CN103685898B - A kind of integrated form camera lens with bayonet socket - Google Patents
A kind of integrated form camera lens with bayonet socket Download PDFInfo
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- CN103685898B CN103685898B CN201410000285.9A CN201410000285A CN103685898B CN 103685898 B CN103685898 B CN 103685898B CN 201410000285 A CN201410000285 A CN 201410000285A CN 103685898 B CN103685898 B CN 103685898B
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- camera lens
- fuselage
- bayonet socket
- integrated form
- catch
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Abstract
The invention discloses one and have Novel bayonet and integrated form camera lens, camera lens rear end is provided with the camera lens bayonet socket docked with fuselage；Described fuselage front panel is provided with the fuselage bayonet socket (5) for docking with camera lens；Described camera lens is integrated form camera lens (2), and fuselage bayonet socket is columnar structured, and the inwall of fuselage bayonet socket is provided with a snap ring (51) with M breach (52)；Each indentation, there is provided with a telescopic catch mechanism；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；After integrated form camera lens completes to dock with fuselage, 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.This has Novel bayonet and integrated form camera lens integrated level is high, easy to use, and takes into account the remarkable optical property of multiple tight shot, good portability.
Description
Technical field
The present invention relates to a kind of integrated form camera lens with bayonet socket.
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 camera lens is therein crucial one
Ring.
Summary of the invention
The technical problem to be solved is to provide a kind of integrated form camera lens with bayonet socket, and this has bayonet socket
Integrated form camera lens integrated level high, easy to use, and take into account the remarkable optical property of multiple tight shot, portable
Property is good.
The technical solution of invention is as follows:
A kind of integrated form camera lens with bayonet socket, camera lens rear end is provided with the camera lens bayonet socket docked with fuselage；
Described 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 extension springs (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 extension springs 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 extension springs；The rear end of dynamic catch is the prominent of circular arc or ellipse arc
Portion；[i.e. protuberance be outline be 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；Fore shaft change
Inwall is provided with M projection；[projection is circular arc or ellipse arc]；Be provided with outside the bayonet socket of the rear end of camera lens with
The quiet catch of the M sheet (18) that described breach is suitable；
M projection, M breach, the quiet catch of M sheet and M dynamic catch are circumference spaced set；
Along with fore shaft change rotates, when the top of the protuberance of catch dynamic described in bump contact, the leading portion of protuberance is stretched
Going out to maximum position to seal described breach (52), [now the quiet catch of camera lens is locked in snap ring and projection
Side, it is achieved the locking of camera lens, now camera lens can rotate relative to fuselage, to switch sub-camera lens]
When the protuberance of projection with described dynamic catch does not contacts, protuberance retracts under the effect of extension spring (11)
Big 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 easy to load onto or take off camera lens]；
After integrated form camera lens completes to dock with fuselage, the optical axis of a sub-camera lens in N number of sub-camera lens and image sensing
Device central point is directed at, and forms imaging optical path.
Fuselage is provided with display screen.
It is provided with a shank 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) they are the common components in existing slr camera opening, additionally, fuselage
On be additionally provided with for driving the camera lens of this bayonet pin to lock/discharge button].
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.
Fore shaft change is provided with axial slide block (7), is provided with the guiding stop chute of circular arc in camera lens bayonet socket
(8) during, slide block external part is positioned at guiding stop chute；(such fore shaft change can not unrestrictedly rotate, only
Can rotate to an angle)
The torsion spring resetted for fore shaft change it is provided with between bayonet socket and fore shaft change.[not shown in figure, for existing
Technology, its effect is: when external force does not acts in fore shaft change, drives fore shaft change to turn to a limit
Position, this position just promote dynamic catch overcome the pulling force of extension spring to block breach, position as described in Figure 10.
Ensure that camera lens will not come off from fuselage in normal condition and falls and break]
Described fuselage can be the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electricity camera body,
Or mobile phone (such as i Phone or other smart mobile phones or non intelligent mobile phone).
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；Fore shaft change is provided with
Axial slide block (7), is provided with guiding stop chute (8) of circular arc in camera lens bayonet socket, slide block external part is positioned at
Guide in stop chute；The torsion spring resetted for fore shaft change it is provided with between bayonet socket and fore shaft change；
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), 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 mobile phone.
Beneficial effect:
The integrated form camera lens with bayonet socket of the present invention, is the camera lens of a kind of brand-new original creation, is totally different from
Existing main flow lens design, its core idea is: be integrated with the imageing sensor of a biasing on fuselage,
This imageing sensor is adaptive, by the phase of camera lens bayonet socket with fuselage bayonet socket with many sub-camera lenses on integrated form camera lens
Rotation is carried out sub-Shot change and realizes manual zoom, thus obtain high-quality image or video.The present invention's
Major advantage is 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) opening and closing of fore shaft change and telescopic catch mechanism controls breach is used, to facilitate the handling of camera lens,
This is a kind of brand-new bayonet socket pattern, constructs ingenious, it is easy to implement, it is easy to operation.
7) use torsion spring, slide block and guiding stop chute that dynamic catch is resetted in time, ensure camera lens safety,
Thus safety is high.
It can be said that this integrated form camera lens with bayonet socket integrates many U.S.s, the existing high image quality focusing head,
The shortcoming overcoming again an anti-portability difference wearing multiple camera lens of list, the portability of existing card camera,
Compare again card camera and there is higher battery durable performance, and, structure novelty.
In sum, the best advantage is that taken into account high image quality, portability, handover convenience,
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 image acquisition system of the integrated form camera lens with bayonet socket；
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 be guide stop chute position view is set；
Fig. 9 is enlarged drawing at A in Fig. 6；
Figure 10 is enlarged drawing at B 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 sectional 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；[not shown quiet gear
The parts such as sheet]
Figure 15 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-fore shaft change, 7-slide block, 8-guides stop chute, and 9-moves catch, 10-projection, 11-extension spring；
12-stationary contact；13-photo-sensitive cell；14-lead, the servo-actuated guide pad of 15-.16-tread plate, 17-circle bullet
Property contact；The quiet catch of 18-, 19-light transmission passage.20-pin-and-hole, 21-shank.
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 integrated form camera lens with bayonet socket, during use, and on fuselage (1) front panel
Fuselage bayonet socket (5) docks；
(1) camera lens described in is integrated form camera lens, and integrated form camera lens is docked on this fuselage bayonet socket (5)；Institute
1 imageing sensor (13) it is provided with in the fuselage stated；
[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 extension springs (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 extension springs 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 extension springs；The rear end of dynamic catch is the prominent of circular arc or ellipse arc
Portion；[i.e. protuberance be outline be 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；Fore shaft change
Inwall is provided with M projection；[projection is circular arc or ellipse arc]；Be provided with outside the bayonet socket of the rear end of camera lens with
The quiet catch of the M sheet (18) that described breach is suitable；
M projection, M breach, the quiet catch of M sheet and M dynamic catch are circumference spaced set；
Along with fore shaft change rotates, when the top of the protuberance of catch dynamic described in bump contact, the leading portion of dynamic catch is stretched
Going out to maximum position to seal described breach (52), [now the quiet catch of camera lens is locked in snap ring and projection
Side, it is achieved the locking of camera lens, now camera lens can rotate relative to fuselage, to switch sub-camera lens]
When the protuberance of projection with described dynamic catch does not contacts, dynamic catch retracts under the effect of extension spring (11)
Big 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 easy to load onto or take off camera lens]；
After integrated form camera lens completes to dock with fuselage, the optical axis of a sub-camera lens in N number of sub-camera lens and image sensing
Device central point is directed at, and forms imaging optical path.
Fuselage is provided with display screen.
It is provided with a shank at fuselage bayonet socket, camera lens bayonet socket is provided with and locks integrated form camera lens N for circumference
Individual pin-and-hole [shank (21) and pin-and-hole (20) they are the common components in existing slr camera opening, additionally, machine
It is additionally provided with it for driving the camera lens of this bayonet pin to lock/discharge button].
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.
Fore shaft change is provided with axial slide block (7), is provided with the guiding stop chute of circular arc in camera lens bayonet socket
(8) during, slide block external part is positioned at guiding stop chute.(such fore shaft change can not unrestrictedly rotate, only
Can rotate to an angle)
The torsion spring resetted for fore shaft change it is provided with between bayonet socket and fore shaft change.[not shown in figure, for existing
Technology, its effect is: when external force does not acts in fore shaft change, drives fore shaft change to turn to a limit
Position, this position just promote dynamic catch overcome the pulling force of extension spring to block breach, position as described in Figure 10.
Ensure that camera lens will not come off from fuselage in normal condition and falls and break]
Described fuselage is the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electricity camera body or hands
Machine fuselage (such as i Phone or other smart mobile phones or non intelligent mobile phone).
Embodiment 2:
Remaining is with embodiment 1, and difference is, is integrated with 3 sub-camera lenses, sees figure in integrated form camera lens
14。
Embodiment 3:
Remaining is with embodiment 1, and difference is, is integrated with 6 sub-camera lenses, sees figure in integrated form camera lens
15。
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), 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 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 is 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 integrated form camera lens with bayonet socket, its method obtaining image is:
The rear end of integrated form camera lens is installed on fuselage bayonet socket, on the round and elastic contact on integrated form camera lens and fuselage
Stationary contact correspondence contacts, it is achieved data communication；
After integrated form camera lens completes to dock with fuselage, rotate integrated form camera lens so that a son in N number of sub-camera lens
The optical axis of camera lens is directed at image sensor center point, forms imaging optical path；Camera lens after alignment, on machine for releasing
Locking/release button, shank (21) is inserted in pin-and-hole (20), prevents camera lens from rotating again；
Described fore shaft change and the opening and closing of telescopic catch mechanism controls breach, along with fore shaft change rotates, work as projection
During the top of the protuberance contacting described dynamic catch, the leading portion of dynamic catch reaches maximum position to seal described lacking
Mouth (52)；
When the protuberance of projection with described dynamic catch does not contacts, dynamic catch retracts under the effect of extension spring (11)
Big position is to concede described breach (52), it is simple to camera lens is loaded onto or taken out.
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 the leading portion of rotary collecting accepted way of doing sth camera lens, and real time imaging is projected electronic viewfinder
In.
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 complete inserting of camera lens
Enter, also allow for rotation of lens, preferably 3-6.
Claims (8)
1. an integrated form camera lens with bayonet socket, it is characterised in that camera lens rear end is provided with docks with fuselage
Camera lens bayonet socket；
Described 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 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 extension springs (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 extension springs 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 extension springs；The rear end of dynamic catch is the prominent of circular arc or ellipse arc
Portion；
The outer ring of fuselage bayonet socket is provided with the fore shaft change (6) for driving described telescopic catch mechanism；Fore shaft change
Inwall is provided with M projection；The M sheet quiet catch suitable with described breach it is provided with outside the bayonet socket of the rear end of camera lens
(18)；
M projection, M breach, the quiet catch of M sheet and M dynamic catch are circumference spaced set；
Along with fore shaft change rotates, when the top of the protuberance of catch dynamic described in bump contact, the leading portion of protuberance is stretched
Go out to maximum position to seal described breach (52)；
When the protuberance of projection with described dynamic catch does not contacts, protuberance retracts under the effect of extension spring (11)
Big position is to concede described breach (52)；
After integrated form camera lens completes to dock with fuselage, the optical axis of a sub-camera lens in N number of sub-camera lens and image sensing
Device central point is directed at, and forms imaging optical path.
The integrated form camera lens with bayonet socket the most according to claim 1, it is characterised in that fuselage is provided with
Display screen.
The integrated form camera lens with bayonet socket the most according to claim 1, it is characterised in that at fuselage bayonet socket
It is provided with a shank, camera lens bayonet socket is provided with and locks the N number of pin-and-hole of integrated form camera lens for circumference.
The integrated form camera lens with bayonet socket the most according to claim 1, it is characterised in that set on fuselage
Electronic viewfinder or optical finder, fuselage or integrated form camera lens is had to be provided with focusing motor, at fuselage or integrated
Formula camera lens is provided with optical anti-vibration system.
The integrated form camera lens with bayonet socket the most according to claim 1, it is characterised in that N is 4-6
Between integer.
The integrated form camera lens with bayonet socket the most according to claim 1, it is characterised in that in fore shaft change
It is provided with axial slide block (7), in camera lens bayonet socket, is provided with guiding stop chute (8) of circular arc, slide block external part
It is positioned in guiding stop chute；
The torsion spring resetted for fore shaft change it is provided with between bayonet socket and fore shaft change.
7. according to the integrated form camera lens with bayonet socket described in any one of claim 1-6, it is characterised in that
Described fuselage is the fuselage of slr camera, card camera fuselage, micro-one camera/mono-electricity camera body or mobile phone.
The integrated form camera lens with bayonet socket the most according to claim 2, it is characterised in that N is 4-6
Between integer；Fuselage is provided with electronic viewfinder, fuselage or integrated form camera lens and is provided with focusing motor, at machine
Body or integrated form camera lens are provided with optical anti-vibration system；Fore shaft change is provided with axial slide block (7), shot card
Being provided with guiding stop chute (8) of circular arc in Kou, slide block external part is positioned in guiding stop chute；Bayonet socket with
The torsion spring resetted for fore shaft change it is provided with between fore shaft change；
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), 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 mobile phone.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410000285.9A CN103685898B (en) | 2014-01-01 | 2014-01-01 | A kind of integrated form camera lens with bayonet socket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410000285.9A CN103685898B (en) | 2014-01-01 | 2014-01-01 | A kind of integrated form camera lens with bayonet socket |
Publications (2)
| Publication Number | Publication Date |
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| CN103685898B true CN103685898B (en) | 2016-09-07 |
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| CN110266929A (en) * | 2019-07-01 | 2019-09-20 | 广东思锐光学股份有限公司 | Lens construction and auxiliary lens mechanism |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101655650A (en) * | 2008-08-19 | 2010-02-24 | 鸿富锦精密工业（深圳）有限公司 | Photographic device |
| CN102768412A (en) * | 2011-05-02 | 2012-11-07 | 索尼公司 | Infrared imaging system and operating method |
| CN103676416A (en) * | 2014-01-01 | 2014-03-26 | 中南林业科技大学 | Camera body with novel bayonet and single offset sensor |
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Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101655650A (en) * | 2008-08-19 | 2010-02-24 | 鸿富锦精密工业（深圳）有限公司 | Photographic device |
| CN102768412A (en) * | 2011-05-02 | 2012-11-07 | 索尼公司 | Infrared imaging system and operating method |
| CN103676416A (en) * | 2014-01-01 | 2014-03-26 | 中南林业科技大学 | Camera body with novel bayonet and single offset sensor |
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