CN103702022B - A kind of image capturing method based on Novel bayonet and integrated form camera lens - Google Patents
A kind of image capturing method based on Novel bayonet and integrated form camera lens Download PDFInfo
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- CN103702022B CN103702022B CN201410000511.3A CN201410000511A CN103702022B CN 103702022 B CN103702022 B CN 103702022B CN 201410000511 A CN201410000511 A CN 201410000511A CN 103702022 B CN103702022 B CN 103702022B
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- fuselage
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Abstract
The invention discloses a kind of image capturing method based on Novel bayonet and integrated form camera lens, using the image acquisition system with Novel bayonet and integrated form camera lens, the system includes fuselage（1）And camera lens, fuselage front panel is provided with the fuselage bayonet socket for docking with camera lens（5）；（1）Described camera lens is integrated form camera lens, and integrated form camera lens is docked at the fuselage bayonet socket（5）On；Imageing sensor offsets the fuselage bayonet socket（5）Axis arrange；（2）N number of sub- camera lens with different focal is integrated with the lens barrel of described integrated form camera lens（4）；Using the new bayonet socket based on fore shaft change and telescopic catch mechanism.The image capturing method based on Novel bayonet and integrated form camera lens is somebody's turn to do, image capturing is convenient, and takes into account remarkable optical property and a machine of multiple tight shots（Fuselage）One mirror（Camera lens）Portability.
Description
Technical field
The present invention relates to a kind of image capturing method based on Novel bayonet and integrated form camera lens.
Background technology
Existing main flow camera system is generally divided into interchangeable lenses camera and not interchangeable lens camera.
Not interchangeable lens camera is mainly card camera, i.e., using a fuselage and a camera lens, and fuselage and camera lens are
It is fixed together completely, cannot dismantles during user's use, the maximum problem of this pattern is exactly, 1) if autozoom mirror
Head, the zoom of its camera lens need to be driven by fuselage, and power consumption is exceedingly fast, and the endurance of battery is poor, and general one piece of battery can only be clapped several
Ten photos or hundred multiple pictures, although generally very light, but battery durable ability cannot meet the requirement of users.
For len changeable camera, mainly single anti-and micro- list (such as the micro- list of the nex series of Sony, the J of Nikon is serial,
The EOS M series of Canon)；Referring to Fig. 1, this camera is all have a piece of imageing sensor in fuselage, due to adopting interchangeable lenses
Bayonet socket, thus by the support of camera lens group obtaining excellent imaging.But the shortcoming of this camera be also it will be apparent that
Because once only having access a camera lens, for professional photographer, need to be equipped with multiple focus head, travelling executes special shooting
During task, need to go out while carrying many pieces of camera lenses, not only weight is big, and the process of cutaway is also relatively complicated：First
Camera lens to be removed, then another camera lens is changed, camera lens bonnet is put, during changing camera lens, being easily caused fuselage interior has ash
Dirt is invaded, and, if worked in adverse circumstances, the process for changing camera lens becomes difficult all the more.
Therefore, it is necessary to design a kind of photography of new mode, image capture method.
Content of the invention
The technical problem to be solved is to provide a kind of based on Novel bayonet and the image capturing of integrated form camera lens
Method, is somebody's turn to do the image capturing method based on Novel bayonet and integrated form camera lens, and image capturing is convenient, and takes into account multiple tight shots
Remarkable optical property and a machine (fuselage) mirror (camera lens) portability.
The technical solution of invention is as follows：
A kind of image capturing method based on Novel bayonet and integrated form camera lens, using with Novel bayonet and integrated form mirror
The image acquisition system of head, described image acquisition system include fuselage and camera lens, fuselage front panel be provided with for camera lens
The fuselage bayonet socket of docking；
(1) camera lens described in is integrated form camera lens, and integrated form camera lens is docked on the fuselage bayonet socket；Set in described fuselage
It is equipped with 1 imageing sensor；
Described imageing sensor offsets the axis of the fuselage bayonet socket and arranges；Described skew can be any direction
Skew, such as relative to 0 ° of the bayonet socket center of circle, 45 °, 90 °, 180 ° (as shown in Figure 3), imageing sensor place plane and the axle
Line is vertical；
(2) N number of sub- camera lens with different focal is integrated with the lens barrel of the integrated form camera lens described in；3≤N≤12, N is
Natural number；Include one group of eyeglass in each sub- camera lens；
Axis parallel of the optical axis of N number of sub- camera lens with integrated form camera lens；And N number of sub- lens arrangement is in the week of axial line
To；
(3) one group of stationary contact is provided with fuselage bayonet socket, and camera lens rear end has one group of round and elastic contact, after integrated form camera lens
After the camera lens bayonet socket at end is installed on fuselage bayonet socket, described stationary contact is corresponding with round and elastic contact to be contacted, complete camera lens with
The docking of fuselage；
Fuselage bayonet socket is columnar structured, and the inwall of fuselage bayonet socket is provided with a snap ring with M breach；2≤M≤9,
M is integer；
Each indentation, there is provided with a telescopic catch mechanism；Telescopic catch mechanism described in each includes dynamic gear
Servo-actuated guide pad, 2 lead columns and 2 extension springs that piece, dynamic catch both sides are arranged；Respectively set in the snap ring of each breach both sides
There are 2 guiding storehouses；2 described lead columns are separately positioned on this 2 and are oriented in storehouse；2 extension springs are set in 2 lead columns
On, 2 servo-actuated guide pads are set in 2 lead columns and are connected with 2 extension springs respectively；The rear end of dynamic catch is circular arc
Or the protuberance of ellipse arc；I.e. protuberance is that outline is elliptic arc or circular arc；
The outer ring of fuselage bayonet socket is provided with for driving the fore shaft change of the telescopic catch mechanism；The inwall of fore shaft change
It is provided with M projection；Projection is circular arc or ellipse arc；It is provided with the outside of the bayonet socket of the rear end of camera lens and is adapted with the breach
The quiet catch of M pieces；
M projection, M breach, the quiet catch of M pieces and M dynamic catch are circumferential spaced set；
A shank is provided with fuselage bayonet socket, is provided with camera lens bayonet socket for the N number of pin-and-hole of circumferential locking integrated form camera lens；
Shank and pin-and-hole are the common components in existing slr camera opening, additionally, being additionally provided with fuselage for driving the bayonet pin
Camera lens locks/discharge button.
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 is correspondingly contacted, and realizes data communication；
After integrated form camera lens and fuselage complete to dock, integrated form camera lens is rotated so that a sub- mirror in N number of sub- camera lens
The optical axis of head is aligned with image sensor center point, forms imaging optical path, and fuselage obtains image or video by imageing sensor；
After alignment, the camera lens on machine for releasing locks/discharges button, and shank is inserted in pin-and-hole, prevents camera lens from occurring again to turn
Dynamic；
Described fore shaft change and the opening and closing of telescopic catch mechanism controls breach, as fore shaft change is rotated, work as projection
During the top of the protuberance for contacting the dynamic catch, the leading portion of dynamic catch reaches maximum position to seal the breach；Now
The quiet catch of camera lens is locked on the inside of snap ring and projection, realizes the locking of camera lens, and now camera lens can be rotated relative to fuselage,
To switch sub- camera lens.
When projection is not contacted with the protuberance of the dynamic catch, dynamic catch retracts to maximum position in the presence of extension spring
To concede the breach, it is easy to camera lens to load onto or take out；Now breach is opened, and the quiet catch on camera lens can be freed in and out, just
In loading onto or remove camera lens.
After integrated form camera lens and fuselage complete to dock, the optical axis and image sensing of a sub- camera lens in N number of sub- camera lens
Device central point is aligned, and forms imaging optical path, and fuselage obtains image or video by imageing sensor.
Fuselage is provided with display screen, for live view or playback picture and video.
Fuselage is provided with electronic viewfinder or optical finder, and fuselage or integrated form camera lens are provided with focusing motor, in machine
Body 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, is provided with the guiding stop chute of circular arc in camera lens bayonet socket, and slide block stretches out
End is located at and is oriented in stop chute；So fore shaft change unrestrictedly can not rotate, and can only rotate to an angle.
The torsion spring resetted for fore shaft change is provided between bayonet socket and fore shaft change, not shown in figure, is prior art, its
Effect is：When external force is not acted in fore shaft change, fore shaft change is driven to turn to an extreme position, this position just pushes away
Dynamic catch overcomes the pulling force of extension spring to block breach, as described in Figure 10 position.Ensure that camera lens will not be from fuselage in normal condition
Come off and fall and break.
Described fuselage is fuselage, card camera fuselage, micro- one camera/mono- electricity camera body or the mobile phone machine of slr camera
Body.Such as i Phone or other smart mobile phones or non-smart mobile phone.
Preferably, N is the integer between 4-6；Fuselage is provided with electronic viewfinder, and fuselage or integrated form camera lens are provided with
Focusing motor, is provided with optical anti-vibration system on fuselage or integrated form camera lens；Fore shaft change is provided with axial slide block (7), mirror
Guiding stop chute (8) of circular arc is provided with head bayonet socket, and slide block external part is located at and is oriented in stop chute；Bayonet socket is turned with fore shaft
The torsion spring resetted for fore shaft change is provided between ring；
Automatic/hand Focusing module is integrated with fuselage, and imageing sensor is square, and display screen is provided with touch sensible
Layer；Imageing sensor is cmos sensor, and imageing sensor is monolayer or three layers of sensor；Be provided with the top of fuselage flash lamp and
Tripper (3), is integrated with automatic/hand Focusing module in fuselage, imageing sensor is square, and display screen is provided with touch sense
Answer layer；The size of imageing sensor is 4/3 picture, 135 silent frames or APS-H pictures, APS-C pictures, 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- electric camera body or
Mobile phone.Beneficial effect：
The image capturing method based on Novel bayonet and integrated form camera lens of the present invention, is a kind of shooting of brand-new original creation
Method, is totally different from existing main flow camera mode, and its core idea is：The image for being integrated with a biasing on fuselage is passed
Sensor, the imageing sensor are adapted to many sub- camera lenses on integrated form camera lens, relative with fuselage bayonet socket by camera lens bayonet socket
Rotation carries out sub- Shot change and realizes manual zoom, so as to obtain high-quality image or video.Main advantages of the present invention are such as
Under：
1) high image quality：Multiple head is focused due to being integrated with, it is well known that focus head and compare, with zoom lens, there is higher light
Performance is learned, therefore, the zoom lens and single anti-zoom lens switched between head compared to traditional card camera is focused, it is easier to
High-quality image quality is ensured, its image quality can be accomplished with single anti-to focus head suitable.
2) focal length easy switching, by rotating against for camera lens bayonet socket and fuselage bayonet socket, can easily from a sub- mirror
Head is switched to another sub- camera lens, and switching is easy.
3) good portability.One integrated form camera lens is integrated with multiple tight shots (sub- camera lens), compares multiple single mirrors
Head, portability are more preferable.
4) battery durable ability is strong.Process due to zoom is directly switched without the need for being driven by motor, thus, energy
Electric energy is saved to greatest extent, when especially using electronic viewfinder, more power saving, endurance can be accomplished anti-phase with general list
When therefore, this point is compared card camera and there is great advantage.
5) docked using len changeable bayonet socket, change camera lens convenient.
6) opening and closing of fore shaft change and telescopic catch mechanism controls breach is adopted, and to facilitate the handling of camera lens, this is one
Brand-new bayonet socket pattern is planted, is constructed ingenious, it is easy to implement, it is easy to operate.
7) dynamic catch is resetted in time using torsion spring, slide block and guiding stop chute, ensures camera lens safety, thus safe
Property high.
It can be said that this image capturing method based on Novel bayonet and integrated form camera lens integrates many beautiful, existing list
Anti- high image quality, overcomes the shortcoming of the anti-portability difference for wearing multiple camera lenses of list again, the portability of existing card camera, and
Compare card camera and there is higher battery durable performance, and, construction is novel.
In sum, the best advantage is that to have taken into account high image quality, portability, handover convenience, endurance good,
Market prospect is good.
Description of the drawings
Fig. 1 is existing airframe structure schematic diagram；
Fig. 2 is the general structure schematic diagram of the image acquisition system based on Novel bayonet and integrated form camera lens；
Structural representations of the Fig. 3 for fuselage front；
Fig. 4 is fuselage bayonet socket outline drawing；
Internal structure schematic diagrams of the Fig. 5 for 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 the set location schematic diagram for being oriented to stop chute；
Fig. 9 is enlarged drawing at A in Fig. 6；
Figure 10 is enlarged drawing at B in Fig. 7；
Outside drawings of the Figure 11 for integrated form camera lens；
Rear end structure schematic diagrams of the Figure 12 for integrated form camera lens；
Axial sectional views of the Figure 13 for integrated form camera lens；
Figure 14 is the structural representation (portion such as not shown quiet catch of the rear end of the integrated form camera lens with 3 sub- camera lenses
Part)；
Figure 15 is the structural representation (portion such as not shown quiet catch of the rear end of the integrated form camera lens with 6 sub- camera lenses
Part)；
Label declaration：1- fuselages, 2- integrated form camera lenses, 3- trippers, 4- camera lenses, 5- fuselage bayonet sockets, 6- fore shafts turn
Ring, 7- slide blocks, 8- are oriented to stop chute, and 9- moves catch, 10- projections, 11- extension springs；12- stationary contacts；13- photo-sensitive cells；14- leads
Xiang Zhu, 15- are servo-actuated guide pad.16- tread plates, 17- round and elastics contact；The quiet catch of 18-, 19- light transmission passages.20- pin-and-holes,
21- shanks.51- snap rings, 52- breach.
Specific embodiment
The present invention is described in further details below with reference to the drawings and specific embodiments：
Embodiment 1：
Such as Fig. 2-13, a kind of image capturing method based on Novel bayonet and integrated form camera lens, using with Novel bayonet
With the image acquisition system of integrated form camera lens, described image acquisition system includes that fuselage 1 and camera lens, fuselage front panel are provided with
For the fuselage bayonet socket 5 docked with camera lens；
(1) camera lens described in is integrated form camera lens, and integrated form camera lens is docked on the fuselage bayonet socket 5；In described fuselage
It is provided with 1 imageing sensor 13；
Described imageing sensor offsets the axis of the fuselage bayonet socket 5 and arranges, and described skew can be any direction
Skew, such as relative to 0 ° of the bayonet socket center of circle, 45 °, 90 °, 180 ° (as shown in Figure 3), imageing sensor place plane with described
Axis is vertical；
(2) N number of sub- camera lens 4 with different focal is integrated with the lens barrel of the integrated form camera lens described in；3≤N≤12, N
For natural number；Include one group of eyeglass in each sub- camera lens；
Axis parallel of the optical axis of N number of sub- camera lens with integrated form camera lens；And N number of sub- lens arrangement is in the week of axial line
To；
(3) one group of stationary contact 12 is provided with fuselage bayonet socket, and camera lens rear end has one group of round and elastic contact 17, integrated form mirror
After the camera lens bayonet socket of head rear end is installed on fuselage bayonet socket 5, the 17 corresponding contact of described stationary contact 12 and round and elastic contact is complete
Into docking for 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 are integer；
Each indentation, there is provided with a telescopic catch mechanism；Telescopic catch mechanism described in each includes dynamic gear
15,2 lead columns 14 of servo-actuated guide pad and 2 extension springs 11 that piece 9, dynamic catch both sides are arranged；Card in each breach both sides
2 guiding storehouses are respectively provided with ring；2 described lead columns are separately positioned on this 2 and are oriented in storehouse；2 extension springs are set in 2
In individual lead column, 2 servo-actuated guide pads are set in 2 lead columns and are connected with 2 extension springs respectively；The rear end of dynamic catch
For circular arc or the protuberance of ellipse arc；I.e. protuberance is that outline is elliptic arc or circular arc；
The outer ring of fuselage bayonet socket is provided with for driving the fore shaft change 6 of the telescopic catch mechanism；Fore shaft change interior
Wall is provided with M projection；Projection is circular arc or ellipse arc；It is provided with the outside of the bayonet socket of the rear end of camera lens and is adapted with the breach
The quiet catch 18 of M pieces；
M projection, M breach, the quiet catch of M pieces and M dynamic catch are circumferential spaced set；
As fore shaft change is rotated, when the top of protuberance of catch is moved described in bump contact, the leading portion of dynamic catch is stretched
Go out to maximum position to seal the breach 52, now the quiet catch of camera lens is locked on the inside of snap ring and projection, realizes camera lens
Locking, now camera lens can rotate relative to fuselage, to switch sub- camera lens；
When projection is not contacted with the protuberance of the dynamic catch, dynamic catch retracts to dominant bit in the presence of extension spring 11
Put to concede the breach 52；Now breach is opened, and the quiet catch on camera lens can free in and out, be easy to load onto or remove mirror
Head；
After integrated form camera lens and fuselage complete to dock, the optical axis and image sensing of a sub- camera lens in N number of sub- camera lens
Device central point is aligned, and forms imaging optical path.
Fuselage is provided with display screen.
A shank is provided with fuselage bayonet socket, is provided with camera lens bayonet socket for the N number of pin-and-hole of circumferential locking integrated form camera lens；
Shank 21 and pin-and-hole 20 are the common components in existing slr camera opening, additionally, being additionally provided with fuselage for driving the bayonet socket
The camera lens of pin locks/discharge button.
Fuselage is provided with electronic viewfinder or optical finder, and fuselage or integrated form camera lens are provided with focusing motor, in machine
Body 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, and 8) slide block is stretched to be provided with the guiding stop chute of circular arc in camera lens bayonet socket
Go out end to be located in guiding stop chute.So fore shaft change unrestrictedly can not rotate, and can only rotate to an angle.
The torsion spring resetted for fore shaft change is provided between bayonet socket and fore shaft change.Not shown in figure, it is prior art, its
Effect is：When external force is not acted in fore shaft change, fore shaft change is driven to turn to an extreme position, this position just pushes away
Dynamic catch overcomes the pulling force of extension spring to block breach, as described in Figure 10 position.Ensure that camera lens will not be from fuselage in normal condition
Come off and fall and break.
Described fuselage can be the fuselage of slr camera, card camera fuselage, micro- one camera/mono- electricity camera body or handss
Machine (such as i Phone or other smart mobile phones or non-smart mobile phone).
Embodiment 2：
, with embodiment 1, difference is for remaining, is integrated with 3 sub- camera lenses, referring to Figure 14 in integrated form camera lens.
Embodiment 3：
, with embodiment 1, difference is for remaining, is integrated with 6 sub- camera lenses, referring to Figure 15 in integrated form camera lens.
Remaining it should be noted that：Fuselage or integrated form camera lens are provided with focusing motor, on fuselage or integrated form camera lens
It is provided with optical anti-vibration system；Imageing sensor is cmos sensor, and imageing sensor is monolayer or three layers of sensor；The top of fuselage
Portion is provided with flash lamp and tripper 3, is integrated with automatic/hand Focusing module in fuselage, and imageing sensor is square, display screen
It is provided with touch sensitive layer；The size of imageing sensor be 4/3 picture, 135 silent frames or APS-H pictures, APS-C pictures, 1/
1.63 inches of pictures or 1/1.7 inch of picture.
Imageing sensor can be ccd sensor, or cmos sensor, can be the mosaic sensing of monolayer
The sensor of device, or three layers, (with reference to the FOVEON X3 full-color imagery sensor chips that sigma companies adopt).
Imageing sensor is ccd sensor or cmos sensor；Imageing sensor is monolayer mosaic sensor or three layers
X3 type sensors (such as the FOVEON X3 full-color imagery sensor chips that sigma companies adopt)；
Adopt this image capturing method based on Novel bayonet and integrated form camera lens for：
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 is correspondingly contacted, and realizes data communication；
After integrated form camera lens and fuselage complete to dock, integrated form camera lens is rotated so that a sub- mirror in N number of sub- camera lens
The optical axis of head is aligned with image sensor center point, forms imaging optical path；After alignment, the camera lens locking/release on machine for releasing is pressed
Key, shank 21 are inserted in pin-and-hole 20, prevent camera lens from rotating again；
Described fore shaft change and the opening and closing of telescopic catch mechanism controls breach, as fore shaft change is rotated, work as projection
During the top of the protuberance for contacting the dynamic catch, the leading portion of dynamic catch reaches maximum position to seal the breach 52；
When projection is not contacted with the protuberance of the dynamic catch, dynamic catch retracts to dominant bit in the presence of extension spring 11
Put to concede the breach 52, be easy to camera lens to load onto or take out.
Light is projected on imageing sensor by the N number of sub- camera lens of integrated form camera lens, integrated in fuselage
Processor is stored in the digital document of the acquisition in integrated memorizer in fuselage；Described digital document is image or regards
Frequently.
When described digital document is image, deposited integrated in fuselage for image storage using any one mode following
In reservoir；
Method 1：The image file that unprocessed form is RAW forms is stored directly in memorizer；
Method 2：After carrying out processing in machine by the image file of RAW forms, the image file for being converted into JPG forms is stored in
In memorizer；
Method 3：Both the image file of RAW forms was stored in memory, also by the converting of image file by RAW forms
The image file of the JPG forms of formation is stored in memory.
Sub- camera lens is selected by rotating the leading portion of integrated form camera lens, and real time imaging is projected in electronic viewfinder.
When live view function is started, real time imaging is shown on a display screen in real time, is easy to real-time focus operation.
The story board of integrated form camera lens can arrange multiple different focals, such as 14mm, 24mm, 35mm, 50mm, 85mm,
100mm, 105mm, 150mm, 180mm, 200mm, 400mm etc..
Imageing sensor is preferably provided in surface, underface, front-left (as shown in Figure 3) or the positive right side of the axis
Side, 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 for camera lens
Enter, also allow for rotation of lens, preferably 3-6 is individual.
Claims (7)
1. a kind of image capturing method based on Novel bayonet and integrated form camera lens, it is characterised in that using having Novel bayonet
With the image acquisition system of integrated form camera lens, described image acquisition system includes fuselage (1) and camera lens, sets on fuselage front panel
There is 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 the fuselage bayonet socket (5)；In described fuselage
It is provided with 1 imageing sensor (13)；
Described imageing sensor offsets the axis setting of fuselage bayonet socket (5), imageing sensor place plane and the axle
Line is vertical；
(2) N number of sub- camera lens (4) with different focal is integrated with the lens barrel of the integrated form camera lens described in；3≤N≤12, N is
Natural number；Include one group of eyeglass in each sub- camera lens；
Axis parallel of the optical axis of N number of sub- camera lens with integrated form camera lens；And N number of sub- lens arrangement is in the circumference of axial line；
(3) one group of stationary contact (12) is provided with fuselage bayonet socket, and camera lens rear end has one group of round and elastic contact (17), integrated form mirror
After the camera lens bayonet socket of head rear end is installed on fuselage bayonet socket (5) above, described stationary contact (12) and round and elastic contact (17) are corresponding
Contact, completes docking for 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 are integer；
Each indentation, there is provided with a telescopic catch mechanism；Telescopic catch mechanism described in each includes dynamic catch
(9) servo-actuated guide pad (15), 2 lead columns (14) and 2 extension springs (11) that catch both sides are arranged, are moved；In each breach two
2 guiding storehouses are respectively provided with the snap ring of side；2 described lead columns are separately positioned on this 2 and are oriented in storehouse；2 extension spring difference
It is sleeved in 2 lead columns, 2 servo-actuated guide pads are set in 2 lead columns and are connected with 2 extension springs respectively；Dynamic gear
The rear end of piece is the protuberance of circular arc or ellipse arc；
The outer ring of fuselage bayonet socket is provided with for driving the fore shaft change (6) of the telescopic catch mechanism；The inwall of fore shaft change
It is provided with M projection；It is quiet catch (18) that the M pieces being adapted with the breach are provided with the outside of the bayonet socket of the rear end of camera lens；
M projection, M breach, the quiet catch of M pieces and M dynamic catch are circumferential spaced set；
A shank is provided with fuselage bayonet socket, is provided with camera lens bayonet socket for the N number of pin-and-hole of circumferential locking integrated form camera lens；
The rear end of integrated form camera lens is installed on fuselage bayonet socket, the stationary contact on the round and elastic contact on integrated form camera lens and fuselage
Point is corresponding to be contacted, and realizes data communication；
After integrated form camera lens and fuselage complete to dock, integrated form camera lens is rotated so that a sub- camera lens in N number of sub- camera lens
Optical axis is aligned with image sensor center point, forms imaging optical path；Fuselage obtains image or video by imageing sensor；Alignment
Afterwards, the camera lens on machine for releasing locks/discharges button, and shank (21) is inserted in pin-and-hole (20), prevents camera lens from rotating again；
Described fore shaft change and the opening and closing of telescopic catch mechanism controls breach, as fore shaft change is rotated, work as bump contact
During the top of the protuberance of the dynamic catch, the leading portion of dynamic catch reaches maximum position to seal the breach (52)；
When projection is not contacted with the protuberance of the dynamic catch, dynamic catch retracts to maximum position in the presence of extension spring (11)
To concede the breach (52), it is easy to camera lens to load onto or take out；
After integrated form camera lens and fuselage complete to dock, in the optical axis of a sub- camera lens in N number of sub- camera lens and imageing sensor
Heart point is aligned, and forms imaging optical path, and fuselage obtains image or video by imageing sensor.
2. the image capturing method based on Novel bayonet and integrated form camera lens according to claim 1, it is characterised in that machine
Display screen is provided with it, for live view or playback picture and video.
3. the image capturing method based on Novel bayonet and integrated form camera lens according to claim 1, it is characterised in that machine
Electronic viewfinder or optical finder are provided with it, and fuselage or integrated form camera lens are provided with focusing motor, in fuselage or integrated form
Camera lens is provided with optical anti-vibration system.
4. the image capturing method based on Novel bayonet and integrated form camera lens according to claim 1, it is characterised in that N
For the integer between 4-6.
5. the image capturing method based on Novel bayonet and integrated form camera lens according to claim 1, it is characterised in that lock
Mouth change is provided with axial slide block (7), is provided with guiding stop chute (8) of circular arc, slide block external part position in camera lens bayonet socket
In guiding stop chute；
The torsion spring resetted for fore shaft change is provided between bayonet socket and fore shaft change.
6. the image capturing method based on Novel bayonet and integrated form camera lens according to any one of claim 1-5, its are special
Levy and be, described fuselage is fuselage, card camera fuselage, micro- one camera/mono- electricity camera body or the handset of slr camera.
7. the image capturing method based on Novel bayonet and integrated form camera lens according to claim 2, it is characterised in that N
For the integer between 4-6；Fuselage is provided with electronic viewfinder, and fuselage or integrated form camera lens are provided with focusing motor, in fuselage or
Integrated form camera lens is provided with optical anti-vibration system；Fore shaft change is provided with axial slide block (7), is provided with circular arc in camera lens bayonet socket
Guiding stop chute (8), slide block external part be located at be oriented to stop chute in；It is provided with for fore shaft between bayonet socket and fore shaft change
The torsion spring that change resets；
Automatic/hand Focusing module is integrated with fuselage, and imageing sensor is square, and display screen is provided with touch sensitive layer；Figure
As sensor is cmos sensor, imageing sensor is monolayer or three layers of sensor；Flash lamp and shutter is provided with the top of fuselage
Button (3), is integrated with automatic/hand Focusing module in fuselage, imageing sensor is square, and display screen is provided with touch sensible
Layer；The size of imageing sensor be 4/3 picture, 135 silent frames or APS-H pictures, APS-C pictures, 1/1.63 inch of picture or
1/1.7 inch of picture；Described fuselage is fuselage, card camera fuselage, micro- one camera/mono- electricity camera body or the handss of slr camera
Machine.
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| CN201410000511.3A CN103702022B (en) | 2014-01-01 | 2014-01-01 | A kind of image capturing method based on Novel bayonet and integrated form camera lens |
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| CN103702022B true CN103702022B (en) | 2017-03-15 |
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| RU2747716C2 (en) | 2017-05-31 | 2021-05-13 | Кэнон Кабусики Кайся | Image capture device, accessory that can be installed on it and camera system |
| CN108989620B (en) | 2017-05-31 | 2021-06-22 | 佳能株式会社 | Accessory, image pickup apparatus capable of mounting accessory, and camera system |
| CN208401980U (en) | 2017-05-31 | 2019-01-18 | 佳能株式会社 | Picture pick-up device and accessory |
| CN112731738B (en) | 2017-05-31 | 2022-08-02 | 佳能株式会社 | Lens mount, accessory, camera mount, camera system, and image pickup apparatus |
| SG10201804096XA (en) | 2017-05-31 | 2018-12-28 | Canon Kk | Adapter device, imaging apparatus, and accessory |
| CN107800942A (en) * | 2017-12-14 | 2018-03-13 | 信利光电股份有限公司 | A kind of camera and terminal |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN102835101A (en) * | 2010-04-16 | 2012-12-19 | 松下电器产业株式会社 | Digital camera |
| CN103200355A (en) * | 2012-11-10 | 2013-07-10 | 罗天成 | Novel intelligent terminal and shell body connected with intelligent terminal |
| CN103207503A (en) * | 2012-01-12 | 2013-07-17 | 单祥太 | Supporting bracket of lens-exchangeable digital camera and with functions of pitching expanding, swinging and shaft moving |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| DE102004009856A1 (en) * | 2004-02-25 | 2005-09-22 | Arnold & Richter Cine Technik Gmbh & Co Betriebs Kg | Device for connecting a camera lens to a motion picture camera |
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Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102835101A (en) * | 2010-04-16 | 2012-12-19 | 松下电器产业株式会社 | Digital camera |
| CN103207503A (en) * | 2012-01-12 | 2013-07-17 | 单祥太 | Supporting bracket of lens-exchangeable digital camera and with functions of pitching expanding, swinging and shaft moving |
| CN103200355A (en) * | 2012-11-10 | 2013-07-10 | 罗天成 | Novel intelligent terminal and shell body connected with intelligent terminal |
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