provided with between bayonet socket and fore shaft change.[not shown, be prior art, its effect is: when external force does not act in fore shaft change, and drive fore shaft change to turn to an extreme position, this position just promotes dynamic catch and overcomes the pulling force of extension spring to block breach, position as described in Figure 10.Ensure camera lens normal condition can not come off from fuselage and fall break]
Described fuselage is the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electric camera body or handset (as i Phone or other smart mobile phones or non intelligent mobile phone).
As preferably, N is the integer between 4-6; Fuselage is provided with electronic viewfinder, and fuselage or integrated form camera lens are provided with focusing motor, and fuselage or integrated form camera lens are provided with optical anti-vibration system; Fore shaft change is provided with axial slide block (7), is provided with the guiding stop chute (8) of circular arc in camera lens bayonet socket, and slide block external part is arranged in guiding stop chute; The torsion spring resetted for fore shaft change is provided with between bayonet socket and fore shaft change;
Be integrated with automatic/hand Focusing module in fuselage, imageing sensor is square, and display screen is provided with touch sensitive layer; Imageing sensor is cmos sensor, and imageing sensor is individual layer or three layers of sensor; The top of fuselage is provided with flashlamp and tripper (3), and be integrated with automatic/hand Focusing module in fuselage, 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, and described fuselage is the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electric camera body or handset.
Beneficial effect:
The camera body with bayonet socket and single offset sensor of the present invention, it is a kind of fuselage of camera system of original creation completely newly, the novel camera system formed after this fuselage docks with integrated form camera lens is different from existing main flow camera system completely, its core idea is: fuselage is integrated with a biased imageing sensor, multiple sub-camera lens on this imageing sensor and integrated form camera lens is adaptive, carry out sub-Shot change by camera lens bayonet socket with the relative rotation of fuselage bayonet socket and realize manual zoom, thus obtain high-quality image or video.Major advantage of the present invention is as follows:
1) high image quality: multiplely focus head because integrated form camera lens is integrated with, as everyone knows, focus head to compare, with zoom lens, there is higher optical property, therefore, focus between head and switch the zoom lens anti-with list compared to the zoom lens of traditional card camera, more easily ensure high-quality image quality, its image quality can be accomplished with single anti-to focus head suitable.
2) focal length easy switching, by the relative rotation of camera lens bayonet socket with fuselage bayonet socket, can, easily from a sub-Shot change to another sub-camera lens, switch easy.
3) good portability.An integrated form camera lens is integrated with multiple tight shot (sub-camera lens), and compare multiple independent camera lens, portability is better.
4) battery durable ability is strong.Because the process of zoom is without the need to driving by motor, directly switch, thus, electric energy can be saved to greatest extent, when especially using electronic viewfinder, more power saving, flying power can accomplish work as anti-phase with general list, and therefore, this point is compared card camera and had great advantage.
5) adopt len changeable bayonet socket to dock, change camera lens convenient.
6) adopt the opening and closing of fore shaft change and telescopic catch mechanism controls breach, to facilitate the handling of camera lens, this is a kind of brand-new bayonet socket pattern, constructs ingenious, easy to implement, is easy to operation.
7) adopt torsion spring, slide block and guiding stop chute that dynamic catch is resetted in time, ensure camera lens safety, thus security is high.
Can say, this camera body with bayonet socket and single offset sensor integrates many U.S.s, the high image quality that existing list is anti-, overcome again an anti-shortcoming wearing the portability difference of multiple camera lens of list, the portability of existing card camera, compare again card camera and there is stronger battery durable performance, and structure is novel.
In sum, the maximum advantage of the present invention is to have taken into account high image quality, portability, handover convenience, flying power are good, and market outlook are good.
Accompanying drawing explanation
Fig. 1 is existing airframe structure schematic diagram;
Fig. 2 is the general structure schematic diagram of the image acquisition system with bayonet socket and integrated form camera lens;
Fig. 3 is the structural representation in fuselage front;
Fig. 4 is fuselage bayonet socket outside drawing;
Fig. 5 is the inner structure schematic diagram of fuselage bayonet socket;
Fig. 6 is fuselage bayonet socket radial section figure (when breach is opened state);
Fig. 7 is fuselage bayonet socket radial section figure (when breach is closed state);
Fig. 8 is the setting position schematic diagram of guiding stop chute;
Fig. 9 is A place enlarged drawing in Fig. 6;
Figure 10 is B place enlarged drawing in Fig. 7;
Figure 11 is the outside drawing of integrated form camera lens;
Figure 12 is the rear end structure schematic diagram of integrated form camera lens;
Figure 13 is the axial cut-open view of integrated form camera lens;
Figure 14 is the structural representation of the rear end of the integrated form camera lens with 3 sub-camera lenses; [parts such as not shown quiet catch]
Figure 15 is the structural representation of the rear end of the integrated form camera lens with 6 sub-camera lenses; [parts such as not shown quiet catch]
Label declaration: 1-fuselage, 2-integrated form camera lens, 3-tripper, 4-camera lens, 5-fuselage bayonet socket, the change of 6-fore shaft, 7-slide block, 8-guiding stop chute, 9-moves catch, 10-projection, 11-extension spring; 12-stationary contact; 13-photo-sensitive cell; 14-guidepost, the servo-actuated orienting lug of 15-.16-tread plate, 17-round and elastic contact; The quiet catch of 18-, 19-light transmission passage.20-pin-and-hole, 21-shank.
51-snap ring, 52-breach.
Embodiment
Below with reference to the drawings and specific embodiments, the present invention is described in further details:
Embodiment 1:
As Fig. 2-13, a kind of camera body with bayonet socket and single offset sensor, fuselage front panel is provided with the fuselage bayonet socket (5) for docking with camera lens; Fuselage and camera lens form the image acquisition system with bayonet socket and integrated form camera lens;
(1) camera lens described in is integrated form camera lens, and integrated form camera lens is docked on this fuselage bayonet socket (5); 1 imageing sensor (13) is provided with in described fuselage;
Described imageing sensor offset described fuselage bayonet socket (5) axis arrange [described skew can be the skew in any direction, as relative to 0 ° of the bayonet socket center of circle, 45 °, 90 °, 180 ° (as shown in Figure 3)], imageing sensor place plane and described axes normal;
(2) camera lens described in is integrated form camera lens (2), is integrated with N number of sub-camera lens (4) with different focal in the lens barrel of described integrated form camera lens; 3≤N≤12, N is natural number; An arrangement of mirrors sheet is included in each sub-camera lens;
The optical axis of N number of sub-camera lens all with the axis parallel of integrated form camera lens; And N number of sub-lens arrangement is in the circumference of axial line;
(3) one group of stationary contact (12) is provided with in fuselage bayonet socket, camera lens rear end has one group of round and elastic contact (17), the camera lens bayonet socket of integrated form camera lens rear end is installed on after on fuselage bayonet socket (5), described stationary contact (12) and round and elastic contact (17) correspondence contacts, and completes docking of camera lens and fuselage;
Fuselage bayonet socket is columnar structured, and the inwall of fuselage bayonet socket is provided with the snap ring (51) that has M breach (52); 2≤M≤9, M is integer;
Each indentation, there is provided with a telescopic catch mechanism; Telescopic catch mechanism described in each comprises dynamic catch (9), the servo-actuated orienting lug (15) of dynamic catch both sides setting, 2 guideposts (14) and 2 extension springs (11); 2 guiding storehouses are respectively provided with in the snap ring of each breach both sides; 2 described guideposts are separately positioned in these 2 guiding storehouses; 2 extension springs are set on 2 guideposts, and 2 servo-actuated orienting lugs are set on 2 guideposts and are also connected with 2 extension springs respectively; The rear end of dynamic catch is the teat of circular arc or ellipse arc; [namely teat is outline is elliptic arc or circular arc]
The outer ring of fuselage bayonet socket is provided with the fore shaft change (6) for driving described telescopic catch mechanism; The inwall of fore shaft change is provided with M projection; [projection is circular arc or ellipse arc]; The M sheet quiet catch (18) suitable with described breach is provided with outside the bayonet socket of the rear end of camera lens;
M projection, a M breach, the quiet catch of M sheet and M dynamic catch is circumferential spaced set;
Along with fore shaft change is rotated, when the top of the teat of catch dynamic described in bump contact, the leading portion of dynamic catch reaches maximum position to seal described breach (52), [now the quiet catch of camera lens is locked in inside snap ring and projection, realize the locking of camera lens, now camera lens can rotate relative to fuselage, to switch sub-camera lens]
When projection does not contact with the teat of described dynamic catch, dynamic catch retracts to maximum position to abdicate described breach (52) under the effect of extension spring (11); [now breach is opened, and the quiet catch on camera lens can free in and out, and is convenient to load onto or take off camera lens];
After integrated form camera lens and fuselage complete and dock, the optical axis of a sub-camera lens in N number of sub-camera lens is aimed at image sensor center point, forms imaging optical path.
Fuselage is provided with display screen.
A shank is provided with at fuselage bayonet socket, camera lens bayonet socket is provided with for circumference locking integrated form camera lens N number of pin-and-hole [shank (21) and pin-and-hole (20) are the common components in existing slr camera opening, in addition, fuselage is also provided with for driving the camera lens of this bayonet pin to lock/discharge button].
Fuselage is provided with electronic viewfinder or optical finder, and fuselage or integrated form camera lens are provided with focusing motor, and fuselage or integrated form camera lens are provided with optical anti-vibration system.
N is the integer between 4-6.
Fore shaft change is provided with axial slide block (7), is provided with the guiding stop chute (8) of circular arc in camera lens bayonet socket, and slide block external part is arranged in guiding stop chute.(such fore shaft change can not unrestrictedly rotate, and can only rotate to an angle)
The torsion spring resetted for fore shaft change is provided with between bayonet socket and fore shaft change.[not shown, be prior art, its effect is: when external force does not act in fore shaft change, and drive fore shaft change to turn to an extreme position, this position just promotes dynamic catch and overcomes the pulling force of extension spring to block breach, position as described in Figure 10.Ensure camera lens normal condition can not come off from fuselage and fall break]
Described fuselage is the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electric camera body or handset (as i Phone or other smart mobile phones or non intelligent mobile phone).
Integrated form camera lens can also adopt following pattern:
(1) 3 sub-camera lenses are integrated with in integrated form camera lens, see Figure 14.
(2) 6 sub-camera lenses are integrated with in integrated form camera lens, see Figure 15.
All the other it should be noted that: fuselage or integrated form camera lens are provided with focusing motor, and fuselage or integrated form camera lens are provided with optical anti-vibration system; Imageing sensor is cmos sensor, and imageing sensor is individual layer or three layers of sensor; The top of fuselage is provided with flashlamp and tripper (3), and be integrated with automatic/hand Focusing module in fuselage, 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, also can be cmos sensor, can be the mosaic sensor of individual layer, also can be the sensor of three layers, (the FOVEONX3 full color image sensing chip with reference to sigma company adopts)
Imageing sensor is ccd sensor or cmos sensor; Imageing sensor is individual layer mosaic sensor or three layers of X3 type sensor [as the FOVEONX3 full color image sensing chip that sigma company adopts];
Adopt this camera body with bayonet socket and single offset sensor, its method obtaining image is:
The rear end of integrated form camera lens is installed on fuselage bayonet socket, and the round and elastic contact on integrated form camera lens contacts with the stationary contact on fuselage is corresponding, realizes data communication;
After integrated form camera lens and fuselage complete and dock, rotate integrated form camera lens, the optical axis of a sub-camera lens in N number of sub-camera lens is aimed at image sensor center point, formation imaging optical path; After aligning, the camera lens on machine for releasing locks/discharges button, and shank (21) is inserted in pin-and-hole (20), prevents camera lens from rotating again;
The opening and closing of described fore shaft change and telescopic catch mechanism controls breach, along with fore shaft change is rotated, when the top of the teat of catch dynamic described in bump contact, the leading portion of dynamic catch reaches maximum position to seal described breach (52);
When projection does not contact with the teat of described dynamic catch, dynamic catch retracts to maximum position to abdicate described breach (52) under the effect of extension spring (11), is convenient to camera lens and loads onto or take out.
Light projects on imageing sensor by the N number of sub-camera lens of integrated form camera lens, and the digital document of this acquisition is stored in storer integrated in fuselage by processor integrated in fuselage; Described digital document is image or video.
When described digital document is image, any one mode following is adopted to be stored into by image in storer integrated in fuselage;
Method 1: the image file of unprocessed form and RAW form is directly stored in memory;
Method 2: carried out by the image file of RAW form in machine after process, the image file converting JPG form to stores in memory;
Method 3: both stored in memory by the image file of RAW form, the image file of the JPG form also formed by the converting of image file by RAW form stores in memory.
By the leading portion chooser camera lens of rotary collecting accepted way of doing sth camera lens, and realtime graphic is projected in electronic viewfinder.
When starting live view function, realtime graphic being shown on a display screen in real time, is convenient to real-time focus operation.
The story board of integrated form camera lens can arrange multiple different focal, as 14mm, 24mm, 35mm, 50mm, 85mm, 100mm, 105mm, 150mm, 180mm, 200mm, 400mm etc.
Imageing sensor is preferably arranged on directly over described axis, immediately below, front-left (as shown in Figure 3) or front-right, or in any one direction.
The value of corresponding M, minimum is 2, also can any one value of 3-10, as long as 2 breach can complete the insertion of camera lens, is also convenient to rotation of lens, preferred 3-6.
Claims (9)
1. have a camera body for bayonet socket and single offset sensor, it is characterized in that, fuselage front panel is provided with the fuselage bayonet socket (5) for docking with camera lens;
(1) 1 imageing sensor (13) is provided with in the fuselage described in; The axis that described imageing sensor offsets described fuselage bayonet socket (5) is arranged, imageing sensor place plane and described axes normal;
(2) camera lens described in is integrated form camera lens (2), and integrated form camera lens is docked on this fuselage bayonet socket (5);
N number of sub-camera lens (4) with different focal is integrated with in the lens barrel of described integrated form camera lens; 3≤N≤12, N is natural number; An arrangement of mirrors sheet is included in each sub-camera lens;
The optical axis of N number of sub-camera lens all with the axis parallel of integrated form camera lens; And N number of sub-lens arrangement is in the circumference of axial line;
(3) one group of stationary contact (12) is provided with in fuselage bayonet socket, camera lens rear end has one group of round and elastic contact (17), the camera lens bayonet socket of integrated form camera lens rear end is installed on after on fuselage bayonet socket (5), described stationary contact (12) and round and elastic contact (17) correspondence contacts, and completes docking of camera lens and fuselage;
Fuselage bayonet socket is columnar structured, and the inwall of fuselage bayonet socket is provided with the snap ring (51) that has M breach (52); 2≤M≤9, M is integer;
Each indentation, there is provided with a telescopic catch mechanism; Telescopic catch mechanism described in each comprises dynamic catch (9), the servo-actuated orienting lug (15) of dynamic catch both sides setting, 2 guideposts (14) and 2 extension springs (11); 2 guiding storehouses are respectively provided with in the snap ring of each breach both sides; 2 described guideposts are separately positioned in these 2 guiding storehouses; 2 extension springs are set on 2 guideposts, and 2 servo-actuated orienting lugs are set on 2 guideposts and are also connected with 2 extension springs respectively; The rear end of dynamic catch is the teat of circular arc or ellipse arc;
The outer ring of fuselage bayonet socket is provided with the fore shaft change (6) for driving described telescopic catch mechanism; The inwall of fore shaft change is provided with M projection; The M sheet quiet catch (18) suitable with described breach is provided with outside the bayonet socket of the rear end of camera lens;
M projection, a M breach, the quiet catch of M sheet and M dynamic catch is circumferential spaced set;
Along with fore shaft change is rotated, when the top of the teat of catch dynamic described in bump contact, the leading portion of dynamic catch reaches maximum position to seal described breach (52);
When projection does not contact with the teat of described dynamic catch, dynamic catch retracts to maximum position to abdicate described breach (52) under the effect of extension spring (11);
After integrated form camera lens and fuselage complete and dock, the optical axis of a sub-camera lens in N number of sub-camera lens is aimed at image sensor center point, forms imaging optical path.
2. the camera body with bayonet socket and single offset sensor according to claim 1, it is characterized in that, fuselage is provided with display screen.
3. the camera body with bayonet socket and single offset sensor according to claim 1, is characterized in that, is provided with a shank at fuselage bayonet socket, camera lens bayonet socket is provided with for the N number of pin-and-hole of circumference locking integrated form camera lens.
4. the camera body with bayonet socket and single offset sensor according to claim 1, it is characterized in that, fuselage is provided with electronic viewfinder or optical finder, and fuselage or integrated form camera lens are provided with focusing motor, and fuselage or integrated form camera lens are provided with optical anti-vibration system.
5. have the camera body of bayonet socket and single offset sensor according to claim 1, it is characterized in that, N is the integer between 4-6.
6. the camera body with bayonet socket and single offset sensor according to claim 1, it is characterized in that, fore shaft change is provided with axial slide block (7), is provided with the guiding stop chute (8) of circular arc in camera lens bayonet socket, and slide block external part is arranged in guiding stop chute.
7. the camera body with bayonet socket and single offset sensor according to claim 6, is characterized in that, is provided with the torsion spring resetted for fore shaft change between bayonet socket and fore shaft change.
8. the camera body with bayonet socket and single offset sensor according to any one of claim 1-7, is characterized in that, described fuselage is the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electric camera body or handset.
9. the camera body with bayonet socket and single offset sensor according to claim 2, is characterized in that, N is the integer between 4-6; Fuselage is provided with electronic viewfinder, and fuselage or integrated form camera lens are provided with focusing motor, and fuselage or integrated form camera lens are provided with optical anti-vibration system; Fore shaft change is provided with axial slide block (7), is provided with the guiding stop chute (8) of circular arc in camera lens bayonet socket, and slide block external part is arranged in guiding stop chute; The torsion spring resetted for fore shaft change is provided with between bayonet socket and fore shaft change;
Be integrated with automatic/hand Focusing module in fuselage, imageing sensor is square, and display screen is provided with touch sensitive layer; Imageing sensor is cmos sensor, and imageing sensor is individual layer or three layers of sensor; The top of fuselage is provided with flashlamp and tripper (3), and be integrated with automatic/hand Focusing module in fuselage, 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, and described fuselage is the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electric camera body or handset.
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| CN201410000131.XA CN103676416B (en) | 2014-01-01 | 2014-01-01 | A kind of camera body with bayonet socket and single offset sensor |
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| CN201410000131.XA CN103676416B (en) | 2014-01-01 | 2014-01-01 | A kind of camera body with bayonet socket and single offset sensor |
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| CN103685898B (en) * | 2014-01-01 | 2016-09-07 | 中南林业科技大学 | A kind of integrated form camera lens with bayonet socket |
| US10345714B2 (en) | 2016-07-12 | 2019-07-09 | Cymer, Llc | Lithography optics adjustment and monitoring |
| JP6758269B2 (en) * | 2017-09-07 | 2020-09-23 | パナソニック フォト・ライティング 株式会社 | Lighting equipment and imaging equipment |
| CN108769487B (en) * | 2018-06-29 | 2020-08-07 | 北京小米移动软件有限公司 | Electronic device, information processing method, and computer-readable storage medium |
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| CN2303318Y (en) * | 1997-06-26 | 1999-01-06 | 叶阁福 | Interchanging apparatus of combination lens |
| JP2005249824A (en) * | 2004-03-01 | 2005-09-15 | Casio Comput Co Ltd | Imaging apparatus |
| CN101655650A (en) * | 2008-08-19 | 2010-02-24 | 鸿富锦精密工业（深圳）有限公司 | Photographic device |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6643457B2 (en) * | 2002-03-28 | 2003-11-04 | Wen Ching Chen | Simple focusable lens combination of a camera |
| CN101266394A (en) * | 2007-03-16 | 2008-09-17 | 鸿富锦精密工业（深圳）有限公司 | Lens slewing disc device and camera possessing lens slewing disc device |
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2014
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Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2303318Y (en) * | 1997-06-26 | 1999-01-06 | 叶阁福 | Interchanging apparatus of combination lens |
| JP2005249824A (en) * | 2004-03-01 | 2005-09-15 | Casio Comput Co Ltd | Imaging apparatus |
| CN101655650A (en) * | 2008-08-19 | 2010-02-24 | 鸿富锦精密工业（深圳）有限公司 | Photographic device |
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