CN207049552U - Remote control - Google Patents
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- CN207049552U CN207049552U CN201720973502.1U CN201720973502U CN207049552U CN 207049552 U CN207049552 U CN 207049552U CN 201720973502 U CN201720973502 U CN 201720973502U CN 207049552 U CN207049552 U CN 207049552U
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- fuselage
- rolled round
- remote control
- round component
- runner
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Abstract
A kind of remote control, for controlling head (200), including：Fuselage (110) and the first rolled round component (131)；Battery (170) is installed on the fuselage (110)；First rolled round (110) component is rotatablely connected by rotating shaft (162) and fuselage (110)；First rolled round (131) component includes the first runner (1311), and first runner (1311) can be rotated by driving force, to control the motion of the head (200) at least one axle.By installing the first rolled round component on the fuselage of remote control, shooting personnel can control the motion of at least one axle of head by rotating the first runner, improve the precision of cradle head control, and its position and angle between fuselage can be adjusted by rotating the first rolled round component, facilitate the operation of shooting personnel.
Description
Technical field
A kind of remote control is the utility model is related to, belongs to movie and television play capture apparatus technical field.
Background technology
With the development of internet, the movie and television play such as film, TV play and documentary film quantity just increasing year by year.In movie and television play
Shooting process in, due to the needs of shooting or the limitation of scene, it is often necessary to video camera is manipulated at a distance, because
This, will be equipped with the remote control that can manipulate the head for carrying capture apparatus.Existing remote control is all rocker-type remote control,
This rocker-type remote control includes：Fuselage, rotatable two rocking bars and it is arranged on the day of front fuselage on fuselage
Line.Wherein, by left and right or it two rocking bars are rotated upwardly and downwardly can control the yaw angle and the angle of pitch of head.It is but existing
The rocking bar of this rocker-type remote control be club, the club has certain Hui Zhongli, and operating personnel can not be precisely controlled and shake
The stop position of bar, so as to cause the control accuracy of rocking bar insufficient, and existing rocker-type remote control can not meet different bats
Take the photograph personnel or the requirement under different application scene for multiposition manipulation.
Utility model content
In order to solve above-mentioned present in prior art or other potential problems, the utility model embodiment provides a kind of distant
Control device.
According to some embodiments of the utility model, there is provided a kind of remote control, for controlling head, including：Fuselage and
First rolled round component；Battery is installed on the fuselage；The first rolled round component is rotatablely connected by rotating shaft and fuselage；It is described
First rolled round component includes the first runner, handle is provided with first runner, first runner can be in driving force
It is rotated by, to control the motion of at least one axle of the head.
Remote control as described above, wherein, be provided with guiding mechanism between the first rolled round component and fuselage, for
First rolled round is oriented to when being rotated relative to the fuselage.
Remote control as described above, wherein, the guiding mechanism includes：The guiding being arranged on the first rolled round component
Groove, and it is slidably installed in the sliding block being connected in the guide groove and with the fuselage；Or the guiding mechanism includes：It is arranged on
Guide groove on the fuselage, and it is slidably installed in the sliding block being connected in the guide groove and with the first rolled round component.
Remote control as described above, wherein, the guide groove is the deep-slotted chip breaker using the rotating shaft as the center of circle.
Remote control as described above, wherein, the guide groove is dovetail groove, and the sliding block is to coordinate with the dovetail groove
Trapezoidal slide block.
Remote control as described above, wherein, in addition to screw rod, screw thread is provided with the screw rod；The connection of the screw rod
End is fixed with the trapezoidal slide block, and the screw rod passes through the fuselage or the first rolled round group away from the free end of the connection end
The screwed hole opened up on part.
Remote control as described above, wherein, in addition to locking knob, the locking knob be installed on the freedom of the screw rod
End.
Remote control as described above, wherein, the fuselage or the first rolled round component include fixture, the screw rod from
Extended to by holding through the through hole opened up on the fixture outside the fuselage or the first rolled round component.
Remote control as described above, wherein, in addition to retaining mechanism, the retaining mechanism includes locking piece, in institute
The first rolled round component is stated to lock the first rolled round component and fuselage relative to after fuselage rotation predetermined angle.
Remote control as described above, wherein, position-limit mechanism is additionally provided between the first rolled round component and the fuselage,
The angular range rotated for limiting the first rolled round component relative to the fuselage.
Remote control as described above, wherein, the position-limit mechanism includes：Locating slot and being plugged in the locating slot is determined
Position post.
Remote control as described above, wherein, the locating slot is arranged on the location-plate of the fuselage installation, the positioning
Post is arranged on the first rolled round component.
Remote control as described above, wherein, the locating slot is the deep-slotted chip breaker centered on the rotating shaft.
Remote control as described above, wherein, the remote control also includes the second rolled round component, the second rolled round component bag
The second runner is included, first runner and the second runner are used for the motion for controlling the axle of head at least two.
Remote control as described above, wherein, first runner is used for the motion for controlling the yaw axis of the head, described
Second runner is used for the motion for controlling the pitch axis of the head.
According to the technical scheme of the utility model embodiment, by installing the first rolled round component on the fuselage of remote control,
So as to which in shooting process, shooting personnel can control the motion of at least one axle of head by rotating the first runner, so as to
The posture of head is controlled, realizes the control to video camera shooting angle.Because the first runner can be rotated by appointing in external force
Meaning angle, thus, it is possible to obtain the controlling curve of approximately linear, so as to improve the precision of cradle head control, and by relative
In fuselage rotate the first rolled round component can obtain multiple manipulation positions, so as to meet different shooting personnel, different application environment,
Or the demand of multi-angled shooting, facilitate the operation of shooting personnel.
Brief description of the drawings
By referring to the described in detail below of accompanying drawing, the above and other purpose of the utility model embodiment, feature and excellent
Point will become more clearly understood from.In the accompanying drawings, will by example and it is nonrestrictive in a manner of to multiple implementations of the present utility model
Example illustrates, wherein：
Fig. 1 is the structural representation for the capture apparatus that the embodiment of the utility model one provides；
Fig. 2 is the structural representation for the remote control that the utility model embodiment provides；
Fig. 3 is Fig. 2 front view；
Fig. 4 is Fig. 2 rearview；
Fig. 5 is Fig. 2 right view；
Fig. 6 is Fig. 2 top view；
Fig. 7 is the top view after the rotation of the first rolled round component in Fig. 2；
Fig. 8 is that the first rolled round component is in the partial sectional view overlooked under visual angle in Fig. 7；
Fig. 9 be in Fig. 8 A-A to sectional view；
Figure 10 is that the first rolled round component is in the partial sectional view looked up under visual angle in Fig. 7；
Figure 11 is B-B direction sectional view in Figure 10；
Figure 12 is the structural representation for the remote control that another embodiment of the utility model provides；
Figure 13 is Figure 12 front view；
Figure 14 is Figure 12 left view；
Figure 15 is Figure 12 right view；
Figure 16 is Figure 12 top view；
Figure 17 is the explosive view of the 3rd rolled round component in Figure 12；
Figure 18 is the structural representation for the radio communication device that the embodiment of the utility model one provides；
Figure 19 is Figure 18 front view；
Figure 20 is Figure 18 right view；
Figure 21 is Figure 18 left view；
Figure 22 is Figure 18 top view.
In figure：
100th, remote control；110th, fuselage；120th, radio communication device；121st, antenna；123rd, main body；125th, interface；127、
Knob；129th, Pin contact；131st, the first rolled round component；1311st, the first runner；1312nd, handle；1313rd, connecting portion；1314、
Speed control knob；1315th, adjusting knob；1316th, switching switch；133rd, the second rolled round component；1331st, the second runner；1332、
Handle；1333rd, connecting portion；1334th, speed control knob；1335th, adjusting knob；1336th, switching switch；135th, the 3rd rolled round group
Part；1351st, the 3rd runner；1352nd, handle；1353rd, connecting portion；1354th, speed control knob；1355th, adjusting knob；1356、
Switching switch；141st, power switch；142nd, shooting switch；143rd, home keys；144th, focusing button；145th, focusing knob；146、
Aperture adjusting knob；147th, output interface；148th, expansion interface；150th, controller；161st, guide；1611st, locating dowel；162、
Rotating shaft；163rd, guide groove；164th, fixture；165th, trapezoidal slide block；166th, location-plate；167th, screw rod；168th, locating slot；169th, lock
Tight knob；170th, battery；181st, card article；1811st, flange；183rd, contiguous block；1831st, neck；1833rd, stopper slot；185th, lock
Knob；190th, display；191st, display battery；200th, head；300th, video camera.
Embodiment
Below in conjunction with the accompanying drawings, some embodiments of the present utility model are elaborated.In the case where not conflicting, under
Feature in the embodiment and embodiment stated can be mutually combined.
Fig. 1 is the structural representation for the capture apparatus that the present embodiment provides.As shown in figure 1, the capture apparatus of the present embodiment
Including：Remote control 100, head 200 and video camera 300.Wherein, head 200 can be fixed on ground or other determine thing
Upper (such as house, trees, rock etc.), can also be arranged in mobile article (such as automobile, rail vehicle or unmanned plane
Deng), in the present embodiment, head 200 can be the head of arbitrary structures in the prior art, such as two axle The Cloud Terraces or three axles
Increase steady head.Video camera 300 is carried by head 200, and can adjust video camera by the adjustment of the posture of head 200
300 shooting direction and angle, multi-angle, multidirectional shooting are realized, to obtain the image or image element needed for photographer
Material, so as to facilitate the later stage to carry out editing editor to it to make movie and television play or from media video etc..In the present embodiment, head
The adjustment of 200 postures is realized by the remote control 100 with the wireless connection of head 200, and the concrete structure of remote control 100 will
It is described in detail later.By remote control 100, shooting personnel can the shooting direction to video camera 300 and bat at a distance
Take the photograph angle to be controlled, so as to obtain preferably shooting material so that the movie material of post-production has more real
Scene Representation ability.For example, by remote control 100 video camera 300 carried on unmanned plane can be controlled to shoot in steep cliff
The real-time performance of the sportsman of free climbing on cliff, either the predation picture of lion or from sky on wide-long shot grassland
In take a crane shot grand the fight scene of historical subject matter movie and television play etc..
Fig. 2 is the structural representation for the remote control that the present embodiment provides；Fig. 3 is Fig. 2 front view；Fig. 4 is Fig. 2 backsight
Figure；Fig. 5 is Fig. 2 right view；Fig. 6 is Fig. 2 top view.
As shown in Figures 2 to 6, remote control 100 includes：The rolled round component 131 of fuselage 110 and first.Wherein, the first rolled round group
Part 131 includes the first runner 1311, and first runner 1311 can be rotated by driving force, with control head 200 to
The motion of a few axle, so as to adjust the posture of head 200 so that the video camera 300 carried on the head 200 obtains suitably
Shooting angle and shooting direction.
Specifically, the first runner 1311 can be controlled in the yaw axis, pitch axis and wobble shaft of head 200 at least
One, with corresponding yaw angle, the angle of pitch and the roll angle for adjusting head 200.In operation, by controlling the first runner
1311 are rotated around its rotation axis, and fuselage 110 is sensed or received after direction and the angle of the rotation of the first runner 1311
The control information that 200 at least one axle of head moves is controlled with regard to generation to change the posture of head 200.When head 200 receives
At least one of the yaw motor on head 200, pitching motor, rolling motor will be controlled to rotate after the control information,
So that at least one axle motion of head 200, and then at least one in the yaw angle of adjustment head 200, the angle of pitch, roll angle
Person.For example, when the first runner 1311 is used to control the yaw axis of head 200, if the first runner 1311 turns clockwise 5
Degree, then the yaw motor of head 200 can be controlled to rotate to drive yaw axis to move, so that the yaw angle of head 200 is also corresponding
5 degree of rotation.In another example when the yaw axis and pitch axis that the first runner 1311 is used to controlling head 200 move, can be the
The pitching motor of head 200 is controlled to rotate to drive pitch axis to move, in the first runner when one runner 1311 turns clockwise
The yaw motor of head 200 is controlled to rotate to drive yaw axis to move during 1311 rotate counterclockwise.It is of course also possible to pass through setting
Switching is switched to realize control of first runner 1311 to yaw axis and pitch axis.For another example when the first runner 1311 is used to control
When yaw axis, pitch axis or the wobble shaft of head 200 processed move, the first runner 1311 can be switched by setting switching push button
The axle of the head 200 controlled.
It should be noted that the first runner that the fuselage 110 of remote control 100 directly can also will be received or sensed
1311 rotation direction and angle and the controller 150 for being sent to head 200, control is generated by the controller 150 of head 200
The control information that yaw motor, pitching motor or the rolling motor of head 200 rotate.Certainly, in reality to remote control 100
In setting up procedure, the rotational angle of the first runner 1311 or rotation direction can also be used as the control running parameter of head 200
Condition.
In the present embodiment, due to control head 200 axial-movement be by way of rotating the first runner 1311 come
Realize, its rocking bar that existing rocker-type remote control is not present has Hui Zhongli, can not accurately control lacking for rocking bar stop position
Fall into, the control to the approximately linear of head 200 can be obtained, so as to improve the control accuracy of remote control 100, stablized and high
The shooting material of quality.Also, the posture of head 200 is adjusted using the first runner 1311, so as to control the bat of video camera 300
Taking the photograph the mode of operation of angle and shooting direction, also shooting custom long-term with shooting personnel is close, so as to cause shooting personnel
For the discomfort of mode of operation, the time that shooting personnel adapt to remote control 100 is reduced, improves the efficiency of shooting.
In order to describe simplicity, exemplified by controlling the yaw angle of head 200 by the first rolled round component 131 below, shaken to first
The structure of wheel assembly 131 is described in detail, it is understood that, description below is equally applicable to the pitch axis of head 200
With the control of wobble shaft.
As shown in Figures 2 to 6, the first rolled round component 131 is arranged on the left side of fuselage 110, to facilitate shooting librarian use
Left hand rotates the first runner 1311 to control the yaw angle of head 200.It is apparent that the first rolled round component 131 can also basis
Need other correct positions installed in fuselage 110.Further, can be more when rotating the first runner 1311 in order to shoot personnel
Good grasping, is alternatively provided with handle 1312 in the outside of the first runner 1311 (left side in Fig. 2).So, personnel are shot
Can rotates the first runner 1311 by grasping member 1312, convenient and labor-saving.It is appreciated that the handle 1312 can
Omit, and first runner 1311. is rotated by gripping the outline of the first runner 1311
With continued reference to Fig. 2 to Fig. 6, the first runner 1311 is connected to the left surface of fuselage 110 by connecting portion 1313.It is optional
Ground, connecting portion 1313 is the structure with the one of the first runner 1311, such as connecting portion 1313 is the medial surface of the first runner 1311
The projection formed.Rotating shaft passes through the through hole opened up on the axis hole and projection at the center of the first runner 1311 to be fixed on fuselage 110
Left side wall on.The gland for being screwed in roller end is provided with the outside of the first runner 1311, can be with by the limitation of gland
The first runner 1311 is avoided to be dropped from rotating shaft.Again alternatively, the runner 1311 of connecting portion 1313 and first is Split type structure, such as
Connecting portion 1313 is a rectangular block.Rotating shaft is fixed in the side wall of contiguous block after passing through the axis hole at the center of the first runner 1311,
So as to which the first runner 1311 can be rotated to control the yaw angle of head 200 around rotating shaft.
In embodiment of the present utility model, connecting portion 1313 and fuselage 110 with the split settings of the first runner 1311
It is rotatablely connected by rotating shaft 162, as shown in fig. 7, wherein, Fig. 7 is the top view after the rotation of the first rolled round component in Fig. 2.Rotating shaft
162 can be fixed on fuselage 110 either on connecting portion 1313 or, rotating shaft 162 be located at hinge center, hinge both ends difference
Fixed with the first rolled round component 131 and connecting portion 1313.
The remote control 100 of the present embodiment, the first rolled round component 131 and fuselage 110 are connected by rotating shaft 162, so as to
To adjust its relative position or relative angle with fuselage 110 by rotating the first rolled round component 131, to obtain suitably
Operating clearance and work angle, the first runner of convenient shooting personnel control 1311 rotate or operated selectivity and shaken installed in first
Wheel assembly 131, fuselage 110 or the function button on both.Understood based on foregoing, the remote control 100 that the present embodiment provides,
Its position and angle between fuselage 110 can be adjusted by rotating the first rolled round component 131, facilitate shooting personnel's
Operation, different operating positions and angle requirement, the operating habit of different personnel are including but not limited to adapted to, and adapted to some
Application environment of special screne (such as narrow space) etc..
It should be noted that in order to which the first rolled round component 131 and fuselage 110 are locked, to avoid the two from turning
It is subjected to displacement when dynamic, any locking mode can be taken to lock the two.For example, when rotating shaft 162 is arranged on fuselage 110
When, the first rolled round component can be realized by rationally setting the stiction between the first rolled round component 131 and rotating shaft 162
Locking between 131 and rotating shaft 162；Similarly, can be by reasonable when rotating shaft 162 is arranged on the first rolled round component 131
Stiction between fuselage 110 and rotating shaft 162 is set to realize locking.
Alternatively, remote control 100 is provided with the locking machine for locking or loosening the rolled round component 131 of fuselage 110 and first
Structure, the retaining mechanism include locking piece.Locking piece can use various structures.In the present embodiment, the locking piece is screw rod
167, screw rod 167 passes through the screwed hole opened up on the rolled round component 131 of fuselage 110 or first, supports in the first rolled round component 131
Or on fuselage.So, can locks the rolled round component 131 of fuselage 110 and first by way of tightening screw rod 167.This
Outside, locking piece can also be lock, and the movable part and fixed part of the lock are separately mounted to the first rolled round component 131 and machine
On body 110, vice versa, to realize the locking to the first rolled round component 131 and fuselage 110.And for example, locking piece is chock, when
After first rolled round component 131 turns to required angle, the chock is inserted into the first rolled round component 131 and fuselage 110
Between, to realize the locking of the rolled round component 131 of fuselage 110 and first.For another example, locking piece is pin, in fuselage 110 or first
Multiple pin-and-holes are provided with rolled round component 131, so as to pin be inserted after the first rolled round component 131 turns to proper angle
Enter the locking that the first rolled round component 131 and fuselage 110 are realized in pin-and-hole.
Fig. 8 is that the first rolled round component is in the partial sectional view overlooked under visual angle in Fig. 7；Fig. 9 be in Fig. 8 A-A to section view
Figure；Figure 10 is that the first rolled round component is in the partial sectional view looked up under visual angle in Fig. 7；Figure 11 is B-B direction sectional view in Figure 10.
As shown in Figure 7 to 10, alternatively, the relative rotation for convenience to the first rolled round component 131 and fuselage 110 is entered
Row is oriented to, and guiding mechanism is additionally provided between fuselage 110 and connecting portion 1313.The guiding mechanism includes being arranged on the first rolled round
Guide groove 163 on component 131, and it is slidably installed in the sliding block being connected in the guide groove 163 and with fuselage.For example, in connecting portion
1313 inner side sets guide 161, and guide groove 163 is opened up on guide 161；Accordingly, set in guide groove 163
The sliding block that can be slided in guide groove 163, the sliding block can be connected to fuselage by connecting rod or other structures form
110.So, when driving 162 rotation around the shaft of the first rolled round component 131, sliding block can is slided in guide groove 163, from
And realize guide effect.In the present embodiment, the sliding block is connected to fuselage 110 by locking piece 167.In another example in fuselage 110
Left side wall on above-mentioned guide 161 is installed, and the sliding block being slidably installed in guide groove 163 is fixed on the suitable of connecting portion 1313
Position.In addition it is also possible to the slide bar being connected with the first rolled round component 131 is directly set to substitute above-mentioned cunning in guide groove 163
Block.In the present embodiment, above-mentioned guide 161 includes but is not limited to platy structure, block structure and frame structure.
The shape of guide groove 163 is not specifically limited, and those skilled in the art can be designed according to being actually needed.Example
Such as, guide groove 163 is the deep-slotted chip breaker using rotating shaft as the center of circle, so as to what is moved with the relatively described fuselage 110 of the first rolled round component 131
Movement locus matches.Dovetail groove as shown in Figure 9 can be designed to along the depth direction of guide groove 163.When guide groove 163
, can be accordingly by slider designs into the trapezoidal slide block 165 coordinated with the dovetail groove when cross section is designed to dovetail groove, this
Sample, it is possible to realize that locking or release first are shaken by changing the size in the gap between trapezoidal slide block 165 and dovetail groove
The effect of wheel assembly 131.
Further, in order to realize the adjustment to trapezoidal slide block 165 and dovetail groove gap to lock the rolled round of fuselage 110 and first
Component 131, locking piece can be arranged to screw rod 167, and trapezoidal slide block 165 and the connection end of screw rod 167 are fixed.Below will
So that guide groove 163 is arranged on the first rolled round component as an example, to screw rod 167 and fuselage 110 and the matching relationship of trapezoidal slide block 165
It is introduced, certainly, following matching relationships can also be arranged on machine directly or through being applied after simple replace in guide groove 163
In remote control on body 110.
Be provided with external screw thread on screw rod 167, for screw rod 167 free end through fuselage 110 through hole in be provided with phase
The internal thread of cooperation.So trapezoidal slide block 165 is promoted to be moved in the axial direction of screw rod 167 by the can of rotary screw 167,
So as to realize the effect of the fit clearance between adjustment trapezoidal slide block 165 and dovetail groove, and then the first rolled round component 131 is locked
On fuselage 110.Alternatively, in order to facilitate rotary screw 167, locking piece also includes installing installed in the free end of screw rod 167
Locking knob 169.In assembling, the locking knob 169 can be fixed on to the free end of screw rod 167 by screw.When need
When locking or discharging the first rolled round component 131, it is only necessary to the locking knob 169 that the free end of rotary screw 167 is installed
Can drives screw rod 167 to move axially, and so as to drive trapezoidal slide block 165 also to be moved axially along screw rod 167, and then adjusts trapezoidal
Fit clearance between sliding block 165 and dovetail groove, realize the purpose of locking or the first rolled round component of release 131 and fuselage 110.
Alternatively, boss can be formed in lead to the hole site, to facilitate the movement of locking knob 169.
Alternatively, fuselage 110 also includes fixture 164, and the free end of screw rod 167 passes through what is opened up on fixture 164 to lead to
Hole.For example, fuselage 110 includes the fixture 164 for being arranged at left side, at this point it is possible to which rotating shaft 162 is arranged on fixture 164.
(such as upper right corner) vertically offers axis hole on connecting portion 1313, and rotating shaft 162 is located in the axis hole, so as to realize the first rolled round
The rotation connection of component 131 and fuselage 110.As a kind of interchangeable mode, rotating shaft 162 can also be arranged on connecting portion
On 1313, while the mounting sleeve on fixture 164, and axle sleeve is set in rotating shaft 162 to realize the first rolled round component 131
With the rotation connection of fuselage 110.Similarly, fixture 164 can also be arranged on the first rolled round component 131, screw rod 167
Free end passes through the through hole opened up on fixture to extend to outside the first rolled round component 131.
The specific constructive form of fixture 164 is not especially limited in the present embodiment, and those skilled in the art can select
Any appropriate structure is selected as fixture.For example, fixture 164 can be two intervals set on fuselage 110
The fixed plate of certain distance, the guide 161 of the first rolled round component 131 are housed between the two fixed plates, or first shakes
When being rotated relative to fuselage 110, its guide 161 at least part can expose wheel assembly 131 between two fixed plates.
Obvious, the first rolled round component 131 may also comprise two spaced guide plates, and correspondingly, fuselage 110 includes fixture,
And it can award between two guide plates of the first rolled round of honor component 131.
Alternatively, as shown in Figure 10 and Figure 11, other position restrainers are additionally provided between fuselage 110 and connecting portion 1313
Structure, the angular range rotated for limiting the first rolled round component 131 relative to fuselage 110.In some alternatively embodiment,
The flexible piece that position-limit mechanism is connected with fuselage and the first rolled round component respectively for both ends, such as rope or chain.Can at other
In selection of land embodiment, position-limit mechanism includes：Locating slot and the locating dowel being plugged in locating slot.For example, locating slot is set
On fuselage 110, locating dowel is arranged on the first rolled round component 131, and vice versa.Specifically, can be set on fuselage 110
Location-plate 166 is put, such as the location-plate 166 is set on the left side wall of fuselage.Further, can also be by location-plate 166 and upper
State two fixed plates to be arranged in parallel, or one of fixed plate is used directly as location-plate.Further, in order to operate
It is convenient, location-plate 166 can be arranged on to the lower section of fixed plate, or using underlying fixed plate as location-plate.Positioning
The locating slot 168 for limiting the maximum rotation angle of the first rolled round component 131 and minimum rotation angle is offered on plate 166.Lead
The surface of part 161 towards location-plate 166 is provided with locating dowel 1611, the locating dowel 1611 is inserted into locating slot 168.In reality
In the design process of border, shape, position or the length of locating slot 168 can be arranged as required to obtain the first rolled round component
131 different size of rotatable angle ranges.By setting position-limit mechanism, the first rolled round component 131 can be caused to turn in maximum
It is dynamic to be moved between angle and minimum rotation angle, so as to facilitate different shooting librarian use remote controls 100.
Further, as shown in Fig. 2 to Fig. 6, following one or more are optionally provided with connecting portion 1313：
For controlling the speed control knob 1314 of the yaw axis of head 200, for controlling the regulation of the yaw axis response speed of head 200 to revolve
Button 1315, the open-close on-off for enabling or closing the first rolled round component 131 or the first runner 1311 and for switching
The switching switch 1316 of left/right hand operation.In the present embodiment, speed control knob 1314, adjusting knob 1315, open-close on-off
It is not construed as limiting with the specific set location of switching switch 1316, those skilled in the art can select suitably according to the actual requirements
Position is designed.For example, above-mentioned speed control knob 1314, adjusting knob 1315, open-close on-off and switching can be switched
1316 are arranged on the top surface of connecting portion 1313 to facilitate shooting librarian use.In addition, in specific set, can be by open-close on-off
And switching switch 1316 is arranged between speed control knob 1314 and adjusting knob 1315.Alternatively, in specific design process
In, open-close on-off and switching switch 1316 can be integrated, to reduce the quantity of switch.For example, as shown in Fig. 2 can
So that open-close on-off and switching switch 1316 are integrated into a deflector rod switch.In operation, driving lever is pushed and middle then disables the
One rolled round component 131 or the first runner 1311；Driving lever is pushed into left side, then enables the first rolled round component 131 or first turn
Wheel 1311, and shoot librarian use left hand and manipulate the first runner 1311；Driving lever is pushed into right side, then enables the first rolled round component
131 or first runner 1311, and shoot the librarian use right hand and manipulate the first runner 1311.It is of course also possible to select other
Suitable integrated switch switchs 1316 function to realize open-close on-off with switching.
In present embodiment, the adjusting knob 1315 is specifically used for response speed when regulation head starts；Switching is opened
The 1316 left/right hand operation corresponding relations for being specifically used for switching remote control 100 and head are closed, facilitate the user of different use habits
Switching uses；Speed control knob 1314 is specifically used for the controlled quentity controlled variable for controlling the controller 100 and the cloud platform rotation amount
Corresponding relation.
In addition, in order to intuitively show the anglec of rotation of the first runner 1311, can in rotating shaft or connecting portion 1313
Selection of land fixes angled marker disc, and pointer is fixed with the first runner 1311.So, when the first runner 1311 turns around rotating shaft
When dynamic, the pointer being fixed on the first runner 1311 also just follows the first runner 1311 to rotate, so that by angle marker disc just
The rotational angle of the first runner 1311 can intuitively be read.It is of course also possible to correspondingly identified when the in angle marker disc
When one runner 1311 turns to certain angle, the yaw angle of head 200, for example, when the first runner 1311 rotates 30 degree, head
200 yaw angle rotates 1 degree.
With continued reference to Fig. 2 to Fig. 7, remote control 100 also alternatively includes the second rolled round component 133.Second rolled round component 133
Including the second runner 1331 that 200 at least one axle of head can be controlled to move.First rolled round component 131 and the second rolled round component
133 can be integrated, or the two can also be disposed on to the outer edge of fuselage 110, for example, the first rolled round component
131 are arranged on the left side of fuselage 110, and the second rolled round component 133 is then arranged on the fuselage 110 relative with the first rolled round component 131
Right side.By setting the second rolled round component 133, realize and head is controlled by the first runner 1311 and the second runner 1331
The motion of 200 at least two axis, it is possible to achieve the control to more than 200 individual axle of head, improve the adjustment effect of the posture of head 200
Rate.
In general, the second runner 1331 and the first runner 1311 are arranged to for controlling the different axle of head 200, but this
Embodiment is not excluded for the scheme of the second runner 1331 and the first runner 1311 control 200 same axle of head.For example, when first turn
When wheel 1311 is used for controlling the motion of the yaw axis of head 200 to adjust the yaw angle of head 200, the second rolled round component 133 is used
To control the motion of the pitch axis of head 200, to adjust the angle of pitch of head 200 or roll angle, vice versa.Below with
One rolled round component 131 controls the motion of yaw axis, to the second rolled round group exemplified by the motion of the second rolled round component 133 control pitch axis
Part 133 is introduced.
Handle 1332 can also be set on second runner 1331 of the second rolled round component 133.Similarly, the second rolled round component
133 can also set connecting portion 1333, also, optionally can also be set on connecting portion 1333 following a kind of or more
Kind：For controlling the speed control knob 1334 of the pitch axis of head 200, the tune for controlling the pitch axis response speed of head 200
Save knob 1335, the open-close on-off for enabling or closing the second rolled round component 133 or the second runner 1331 and for cutting
Change the switching switch 1336 of left/right hand operation.
Further, can be fixedly connected or be rotatablely connected between the second rolled round component 133 and fuselage 110.For example, the
One rolled round component 131 and the second rolled round component 133 are fixedly connected with fuselage 110, and certain this mode that is fixedly connected can be
It is dismountable or non-removable.In another example the first rolled round component 131 is rotatablely connected with fuselage 110 by rotating shaft 162, the
Two rolled round components 133 are fixedly connected with fuselage 110, and vice versa.So, by rotating the first rolled round rotated with fuselage 110
Between the can of 131 or second rolled round component of component 133 is adjusted between the first rolled round component 131 and the second rolled round component 133
Away from so as to facilitate different shooting personnel to manipulate remote control 100.
Figure 12 is the structural representation for another remote control that the present embodiment provides；Figure 13 is Figure 12 front view；Figure 14
For Figure 12 left view；Figure 15 is Figure 12 right view；Figure 16 is Figure 12 top view；Figure 17 is the 3rd rolled round component in Figure 12
Explosive view.
As shown in Figure 12 to Figure 17, the remote control 100 of the present embodiment also includes the 3rd rolled round group being arranged on fuselage 110
Part 135, the 3rd rolled round component 135 include rotatable 3rd runner 1351, by driving the 3rd runner 1351 to rotate, together
Sample can control the motion of 200 at least one axle of head., can be 1311, second turns by the first runner when actual disposition
The runner 1351 of wheel 1331 and the 3rd is arranged respectively to for controlling an axle of head 200 to move, such as the first runner 1311 is used
To control the motion of the yaw axis of head 200 to adjust the yaw angle of head 200, the second runner 1331 is used for controlling head 200
Pitch axis motion to adjust the angle of pitch, the 3rd runner 1351 is used for controlling the motion of the wobble shaft of head 200 to adjust cloud
The roll angle of platform 200, the other structures of the 3rd rolled round component 135 will be introduced with the above-mentioned example that is arranged to below.
Handle 1352 can also be set on 3rd runner 1351 of the 3rd rolled round component 135.Similarly, the 3rd rolled round component
135 can also set connecting portion 1353, also, optionally can also be set on connecting portion 1353 following a kind of or more
Kind：For controlling the speed control knob 1354 of the wobble shaft of head 200, the tune for controlling the wobble shaft response speed of head 200
Save knob 1355, the open-close on-off for enabling or closing the 3rd rolled round component 135 or the 3rd runner 1351 and for cutting
Change the switching switch 1356 of left/right hand operation.
Further, can also be fixedly connected or be rotatablely connected between the 3rd rolled round component 135 and fuselage 110.For example,
First rolled round component 131, the second rolled round component 133 and the 3rd rolled round component 135 are fixedly connected with fuselage 110, certainly this
It can be dismountable or non-removable that kind, which is fixedly connected with mode,.In another example the first rolled round component 131 and fuselage 110 are logical
Cross rotating shaft 162 to be rotatablely connected, the second rolled round component 133 is fixedly connected with fuselage 110, and the 3rd rolled round component 135 can with fuselage 110
Dismantling connection.Alternatively, the 3rd rolled round component 135 is detachably connected by quick-disassembly structure and fuselage 110, so as to
3rd rolled round component 135 is quickly installed as needed or disassembles the 3rd rolled round component 135 from fuselage 110, is reached
To the purpose of the function of Quick Extended remote control 100.
Refering to Figure 12 to Figure 17, in some alternatively embodiment, quick-disassembly structure includes：The card article formed on connecting portion
181 and fuselage 110 on the neck 1831 for being used for the clamping card article 181 that is formed, can in some alternatively embodiment
So that neck 1831 is designed into dovetail groove.Neck 1831 can be directly opened in the side wall of fuselage 110, or can also be as
A contiguous block 183 being fixed in the side wall of fuselage 110 is separately provided shown in Figure 17, neck 1831 is then opened in the company
Connect on block 183.Alternatively, stopper slot 1833 is further opened with the inwall of neck 1831, an end of the stopper slot 1833
Closing, formed with the flange 1811 being connected in stopper slot 1833 on card article 181.For example, in fig. 17, at the bottom of neck 1831
The stopper slot 1833 of upper end open, lower end closed is offered on wall.Pass through the restriction of flange 1811 and stopper slot 1833, Ke Yiwei
Quick-disassembly structure provides additional clamping force, avoids card article 181 and the clamping force of neck 1831 deficiency and departs from.Again alternatively, it is corresponding
The end set of the flange 1811 of the opening end position of stopper slot 1833 has locking knob 185.For example, in fig. 17, in flange
1811 upper end sets locking knob 185, and in assembling, the bottom of card article 181 is inserted from the upper end of neck 1831, and makes flange
The opening of 1811 bottom alignment stopper slot 1833, from top to bottom inserts card article 181 in neck 1831, then rotational lock revolves
Button 185 reduces the gap of knob bottom and the top of contiguous block 183, because the side wall of locking knob 185 has exceeded stopper slot 1833,
Therefore, can locks the rolled round component 135 of contiguous block 183 and the 3rd after locking knob 185 are screwed.
In other alternatively embodiment, quick-disassembly structure includes the card article 181, Yi Ji being arranged on fuselage 110
The neck 1831 for clamping card article 181 opened up on the connecting portion of three rolled round components 135.In addition, card article 181 and neck 1831
Partial structurtes can be identical with the partial structurtes described by the preceding paragraph, will not be repeated here.
It is appreciated that the first rolled round component 131, the second rolled round component 133 can also use above-mentioned quick-disassembly structure and fuselage
110 connections.
Further, remote control 100 also alternatively also includes focusing rolled round, and the focusing rolled round includes being used for controlling head 200
On focus tracking adjustment video camera 300 on physical lens stop focusing runner.Certainly, remote control 100 can also include more shaking
Wheel, the function that those skilled in the art can set suitable rolled round number and each rolled round according to being actually needed.
It is appreciated that the first rolled round component 131, the second rolled round component 133, the 3rd rolled round component 135 and described
Focusing rolled round is not limited to address the mode presented in figure with the position relationship of the fuselage 110.
As shown in Fig. 2-16, radio communication device 120 is arranged on fuselage 110, and such can of head 200 passes through the nothing
Line communicator 120 is established with fuselage 110 and communicated to connect, and the control information of coming is transmitted so as to receive fuselage 110.Radio communication fills
Any appropriate radio communication device 120, such as WiFi module, bluetooth module etc. can be used by putting 120.It is wireless in specific assembling
During communicator 120, radio communication device 120 can be directly assembled in fuselage 110, so as to form one with fuselage 110
Structure, naturally it is also possible to by radio communication device 120 by way of interface or connecting line with fuselage 110 be connected to one
Rise, to facilitate the wireless receiving ability for improving remote control 100 in some scenarios.For example, in some alternatively embodiment,
Radio communication device 120 is detachably connected to the trailing flank of fuselage 110, so, would not when the personnel of shooting manipulate runner
Influenceed by radio communication device 120., can be by radio communication device when needing in the car to be remotely controlled head 200
120 pull down from fuselage 110 and are then placed within roof, to improve the ability of the reception signal of remote control 100.
Figure 18 to Figure 22 gives a kind of quick disassembled radio communication device 120, wherein, Figure 18 is the component of antenna 121
Structural representation；Figure 19 is Figure 18 front view；Figure 20 is Figure 18 right view；Figure 21 is Figure 18 left view；Figure 22 is figure
18 top view.
Refering to Figure 18 to Figure 22, the radio communication device 120 includes：Main body 123 and the day in main body 123
Line 121.Plug or socket are provided with main body 123, the socket or plug being engaged are provided with fuselage 110, this
Radio communication device 120 is quickly installed on fuselage 110 by sample can, or is quickly pulled down from fuselage 110.Alternatively,
As shown in figure 20, Pin contact 129 is set in main body 123.Further, the outer peripheral edge of Pin contact 129 is designed with projection, in machine
Guide groove is designed with the socket inner walls of body 110, with the correct installation of convenient plug and socket.Further, in plug and socket
Sealing structure is inside provided with, for example, being designed with the end of plug formed with seal groove in the bottom of socket and being contained in the sealing
Sealing strip in groove；In another example it is arranged with sealing ring in plug or socket.In addition, also it is optionally provided with main body 123
Interface 125, so as to when radio communication device 120 is disassembled from fuselage 110, be connected by being inserted in interface 125
The mode of wiring links together itself and fuselage 110.Again alternatively, some control radio communications also can be set in main body 123
The function knob 127 of function.
With continued reference to Fig. 2, Fig. 7 and Figure 12, the shape of fuselage 110 can select suitable shape, example according to specific needs
Such as, rectangle box body or cube box body can be selected as fuselage 110, in another example, fuselage 110 is it is also an option that such as Figure 12
Shown irregular shape box body structure, to install three or more than three rolled rounds.It is appreciated that it is provided with fuselage 110
The electronic devices such as circuit board, sensor, are no longer described in detail herein, and those skilled in the art can be according to being actually needed to fuselage
The species of electronic device and connected mode are configured in 110.
Alternatively, battery 170 is installed on fuselage 110.For example, when the first rolled round component 131 and the second rolled round component
133 set up separately in the left surface and right flank of fuselage 110, and battery 170 may be mounted at the leading flank of fuselage 110.Can at some
In selection of land embodiment, accommodating case can be set on fuselage 110, then battery 170 is arranged in the accommodating case.Accommodating case
Concrete structure and set-up mode can according to be actually needed design, be not especially limited herein.For example, accommodating case can be by
The front side wall of fuselage 110 is recessed；In another example accommodating case is the part with the split of fuselage 110, it is fixed on fuselage 110.
Further, battery 170 is contained in accommodating case by elastic mechanism, by the elastic reaction of elastic mechanism, is applied when to battery 170
Battery 170 is ejected accommodating case or is locked in accommodating case by can when adding thrust.For example, elastic mechanism is installed in battery
The spring of 170 directions of motion.When needing to install battery 170, the compression spring of battery 170 is promoted to be fully advanced battery 170
In accommodating case, and the limited wall for being received the setting of box opening blocks, and prevents battery 170 from dropping out；When needing to take out battery 170,
The compression spring of battery 170 is promoted again, battery 170 is departed from conflict state with limited wall, then makes battery 170 toward perpendicular to spring
Direction displacement, so that it may so that battery 170 is ejected by the elastic force of spring from accommodating chamber.
As shown in Fig. 2 to 12, controller 150, such as GCU controllers are also alternatively installed on fuselage 110, so as to side
Just shooting personnel are set or changed to the parameter of head 200.For example, shooting personnel can input in controller 150
Corresponding relation between the yaw axis of each rolled round and head 200, pitch axis and wobble shaft, that is to say, in controller
The corresponding control of the first rolled round component 131 is inputted in 150 is which of yaw axis, pitch axis and wobble shaft of head 200
Or which.Certainly, this corresponding relation can also be preset by manufacturer or retailer.In another example shooting personnel can
Specifically rotation is more for some axle of the head 200 of corresponding control during inputting the first runner 1,311 one circle of rotation by controller 150
Few degree.When being designed, controller 150 can be arranged on any correct position of fuselage 110, for example, controller 150 can be with
It is arranged between the first rolled round component 131 and the second rolled round component 133, in another example, show that controller 150 can be set in Fig. 2
The top surface in fuselage 110 is put, to facilitate shooting personnel to input corresponding control parameter.In some alternatively embodiment, control
Device 150 processed is removably mounted on fuselage 110, can so facilitate the replacing to controller 150.In addition, controller 150 can
With including display screen.
Also be optionally provided with fuselage 110 power switch 141, shooting switch 142, photographing switch, focusing button 144,
It is a kind of or more in focusing knob 145, aperture adjusting knob 146, home keys 143, output interface 147, expansion interface 148
Kind.In general, said structure can be arranged on any suitable location of fuselage 110, can be with for example, as shown in Fig. 6 to Figure 16
The trailing flank that output interface 147 and expansion interface 147 are arranged on to fuselage 110 connects other external equipments, other portions to facilitate
The top surface that part can then be arranged on fuselage 110 shoots human users to facilitate.In a kind of optional embodiment, it will can control
Device 150 processed is arranged on the longitudinal axis of fuselage 110, and shooting 142 and home of switch keys 143 are arranged on to the left side of controller 150,
Power switch 141, focusing button 144, focusing knob 145 and aperture adjusting knob 146 are arranged on to the right side of controller 150.
It should be appreciated that the aperture adjusting knob 146 set on fuselage 110 can be used for adjusting electric aperture, the physics of video camera 200
One or more in aperture, but when remote control 100 is provided with above-mentioned focusing rolled round, then aperture adjusting knob 146 can be with
It is only used for adjusting the electric aperture of video camera.
Finally, property is also an option that on fuselage 110 display 190 is set, thus can be real on remote control 100
When play or the shooting picture that is returned by video camera 300 of playback.In actual design process, display 190 can be independent
The mobile electronic device such as the display or mobile phone of configuration or tablet personal computer.Can between display 190 and fuselage 110
To be linked together by wireless or wired mode, to realize the transmission of data.Specifically, in some alternatively embodiments
In, angle-adjusting bracket is installed on fuselage 110, display 190 is carried on the angle-adjusting bracket, so as to realize fuselage
110 and the mechanical connection of display 190.Angle-adjusting bracket can use various structures, for example, it may be linkage.It is logical
Over-angle adjusting bracket can realize the adjustment to angle of inclination between display 190 and fuselage 110, so as to facilitate shooting personnel
The content played on viewing display 190.In addition, display 190 can use on fuselage 110 battery 170 that carries or
Single battery can be set.
Finally, although being described in the context of these embodiments associated with certain embodiments of the present technology
Advantage, but other embodiment can also include the advantages of such, and simultaneously this practicality is all described in detail in not all embodiments
New all advantages, the utility model is regarded as objective the advantages of bringing by the technical characteristic institute in embodiment and is different from now
There is the advantages of technology, belong to the scope of protection of the utility model.
Claims (15)
- A kind of 1. remote control, for controlling head, it is characterised in that including：Fuselage and the first rolled round component；Battery is installed on the fuselage；The first rolled round component is rotatablely connected by rotating shaft and fuselage；The first rolled round component includes the first runner, and first runner can be rotated by driving force, with control The motion of at least one axle of head.
- 2. remote control according to claim 1, it is characterised in that be provided with and lead between the first rolled round component and fuselage To mechanism, for being oriented to when the first rolled round component rotates relative to the fuselage.
- 3. remote control according to claim 2, it is characterised in thatThe guiding mechanism includes：The guide groove being arranged on the first rolled round component, and be slidably installed in the guide groove And the sliding block being connected with the fuselage；OrThe guiding mechanism includes：The guide groove being arranged on the fuselage, and be slidably installed in the guide groove and with it is described The sliding block of first rolled round component connection.
- 4. remote control according to claim 3, it is characterised in that the guide groove is the arc using the rotating shaft as the center of circle Groove.
- 5. remote control according to claim 4, it is characterised in that the guide groove is dovetail groove, the sliding block for institute State the trapezoidal slide block of dovetail groove cooperation.
- 6. remote control according to claim 5, it is characterised in that also including screw rod, screw thread is provided with the screw rod；Institute The connection end and the trapezoidal slide block for stating screw rod are fixed, the screw rod away from the free end of the connection end through the fuselage or The screwed hole opened up on person's the first rolled round component.
- 7. remote control according to claim 6, it is characterised in that be also installed on including locking knob, the locking knob The free end of the screw rod.
- 8. remote control according to claim 7, it is characterised in that the fuselage or the first rolled round component include fixing Part, the free end of the screw rod pass through the through hole opened up on the fixture to extend to the fuselage or the first rolled round component Outside.
- 9. according to the remote control described in claim any one of 1-5, it is characterised in that also including retaining mechanism, the locking machine Structure includes locking piece, for after the first rolled round component rotates predetermined angle relative to the fuselage by first rolled round Component and fuselage locking.
- 10. according to the remote control described in claim any one of 1-8, it is characterised in that the first rolled round component and the machine Position-limit mechanism is additionally provided between body, the angular range rotated for limiting the first rolled round component relative to the fuselage.
- 11. remote control according to claim 10, it is characterised in that the position-limit mechanism includes：Locating slot and it is plugged in Locating dowel in the locating slot.
- 12. remote control according to claim 11, it is characterised in that the locating slot is arranged on determining for the fuselage installation On the plate of position, the locating dowel is arranged on the first rolled round component.
- 13. remote control according to claim 11, it is characterised in that the locating slot is the arc centered on the rotating shaft Shape groove.
- 14. according to the remote control described in claim any one of 1-8, it is characterised in that the remote control also includes the second rolled round Component, the second rolled round component include the second runner, and first runner and the second runner are used to control the head at least The motion of two axles.
- 15. remote control according to claim 14, it is characterised in that first runner is used to control the inclined of the head The motion of boat axle, second runner are used for the motion for controlling the pitch axis of the head.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720973502.1U CN207049552U (en) | 2017-08-04 | 2017-08-04 | Remote control |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720973502.1U CN207049552U (en) | 2017-08-04 | 2017-08-04 | Remote control |
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| Publication Number | Publication Date |
|---|---|
| CN207049552U true CN207049552U (en) | 2018-02-27 |
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ID=61499250
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720973502.1U Expired - Fee Related CN207049552U (en) | 2017-08-04 | 2017-08-04 | Remote control |
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| CN (1) | CN207049552U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019024119A1 (en) * | 2017-08-04 | 2019-02-07 | 深圳市大疆灵眸科技有限公司 | Remote controller and photographing device |
| WO2019024118A1 (en) * | 2017-08-04 | 2019-02-07 | 深圳市大疆灵眸科技有限公司 | Remote controller |
| WO2019144408A1 (en) * | 2018-01-29 | 2019-08-01 | 深圳市大疆创新科技有限公司 | Remote control |
| CN113983333A (en) * | 2018-11-29 | 2022-01-28 | 深圳市大疆创新科技有限公司 | Rocker structure and handheld cloud platform |
-
2017
- 2017-08-04 CN CN201720973502.1U patent/CN207049552U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019024119A1 (en) * | 2017-08-04 | 2019-02-07 | 深圳市大疆灵眸科技有限公司 | Remote controller and photographing device |
| WO2019024118A1 (en) * | 2017-08-04 | 2019-02-07 | 深圳市大疆灵眸科技有限公司 | Remote controller |
| US11089198B2 (en) | 2017-08-04 | 2021-08-10 | Sz Dji Osmo Technology Co., Ltd. | Remote controller and photographing device |
| WO2019144408A1 (en) * | 2018-01-29 | 2019-08-01 | 深圳市大疆创新科技有限公司 | Remote control |
| CN110325782A (en) * | 2018-01-29 | 2019-10-11 | 深圳市大疆创新科技有限公司 | Remote controler |
| CN110325782B (en) * | 2018-01-29 | 2021-05-14 | 深圳市大疆创新科技有限公司 | Remote controller |
| CN113983333A (en) * | 2018-11-29 | 2022-01-28 | 深圳市大疆创新科技有限公司 | Rocker structure and handheld cloud platform |
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Granted publication date: 20180227 |