CN207112256U - Head device for shooting - Google Patents

Head device for shooting Download PDF

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Publication number
CN207112256U
CN207112256U CN201720946265.XU CN201720946265U CN207112256U CN 207112256 U CN207112256 U CN 207112256U CN 201720946265 U CN201720946265 U CN 201720946265U CN 207112256 U CN207112256 U CN 207112256U
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CN
China
Prior art keywords
head
bearing
head device
shooting
camera
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201720946265.XU
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Chinese (zh)
Inventor
刘以奋
蓝求
胡登峰
赵天菲
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SZ DJI Osmo Technology Co Ltd
Original Assignee
SZ DJI Osmo Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SZ DJI Osmo Technology Co Ltd filed Critical SZ DJI Osmo Technology Co Ltd
Priority to CN201720946265.XU priority Critical patent/CN207112256U/en
Application granted granted Critical
Publication of CN207112256U publication Critical patent/CN207112256U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A kind of head device for shooting (100), including fuselage (10), fold mechanism (20) and head camera (30), head camera (30) length are less than fuselage (10) length.Fuselage (10) includes supporting walls (101), and head camera (30) includes deployed condition and folded state, and fold mechanism (20) includes:The bearing (50) that is connected with head camera (30) and the locating part (40) for being connected to supporting walls (101), bearing (50) are axially rotationally connected with supporting walls (101) around a rotation parallel with supporting walls (101).Locating part (40) is positioned at the vertical direction for rotating axial direction.Bearing (50) drives head camera (30) to go to deployed condition, and bearing (50) is connected to locating part (40).Bearing (50) drives head camera (30) to go to folded state, and head camera (30) fits in supporting walls (101), reduces the space that head camera takes.

Description

Head device for shooting
Technical field
Head technical field is the utility model is related to, more particularly to a kind of head device for shooting.
Background technology
In the prior art, head device for shooting or hand-held head device for shooting can shoot stable image under motion state, Because liked by users.Head device for shooting is completed to increase surely camera device for shooting using gyroscope and motor, makes The stable stabilization of image taking.
Head device for shooting generally includes fuselage and the head camera being installed on fuselage, and head device for shooting can root when working The position of head camera is adjusted according to the motion state of user, the camera of head camera is in certain position shooting figure all the time Picture, so as to steady shot image.But when head device for shooting does not work, the position of head camera can arbitrarily rock and take larger Space, cause the structure of head device for shooting unstable and be unfavorable for carrying and store.
Utility model content
The utility model provides a kind of head device for shooting, including:Fuselage, the fold mechanism being connected with the fuselage and The head camera being connected with the fold mechanism, the length of the head camera are less than the length of the fuselage, the head phase Machine can fit in the fuselage by the fold mechanism;Wherein, the fuselage includes being used to support the fold mechanism and institute The supporting walls of head camera are stated, the head camera includes deployed condition and folded state, and the fold mechanism includes:
The bearing being connected with the head camera, the bearing rotate around one and are axially rotationally connected with the supporting walls, with The head camera is driven to be rotated relative to the fuselage, the rotation axially be arranged in parallel with the supporting walls;
Locating part, the supporting walls are connected to along the direction axially vertical with the rotation;
The bearing drives the head camera to turn to deployed condition, and the bearing is connected to the locating part;It is described Bearing drives the head camera to turn to folded state, and the head camera fits in the supporting walls.
Further, one end on the bearing close to the locating part is provided with bearing surface, remote on the head camera One end of the locating part is provided with binding face;
The bearing drives the head camera to turn to deployed condition, and the bearing surface is connected to the locating part;Institute Stating bearing drives the head camera to turn to folded state, and the binding face fits in the supporting walls.
Further, in addition to the bearing motor being connected, the motor drive the bearing to rotate.
Further, in addition to for locking the latch-up structure of the bearing.
Further, in addition to it is connected to the rotating assemblies of the supporting walls, the rotating assembly includes rotating shaft, described turn Axle is axially arranged along the rotation, and the bearing is articulated in the rotating shaft.
Further, the rotating assembly also includes two supporting parts for being connected to the supporting walls, the two supporting parts edge The rotation is axially oppositely arranged, and the both ends of the rotating shaft are connected with two supporting parts respectively.
Further, the bearing is provided with the through hole that setting is axially penetrated through along the rotation, and the rotating shaft is arranged in described Through hole.
Further, the supporting parts are provided with bracing strut, and the rotating shaft is fixed with the bracing strut.
Further, the both ends of the rotating shaft are respectively equipped with axle bed body, and the axle bed body passes through fastener and the axle branch Frame is fixed.
Further, the rotating assembly also including the locating shaft with the concentric setting of the rotating shaft and is connected to the branch Two supporting parts of wall are supportted, two supporting parts are axially oppositely arranged along the rotation;
The rotating shaft is connected with supporting parts one of them described, and the locating shaft is connected with supporting parts another described;Institute The one end for stating bearing is articulated in the rotating shaft, and the other end of the bearing is articulated in the locating shaft.
Further, the bearing is provided with the through hole that setting is axially penetrated through along the rotation, and the rotating shaft is arranged in described One end of through hole, the locating shaft are arranged in the other end of the through hole.
Further, the both ends of the bearing are respectively equipped with blind hole, and the rotating shaft is arranged in one of them described blind hole, institute State locating shaft and be arranged in another blind hole.
Further, two supporting parts are equipped with bracing strut, the rotating shaft and the locating shaft respectively with corresponding institute The bracing strut for stating supporting parts is fixed.
Further, one end of two supporting parts is connected with the locating part, the other ends of two supporting parts it Between formed with the breach that passes through when being rotated for the head camera.
Further, the locating part is formed in one with two supporting parts.
Further, the locating part is integrally molded so as U-shape structure with two supporting parts.
Further, the both ends of the bearing fit in two supporting parts respectively.
Further, the locating part is inclined to set with the supporting walls.
Further, the scope at the inclination angle between the locating part and the supporting walls is 85 ° to 95 °.
Further, the head camera includes three axle head supports and is equipped on the shooting of the three axles head support Device.
Further, the three axles head support include is flexibly connected with the bearing translation shaft assembly, with it is described put down Move the roll shaft assembly that shaft assembly is flexibly connected and the pitching shaft assembly being flexibly connected with the roll shaft assembly, the bat Take the photograph device and be equipped on the pitching shaft assembly.
Further, the rotary shaft of the translation shaft assembly is axially vertically arranged with the rotation.
Further, in addition to display screen, the display screen are installed in the fuselage.
Further, in addition to it is used for the mounting bracket for installing external display device, the mounting bracket is installed in the fuselage.
Further, in addition to the first button, first button are arranged at the supporting walls, in the head phase Machine operates the head camera and shot when being in deployed condition.
Further, in addition to the second button, second button are arranged at adjacent with the supporting walls on the fuselage Side wall, shot for operating the head camera when the head camera is in folded state.
Further, in addition to the second button, second button are arranged at adjacent with the supporting walls on the fuselage Side wall, for adjusting the shooting angle or screening-mode of the head camera when the head camera is in deployed condition.
Further, in addition to it is used for the power knob for opening and closing the head device for shooting, is arranged on the fuselage and institute State the adjacent side wall of supporting walls.
Head device for shooting of the present utility model, head camera is driven in deployed condition and folding by the bearing of fold mechanism Switched between state two states, realize the folder function to head camera.Rugosity is in when head camera does not work State, it not only may be at deployed condition but also may be at folded state during work.When head camera deploys, pass through locating part and bearing Cooperation the position of head camera is carried out spacing, position of the head camera in deployed condition is kept stable.Head camera When not working, head camera can be folded to and fit in fuselage, the volume for reducing head device for shooting is existed with solving head camera The problem of folded state space-consuming when not working is larger, and prevent folded state of the head camera when not working from shaking It is dynamic, so as to preferably realize the portable carrying and storage of head device for shooting, and the design of integration compact structure.
Brief description of the drawings
Fig. 1 is that the utility model one implements a kind of schematic perspective view of head device for shooting for exemplifying in the deployed state.
Fig. 2 is that the utility model one implements a kind of side view of head device for shooting for exemplifying in the deployed state.
Fig. 3 is that the utility model one implements a kind of schematic perspective view of head device for shooting for exemplifying in a folded configuration.
Fig. 4 is the solid that the utility model one implements a kind of head device for shooting for exemplifying another visual angle in a folded configuration Schematic diagram.
Fig. 5 is that the utility model one implements a kind of side view of head device for shooting for exemplifying in a folded configuration.
Fig. 6 is the first sectional view of axis of rotation mode along A-A directions of the head device for shooting shown in Fig. 2.
Fig. 7 is sectional view of second of the axis of rotation mode of the head device for shooting shown in Fig. 2 along A-A directions.
Fig. 8 is that the utility model one implements a kind of schematic perspective view of head device for shooting for exemplifying in rotation process.
Fig. 9 is that the utility model one implements a kind of side view of head device for shooting for exemplifying in rotation process.
Embodiment
Here exemplary embodiment will be illustrated in detail, its example is illustrated in the accompanying drawings.Following description is related to During accompanying drawing, unless otherwise indicated, the same numbers in different accompanying drawings represent same or analogous key element.Following exemplary embodiment Described in embodiment do not represent all embodiments consistent with the utility model.On the contrary, they be only with such as The example of the consistent apparatus and method of some aspects being described in detail in appended claims, of the present utility model.
It is only merely for the purpose of description specific embodiment in the term that the utility model uses, and is not intended to be limiting this reality With new." one kind ", " described " and "the" of singulative used in the utility model and appended claims It is intended to include most forms, unless context clearly shows that other implications.It is also understood that term used herein " and/ Or " refer to and any or all may be combined comprising the associated list items purposes of one or more.
It should be appreciated that " first " " second " that is used in present specification and claims and similar word Any order, quantity or importance are not offered as, and is used only to distinguish different parts.Equally, "one" or The similar word such as " one " does not indicate that quantity limits yet, but represents to exist at least one.Unless otherwise noted, " front portion ", " after The similar word such as portion ", " bottom " and/or " top " is not limited to a position or a kind of empty only to facilitate explanation Between orient.Either the similar word such as "comprising" means to appear in element or object before " comprising " or "comprising" to " comprising " Cover and appear in the " comprising " either element of "comprising" presented hereinafter or object and its equivalent, it is not excluded that other elements or Object." connection " either the similar word such as " connected " is not limited to physics or mechanical connection, and can include Electrical connection, it is either directly or indirect.
For current head device for shooting when not working, head camera arbitrarily rocks structure shakiness and the big inconvenience of space-consuming In carry the problem of, the utility model provides one kind and occupied little space when not working and portable head device for shooting.Below With reference to accompanying drawing, head device for shooting of the present utility model is described in detail.In the case where not conflicting, following embodiments and Feature in embodiment can be mutually combined.
Referring to a kind of head device for shooting 100 that shown in Fig. 1 to Fig. 5, the utility model embodiment provides, including:Fuselage 10, The fold mechanism 20 being connected with the fuselage 10 and the head camera 30 being connected with the fold mechanism 20, the head phase The length that the length (it is appreciated that in order that along the length of Y-direction in Fig. 1) of machine 30 is less than the fuselage 10 (again it will be understood that In order that along the length of Y-direction in Fig. 1), the head camera 30 can fit in the fuselage 10 by the fold mechanism 20. The fuselage 10 includes being used for the supporting walls 101 for supporting the fold mechanism 20 and the head camera 30, the head camera 30 include deployed condition (non-folded state as depicted in figs. 1 and 2) and folded state (as shown in Figures 3 to 5), pass through folding Mechanism 20 drives head camera 30 to be switched between deployed condition and folded state two states.Under normal circumstances, head It is in folded state when camera 30 does not work, had not only may be at deployed condition but also may be at folded state during work.In this reality Apply in example, the installation site of the fold mechanism 20 can be located at the left hand edge of supporting walls 101 of fuselage 10, can also be located at The right edge of the supporting walls 101 of fuselage 10.In the example depicted in figure 1, the installation site of fold mechanism 20 is located at fuselage 10 Supporting walls 101 left hand edge at.The fuselage 10 is rectangular configuration, and the supporting walls 101 are located at the top surface of the fuselage 10.
Wherein, the fold mechanism 20 includes locating part 40 and bearing 50.The bearing 50 connects with the head camera 30 Connect, the bearing 50 rotates around one and axially 70 is rotationally connected with the supporting walls 101, to drive the head camera 30 with respect to institute State fuselage 10 to rotate, switched over so as to realize head camera 30 between deployed condition and folded state two states, it is described Rotate and axially 70 be arranged in parallel with the supporting walls 101, the setting direction for rotating axial direction 70 is in Fig. 1 as shown in X-direction. The locating part 40 is connected to the supporting walls 101 along with the axially 70 vertical directions that rotate, in Fig. 1 such as Y-direction institute Show.
The bearing 50 drives the head camera 30 to turn to deployed condition, and the bearing 50 is connected to the locating part 40, the cooperation by locating part 40 and bearing 50 is spacing by the position progress of head camera 30, makes head camera 30 in expansion shape Position during state keeps stable.The bearing 50 drives the head camera 30 to turn to folded state, the head camera 30 The supporting walls 101 are fitted in, equivalent to the top surface for being housed in fuselage 10, the volume of head device for shooting 100 can be reduced to solve The problem of certainly folded state space-consuming of the head camera 30 when not working is larger, and prevent head camera 30 when not working Folded state shake, so as to preferably realize the portable carrying and storage of head device for shooting 100.Head camera 30 Length be less than fuselage 10 length, head camera 30 can be ensured in folded state in the range of structures of fuselage 10.
From above-described embodiment, head device for shooting 100 of the present utility model, driven by the bearing 50 of fold mechanism 20 Head camera 30 switches between deployed condition and folded state two states, realizes the folding work(to head camera 30 Energy.When head camera 30 is organized work, the cooperation by locating part 40 and bearing 50 is spacing by the position progress of head camera 30, Position of the head camera 30 in deployed condition is set to keep stable., can be by the folding of head camera 30 when head camera 30 does not work It is stacked to and fits in fuselage 10, reduces the volume of head device for shooting 100 to solve folded state of the head camera 30 when not working The problem of space-consuming is larger, and prevent folded state of the head camera 30 when not working from shaking, so as to preferably real The portable carrying and storage of existing head device for shooting 100, and the design of integration compact structure.
In an optional embodiment, the head camera 30 includes head support and is equipped on the bat of the head support Take the photograph device 302.Wherein, the head support can be single shaft, twin shaft or multiaxis head support, in example shown in the figure, institute It is three axle head supports to state head support, and the three axles head support includes the translation shaft assembly being flexibly connected with the bearing 50 303rd, with the roll shaft assembly 304 that is flexibly connected of translation shaft assembly 303 and with the activity of roll shaft assembly 304 company The pitching shaft assembly 305 connect, the device for shooting 302 are equipped on the pitching shaft assembly 305.The translation shaft assembly 303 passes through The translational motion of translation shaft motor control head camera 30, roll shaft assembly 304 control head camera 30 by roll spindle motor Roll motion, pitching shaft assembly 305 controls device for shooting by the elevating movement of pitch axis motor control head camera 30 302 can carry out image taking with different shooting angle, and shooting angle that can be as needed is to the position of head camera 30 Put and be adjusted.When the head assembly 30 is in folded state (as shown in Figure 3), the rotary shaft of the translation shaft assembly 303 Axially 70 it is vertically arranged with described rotate, the rotary shaft of the roll shaft assembly 304 axially 70 be arranged in parallel with described rotate, institute The rotary shaft and described rotate for stating pitching shaft assembly 305 axially 70 are vertically arranged.When the head assembly 30 is in deployed condition (as shown in Figure 1), rotary shaft and described rotate of the translation shaft assembly 303 axially 70 are vertically arranged, the roll shaft assembly 304 rotary shaft can change relative to the position for rotating axial direction 70 according to the rotation of translation shaft assembly 303, described The rotary shaft of pitching shaft assembly 305 can be sent out relative to the position for rotating axial direction 70 according to the rotation of roll shaft assembly 304 Changing.
In an optional embodiment, with reference to shown in Fig. 1 and Fig. 2, the device for shooting 302 of the head camera 30 is away from described One end of locating part 40 is provided with binding face 301.When head camera 30 does not work, the bearing 50 drives 30 turns of the head camera Move to folded state, the binding face 301 fits in the supporting walls 101.Pass through the binding face 301 and fuselage of head camera 30 The mutual cooperation of 10 supporting walls 101, the position progress of head camera 30 is spacing, the volume of head device for shooting 100 can be reduced, And the position of folded state of the head camera 30 when not working can be made to keep stable, prevent head camera 30 from shaking.Knot Close shown in Fig. 3 to Fig. 5, one end on the bearing 50 close to the locating part 40 is provided with bearing surface 501, and the bearing 50 drives The head camera 30 turns to deployed condition, and the bearing surface 501 is connected to the locating part 40, passes through locating part 40 and branch The mutual cooperation of the bearing surface 501 of seat 50, the position progress of head camera 30 is spacing, make head camera 30 in deployed condition Position keep stable.
Further, can be in head camera 30 in order that position of the head camera 30 in folded state is more stable Binding face 301 and fuselage 10 supporting walls 101 on the 301 corresponding position of binding face of head camera 30 phase is set respectively The fixed structure mutually coordinated, it is more difficult when head camera 30 is fitted in the supporting walls 101 of fuselage 10 to rock.It is for example, described The fixed structure of mutual cooperation can be one kind in buckle structure or magnet adsorbing structure or buckle structure.
In an optional embodiment, the head device for shooting 100 also includes the rotating shaft group for being connected to the supporting walls 101 Part, the rotating assembly include rotating shaft 201, and the rotating shaft 201 is set along the direction for rotating axial direction 70, the pivot of bearing 50 It is connected to the rotating shaft 201.It should be noted that realize that bearing 50 is not limited in setting relative to the mode that fuselage 10 is rotated The mode of rotating shaft, can also be by setting other pin-joint mechanisms or multi-connecting-rod mechanism to be realized, the realization of such Variations similar Mode, it should be included in the scope of protection of the utility model.
Wherein, rotating shaft 201 can use a variety of different rotation formulas, such as integral rotating shaft, rotating shaft to coordinate locating shaft, resistance The rotation formulas such as Buddhist nun's axle, spring shaft.Separately below so that rotating shaft 201 coordinates locating shaft using integral rotating shaft and rotating shaft as an example, to turning The rotation formula of axle 201 is introduced.
(1) rotating shaft 201 uses the rotation formula of integral rotating shaft:Referring to shown in Fig. 1, Fig. 3 and Fig. 6, the rotating assembly is also Two supporting parts 102 including being connected to the supporting walls 101, direction phase of two supporting parts 102 along the rotation axial direction 70 To setting, the both ends of the rotating shaft 201 are connected with two supporting parts 102 respectively.The supporting parts 102 can be regarded as by institute The supporting walls 101 for stating fuselage 10 extend vertically formed projective structure upwards.The bearing 50 is provided with along described and rotated axially 70 direction is arranged in the through hole 502, bearing 50 is articulated in the rotating shaft through the through hole 502 set, the rotating shaft 201 201, and then enable bearing 50 to drive head camera 30 to be rotated relative to fuselage 10.
Further, the supporting parts 102 are provided with bracing strut 103, and the both ends of the rotating shaft 201 are respectively equipped with axle bed body 202, the axle bed body 202 is fixed by fastener 203 and the bracing strut 103, and then the rotating shaft 201 is held with described two Supporting piece 102 is fixed.Alternatively, the fastener 203 can use screw, can also use what pin, splicing etc. were fixedly connected Form, the connected mode of such Variations similar, should be included in the scope of protection of the utility model.
(2) rotating shaft 201 coordinates the rotation formula of locating shaft using rotating shaft:Referring to shown in Fig. 1, Fig. 3 and Fig. 7, the rotating shaft Component also includes with the locating shaft 204 of the 201 concentric setting of rotating shaft and is connected to two supporting parts of the supporting walls 101 102, two supporting parts 102 are oppositely arranged along the direction for rotating axial direction 70.The rotating shaft 201 and one of supporting parts 102 connections, the locating shaft 204 are connected with another supporting parts 102.One end of the bearing 50 is articulated in the rotating shaft 201, The other end of the bearing 50 is articulated in the locating shaft 204.
The bearing 50 is provided with along the direction for rotating axial direction 70 and worn through the through hole 502 set, the rotating shaft 201 In one end of the through hole 502, the locating shaft 204 is arranged in the other end of the through hole 502, is articulated in bearing 50 described Rotating shaft 201, and then enable bearing 50 to drive head camera 30 to be rotated relative to fuselage 10.Certainly, the through hole 502 can also be by The both ends of the hole that axis overlaps substitutes, i.e., the both ends of described bearing 50 are respectively equipped with blind hole, and the rotating shaft 201 is arranged in one of them The blind hole, the locating shaft 204 are arranged in another blind hole.Or blind hole is opened up on two supporting parts 102, The rotating shaft 201 and locating shaft 204 are respectively provided to the both ends of bearing 50, the rotating shaft 201 is arranged in described in one of them Blind hole, the locating shaft 204 are arranged in another blind hole.Bearing 50 can be equally set to be articulated in the rotating shaft 201, and then Bearing 50 is set to drive head camera 30 to be rotated relative to fuselage 10.
Further, two supporting parts 102 are equipped with the end of bracing strut 103, the rotating shaft 201 and locating shaft 204 Axle bed body 202 is equipped with, the axle bed body 202 is fixed with the bracing strut 103 of corresponding supporting parts 102 by fastener 203, entered And the rotating shaft 201 and locating shaft 204 are fixed with corresponding supporting parts 102 respectively.Alternatively, the fastener 203 can be with Using screw, the form that pin, splicing etc. can also be used to be fixedly connected, the connected mode of such Variations similar, all should include In the scope of protection of the utility model.
In an optional embodiment, the first end of two supporting parts 102 is connected with the locating part 40, and then will The locating part 40 and two supporting parts 102 form an overall structure, can strengthen the strong of locating part 40 and supporting parts 102 Degree., can be with formed with the breach 1020 that passes through when being rotated for the head camera 30 between the other end of two supporting parts 102 Understand, it is necessary to pass through the breach 1020 during head camera 30 rotates between deployed condition and folded state. Further, the both ends of the bearing 50 fit in two supporting parts 102 respectively, can ensure 201 turns around the shaft of bearing 50 Dynamic stability.Alternatively, the locating part 40 is formed in one with two supporting parts 102, and the locating part 40 with Link position between the supporting parts 102 is rounding off.In example shown in the figure, the locating part 40 and described two Supporting parts 102 are integrally molded so as U-shape structure.
Further, the size of head camera 30 is also required to be adapted with bearing 50, avoids head camera 30 from being in folding During state, the problem of can not being bonded due to the oversized or too small of head assembly 30 with the supporting walls 101 of fuselage 10.Example As in example shown in the figure, the size of head camera 30 is identical with the size of bearing 50.
In an optional embodiment, the locating part 40 is inclined to set with the supporting walls 101, and then to head phase The rotational angle of machine 30 is limited.Alternatively, the scope at the inclination angle between the locating part 40 and the supporting walls 101 is 85 ° to 95 °, it is therefore preferable to 90 °, and then control head camera 30 (can fold from folded state and fit in the upper of fuselage 10 90 ° just) are rotated to rotate to deployed condition (i.e. such as the top for being erected in fuselage 10 in Fig. 1 along Z-direction), or from deployed condition 90 ° to folded state.And head camera 30 is during rotation, it is necessary to breach by being formed between two supporting parts 102 1020。
In an optional embodiment, be additionally provided with the fuselage 10 device for shooting 302 can be controlled to be shot (can To be that image taking can also be video capture) button.Alternatively, the supporting walls 101 of the fuselage 10 can set first Button 80a (the first button 80a shown in figure is located at the top surface of fuselage 10), deployed condition is in for user in head camera 30 When operation device for shooting 302 shot.Alternatively, side wall adjacent with the supporting walls 101 on the fuselage 10 can be set Second button 80b (the second button 80b shown in figure is located at the side of fuselage 10), such as the second button 80b are located on fuselage 10 Away from the side of the camera lens of device for shooting 302, operate device for shooting 302 when head camera 30 is in folded state for user and clapped Take the photograph, head camera 30 is still available for shooting when being in folded state and use.In addition, when head camera 30 is in deployed condition, The head support of head camera 30 can also be adjusted to change the shooting angle of device for shooting 302 by the second button 80b, And the screening-mode of device for shooting 302 is changed.For example, when head camera 30 is in deployed condition, is pressed Two button 80b can be changed the screening-mode of device for shooting 302 between exposal model and image pickup mode.Continuously press two Head support can be adjusted to back positive status by lower second button 80b, realize automatic aligning function.It is continuous press three times second by Button 80b can control the translation shaft assembly 303 of head support to be rotated, and device for shooting 302 is gone to towards user to realize Self-timer.It is understood that the corresponding pattern realized of number and head camera 30 that button connects are pressed can basis Demand and set, however it is not limited to the present embodiment.
Further, power knob 90 is additionally provided with the fuselage 10, for opening or closing head device for shooting 100.Can Selection of land, the side wall adjacent with the supporting walls 101 on the fuselage 10 of power knob 90.In example shown in the figure, The button 80b of power knob 90 and second is located at the same side of fuselage 10, and positioned at the second button 80b top.
Referring to Fig. 1, Fig. 3 and with reference to shown in Fig. 8 and Fig. 9, head camera 30 from deployed condition turn to folded state when, cloud The change in location process of platform camera 30 is first to turn to Fig. 8 from the position of the supporting walls 101 for being erected in fuselage 10 as shown in Figure 1 The position of the shown supporting walls 101 for favouring fuselage 10, then turned to from the position shown in Fig. 8 and fit in machine shown in Fig. 3 The position of the supporting walls 101 of body 10.Correspondingly, head camera 30 from deployed condition be transformed into off working state when change in location And so.Head camera 30 from folded state turn to deployed condition when, the change in location process of head camera 30 be first from The position of the supporting walls 101 for fitting in fuselage 10 as shown in Figure 3 turns to the supporting walls for favouring fuselage 10 shown in Fig. 8 101 position, then turn to from the position shown in Fig. 8 the position of the supporting walls 101 for being erected in fuselage 10 shown in Fig. 1.Accordingly Ground, head camera 30 from off working state be transformed into deployed condition when change in location be also such.When head camera 30 is being opened up When being worked under open state, device for shooting 302 can be operated by the first button 80a and be shot.When head camera 30 is being rolled over When needing work under overlapping state, device for shooting 302 can be operated by the second button 80b and be shot.
In an optional embodiment, head camera 30 can be rotated manually.The head device for shooting 100 also wraps The latch-up structure for locking the bearing 50 is included, when the bearing 50 drives head camera 30 to turn to deployed condition, is led to Cross the latch-up structure to be locked the position of the bearing 50, to cause position of the head camera 30 in deployed condition to protect It is fixed to keep steady.The concrete structure of the latch-up structure can design according to different demands.For example, the latch-up structure can be card Button, latch etc..In another optional embodiment, head camera 30 can be directly driven by motor and be rotated, no Need to set above-mentioned latch-up structure.The head device for shooting 100 also includes the motor being connected with the bearing 50, passes through institute Stating motor drives the bearing 50 to be rotated around the rotating shaft 201, and then drives relative 10 turns of the fuselage of head camera 30 It is dynamic.The rotational angle of head camera 30 can be set by setting action time or the speed of motor.
In an optional embodiment, the head device for shooting 100 can include display screen 60, and the display screen 60 is installed Observed in the one side of the fuselage 10, during so as to be available for users to shooting.In example shown in the figure, the display screen 60 The same side of fuselage 10 is located at the second button 80b and power knob 90, i.e., deviates from device for shooting on described fuselage 10 302 side.In another optional embodiment, the head device for shooting 100 can include being used to install external display device Mounting bracket, the mounting bracket is installed in the fuselage 10.The external display device can receive device for shooting 302 to clap The equipment for taking the photograph image, such as mobile phone or tablet personal computer etc., are observed when being equally available for users to shooting.
To sum up, head device for shooting 100 of the present utility model, head camera 30 is driven to exist by the bearing 50 of fold mechanism 20 Switched between deployed condition and folded state two states, realize the folder function to head camera 30.Head camera 30 When working in the deployed state, head camera 30 can be deployed normal work, will by the cooperation of locating part 40 and bearing 50 The position progress of head camera 30 is spacing, position of the head camera 30 in deployed condition is kept stable.Head camera 30 is not During work, head camera 30 can be folded and fit in fuselage 10, reduce the volume of head device for shooting 100 to solve head camera The problem of 30 folded state space-consuming when not working is larger, and prevent folded state of the head camera 30 when not working Shake, so as to preferably realize that the portable carrying and storage of head device for shooting 100, and integration compact structure are set Meter.
Described above is only preferred embodiment of the present utility model, not the utility model is done any formal Limitation, although the utility model is disclosed above with preferred embodiment, but is not limited to the utility model, any to be familiar with Professional and technical personnel, in the range of technical solutions of the utility model are not departed from, when in the technology using the disclosure above Hold the equivalent embodiment made a little change or be modified to equivalent variations, as long as being without departing from technical solutions of the utility model Hold, any simple modification, equivalent change and modification made according to the technical essence of the utility model to above example, still Belong in the range of technical solutions of the utility model.
This patent document disclosure includes material protected by copyright.The copyright owns for copyright holder.Copyright Owner does not oppose that anyone replicates the patent document in the presence of the proce's-verbal of Patent&Trademark Office and archives or should Patent discloses.

Claims (28)

  1. A kind of 1. head device for shooting, it is characterised in that including:Fuselage, the fold mechanism being connected with the fuselage and with it is described The head camera of fold mechanism connection, the length of the head camera are less than the length of the fuselage, and the head camera can lead to Cross the fold mechanism and fit in the fuselage;Wherein, the fuselage includes being used to support the fold mechanism and the head The supporting walls of camera, the head camera include deployed condition and folded state, and the fold mechanism includes:
    The bearing being connected with the head camera, the bearing rotate around one and are axially rotationally connected with the supporting walls, to drive The head camera rotates relative to the fuselage, and the rotation axially be arranged in parallel with the supporting walls;
    Locating part, the supporting walls are connected to along the direction axially vertical with the rotation;
    The bearing drives the head camera to turn to deployed condition, and the bearing is connected to the locating part;The bearing The head camera is driven to turn to folded state, the head camera fits in the supporting walls.
  2. 2. head device for shooting according to claim 1, it is characterised in that close to one end of the locating part on the bearing Provided with bearing surface, one end away from the locating part is provided with binding face on the head camera;
    The bearing drives the head camera to turn to deployed condition, and the bearing surface is connected to the locating part;The branch Seat drives the head camera to turn to folded state, and the binding face fits in the supporting walls.
  3. 3. head device for shooting according to claim 1, it is characterised in that also include the driving electricity being connected with the bearing Machine, the motor drive the bearing to rotate.
  4. 4. head device for shooting according to claim 1, it is characterised in that also include being used for the locking knot for locking the bearing Structure.
  5. 5. head device for shooting according to claim 1, it is characterised in that also include the rotating shaft group for being connected to the supporting walls Part, the rotating assembly include rotating shaft, and the rotating shaft is axially arranged along the rotation, and the bearing is articulated in the rotating shaft.
  6. 6. head device for shooting according to claim 5, it is characterised in that the rotating assembly also includes being connected to the branch Two supporting parts of wall are supportted, two supporting parts are axially oppositely arranged along the rotation, and the both ends of the rotating shaft are respectively with described two Supporting parts connect.
  7. 7. head device for shooting according to claim 6, it is characterised in that the bearing is provided with along the rotation and axially penetrated through The through hole of setting, the rotating shaft are arranged in the through hole.
  8. 8. head device for shooting according to claim 6, it is characterised in that the supporting parts are provided with bracing strut, the rotating shaft Fixed with the bracing strut.
  9. 9. head device for shooting according to claim 8, it is characterised in that the both ends of the rotating shaft are respectively equipped with axle bed body, The axle bed body is fixed by fastener and the bracing strut.
  10. 10. head device for shooting according to claim 5, it is characterised in that the rotating assembly also includes and the rotating shaft The locating shaft of concentric setting and two supporting parts for being connected to the supporting walls, two supporting parts are axially opposing along the rotation Set;
    The rotating shaft is connected with supporting parts one of them described, and the locating shaft is connected with supporting parts another described;The branch One end of seat is articulated in the rotating shaft, and the other end of the bearing is articulated in the locating shaft.
  11. 11. head device for shooting according to claim 10, it is characterised in that the bearing is provided with along the rotation and axially passed through The through hole put is worn, the rotating shaft is arranged in one end of the through hole, and the locating shaft is arranged in the other end of the through hole.
  12. 12. head device for shooting according to claim 10, it is characterised in that the both ends of the bearing are respectively equipped with blind hole, The rotating shaft is arranged in one of them described blind hole, and the locating shaft is arranged in another blind hole.
  13. 13. head device for shooting according to claim 10, it is characterised in that two supporting parts are equipped with bracing strut, institute The bracing strut of rotating shaft and the locating shaft respectively with the corresponding supporting parts is stated to fix.
  14. 14. the head device for shooting according to claim 6 or 10, it is characterised in that one end of two supporting parts is and institute State locating part to connect, formed with the breach passed through when rotating for the head camera between the other end of two supporting parts.
  15. 15. head device for shooting according to claim 14, it is characterised in that the locating part is one with two supporting parts It is body formed.
  16. 16. head device for shooting according to claim 15, it is characterised in that the locating part and two supporting parts one It is shaped to U-shape structure.
  17. 17. the head device for shooting according to claim 6 or 10, it is characterised in that the both ends of the bearing fit in respectively Two supporting parts.
  18. 18. head device for shooting according to claim 1, it is characterised in that the locating part and the supporting walls are inclined Set.
  19. 19. head device for shooting according to claim 18, it is characterised in that between the locating part and the supporting walls The scope at inclination angle is 85 ° to 95 °.
  20. 20. head device for shooting according to claim 1, it is characterised in that the head camera includes three axle head supports With the device for shooting for being equipped on the three axles head support.
  21. 21. head device for shooting according to claim 20, it is characterised in that the three axles head support includes and the branch Translation shaft assembly that seat is flexibly connected, with it is described translate the roll shaft assembly that is flexibly connected of shaft assembly and with the roll axle The pitching shaft assembly that component is flexibly connected, the device for shooting are equipped on the pitching shaft assembly.
  22. 22. head device for shooting according to claim 21, it is characterised in that it is described translation shaft assembly rotary shaft with it is described Rotate and be axially vertically arranged.
  23. 23. head device for shooting according to claim 1, it is characterised in that be also installed in including display screen, the display screen The fuselage.
  24. 24. head device for shooting according to claim 1, it is characterised in that also include being used to install external display device Mounting bracket, the mounting bracket are installed in the fuselage.
  25. 25. head device for shooting according to claim 1, it is characterised in that also set including the first button, first button The supporting walls are placed in, are shot for operating the head camera when the head camera is in deployed condition.
  26. 26. head device for shooting according to claim 1, it is characterised in that also set including the second button, second button Side wall adjacent with the supporting walls on the fuselage is placed in, for described in the operation when the head camera is in folded state Head camera is shot.
  27. 27. head device for shooting according to claim 1, it is characterised in that also set including the second button, second button Side wall adjacent with the supporting walls on the fuselage is placed in, for described in the regulation when the head camera is in deployed condition The shooting angle or screening-mode of head camera.
  28. 28. head device for shooting according to claim 1, it is characterised in that also include being used to open and close the head device for shooting Power knob, be arranged at side wall adjacent with the supporting walls on the fuselage.
CN201720946265.XU 2017-07-31 2017-07-31 Head device for shooting Expired - Fee Related CN207112256U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720946265.XU CN207112256U (en) 2017-07-31 2017-07-31 Head device for shooting

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Application Number Priority Date Filing Date Title
CN201720946265.XU CN207112256U (en) 2017-07-31 2017-07-31 Head device for shooting

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109538899A (en) * 2018-08-27 2019-03-29 幻想动力(上海)文化传播有限公司 Supporting mechanism and photographic equipment for photographic equipment
WO2019061774A1 (en) * 2017-09-28 2019-04-04 深圳市大疆创新科技有限公司 Gimbal image capture device
CN110312890A (en) * 2018-06-29 2019-10-08 深圳市大疆创新科技有限公司 Hand-held holder and hand-held cradle head device
CN110494816A (en) * 2018-06-01 2019-11-22 深圳市大疆创新科技有限公司 Rotate angle control method, holder and computer-readable recording medium
WO2020010518A1 (en) * 2018-07-10 2020-01-16 深圳市大疆创新科技有限公司 Pan-tilt
CN110832423A (en) * 2018-11-28 2020-02-21 深圳市大疆创新科技有限公司 Control method of holder, mobile platform and computer readable storage medium
WO2020147124A1 (en) * 2019-01-18 2020-07-23 深圳市大疆创新科技有限公司 Method and device for affixing electronic device and storage medium
CN113739047A (en) * 2018-09-19 2021-12-03 深圳市大疆创新科技有限公司 Hand-held cloud platform

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019061774A1 (en) * 2017-09-28 2019-04-04 深圳市大疆创新科技有限公司 Gimbal image capture device
CN110494816A (en) * 2018-06-01 2019-11-22 深圳市大疆创新科技有限公司 Rotate angle control method, holder and computer-readable recording medium
CN110312890A (en) * 2018-06-29 2019-10-08 深圳市大疆创新科技有限公司 Hand-held holder and hand-held cradle head device
CN113280244A (en) * 2018-06-29 2021-08-20 深圳市大疆创新科技有限公司 Handheld cloud platform and handheld cloud platform device
US11460755B2 (en) 2018-06-29 2022-10-04 SZ DJI Technology Co., Ltd. Hand-held gimbal and hand-held gimbal apparatus
CN113280244B (en) * 2018-06-29 2023-01-24 深圳市大疆创新科技有限公司 Handheld cloud platform and handheld cloud platform device
WO2020010518A1 (en) * 2018-07-10 2020-01-16 深圳市大疆创新科技有限公司 Pan-tilt
CN109538899A (en) * 2018-08-27 2019-03-29 幻想动力(上海)文化传播有限公司 Supporting mechanism and photographic equipment for photographic equipment
CN113739047A (en) * 2018-09-19 2021-12-03 深圳市大疆创新科技有限公司 Hand-held cloud platform
CN110832423A (en) * 2018-11-28 2020-02-21 深圳市大疆创新科技有限公司 Control method of holder, mobile platform and computer readable storage medium
WO2020147124A1 (en) * 2019-01-18 2020-07-23 深圳市大疆创新科技有限公司 Method and device for affixing electronic device and storage medium

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