CN103702023B - Camera body with electric control bayonet and single offset sensor - Google Patents
Camera body with electric control bayonet and single offset sensor Download PDFInfo
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- CN103702023B CN103702023B CN201410000513.2A CN201410000513A CN103702023B CN 103702023 B CN103702023 B CN 103702023B CN 201410000513 A CN201410000513 A CN 201410000513A CN 103702023 B CN103702023 B CN 103702023B
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- fuselage
- camera lens
- bayonet socket
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Abstract
The invention discloses a camera body with a electric control bayonet and a single offset sensor; one image sensor (13) is arranged in the camera body; N sub lenses (4) with different focal lengths are integrated in a lens column of the integrated lens, wherein N is larger than or equal to 3 and is smaller than or equal to 12 and is a natural number; the machine body bayonet has a cylindrical structure; one clamping ring (51) with M notches (52) is arranged at the inner wall of the machine body bayonet, wherein M is larger than or equal to 2 and is smaller than or equal to 9 and is an integer; each notch is provided with a telescopic check piece mechanism; M electromagnets (6) for controlling movable check pieces are arranged at the machine body bayonet. The camera body with the electric control bayonet and the single offset sensor is high in integration degree, convenient to use, and can achieve the excellent optical performance of multiple prime lenses and the portability of one machine (the machine body) and one lens (the lens) after being matched with the integrated bayonet.
Description
Technical field
The present invention relates to a kind of camera body with automatically controlled bayonet socket and single offset sensor.
Background technology
Existing main flow camera system is divided into interchangeable lenses camera and the most interchangeable lens camera generally.
The most interchangeable lens camera is mainly card camera, i.e. one fuselage of employing and a camera lens, and fuselage and mirror
Head is fixed together completely, cannot dismantle when user uses, and the problem of this pattern maximum is exactly, and 1)
If automatic zoom camera lens, the zoom of its camera lens needs to be driven by fuselage, and power consumption is exceedingly fast, the continuation of the journey energy of battery
Power is poor, and general one piece of battery can only take tens photos or hundred multiple pictures, although the lightest, but
Battery durable ability cannot meet the requirement of users.
For len changeable camera, the most single anti-and micro-list (micro-list as serial in the nex of Sony, Nikon
J series, the EOS M series of Canon)；Seeing Fig. 1, this camera is all to have a piece of imageing sensor in fuselage,
Owing to using len changeable bayonet socket, thereby through the support of camera lens group to obtain excellent imaging.But it is this
The shortcoming of camera is also apparent from, because once only having access a camera lens, for professional photographer, needs
It is equipped with and multiple focuses head, when travelling or perform to shoot task specially, need to carry many pieces of camera lenses simultaneously and go out,
Not only weight is big, and the process of cutaway is also relatively complicated: camera lens to be taken off, then changes another
Camera lens, puts camera lens bonnet, and during changing camera lens, being easily caused fuselage interior has dust to invade, and,
If worked in adverse circumstances, the process changing camera lens becomes the most difficult.
Therefore, it is necessary to design the camera system of a kind of brand-new style, and the design of fuselage is this brand-new style
One of the core of camera system.
Summary of the invention
The technical problem to be solved is to provide a kind of phase with automatically controlled bayonet socket and single offset sensor
Machine fuselage, this camera body integrated level with Novel bayonet and single offset sensor is high, easy to use, with collection
After accepted way of doing sth bayonet socket adaptation, remarkable optical property and a machine (fuselage) mirror (mirror of multiple tight shot can be taken into account
Head) portability.
The technical solution of invention is as follows:
A kind of camera body with automatically controlled bayonet socket and single offset sensor, the front panel of fuselage (1) is provided with
For the fuselage bayonet socket (5) docked with camera lens；
(1) camera lens described in is integrated form camera lens (2), and integrated form camera lens is docked on this fuselage bayonet socket (5)；
1 imageing sensor (13) it is provided with in described fuselage；
Described imageing sensor offsets the axis of described fuselage bayonet socket (5) and arranges, and 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 is vertical with described axis；
(2) N number of sub-camera lens (4) with different focal it is integrated with in the lens barrel of the integrated form camera lens described in；3≤N
≤ 12, N are natural number；Each sub-camera lens includes one group of eyeglass；
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 at axial line
Circumference；
(3) being provided with one group of stationary contact (12) 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 be installed on fuselage bayonet socket (5) upper after, described stationary contact (12) and
The corresponding contact in round and elastic contact (17), completes docking of camera lens and fuselage；
Fuselage bayonet socket is columnar structured, and the inwall of fuselage bayonet socket is provided with a snap ring with M breach (52)
(51)；2≤M≤9, M is integer；
Each indentation, there is provided with a telescopic catch mechanism；Each described telescopic catch mechanism includes dynamic gear
Servo-actuated guide pad (15), 2 leads (14) and 2 stage clips (11) that sheet (9), dynamic catch both sides are arranged；
In the snap ring of each breach both sides, it is respectively provided with 2 guides storehouse；2 described leads are separately positioned on this
2 guide in storehouse；2 stage clips are set on 2 leads, and 2 servo-actuated guide pads are set in 2
It is connected on individual lead and respectively with 2 stage clips；I.e. protuberance be outline be elliptic arc or circular arc；
Fuselage bayonet socket is provided with M electric magnet (6)；M electric magnet is corresponding with M dynamic catch position respectively；Fuselage
Or fuselage bayonet socket is provided with one for the control knob (20) controlling M electric magnet energising；
The M sheet quiet catch (18) suitable with described breach it is provided with outside the bayonet socket of the rear end of camera lens；
M electric magnet, M breach, the quiet catch of M sheet and M dynamic catch are circumference spaced set；
When control knob is not pressed, electric magnet dead electricity, under the effect of stage clip (11), the leading portion of dynamic catch stretches out
To maximum position to seal described breach (52), now the quiet catch of camera lens is locked in snap ring and dynamic catch
Inner side, it is achieved the locking of camera lens, now camera lens can rotate relative to fuselage, to switch sub-camera lens；
When control knob is pressed, electric magnet obtains electric, and dynamic catch and electromagnetic actuation, dynamic catch overcomes the elastic force of stage clip
Retract to maximum position to concede described breach (52)；Now breach is opened, and the quiet catch on camera lens can be certainly
By passing in and out, it is simple to load onto or take off camera lens；
It is provided with a shank (21) at fuselage bayonet socket, camera lens bayonet socket is provided with adaptive with described shank for week
To the locking N number of pin-and-hole of integrated form camera lens；Shank (21) and pin-and-hole (22) are in existing slr camera opening
Common components, additionally, be additionally provided with on fuselage for driving the camera lens of this bayonet pin to lock/discharge button；
After integrated form camera lens completes to dock with fuselage, shank is inserted in a pin-and-hole, completes camera lens locking, N number of
The optical axis of a sub-camera lens in sub-camera lens is directed at image sensor center point, forms imaging optical path.
The camera body with automatically controlled bayonet socket and single offset sensor the most according to claim 1, its feature exists
In, fuselage is provided with display screen.
Fuselage is provided with electronic viewfinder or optical finder, fuselage or integrated form camera lens and is provided with focusing motor,
Fuselage or integrated form camera lens are provided with optical anti-vibration system.
N is the integer between 4-6.
Described fuselage can be the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electricity camera body
Or handset (such as i Phone or other smart mobile phones or non intelligent mobile phone).
N is the integer between 4-6；Fuselage be provided with electronic viewfinder, fuselage or integrated form camera lens be provided with right
Burnt motor, is provided with optical anti-vibration system on fuselage or integrated form camera lens；
Being integrated with automatic/hand Focusing module in fuselage, imageing sensor is square, and display screen is provided with touch
Inductive layer；Imageing sensor is cmos sensor, and imageing sensor is monolayer or three layers of sensor；Fuselage
Top be provided with flash lamp and tripper (3), the size of imageing sensor is 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
Fuselage, card camera fuselage, micro-one camera/mono-electricity camera body or handset for slr camera.
Beneficial effect:
The present invention has automatically controlled bayonet socket and the camera body of single offset sensor, is a kind of brand-new original creation
The fuselage of camera system, is totally different from existing main flow camera body, and its core idea is: collect on fuselage
The imageing sensor of Cheng Youyi biasing, this imageing sensor is adaptive with many sub-camera lenses on integrated form camera lens,
Carry out sub-Shot change realize manual zoom by rotating against of camera lens bayonet socket and fuselage bayonet socket, thus obtain height
The image of quality or video.Main advantages of the present invention are as follows:
1) high image quality: multiple focus head owing to being integrated with, it is well known that focus head and compare and have with zoom lens
Higher optical property, therefore, focuses the varifocal mirror switched between head compared to traditional card camera
Head and single anti-zoom lens, it is easier to ensureing high-quality image quality, its image quality is permissible
Accomplish with single the most anti-to focus head suitable.
2) focal length easy switching, by rotating against of camera lens bayonet socket and fuselage bayonet socket, can be easily from one
Individual sub-Shot change is to another sub-camera lens, switching simplicity.
3) good portability.One integrated form camera lens is integrated with multiple tight shot (sub-camera lens), compares multiple
Individually camera lens, portability is more preferable.
4) battery durable ability is strong.Owing to the process of zoom is without driving by motor, directly switch,
Thus, electric energy can be saved to greatest extent, especially use electronic viewfinder or optical finder (with
The mechanism such as illuminator coordinates) time, more power saving, flying power can accomplish work as anti-phase with general list,
Therefore, this point is compared card camera and is had great advantage.
5) use len changeable bayonet socket to dock, change camera lens convenient.
6) use control knob, electric magnet and telescopic catch mechanism to cooperate and control the opening and closing of breach, with
Facilitating the handling of camera lens, this is a kind of brand-new bayonet socket pattern, constructs ingenious, it is easy to implement, easily
In operation.
7) use control knob (Automatic-reset button) and stage clip that dynamic catch is resetted in time, ensure
Camera lens safety, thus safety is high.
It can be said that this camera body with automatically controlled bayonet socket and single offset sensor integrates many U.S.s, both
There is single anti-high image quality, the shortcoming overcoming again an anti-portability difference wearing multiple camera lens of list, both
There is the portability of card camera, compare again card camera and there is higher battery durable performance, and, structure
Novel.
In sum, the best advantage is that taken into account high image quality, portability, handover convenience,
Flying power is good, and market prospect is good.
Accompanying drawing explanation
Fig. 1 is existing airframe structure schematic diagram；
Fig. 2 is the population structure schematic diagram of the camera system with automatically controlled bayonet socket and single offset sensor；
Fig. 3 is the structural representation in fuselage front；
Fig. 4 is fuselage bayonet socket outline drawing；
Fig. 5 is the internal structure schematic diagram of fuselage bayonet socket；
Fig. 6 is fuselage bayonet socket radial cutaway view (state when breach is opened)；
Fig. 7 is fuselage bayonet socket radial cutaway view (state when breach is closed)；
Fig. 8 is enlarged drawing at A in Fig. 6；
Fig. 9 is enlarged drawing at B in Fig. 7；
Figure 10 is the outside drawing of integrated form camera lens；
Figure 11 is the rear end structure schematic diagram of integrated form camera lens；
Figure 12 is the axial sectional view of integrated form camera lens；
Figure 13 is structural representation (the not shown quiet catch of the rear end of the integrated form camera lens with 3 sub-camera lenses
Deng parts)；
Figure 14 is structural representation (the not shown quiet catch of the rear end of the integrated form camera lens with 6 sub-camera lenses
Deng parts)；
Label declaration:
1-fuselage, 2-integrated form camera lens, 3-tripper, 4-camera lens, 5-fuselage bayonet socket, 6-electric magnet,
9-moves catch, 11-stage clip；
12-stationary contact；13-photo-sensitive cell；14-lead, the servo-actuated guide pad of 15-.16-tread plate, 17-
Round and elastic contact；The quiet catch of 18-, 19-light transmission passage.20-control knob, 21-shank, 22-pin-and-hole
51-snap ring, 52-breach.
Detailed description of the invention
Below with reference to the drawings and specific embodiments, the present invention is described in further details:
Embodiment 1:
Such as Fig. 2-13, a kind of camera body with automatically controlled bayonet socket and single offset sensor, before fuselage (1)
Panel is provided with the fuselage bayonet socket (5) for docking with camera lens；
(1) camera lens described in is integrated form camera lens (2), and integrated form camera lens is docked on this fuselage bayonet socket (5)；
1 imageing sensor (13) it is provided with in described fuselage；
Described imageing sensor offsets the axis of described fuselage bayonet socket (5) and arranges, and 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 is vertical with described axis；
(2) N number of sub-camera lens (4) with different focal it is integrated with in the lens barrel of the integrated form camera lens described in；3≤N
≤ 12, N are natural number；Each sub-camera lens includes one group of eyeglass；
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 at axial line
Circumference；
(3) being provided with one group of stationary contact (12) 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 be installed on fuselage bayonet socket (5) upper after, described stationary contact (12) and
The corresponding contact in round and elastic contact (17), completes docking of camera lens and fuselage；
Fuselage bayonet socket is columnar structured, and the inwall of fuselage bayonet socket is provided with a snap ring with M breach (52)
(51)；2≤M≤9, M is integer；
Each indentation, there is provided with a telescopic catch mechanism；Each described telescopic catch mechanism includes dynamic gear
Servo-actuated guide pad (15), 2 leads (14) and 2 stage clips (11) that sheet (9), dynamic catch both sides are arranged；
In the snap ring of each breach both sides, it is respectively provided with 2 guides storehouse；2 described leads are separately positioned on this
2 guide in storehouse；2 stage clips are set on 2 leads, and 2 servo-actuated guide pads are set in 2
It is connected on individual lead and respectively with 2 stage clips；I.e. protuberance be outline be elliptic arc or circular arc；
Fuselage bayonet socket is provided with M electric magnet (6)；M electric magnet is corresponding with M dynamic catch position respectively；Fuselage
Or fuselage bayonet socket is provided with one for the control knob (20) controlling M electric magnet energising；
The M sheet quiet catch (18) suitable with described breach it is provided with outside the bayonet socket of the rear end of camera lens；
M electric magnet, M breach, the quiet catch of M sheet and M dynamic catch are circumference spaced set；
When control knob is not pressed, electric magnet dead electricity, under the effect of stage clip (11), the leading portion of dynamic catch stretches out
To maximum position to seal described breach (52), now the quiet catch of camera lens is locked in snap ring and dynamic catch
Inner side, it is achieved the locking of camera lens, now camera lens can rotate relative to fuselage, to switch sub-camera lens；
When control knob is pressed, electric magnet obtains electric, and dynamic catch and electromagnetic actuation, dynamic catch overcomes the elastic force of stage clip
Retract to maximum position to concede described breach (52)；Now breach is opened, and the quiet catch on camera lens can be certainly
By passing in and out, it is simple to load onto or take off camera lens；
It is provided with a shank (21) at fuselage bayonet socket, camera lens bayonet socket is provided with adaptive with described shank for week
To the locking N number of pin-and-hole of integrated form camera lens；Shank (21) and pin-and-hole (22) are in existing slr camera opening
Common components, additionally, be additionally provided with on fuselage for driving the camera lens of this bayonet pin to lock/discharge button；
After integrated form camera lens completes to dock with fuselage, shank is inserted in a pin-and-hole, completes camera lens locking, N number of
The optical axis of a sub-camera lens in sub-camera lens is directed at image sensor center point, forms imaging optical path.
Fuselage is provided with display screen.
Fuselage is provided with electronic viewfinder or optical finder, fuselage or integrated form camera lens and is provided with focusing motor,
Fuselage or integrated form camera lens are provided with optical anti-vibration system.
N is the integer between 4-6.
Described fuselage can be the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electricity camera body
Or handset (such as i Phone or other smart mobile phones or non intelligent mobile phone).
N is the integer between 4-6；Fuselage be provided with electronic viewfinder, fuselage or integrated form camera lens be provided with right
Burnt motor, is provided with optical anti-vibration system on fuselage or integrated form camera lens；
Being integrated with automatic/hand Focusing module in fuselage, imageing sensor is square, and display screen is provided with touch
Inductive layer；Imageing sensor is cmos sensor, and imageing sensor is monolayer or three layers of sensor；Fuselage
Top be provided with flash lamp and tripper (3), the size of imageing sensor is 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
Fuselage, card camera fuselage, micro-one camera/mono-electricity camera body or handset for slr camera.
The rear end of dynamic catch uses ferrum or steel matter, it is simple to by electromagnetic actuation.
Camera lens is also designed to other patterns, such as:
(1) integrated form camera lens is integrated with 3 sub-camera lenses, sees Figure 13.
(2) Figure 14 is seen.
Remaining is it should be understood that fuselage or integrated form camera lens are provided with focusing motor, at fuselage or integrated form mirror
Head is provided with optical anti-vibration system；Imageing sensor is cmos sensor, and imageing sensor is monolayer or three layers
Sensor；The top of fuselage is provided with flash lamp and tripper (3), the size of imageing sensor be 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, it is also possible to be cmos sensor, can be the Marseille of monolayer
Gram sensor, it is also possible to be the sensor of three layers, (the FOVEON X3 full color used with reference to sigma company
Image sensing chip)
Imageing sensor is ccd sensor or cmos sensor；Imageing sensor be monolayer mosaic sensor or
Three layers of X3 type sensor (the FOVEON X3 full-color imagery sensor chip used such as sigma company)；
Using this camera body with automatically controlled bayonet socket and single offset sensor, its method obtaining image is:
The opening and closing of M electric magnet telescopic catch mechanism controls M breach individual with M,
When control knob is not pressed, electric magnet dead electricity, under the effect of stage clip (11), before dynamic catch
Section reaches maximum position to seal described breach (52), is now the state not connecing camera lens, or camera lens is locked
The quiet catch of fixed state, i.e. camera lens is locked in snap ring and the inner side of dynamic catch, it is achieved the locking of camera lens, this
Shi Jingtou can rotate relative to fuselage, to switch sub-camera lens；
When control knob is pressed, electric magnet obtains electric, and dynamic catch and electromagnetic actuation, dynamic catch overcomes stage clip
Elastic force retract to maximum position to concede described breach (52)；Now breach is opened, the quiet catch on camera lens
Can free in and out, it is simple to load onto or take off camera lens；
Be provided with a shank (21) at fuselage bayonet socket, camera lens bayonet socket is provided with adaptive with described shank for
The circumference locking N number of pin-and-hole of integrated form camera lens；Shank (21) and pin-and-hole (22) are in existing slr camera opening
Common components, additionally, be additionally provided with on fuselage for driving the camera lens of this bayonet pin to lock/discharge button；
After integrated form camera lens completes to dock with fuselage, shank is inserted in a pin-and-hole, completes camera lens locking,
The optical axis of a sub-camera lens in N number of sub-camera lens is directed at image sensor center point, forms imaging optical path, machine
Body obtains image or video by imageing sensor.
Light projects on imageing sensor by the N number of sub-camera lens of integrated form camera lens, collects in fuselage
In the memorizer that the processor become is integrated in the digital document of this acquisition is stored in fuselage；Described digital document
For image or video.
When described digital document is image, any one mode following is used to be stored in fuselage by image integrated
Memorizer in；
Method 1: the image file of unprocessed form i.e. RAW form is stored directly in memorizer；
Method 2: after processing in the image file of RAW form carries out machine, is converted into the image literary composition of JPG form
Part stores in memory；
Method 3: both the image file of RAW form was stored in memory, also by the image by RAW form
The image file of the JPG form that file conversion is formed stores in memory.
Select sub-camera lens by rotary collecting accepted way of doing sth camera lens, and real time imaging is projected in electronic viewfinder.
When starting live view function, real time imaging is shown the most in real time, it is simple to focus in real time
Operation.
The story board of integrated form camera lens can arrange multiple different focal, such as 14mm, 24mm, 35mm, 50mm,
85mm, 100mm, 105mm, 150mm, 180mm, 200mm, 400mm etc..
Imageing sensor is preferably provided in the surface of described axis, underface, front-left (such as Fig. 3 institute
Show) or front-right, or in any one direction.
The value of corresponding M, minimum 2, it is also possible to any one value of 3-10, as long as 2 breach can be complete
Become the insertion of camera lens, also allow for rotation of lens, preferably 3-6.
Claims (6)
1. a camera body with automatically controlled bayonet socket and single offset sensor, it is characterised in that fuselage (1)
Front panel be provided with the fuselage bayonet socket (5) for docking with camera lens；
(1) camera lens described in is integrated form camera lens (2), and integrated form camera lens is docked on this fuselage bayonet socket (5)；
1 imageing sensor (13) it is provided with in described fuselage；
Described imageing sensor offsets the axis of described fuselage bayonet socket (5) and arranges, and imageing sensor place is put down
Face is vertical with described axis；
(2) N number of sub-camera lens (4) with different focal it is integrated with in the lens barrel of the integrated form camera lens described in；3≤N
≤ 12, N are natural number；Each sub-camera lens includes one group of eyeglass；
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 at axial line
Circumference；
(3) being provided with one group of stationary contact (12) 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 be installed on fuselage bayonet socket (5) upper after, described stationary contact (12) and
The corresponding contact in round and elastic contact (17), completes docking of camera lens and fuselage；
Fuselage bayonet socket is columnar structured, and the inwall of fuselage bayonet socket is provided with a snap ring with M breach (52)
(51)；2≤M≤9, M is integer；
Each indentation, there is provided with a telescopic catch mechanism；Each described telescopic catch mechanism includes dynamic gear
Servo-actuated guide pad (15), 2 leads (14) and 2 stage clips (11) that sheet (9), dynamic catch both sides are arranged；
In the snap ring of each breach both sides, it is respectively provided with 2 guides storehouse；2 described leads are separately positioned on this
2 guide in storehouse；2 stage clips are set on 2 leads, and 2 servo-actuated guide pads are set in 2
It is connected on individual lead and respectively with 2 stage clips；
Fuselage bayonet socket is provided with M electric magnet (6)；M electric magnet is corresponding with M dynamic catch position respectively；Fuselage
Or fuselage bayonet socket is provided with one for the control knob (20) controlling M electric magnet energising；
The M sheet quiet catch (18) suitable with described breach it is provided with outside the bayonet socket of the rear end of camera lens；
M electric magnet, M breach, the quiet catch of M sheet and M dynamic catch are circumference spaced set；
When control knob is not pressed, electric magnet dead electricity, under the effect of stage clip (11), the leading portion of dynamic catch stretches out
To maximum position to seal described breach (52)；
When control knob is pressed, electric magnet obtains electric, and dynamic catch and electromagnetic actuation, dynamic catch overcomes the elastic force of stage clip
Retract to maximum position to concede described breach (52)；
It is provided with a shank (21) at fuselage bayonet socket, camera lens bayonet socket is provided with adaptive with described shank for circumference
The locking N number of pin-and-hole of integrated form camera lens；
After integrated form camera lens completes to dock with fuselage, shank is inserted in a pin-and-hole, completes camera lens locking, N number of
The optical axis of a sub-camera lens in sub-camera lens is directed at image sensor center point, forms imaging optical path.
The camera body with automatically controlled bayonet socket and single offset sensor the most according to claim 1, its feature exists
In, fuselage is provided with display screen.
The camera body with automatically controlled bayonet socket and single offset sensor the most according to claim 1, it is special
Levying and be, fuselage is provided with electronic viewfinder or optical finder, fuselage or integrated form camera lens and is provided with focusing horse
Reach, fuselage or integrated form camera lens are provided with optical anti-vibration system.
The camera body with automatically controlled bayonet socket and single offset sensor the most according to claim 1, it is special
Levying and be, N is the integer between 4-6.
5. according to the camera machine with automatically controlled bayonet socket and single offset sensor described in any one of claim 1-4
Body, it is characterised in that described fuselage can be the fuselage of slr camera, card camera fuselage, micro-one camera/
Single electricity camera body or handset.
The camera body with automatically controlled bayonet socket and single offset sensor the most according to claim 2, it is special
Levying and be, N is the integer between 4-6；Fuselage is provided with on electronic viewfinder, fuselage or integrated form camera lens
It is provided with focusing motor, fuselage or integrated form camera lens are provided with optical anti-vibration system；
Being integrated with automatic/hand Focusing module in fuselage, imageing sensor is square, and display screen is provided with touch
Inductive layer；Imageing sensor is cmos sensor, and imageing sensor is monolayer or three layers of sensor；Fuselage
Top be provided with flash lamp and tripper (3), the size of imageing sensor is 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
Fuselage, card camera fuselage, micro-one camera/mono-electricity camera body or handset for slr camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410000513.2A CN103702023B (en) | 2014-01-01 | 2014-01-01 | Camera body with electric control bayonet and single offset sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410000513.2A CN103702023B (en) | 2014-01-01 | 2014-01-01 | Camera body with electric control bayonet and single offset sensor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103702023A CN103702023A (en) | 2014-04-02 |
| CN103702023B true CN103702023B (en) | 2017-01-11 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410000513.2A Expired - Fee Related CN103702023B (en) | 2014-01-01 | 2014-01-01 | Camera body with electric control bayonet and single offset sensor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103702023B (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005249824A (en) * | 2004-03-01 | 2005-09-15 | Casio Comput Co Ltd | Imaging apparatus |
| CN100552485C (en) * | 2006-11-22 | 2009-10-21 | 富准精密工业(深圳)有限公司 | Embedded focus lens structure |
| CN101668115A (en) * | 2008-09-03 | 2010-03-10 | 中国科学院自动化研究所 | Multi-lens multi-resolution camera |
-
2014
- 2014-01-01 CN CN201410000513.2A patent/CN103702023B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005249824A (en) * | 2004-03-01 | 2005-09-15 | Casio Comput Co Ltd | Imaging apparatus |
| CN100552485C (en) * | 2006-11-22 | 2009-10-21 | 富准精密工业(深圳)有限公司 | Embedded focus lens structure |
| CN101668115A (en) * | 2008-09-03 | 2010-03-10 | 中国科学院自动化研究所 | Multi-lens multi-resolution camera |
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| Publication number | Publication date |
|---|---|
| CN103702023A (en) | 2014-04-02 |
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