CN103685901B - A kind of image capturing method based on automatically controlled bayonet socket and integrated form camera lens - Google Patents
A kind of image capturing method based on automatically controlled bayonet socket and integrated form camera lens Download PDFInfo
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- CN103685901B CN103685901B CN201410000574.9A CN201410000574A CN103685901B CN 103685901 B CN103685901 B CN 103685901B CN 201410000574 A CN201410000574 A CN 201410000574A CN 103685901 B CN103685901 B CN 103685901B
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Abstract
The invention discloses a kind of image capturing method based on automatically controlled bayonet socket and integrated form camera lens, including fuselage (1) and camera lens, described camera lens is integrated form camera lens (2), is provided with 1 imageing sensor (13) in described fuselage；N number of sub-camera lens (4) with different focal it is integrated with in the lens barrel of described integrated form camera lens；3≤N≤12, N is natural number；Fuselage bayonet socket is columnar structured, and the inwall of fuselage bayonet socket is provided with a snap ring (51) with M breach (52)；2≤M≤9, M is integer；Each indentation, there is provided with a telescopic catch mechanism；Fuselage bayonet socket is provided with M for the electromagnet (6) controlling dynamic catch；It is somebody's turn to do image capturing method image capturing based on automatically controlled bayonet socket and integrated form camera lens convenient, and takes into account remarkable optical property and the portability of a machine (fuselage) mirror (camera lens) of multiple tight shot.
Description
Technical field
The present invention relates to a kind of image capturing method based on automatically controlled bayonet socket and integrated form camera lens.
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 photography of a kind of new mode, image capture method.
Summary of the invention
The technical problem to be solved is to provide a kind of based on automatically controlled bayonet socket with the image of integrated form camera lens
Acquisition methods, is somebody's turn to do image capturing method image capturing based on automatically controlled bayonet socket and integrated form camera lens conveniently, and takes into account
The remarkable optical property of multiple tight shots and the portability of a machine (fuselage) mirror (camera lens).
The technical solution of invention is as follows:
A kind of image capturing method based on automatically controlled bayonet socket and integrated form camera lens, it is characterised in that use and there is electricity
Control bayonet socket and the camera system of integrated form camera lens, described camera system includes fuselage (1) and camera lens, 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 (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 skew can be in the axis setting of the described imageing sensor described fuselage bayonet socket (5) of skew
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；
Fuselage bayonet socket is provided with M electromagnet (6)；M electromagnet is corresponding with M dynamic catch position respectively；Fuselage
Or fuselage bayonet socket is provided with one for the control button (20) controlling M electromagnet 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 electromagnet, M breach, the quiet catch of M sheet and M dynamic catch are circumference spaced set；
The opening and closing of M electromagnet telescopic catch mechanism controls M breach individual with M,
When control button is not pressed, electromagnet 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), it is now the state not connecing camera lens, or the shape that camera lens is locked
The quiet catch of 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, now camera lens
Can rotate relative to fuselage, to switch sub-camera lens；
When control button is pressed, electromagnet 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, and fuselage leads to
Cross imageing sensor and obtain image or video.
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).
As preferably, N is the integer between 4-6；Fuselage is provided with electronic viewfinder, fuselage or integrated form mirror
Head is provided with focusing 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 individual layer or three layers of sensor；Fuselage
Top be provided with flash lamp and tripper (3), fuselage is integrated with automatic/hand Focusing module, image passes
Sensor is square, and display screen is provided with touch sensitive layer；The size of imageing sensor is 4/3 picture, 135 complete
Picture or APS-H picture, APS-C picture, 1/1.63 inch of picture or 1/1.7 inch of picture.Described
Fuselage is the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electricity camera body or handset.
Beneficial effect:
The image capturing method based on automatically controlled bayonet socket and integrated form camera lens of the present invention, is a kind of brand-new original creation
Image capture method, be totally different from existing main flow camera use scheme, its core idea is: on fuselage
Being integrated with the imageing sensor of a biasing, this imageing sensor is fitted with many sub-camera lenses on integrated form camera lens
Join, carry out sub-Shot change realize manual zoom by rotating against of camera lens bayonet socket and fuselage bayonet socket, thus obtain
Take high-quality image 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, when especially using electronic viewfinder, more power saving, continuation of the journey
Ability can accomplish work as anti-phase with general list, and therefore, this point is compared card camera and had greatly
Advantage.
5) use len changeable bayonet socket to dock, change camera lens convenient.
6) use control button, electromagnet 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 button (automatically reseting) and stage clip that dynamic catch is resetted in time, ensure camera lens peace
Entirely, thus security is high.
It can be said that this image capturing method based on automatically controlled bayonet socket and integrated form camera lens integrates many U.S.s,
The high image quality that existing list is anti-, the shortcoming overcoming again an anti-portability difference wearing multiple camera lens of list,
The portability of existing card camera, compares again card camera and has higher battery durable performance, and, structure
Make novelty.
In sum, the best advantage is that taken into account high image quality, portability, handover convenience,
Flying power is good, and market prospects are good.
Accompanying drawing explanation
Fig. 1 is existing airframe structure schematic diagram；
Fig. 2 is general structure schematic diagram based on automatically controlled bayonet socket and the image acquisition system of integrated form camera lens；
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 the structural representation of the rear end of the integrated form camera lens with 3 sub-camera lenses；[not shown quiet gear
The parts such as sheet]
Figure 14 is the structural representation of the rear end of the integrated form camera lens with 6 sub-camera lenses；[not shown quiet gear
The parts such as sheet]
Label declaration:
1-fuselage, 2-integrated form camera lens, 3-tripper, 4-camera lens, 5-fuselage bayonet socket, 6-electromagnet, 9-
Dynamic catch, 11-stage clip；
12-stationary contact；13-photo-sensitive cell；14-lead, the servo-actuated guide pad of 15-.16-tread plate, 17-circle bullet
Property contact；18-card, 19-light transmission passage.20-control button, 21-shank, 22-pin-and-hole
The quiet catch of 51-, 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 image capturing method based on automatically controlled bayonet socket and integrated form camera lens, use and there is electricity
Control bayonet socket and the camera system of integrated form camera lens, described system includes fuselage (1) and camera lens, before fuselage
Plate 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 skew can be in the axis setting of the described imageing sensor described fuselage bayonet socket (5) of skew
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；
Fuselage bayonet socket is provided with M electromagnet (6)；M electromagnet is corresponding with M dynamic catch position respectively；Fuselage
Or fuselage bayonet socket is provided with one for the control button (20) controlling M electromagnet 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 electromagnet, M breach, the quiet catch of M sheet and M dynamic catch are circumference spaced set；
When control button is not pressed, electromagnet 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 button is pressed, electromagnet 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 individual layer or three layers of sensor；Fuselage
Top be provided with flash lamp and tripper (3), fuselage is integrated with automatic/hand Focusing module, image passes
Sensor is square, and display screen is provided with touch sensitive layer；The size of imageing sensor is 4/3 picture, 135 complete
Picture or APS-H picture, APS-C picture, 1/1.63 inch of picture or 1/1.7 inch of picture.Described
Fuselage is the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electricity camera body or handset.
The rear end of dynamic catch uses iron or steel matter, it is simple to by electromagnetic actuation.
Embodiment 2:
Remaining is with embodiment 1, and difference is, is integrated with 3 sub-camera lenses, sees figure in integrated form camera lens
13。
Embodiment 3:
Remaining is with embodiment 1, and difference is, is integrated with 6 sub-camera lenses, sees figure in integrated form camera lens
14。
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 individual layer or three layers
Sensor；The top of fuselage is provided with flash lamp and tripper (3), is integrated with automatic/hand focusing in fuselage
Module, imageing sensor is square, and display screen is provided with touch sensitive layer；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
Width.
Imageing sensor can be ccd sensor, it is also possible to be cmos sensor, can be the Marseille of individual layer
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 individual layer mosaic sensor or
Three layers of X3 type sensor [the FOVEON X3 full-color imagery sensor chip used such as sigma company]；
Using this image capturing method based on automatically controlled bayonet socket and integrated form camera lens, its method obtaining image is:
The opening and closing of M electromagnet telescopic catch mechanism controls M breach individual with M,
When control button is not pressed, electromagnet 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 button is pressed, electromagnet 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 existing slr camera opening
In 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 memory 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
Memory in；
Method 1: the image file of unprocessed form i.e. RAW form is stored directly in memory；
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 realtime graphic is projected in electronic viewfinder.
When starting live view function, realtime graphic 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. an image capturing method based on automatically controlled bayonet socket and integrated form camera lens, it is characterised in that use have automatically controlled bayonet socket and
The camera system of integrated form camera lens, described camera system includes fuselage (1) and camera lens, and fuselage front panel is provided with use
In 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)；Described
Fuselage in be provided with 1 imageing sensor (13)；
Described imageing sensor offsets the axis of described fuselage bayonet socket (5) and arranges, imageing sensor place plane and institute
State axis vertical；
(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
For 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 in the circumference of axial line；
(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), integrated
After the camera lens bayonet socket of formula camera lens rear end is installed on fuselage bayonet socket (5), described stationary contact (12) and round and elastic are touched
The corresponding contact of point (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 (51) with M breach (52)；
2≤M≤9, M is integer；
Each indentation, there is provided with a telescopic catch mechanism；Each described telescopic catch mechanism include dynamic catch (9),
Servo-actuated guide pad (15), 2 leads (14) and 2 stage clips (11) that dynamic catch both sides are arranged；Lack at each
It is respectively provided with 2 in the snap ring of mouth both sides and guides storehouses；2 described leads are separately positioned on these 2 and guide in storehouse；2
Individual stage clip is set on 2 leads, and 2 servo-actuated guide pads are set on 2 leads and respectively with 2
Individual stage clip is connected；
Fuselage bayonet socket is provided with M electromagnet (6)；M electromagnet is corresponding with M dynamic catch position respectively；Fuselage or fuselage
Bayonet socket is provided with one for the control button (20) controlling M electromagnet 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 electromagnet, M breach, the quiet catch of M sheet and M dynamic catch are circumference spaced set；
The opening and closing of M electromagnet telescopic catch mechanism controls M breach individual with M,
When control button is not pressed, electromagnet dead electricity, under the effect of stage clip (11), the leading portion of dynamic catch reaches maximum
Position, to seal described breach (52), is now the state not connecing camera lens, or the state that camera lens is locked, i.e. camera lens
Quiet catch is locked in snap ring and the inner side of dynamic catch, it is achieved the locking of camera lens, and now camera lens can rotate relative to fuselage,
To switch sub-camera lens；
When control button is pressed, electromagnet obtains electric, and dynamic catch and electromagnetic actuation, dynamic catch overcomes the elastic force of stage clip to retract to
Maximum position is to concede described breach (52)；Now breach is opened, and the quiet catch on camera lens can free 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 for circumference lock adaptive with described shank
The 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 son
The optical axis of a sub-camera lens in camera lens is directed at image sensor center point, forms imaging optical path, and fuselage is passed by image
Sensor obtains image or video.
Image capturing method based on automatically controlled bayonet socket and integrated form camera lens the most according to claim 1, it is characterised in that machine
It is provided with display screen with it.
Image capturing method based on automatically controlled bayonet socket and integrated form camera lens the most according to claim 1, its feature exists
In, fuselage is provided with electronic viewfinder or optical finder, fuselage or integrated form camera lens and is provided with focusing motor, at fuselage
Or integrated form camera lens is provided with optical anti-vibration system.
Image capturing method based on automatically controlled bayonet socket and integrated form camera lens the most according to claim 1, its feature exists
In, N is the integer between 4-6.
5. according to the image capturing method based on automatically controlled bayonet socket and integrated form camera lens described in any one of claim 1-4,
It is characterized in that, described fuselage be the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electricity camera body or
Handset.
Image capturing method based on automatically controlled bayonet socket and integrated form camera lens the most according to claim 2, its feature exists
In, N is the integer between 4-6；Fuselage is provided with electronic viewfinder, 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；
Being 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 flash of light
Lamp and tripper (3), be integrated with automatic/hand Focusing module in fuselage, imageing sensor is square, on display screen
It is provided with touch sensitive layer；The size of imageing sensor is 4/3 picture, 135 silent frames or APS-H picture, APS-C picture
Width, 1/1.63 inch of picture or 1/1.7 inch of picture；Described fuselage be the fuselage of slr camera, card camera fuselage,
Micro-one camera/mono-electricity camera body or handset.
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Citations (4)
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|---|---|---|---|---|
| JP2005249824A (en) * | 2004-03-01 | 2005-09-15 | Casio Comput Co Ltd | Imaging apparatus |
| CN101042456A (en) * | 2006-03-24 | 2007-09-26 | 鸿富锦精密工业（深圳）有限公司 | Lens module group |
| JP2008129597A (en) * | 2006-11-22 | 2008-06-05 | Fuzhun Precision Industry (Shenzhen) Co Ltd | Focusing structure |
| CN101637019A (en) * | 2007-03-09 | 2010-01-27 | 伊斯曼柯达公司 | Multiple lens camera providing a range map |
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2014
- 2014-01-01 CN CN201410000574.9A patent/CN103685901B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005249824A (en) * | 2004-03-01 | 2005-09-15 | Casio Comput Co Ltd | Imaging apparatus |
| CN101042456A (en) * | 2006-03-24 | 2007-09-26 | 鸿富锦精密工业（深圳）有限公司 | Lens module group |
| JP2008129597A (en) * | 2006-11-22 | 2008-06-05 | Fuzhun Precision Industry (Shenzhen) Co Ltd | Focusing structure |
| CN101637019A (en) * | 2007-03-09 | 2010-01-27 | 伊斯曼柯达公司 | Multiple lens camera providing a range map |
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