WO2021008623A1 - 旋转传输信号机构以及无人机云台 - Google Patents

旋转传输信号机构以及无人机云台 Download PDF

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Publication number
WO2021008623A1
WO2021008623A1 PCT/CN2020/102880 CN2020102880W WO2021008623A1 WO 2021008623 A1 WO2021008623 A1 WO 2021008623A1 CN 2020102880 W CN2020102880 W CN 2020102880W WO 2021008623 A1 WO2021008623 A1 WO 2021008623A1
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WIPO (PCT)
Prior art keywords
wiring assembly
wiring
shaft core
cylinder
brush
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Application number
PCT/CN2020/102880
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English (en)
French (fr)
Inventor
韩涛
Original Assignee
深圳市道通智能航空技术有限公司
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Publication of WO2021008623A1 publication Critical patent/WO2021008623A1/zh

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • B64D47/08Arrangements of cameras
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R35/00Flexible or turnable line connectors, i.e. the rotation angle being limited
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R2201/00Connectors or connections adapted for particular applications
    • H01R2201/26Connectors or connections adapted for particular applications for vehicles

Definitions

  • This application relates to the field of unmanned aerial vehicles, and in particular to a rotating transmission signal mechanism and an unmanned aerial vehicle pan/tilt using the rotating transmission signal mechanism.
  • the gimbal is a device for stabilizing shooting equipment and is widely used in the field of unmanned aerial vehicles.
  • the gimbal includes a first axis arm for connecting to the body of the unmanned aerial vehicle, and for connecting the camera and connecting with the first axis arm.
  • a second shaft arm rotatably connected with a shaft arm and a motor installed on the first shaft arm for driving the second shaft arm to rotate.
  • Most of the existing ones use lines between the drone body and the camera to realize the signal transmission between the drone body and the camera.
  • the first axis arm and the second axis arm will twist the line during the relative rotation, and the first axis arm and the second axis arm cannot rotate 360°, which limits the shooting angle of the shooting device .
  • one of the objectives of the present invention is to disclose a rotation transmission signal mechanism, which is used to solve the problem that the first axis arm and the second axis arm of the existing pan/tilt head will cause the line to occur during relative rotation.
  • the problem of entanglement discloses an unmanned aerial vehicle pan/tilt which adopts the above-mentioned rotating transmission signal mechanism.
  • a rotation transmission signal mechanism comprising a first wiring assembly with a first wiring terminal and a second wiring assembly with a second wiring terminal and rotatably connected to the first wiring assembly
  • the first wiring assembly is provided with a plurality of A plurality of first conductive structures arranged at intervals and electrically connected to the first connecting terminal
  • the second connecting assembly is provided with a plurality of second conductive structures arranged at intervals and all electrically connected to the second connecting terminal
  • One of the first conductive structure and the second conductive structure is a ring-shaped conductive structure, and the other is a brush, and each of the brushes is in contact with one of the ring-shaped conductive structures.
  • the first wiring assembly includes the first wiring terminal, a first end cover, and a shaft core rotatably connected to the second wiring assembly, and the first wiring terminal and the shaft core are respectively Fixed on the opposite sides of the first end cover, the plurality of annular conductive structures are arranged on the outer surface of the shaft core along the axial interval of the shaft core, and the shaft core is penetrated A plurality of first wires for electrically connecting the first connection terminal and the ring-shaped conductive structure.
  • the outer surface of the shaft core is provided with a plurality of first annular grooves, and the plurality of first annular grooves are arranged at intervals along the axial direction of the shaft core, and each of the first annular grooves One said ring-shaped conductive structure is arranged in the groove; and/or,
  • the shaft core is provided with a plurality of first through holes, and each of the first through holes includes a first hole portion and a second hole portion communicating with the first hole portion, and the first hole portion extends from the shaft
  • the end face of the core facing the first end cover extends in the axial direction of the shaft core, and the second hole portion extends along the shaft core from the end of the first hole portion away from the first end cover Extend radially outward to the outer surface of the shaft core, and each of the first through holes is penetrated with one first wire; and/or,
  • the ring-shaped conductive structure is a conductive ring ringed on the outer surface of the shaft core, or a ring-shaped wire ring ringed on the outer surface of the shaft core, or a ring-shaped conductive plating layer ringed on the outer surface of the shaft core.
  • the second wiring assembly includes the second wiring terminal, a second end cover, and a first cylinder, and the second wiring terminal and the first cylinder are respectively fixedly arranged on the first cylinder.
  • the first cylinder is sleeved on the outer circumference of the shaft core and is rotatably connected with the shaft core, and the inner side wall of the first cylinder is axially spaced apart with a plurality of electric brushes
  • Each of the brush holes is provided with one brush, and a plurality of second wires for electrically connecting the second connection terminal and the brush are penetrated in the first cylinder.
  • the second wiring assembly further includes a second cylinder sleeved on the outer periphery of the first cylinder and fixedly connected to the first cylinder and/or the second end cover, so
  • the outer side surface of the first cylinder is concavely provided with strip grooves extending axially to the end surface of the first cylinder, and each of the strip grooves is embedded with two grooves along the first cylinder.
  • the second wires arranged side by side in the radial direction and the first insulating member arranged between the two second wires, the second wires and the second wires located radially outside of the first cylinder
  • a second insulating member is arranged between the cylinders; and/or,
  • the brush is an elastic conductive member bent and compressed in the brush hole, or the brush is elastically compressed and mounted in the brush hole.
  • the rotation transmission signal mechanism further includes two first bearings sleeved on both ends of the shaft core, and the first cylinder rotates with the shaft core through the two first bearings. Connected; and/or,
  • the rotation transmission signal mechanism further includes a first washer, and the first washer is disposed between the second cylinder and the first end cover.
  • the first wiring assembly includes the first wiring terminal and a top cover that is rotatably connected to the second wiring assembly, and the first wiring terminal is disposed on the top cover away from the first On one side of the second wiring assembly, the top cover is provided with a plurality of spaced second annular grooves at intervals on the side facing the second wiring assembly, and the plurality of second annular grooves are arranged coaxially, each An annular conductive structure is embedded in the second annular groove.
  • the second wiring assembly includes the second wiring terminal and a bottom cover rotatably connected to the top cover, and the second wiring terminal is disposed on the bottom cover away from the first wiring.
  • a plurality of mounting holes are arranged at intervals from the inside to the outside of the bottom cover facing the top cover, and each mounting hole is equipped with a brush.
  • the rotation transmission signal mechanism further includes a connecting shaft and two second bearings.
  • a bearing hole penetrates through the top cover and the bottom cover, and a bearing hole is installed in each bearing hole.
  • the connecting shaft passes through the two second bearings; and/or,
  • the rotation transmission signal mechanism further includes a second washer which is arranged between the top cover and the bottom cover.
  • An unmanned aerial vehicle pan/tilt comprising a mounting seat for the fuselage of the drone, a first shaft arm connected with the mounting seat, and a first shaft arm for connecting a camera and rotatingly connected with the first shaft arm A second shaft arm, a motor installed on the first shaft arm for driving the second shaft arm to rotate, and the above-mentioned rotation transmission signal mechanism, one of the first wiring assembly and the second wiring assembly One is fixedly connected to the first shaft arm, and the other is fixedly connected to the second shaft arm.
  • the present invention has the following beneficial effects:
  • the present invention provides a rotating transmission signal mechanism by providing a ring-shaped conductive structure on one of the first wiring assembly and the second wiring assembly, and the other is provided with a brush against which the ring-shaped conductive structure abuts.
  • the brushes and the ring-shaped conductive structure can realize the signal retention connection between the first wiring assembly and the second wiring assembly, without passing through the first wiring assembly and the second wiring assembly.
  • Wires are pierced through the components to realize the signal connection between the first wiring component and the second wiring component. Therefore, there is no problem of wire entanglement during the relative rotation of the first wiring component and the second wiring component.
  • the relative rotation angle of the first wiring assembly and the second wiring assembly is not limited.
  • FIG. 1 is a schematic structural diagram of a rotation transmission signal mechanism disclosed in the first embodiment of the present invention
  • FIG. 2 is a schematic cross-sectional view of the rotation transmission signal mechanism disclosed in the first embodiment of the present invention
  • FIG. 3 is an exploded schematic diagram of the rotating transmission signal mechanism disclosed in the first embodiment of the present invention.
  • FIG. 4 is a schematic cross-sectional view of the shaft core disclosed in the first embodiment of the present invention.
  • FIG. 5 is a schematic cross-sectional view of the first cylinder disclosed in the first embodiment of the present invention.
  • Figure 6 is an exploded schematic diagram of the first cylinder disclosed in the first embodiment of the present invention.
  • FIG. 7 is a schematic structural diagram of the rotation transmission signal mechanism disclosed in the second embodiment of the present invention.
  • FIG. 8 is an exploded schematic diagram of the rotation transmission signal mechanism disclosed in the second embodiment of the invention from a first perspective
  • FIG. 9 is an exploded schematic diagram from a second perspective of the rotation transmission signal mechanism disclosed in the second embodiment of the present invention.
  • FIG. 10 is a schematic structural diagram of a drone pan/tilt disclosed in Embodiment 3 of the present invention.
  • Fig. 11 is an exploded schematic diagram of the drone pan/tilt disclosed in the third embodiment of the present invention.
  • the first embodiment of the present invention discloses a rotation transmission signal mechanism 40, which includes a first wiring assembly 41 having a first wiring terminal 411 and a second wiring terminal 421 connected to the first wiring assembly 41
  • the second wiring assembly 42 is rotatably connected.
  • the first wiring assembly 41 is provided with a plurality of first conductive structures 51 arranged at intervals and electrically connected to the first wiring terminal 411, and the second wiring assembly 42 is provided with several spacing arrangements
  • the second conductive structure 52 is electrically connected to the second connection terminal 421.
  • the first conductive structure 51 is a ring-shaped conductive structure
  • the second conductive structure 52 is a brush. Each brush corresponds to a ring-shaped conductive structure. .
  • the signal is transmitted through the first conductive structure 51 and the second conductive structure 52, there is no need to run wires in the first wiring assembly 41 and the second wiring assembly 42 to maintain the first terminal 411 and the second terminal 411.
  • the rotation signal transmission mechanism 40 is applied to the UAV PTZ, it can avoid the influence of the winding problem on the camera rotation angle.
  • the camera can realize 360° rotation, which greatly expands the camera. The shooting angle.
  • the rotation transmission signal mechanism 40 is not limited to use on the UAV pan/tilt. Any two relatively rotating components that require signal transmission during rotation can be avoided by using the rotation transmission signal mechanism 40. The problem of winding wires.
  • the ring-shaped conductive structure and the brushes can be arranged in reverse, that is, the ring-shaped conductive structure is arranged on the second wiring assembly 42 and the brushes are arranged on the first wiring assembly 41, as long as the first wiring assembly During the relative rotation of 41 and the second wiring assembly 42, the brush and the ring-shaped conductive member can always keep in contact.
  • the first wiring assembly 41 includes a first wiring terminal 411, a first end cover 412, and a shaft core 413 that is rotatably connected to the second wiring component 42, the first wiring terminal 411 and the shaft core 413 They are respectively fixed on the opposite sides of the first end cover 412, the ring-shaped conductive structure is ring-shaped on the outer side of the shaft core 413 along the axial interval of the shaft core 413, and a number of holes for electrical connection to the A connecting terminal 411 and a first wire 414 of a ring-shaped conductive structure.
  • the shaft core 413 is substantially cylindrical, and one end of the shaft core 413 is fastened to the first end cover 412 by bolts.
  • the ring-shaped conductive structure can be a conductive ring ringed on the outer surface of the shaft core 413, or a ring-shaped wire ringed on the outer surface of the shaft core 413, or a ring-shaped conductive ring. Ring-shaped conductive plating on the outer surface of the shaft core 413.
  • the outer surface of the shaft core 413 is provided with a plurality of first annular grooves 4131, and the plurality of first annular grooves 4131 are arranged at intervals along the axial direction of the shaft core 413, and each first annular groove 4131 A ring-shaped conductive structure is provided in the groove 4131.
  • a plurality of first through holes 4132 are provided on the shaft core 413, and each first through hole 4132 includes a first hole portion 4133 and a second hole portion 4134 communicating with the first hole portion 4133.
  • the first hole 4133 extends from the end surface of the shaft core 413 toward the first end cover 412 to the axial direction of the shaft core 413, and the second hole 4134 extends from the end of the first hole 4133 away from the first end cover 412 along the shaft.
  • the core 413 extends radially outward to the outer surface of the shaft core 413, and each of the first through holes 4132 passes through the aforementioned first wire 414.
  • the second wiring assembly 42 includes a second wiring terminal 421, a second end cover 422, and a first cylinder 423.
  • the second wiring terminal 422 and the first cylinder 423 are respectively fixedly arranged on the first cylinder.
  • the first cylinder 423 is sleeved on the outer circumference of the shaft core 413 and is rotatably connected with the shaft core 413.
  • the inner wall of the first cylinder 423 is axially spaced with a plurality of brush holes 4231, Each brush hole 4231 is provided with one brush as described above, and a plurality of second wires 424 for electrically connecting the second connection terminal 421 and the brush are penetrated in the first cylinder 423.
  • the brush is an elastic conductive member bent and compressed in the brush hole 4231.
  • the brush is an elastic conductive member, and its length is greater than the distance from the second wire 424 to the ring-shaped conductive structure.
  • the purpose of this setting method is to prolong the service life of the rotating transmission signal mechanism 40.
  • the brush will extend towards the ring-shaped conductive structure by its own elastic force, which can ensure that the brush and the The contact of the ring-shaped conductive structure does not lead to poor contact due to the wear of the brush, which prolongs the service life of the rotation transmission signal mechanism 40.
  • the brush is not limited to the above arrangement.
  • the brush it is also possible for the brush to be elastically compressed and installed in the brush hole 4231.
  • an elastic member such as a spring, is installed in the brush hole 4231, and then the brush Installed in the brush hole 4231, the elastic member is in a compressed state.
  • the brush When the brush is worn during use, due to the squeezing effect of the elastic member, the brush will always keep in contact with the ring-shaped conductive structure to avoid poor contact and extend The service life of the rotating transmission signal mechanism 40
  • the rotation transmission signal mechanism 40 further includes two first bearings 43 sleeved on both ends of the shaft core 413, and the first cylinder 423 rotates through the two first bearings 43 and the shaft core 413. connection. Specifically, the inner rings of the two first bearings 43 are respectively in interference fit with the two ends of the shaft core 413, and the outer rings of the two first bearings 43 are in interference fit with the inner walls of the two ends of the first cylinder 423 respectively, so as to realize the shaft The core 413 is rotatably connected with the first cylinder 423.
  • the second wiring assembly 42 further includes a second cylinder 425 sleeved on the outer circumference of the first cylinder 423 and fixedly connected to the first cylinder 423 and/or the second end cover 422,
  • the outer surface of the first cylinder 423 is recessed with strip grooves 4232 extending axially along the first cylinder 423 to the end surface of the first cylinder 423, and each strip groove 4232 is embedded with two strips along the diameter of the first cylinder 423.
  • the second wire 424 arranged side by side and the first insulator 426 arranged between the two second wires 424 are arranged between the second wire 424 located radially outside the first cylinder 423 and the second cylinder 425 Second insulation 427.
  • the installation of the second wire 424 is facilitated.
  • the second wire 424/first insulating member 426/second wire 424/second insulating member 427 is arranged in the strip groove in a stacked relationship.
  • the second cylinder 425 is then sleeved on the outer circumference of the first cylinder 423.
  • the first cylinder 423 is not limited to installing the second wire 424 by providing the strip-shaped groove 4232, for example, by following the end surface of the first cylinder 423 toward the second end cap 422 along the axis of the first cylinder 42 It is also possible to open two through holes at intervals to pass through the second wire 424.
  • the rotation transmission signal mechanism 40 further includes a first washer 44 disposed between the second cylinder 425 and the first end cover 412.
  • the surface of the second cylinder 425 facing the first end cover 412 is recessed with a second annular groove 4251, and the first gasket 44 is embedded in the first annular groove 4241, and the first gasket 44 is used to prevent moisture.
  • Dust enters the rotation transmission signal mechanism from the gap between the second cylinder 425 and the first end cover 412.
  • the first gasket 44 is not limited to be disposed between the second cylinder 425 and the first end cover 412.
  • the first gasket 44 is disposed between the first cylinder 423 and the first end cover 412. .
  • the second embodiment of the present invention provides a rotation transmission signal mechanism 70.
  • the rotation transmission signal mechanism 70 provided in the second embodiment of the present invention is the same as the rotation transmission signal mechanism 40 provided in the first embodiment of the present invention.
  • the place is:
  • the rotation transmission signal mechanism 70 of this embodiment also includes a first wiring assembly 71 having a first wiring terminal 711 and a second wiring assembly 72 having a second wiring terminal 721 and rotatably connected to the first wiring assembly 71.
  • the first wiring assembly 71 is also provided with a number of first conductive structures 81 spaced apart and electrically connected to the first terminal 711
  • the second wiring assembly 72 is also provided with a number of spaced apart and electrically connected to the second terminal 721
  • the second conductive structure 82, the first conductive structure 81 is a ring-shaped conductive structure
  • the second conductive structure 82 is a brush abutting against the ring-shaped conductive structure.
  • the first wiring assembly 71 and the second wiring assembly 72 can rotate 360°, that is, the first shaft arm 10 and the The two-axis arms 20 can be rotated 360°.
  • the rotation signal transmission mechanism 40 When the rotation signal transmission mechanism 40 is applied to the UAV PTZ, it can avoid the influence of the winding problem on the rotation angle of the camera.
  • the camera can achieve 360° rotation, which is extremely The earth expands the shooting angle of the camera.
  • the difference between the rotation transmission signal mechanism 70 provided in the second embodiment of the present invention and the rotation transmission signal mechanism 40 provided in the first embodiment is:
  • the first wiring assembly 71 includes a first wiring terminal 711 and a top cover 712 rotatably connected to the second wiring assembly 72.
  • the first wiring terminal 711 is disposed on the top cover 712 away from the second wiring.
  • One side of the component 72, the top cover 712 facing the second wiring component 72 is provided with a plurality of second annular grooves 7121 spaced apart, and a plurality of second annular grooves 7121 are arranged coaxially, each of the second annular grooves A ring-shaped conductive structure is embedded in the groove 7121.
  • the second wiring assembly 72 includes a second wiring terminal 721 and a bottom cover 722 rotatably connected to the top cover 712.
  • the second wiring terminal 721 is disposed on the bottom cover 722 away from the first wiring assembly 71.
  • a number of mounting holes 7221 are spaced from the inside to the outside, and a brush is installed in each mounting hole 7221.
  • the brush is an elastic conductive member bent and compressed in the mounting hole 7221.
  • the rotation transmission signal mechanism 70 further includes a connecting shaft 73 and two second bearings 74.
  • the top cover 712 and the bottom cover 722 are respectively provided with a bearing hole 7122, each bearing hole 7122 One second bearing 73 is installed, and the connecting shaft 73 passes through the two second bearings 74.
  • the outer rings of the two second bearings 74 are respectively in interference fit with the bearing holes 7122 opened on the top cover 712 and the bottom cover 722, the connecting shaft 73 is inserted through the two second bearings 73, and the two ends are respectively connected with The inner rings of the two second bearings 73 are interference fit, so as to realize the rotational fit of the first wiring assembly 71 and the second wiring assembly 72.
  • the rotation transmission signal mechanism 70 further includes a second washer 75 disposed between the top cover 712 and the bottom cover 722.
  • the surface of the bottom cover 722 facing the top cover 712 is provided with a third annular groove 7222, and the second gasket 75 is embedded in the third annular groove 7222.
  • the second gasket 75 is used to prevent moisture and dust from being removed from the top.
  • the gap between the cover 712 and the bottom cover 722 enters the rotation transmission signal mechanism.
  • the third annular groove 7222 is not limited to being provided on the bottom cover 722, and it can also be provided on the top cover 712.
  • the third embodiment of the present invention discloses an unmanned aerial vehicle pan/tilt 100, including a mounting seat 101, a first shaft arm 102, a second shaft arm 103, a motor 104, and or
  • the rotation signal transmission mechanism described in the second embodiment is described in this embodiment by taking the rotation signal transmission mechanism 70 disclosed in the second embodiment as an example.
  • the mounting base 101 is used to install and fix the fuselage of the drone.
  • the first axis arm 102 is connected to the mounting base 101, the second axis arm 103 is rotatably connected to the first axis arm 102, and the camera is mounted on the second axis arm 103.
  • the motor 104 is installed on the first shaft arm 102 for driving the second shaft arm 103 to rotate relative to the first shaft arm 102, and the rotation signal transmission mechanism 70 is installed between the first shaft arm 102 and the second shaft arm 103 for Communication between the drone body and the camera.
  • the first wiring assembly 71 of the rotation signal transmission mechanism 70 is fixedly installed on the first shaft arm 102
  • the second wiring assembly 72 of the rotation signal transmission mechanism 70 is fixedly installed on the second shaft arm 103
  • the output shaft of the motor 104 After passing through the bearing hole 7122, 1041 is fixedly connected to the second shaft arm 103, the wire from the drone body is connected to the first terminal 711, and the wire from the camera is connected to the second terminal 721.
  • the motor 104 drives the second shaft arm 103 to rotate in the E-E direction relative to the first shaft arm 102, thereby driving the camera to rotate in the E-E direction.
  • the first wiring assembly 71 and the second wiring assembly 72 achieve signal transmission through the first conductive structure 81 and the second conductive structure 82, there is no need to thread wires in the first wiring assembly 71 and the second wiring assembly 72 to maintain the first wiring.
  • the signal is transmitted between the terminal 711 and the second connection terminal 721, so that when the motor 104 drives the second shaft arm 103 to rotate relative to the first shaft arm 102, between the first connection assembly 71 and the second connection assembly 72
  • the first wiring assembly 71 and the second wiring assembly 72 can be rotated 360°, that is, the first shaft arm 102 and the second shaft arm 103 can be rotated 360°.
  • the earth expands the shooting angle of the camera.
  • first wiring assembly 71 and the second wiring assembly 72 can be interchanged, that is, the first wiring assembly 71 is fixedly installed on the second shaft arm 103, and the first wiring component 72 is fixedly installed on the first shaft. Arm 71 is also possible.

Abstract

本发明公开了旋转传输信号机构以及无人机云台,其中,旋转传输信号机构通过在第一接线组件和第二接线组件中的一者上设置有环状导电结构,另一者上设置有与环状导电结构抵接的电刷,当第一接线组件和第二接线组件相对转动时,电刷和环状导电结构可以实现第一接线组件和第二接线组件之间的信号保持连接,而不用在第一接线组件和第二接线组件中穿设信号导线,因而也就不会在第一接线组件和第二接线组件相对转动的过程中出现线路缠绕的问题,从而不会限制第一接线组件和第二接线组件相对的旋转角度。当该旋转信号传输机构运用于无人机云台上时,可以避免线路缠绕问题对摄像头旋转角度的影响,摄像头可以实现360°旋转。

Description

旋转传输信号机构以及无人机云台
本申请要求于2019年7月18日提交中国专利局、申请号为201910650392.9、申请名称为“旋转传输信号机构以及无人机云台”的中国专利申请的优先权,其全部内容通过引用结合在本申请中。
技术领域
本申请涉及无人机领域,尤其涉及一种旋转传输信号机构以及一种采用该旋转传输信号机构的无人机云台。
背景技术
云台是一种对拍摄设备进行增稳的装置,在无人机领域具有广泛的运用,通常云台包括用于连接在无人机机体上的第一轴臂、用于连接摄像头并与第一轴臂转动连接的第二轴臂和安装于第一轴臂上以用于驱动第二轴臂转动的电机。现有的多是采用在无人机机体和摄像头之间穿设线路以实现无人机机体和摄像头之间的信号传输。但是,该设计方式,第一轴臂和第二轴臂在相对转动的过程中会使线路发生缠绕,第一轴臂和第二轴臂无法做到360°旋转,限制了拍摄设备的拍摄角度。
发明内容
为了克服现有技术的不足,本发明的目的之一公开一种旋转传输信号机构,用以解决现有的云台的第一轴臂和第二轴臂在相对转动的过程中会使线路发生缠绕的问题。本发明的目的之二公开一种无人机云台,该无人机云台采用上述的旋转传输信号机构。
本发明的目的之一采用如下技术方案实现:
一种旋转传输信号机构,包括具有第一接线端子的第一接线组件和具有第二接线端子并与所述第一接线组件转动连接的第二接线组件,所述第一接线组件上设有若干个间隔设置且都与所述第一接线端子电连接的第一导电结构,所述第二接线组件上设有若干个间隔设置且都与所述第二接线端子电连接的第 二导电结构,所述第一导电结构和所述第二导电结构中的一者为环状导电结构、另一者为电刷,每个所述电刷对应与一个所述环状导电结构抵接。
作为一种改进方式,所述第一接线组件包括所述第一接线端子、第一端盖以及与所述第二接线组件转动连接的轴芯,所述第一接线端子和所述轴芯分别固定于所述第一端盖相背的两侧,所述若干个环状导电结构沿所述轴芯的轴向间隔环设于所述轴芯的外侧面,所述轴芯中穿设有若干个用于电连接所述第一接线端子和所述环状导电结构的第一导线。
作为一种改进方式,所述轴芯的外侧面设置有若干个第一环形凹槽,所述若干个第一环形凹槽沿所述轴芯的轴向间隔设置,每个所述第一环形凹槽中设置一个所述环状导电结构;且/或,
所述轴芯上设置有若干个第一穿孔,每个所述第一穿孔包括第一孔部和与所述第一孔部连通的第二孔部,所述第一孔部从所述轴芯之朝向所述第一端盖的端面往所述轴芯的轴向延伸,所述第二孔部从所述第一孔部之远离所述第一端盖的端部沿所述轴芯径向向外延伸至所述轴芯的外侧面,每个所述第一穿孔中穿设一个所述第一导线;且/或,
所述的环状导电结构为环设在轴芯外侧面的导电环,或者为环设在轴芯外侧面的环状导线,或者为环设在轴芯外侧面的环状导电镀层。
作为一种改进方式,所述第二接线组件包括所述第二接线端子、第二端盖以及第一筒体,所述第二接线端子和所述第一筒体分别固定设置于所述第二端盖相背的两侧,所述第一筒体套设于所述轴芯外周并与所述轴芯转动连接,所述第一筒体的内侧壁轴向间隔开设有若干个电刷孔,每个所述电刷孔中设置一个所述电刷,所述第一筒体中穿设有若干个用于电连接所述第二接线端子和所述电刷的第二导线。
作为一种改进方式,所述第二接线组件还包括套设于所述第一筒体外周并与所述第一筒体和/或所述第二端盖固定连接的第二筒体,所述第一筒体的外侧面凹设有沿所述第一筒体轴向延伸至所述第一筒体的端面的条形槽,每个所述条形槽内嵌两条沿第一筒体径向并排设置的所述第二导线和设于两条所述第二导线之间的第一绝缘件,位于所述第一筒体径向外侧的所述第二导线与所述第二筒体之间设置有第二绝缘件;且/或,
所述电刷为弯折压缩于所述电刷孔中的弹性导电件,或者,所述电刷弹性压缩安装于所述电刷孔中。
作为一种改进方式,所述旋转传输信号机构还包括两个分别套设于所述轴芯两端的第一轴承,所述第一筒体通过两个所述第一轴承与所述轴芯转动连接;且/或,
所述旋转传输信号机构还包括第一垫圈,所述第一垫圈设置于所述第二筒体与所述第一端盖之间。
作为一种改进方式,所述第一接线组件包括所述第一接线端子和与所述第二接线组件转动连接的顶盖,所述第一接线端子设置于所述顶盖之远离所述第二接线组件的一侧,所述顶盖朝向所述第二接线组件的一侧间隔设置有若干个间隔设置的第二环形凹槽,所述若干个第二环形凹槽同轴设置,每个所述第二环形凹槽中内嵌一个所述环状导电结构。
作为一种改进方式,所述第二接线组件包括所述第二接线端子和与所述顶盖转动连接的底盖,所述第二接线端子设置于所述底盖之远离所述第一接线组件的一侧,所述底盖朝向所述顶盖的一侧由里向外间隔设置有若干个安装孔,每个安装孔中安装一个所述电刷。
作为一种改进方式,所述旋转传输信号机构还包括连接轴和两个第二轴承,所述顶盖和所述底盖上分别贯穿开设一个轴承孔,每个所述轴承孔中安装一个所述第二轴承,所述连接轴穿设于两个所述第二轴承中;且/或,
所述旋转传输信号机构还包括第二垫圈,所述第二垫圈设置于所述顶盖和所述底盖之间。
本发明的目的之二采用如下技术方案实现:
一种无人机云台,包括用于供无人机机身安装的安装座、与所述安装座连接的第一轴臂、用于连接摄像头并与所述第一轴臂转动连接的第二轴臂、安装于所述第一轴臂上以用于驱动所述第二轴臂转动的电机以及上述的旋转传输信号机构,所述第一接线组件与所述第二接线组件中的一者与所述第一轴臂固定连接,另一者与所述第二轴臂固定连接。
相比现有技术,本发明的有益效果在于:
本发明通过设置旋转传输信号机构通过在第一接线组件和第二接线组件 中的一者上设置有环状导电结构,另一者上设置有环状导电结构抵接的电刷,这样,当第一接线组件和第二接线组件相对转动时,电刷和环状导电结构可以实现第一接线组件和第二接线组件之间的信号保持连接,而不用通过在第一接线组件和第二接线组件中穿设导线来实现第一接线组件和第二接线组件之间的信号连接,因而,也就不会在第一接线组件和第二接线组件相对转动的过程中出现线路缠绕的问题,从而不会限制第一接线组件和第二接线组件相对的旋转角度。当该旋转信号传输机构运用于无人机云台上时,可以避免线路缠绕问题对摄像头旋转角度的影响,摄像头可以实现360°旋转,极大地扩大了摄像头的拍摄角度。
附图说明
图1为本发明实施例一公开的旋转传输信号机构的结构示意图;
图2为本发明实施例一公开的旋转传输信号机构的剖面示意图;
图3为本发明实施例一公开的旋转传输信号机构的爆炸示意图;
图4为本发明实施例一公开的轴芯的剖面示意图;
图5为本发明实施例一公开的第一筒体的剖面示意图;
图6为本发明实施例一公开的第一筒体的爆炸示意图;
图7为本发明实施例二公开的旋转传输信号机构的结构示意图;
图8为本发明实施例二公开的旋转传输信号机构第一视角的爆炸示意图;
图9为本发明实施例二公开的旋转传输信号机构第二视角的爆炸示意图;
图10为本发明实施例三公开的无人机云台的结构示意图;
图11为本发明实施例三公开的无人机云台的爆炸示意图。
具体实施方式
下面,结合附图以及具体实施方式,对本发明做进一步描述,需要说明的是,在不相冲突的前提下,以下描述的各实施例之间或各技术特征之间可以任意组合形成新的实施例。
实施例一:
请参阅图1-6,本发明的实施例一公开了一种旋转传输信号机构40,包括具有第一接线端子411的第一接线组件41和具有第二接线端子421并与第一接线组件41转动连接的第二接线组件42,第一接线组件41上设有若干个间隔设置且都与第一接线端子411电连接的第一导电结构51,第二接线组件42上设有若干个间隔设置且都与第二接线端子421电连接的第二导电结构52,第一导电结构51为环状导电结构,第二导电结构52为电刷,每个电刷对应与一个环状导电结构抵接。
以该设计方式,由于信号是通过第一导电结构51和第二导电结构52进行传递,无需在第一接线组件41和第二接线组件42中穿设线路来保持第一接线端子411和第二接线端子421之间信号的传递,这样,第一接线组件41和第二接线组件42在相对转动的过程中不会存在系统线路缠绕的问题,第一接线组件41和第二接线组件42可以做到360°旋转的同时传递信号,当该旋转信号传输机构40运用于无人机云台上时,可以避免线路缠绕问题对摄像头旋转角度的影响,摄像头可以实现360°旋转,极大地扩大了摄像头的拍摄角度。
当然,该旋转传输信号机构40不局限于使用在无人机云台上,任何两个相对转动的组件,在转动的过程中还需要进行信号的传输均可以采用该旋转传输信号机构40来避免线路缠绕的问题。
进一步地,环状导电结构和电刷可以对调设置,也即,环状导电结构设置于第二接线组件42上,而电刷设置于第一接线组件41上也是可以的,只要第一接线组件41和第二接线组件42相对转动的过程中,电刷和环状导电件可以始终保持接触即可。
作为本实施例的一种改进方式,第一接线组件41包括第一接线端子411、第一端盖412以及与第二接线组件42转动连接的轴芯413,第一接线端子411和轴芯413分别固定于第一端盖412相背的两侧,环状导电结构沿轴芯413的轴向间隔环设于轴芯413的外侧面,轴芯413中穿设有若干个用于电连接第一接线端子411和环状导电结构的第一导线414。轴芯413大致呈圆柱状,轴芯413的一端通过螺栓与第一端盖412紧固连接。
作为本实施例的一种改进方式,所述的环状导电结构可以为环设在轴芯413外侧面的导电环,或者为环设在轴芯413外侧面的环状导线,或者为环设 在轴芯413外侧面的环状导电镀层。
作为本实施例的一种改进方式,轴芯413的外侧面设置有若干个第一环形凹槽4131,若干个第一环形凹槽4131沿轴芯413的轴向间隔设置,每个第一环形凹槽4131中设置一个环状导电结构。
作为本实施例的一种改进方式,轴芯413上设置有若干个第一穿孔4132,每个第一穿孔4132包括第一孔部4133和与第一孔部4133连通的第二孔部4134,第一孔部4133从轴芯413之朝向第一端盖412的端面往轴芯413的轴向延伸,第二孔部4134从第一孔部4133之远离第一端盖412的端部沿轴芯413径向向外延伸至轴芯413的外侧面,每个第一穿孔4132中穿设一个上述的第一导线414。
作为本实施例的一种改进方式,第二接线组件42包括第二接线端子421、第二端盖422以及第一筒体423,第二接线端子422和第一筒体423分别固定设置于第二端盖422相背的两侧,第一筒体423套设于轴芯413外周并与轴芯413转动连接,第一筒体423的内侧壁轴向间隔开设有若干个电刷孔4231,每个电刷孔4231中设置一个上述的电刷,第一筒体423中穿设有若干个用于电连接第二接线端子421和电刷的第二导线424。
作为本实施例的一种改进方式,电刷为弯折压缩于电刷孔4231中的弹性导电件。具体地,该电刷是具有弹性的弹性导电件,且其长度大于第二导线424到环状导电结构的距离,这样,电刷安装于电刷孔4231中时,电刷呈弯折压缩形态。该设置方式的目的在于延长旋转传输信号机构40的使用寿命,电刷在使用的过程中每磨损一点,由自身弹力作用电刷会朝向环状导电结构延伸一点,从而可以长时间保证电刷与环状导电结构的接触,而不会由于电刷的磨损导致接触不良,延长了旋转传输信号机构40的使用寿命。
当然,电刷不局限于采用上述的设置方式,例如,电刷弹性压缩安装于电刷孔4231也是可以的,具体地,在电刷孔4231中安装一个弹性件,例如弹簧,然后将电刷安装于电刷孔4231中,弹性件处于压缩状态,当电刷在使用过程中产生磨损时,由于弹性件的挤压作用,电刷会始终与环状导电结构保持接触,避免接触不良,延长旋转传输信号机构40的使用寿命
作为本实施例的一种改进方式,旋转传输信号机构40还包括两个分别套 设于轴芯413两端的第一轴承43,第一筒体423通过两个第一轴承43与轴芯413转动连接。具体地,两个第一轴承43的内圈分别与轴芯413的两端过盈配合,两个第一轴承43的外圈分别与第一筒体423两端的内壁过盈配合,从而实现轴芯413与第一筒体423的转动连接。
作为本实施例的一种改进方式,第二接线组件42还包括套设于第一筒体423外周并与第一筒体423和/或第二端盖422固定连接的第二筒体425,第一筒体423的外侧面凹设有沿第一筒体423轴向延伸至第一筒体423端面的条形槽4232,每个条形槽4232内嵌两条沿第一筒体423径向并排设置的第二导线424和设于两条第二导线424之间的第一绝缘件426,位于第一筒体423径向外侧的第二导线424与第二筒体425之间设置有第二绝缘件427。以该设计方式,便于第二导线424的安装,安装时,只需将第二导线424/第一绝缘件426/第二导线424/第二绝缘件427按照依次层叠的关系设置于条形槽4232中,然后将第二筒体425套设在第一筒体423的外周即可。可以理解地,第一筒体423不局限于通过设置条形槽4232来安装第二导线424,例如,通过从第一筒体423朝向第二端盖422的端面沿第一筒体42的轴向间隔开设两个通孔来穿设所述的第二导线424也是可以的。
作为本实施例的一种改进方式,旋转传输信号机构40还包括第一垫圈44,第一垫圈44设置于第二筒体425与第一端盖412之间。具体地,第二筒体425朝向第一端盖412的面凹设有第二环形凹槽4251,第一垫圈44嵌设于第一环形凹槽4241中,该第一垫圈44用于防止水分、灰尘从第二筒体425与第一端盖412之间的空隙进入到旋转传输信号机构内部。可以理解地,第一垫圈44不局限设置于第二筒体425与第一端盖412之间,例如,第一垫圈44设置于第一筒体423与第一端盖412之间也是可以的。
实施例二:
请参阅图7-9,本发明的实施例二提供了一种旋转传输信号机构70,本发明实施例二提供的旋转传输信号机构70与本发明实施例一提供的旋转传输信号机构40相同的地方在于:
本实施例的旋转传输信号机构70也包括具有第一接线端子711的第一接线组件71和具有第二接线端子721并与第一接线组件71转动连接的第二接线 组件72,第一接线组件71上也设有若干个间隔设置且都与第一接线端子711电连接的第一导电结构81,第二接线组件72上也设有若干个间隔设置且都与第二接线端子721电连接的第二导电结构82,第一导电结构81为环状导电结构,第二导电结构82为与环状导电结构抵接的电刷。
同理,以该设计方式,由于无需在第一接线组件71和第二接线组件72中穿设线路来保持第一接线端子711和第二接线端子721之间信号的传递,这样,第一接线组件71和第二接线组件72在相对转动的过程中不会存在系统线路缠绕的问题,第一接线组件71和第二接线组件72可以做到360°旋转,也即第一轴臂10和第二轴臂20之间可以做到360°旋转,当该旋转信号传输机构40运用于无人机云台上时,可以避免线路缠绕问题对摄像头旋转角度的影响,摄像头可以实现360°旋转,极大地扩大了摄像头的拍摄角度。
本发明实施例二提供的旋转传输信号机构70与实施例一提供的旋转传输信号机构40不同的地方在于:
作为本实施例的一种改进方式,第一接线组件71包括第一接线端子711和与第二接线组件72转动连接的顶盖712,第一接线端子711设置于顶盖712之远离第二接线组件72的一侧,顶盖712朝向第二接线组件72的一侧间隔设置有若干个间隔设置的第二环形凹槽7121,若干个第二环形凹槽7121同轴设置,每个第二环形凹槽7121中内嵌一个环状导电结构。
作为本实施例的一种改进方式,第二接线组件72包括第二接线端子721和与顶盖712转动连接的底盖722,第二接线端子721设置于底盖722之远离第一接线组件71的一侧,底盖722朝向顶盖712的一侧由里向外间隔设置有若干个安装孔7221,每个安装孔7221中安装一个电刷。优选地,电刷为弯折压缩于安装孔7221中的弹性导电件。
作为本实施例的一种改进方式,旋转传输信号机构70还包括连接轴73和两个第二轴承74,顶盖712和底盖722上分别贯穿开设一个轴承孔7122,每个轴承孔7122中安装一个第二轴承73,连接轴73穿设于两个第二轴承74中。具体地,两个第二轴承74的外圈分别和顶盖712、底盖722上开设的轴承孔7122过盈配合,连接轴73穿设于两个第二轴承73中,且两端分别与两个第二轴承73的内圈过盈配合,从而实现第一接线组件71和第二接线组件 72的转动配合。
作为本实施例的一种改进方式,旋转传输信号机构70还包括第二垫圈75,第二垫圈75设置于顶盖712和底盖722之间。具体地,底盖722之朝向顶盖712的面设置有第三环形凹槽7222,第二垫圈75嵌设于第三环形凹槽7222中,该第二垫圈75用于防止水分、灰尘从顶盖712和底盖722之间的空隙进入到旋转传输信号机构内部。可以理解地,第三环形凹槽7222不局限于设置在底盖722上,设置于顶盖712上也是可以的。
实施例三:
请参阅图7-11,本发明的实施例三公开了一种无人机云台100,包括安装座101、第一轴臂102、第二轴臂103、电机104以及如实施例一中或者实施例二中所述的旋转信号传输机构,本实施例中以实施例二中公开的旋转信号传输机构70为例进行说明。安装座101用于供无人机的机身安装固定,第一轴臂102与安装座101连接,第二轴臂103与第一轴臂102转动连接,摄像机安装在第二轴臂103上,电机104安装于第一轴臂102上以用于驱动第二轴臂103相对于第一轴臂102转动,旋转信号传输机构70安装于第一轴臂102与第二轴臂103之间以供无人机机身和摄像机之间的通信。
具体地,旋转信号传输机构70的第一接线组件71固定安装在第一轴臂102上,旋转信号传输机构70的第二接线组件72固定安装在第二轴臂103上,电机104的输出轴1041穿过轴承孔7122后与第二轴臂103固定连接,来自无人机机身的导线与第一接线端子711连接,来自摄像头的导线与第二接线端子721连接。使用时,电机104驱动第二轴臂103相对于第一轴臂102沿E-E方向旋转,从而带动相机沿E-E方向旋转。由于第一接线组件71和第二接线组件72通过第一导电结构81和第二导电结构82实现信号传递,无需在第一接线组件71和第二接线组件72中穿设线路来保持第一接线端子711和第二接线端子721之间信号的传递,这样,电机104在驱动第二轴臂103相对于第一轴臂102转动的过程中,第一接线组件71和第二接线组件72之间不会存在系统线路缠绕的问题,第一接线组件71和第二接线组件72可以做到360°旋转,也即第一轴臂102和第二轴臂103之间可以做到360°旋转,极大地扩大了摄像头的拍摄角度。可以理解地,第一接线组件71和第二接线组件72的安装位 置可以互换,也即第一接线组件71固定安装于第二轴臂103,而第一接线组件72固定安装于第一轴臂71也是可以的。
上述实施方式仅为本发明的优选实施方式,不能以此来限定本发明保护的范围,本领域的技术人员在本发明的基础上所做的任何非实质性的变化及替换均属于本发明所要求保护的范围。

Claims (10)

  1. 一种旋转传输信号机构,其特征在于,包括具有第一接线端子的第一接线组件和具有第二接线端子并与所述第一接线组件转动连接的第二接线组件,所述第一接线组件上设有若干个间隔设置且都与所述第一接线端子电连接的第一导电结构,所述第二接线组件上设有若干个间隔设置且都与所述第二接线端子电连接的第二导电结构,所述第一导电结构和所述第二导电结构中的一者为环状导电结构、另一者为电刷,每个所述电刷对应与一个所述环状导电结构抵接。
  2. 根据权利要求1所述的旋转传输信号机构,其特征在于,所述第一接线组件包括所述第一接线端子、第一端盖以及与所述第二接线组件转动连接的轴芯,所述第一接线端子和所述轴芯分别固定于所述第一端盖相背的两侧,所述若干个环状导电结构沿所述轴芯的轴向间隔环设于所述轴芯的外侧面,所述轴芯中穿设有若干个用于电连接所述第一接线端子和所述环状导电结构的第一导线。
  3. 根据权利要求2所述的旋转传输信号机构,其特征在于,所述轴芯的外侧面设置有若干个第一环形凹槽,所述若干个第一环形凹槽沿所述轴芯的轴向间隔设置,每个所述第一环形凹槽中设置一个所述环状导电结构;且/或,
    所述轴芯上设置有若干个第一穿孔,每个所述第一穿孔包括第一孔部和与所述第一孔部连通的第二孔部,所述第一孔部从所述轴芯之朝向所述第一端盖的端面往所述轴芯的轴向延伸,所述第二孔部从所述第一孔部之远离所述第一端盖的端部沿所述轴芯径向向外延伸至所述轴芯的外侧面,每个所述第一穿孔中穿设一个所述第一导线;且/或,
    所述的环状导电结构为环设在轴芯外侧面的导电环,或者为环设在轴芯外侧面的环状导线,或者为环设在轴芯外侧面的环状导电镀层。
  4. 根据权利要求2或3所述的旋转传输信号机构,其特征在于,所述第二接线组件包括所述第二接线端子、第二端盖以及第一筒体,所述第二接线端子和所述第一筒体分别固定设置于所述第二端盖相背的两侧,所述第一筒体套设于所述轴芯外周并与所述轴芯转动连接,所述第一筒体的内侧壁轴向间隔开 设有若干个电刷孔,每个所述电刷孔中设置一个所述电刷,所述第一筒体中穿设有若干个用于电连接所述第二接线端子和所述电刷的第二导线。
  5. 根据权利要求4所述的旋转传输信号机构,其特征在于,所述第二接线组件还包括套设于所述第一筒体外周并与所述第一筒体和/或所述第二端盖固定连接的第二筒体,所述第一筒体的外侧面凹设有沿所述第一筒体轴向延伸至所述第一筒体的端面的条形槽,每个所述条形槽内嵌两条沿第一筒体径向并排设置的所述第二导线和设于两条所述第二导线之间的第一绝缘件,位于所述第一筒体径向外侧的所述第二导线与所述第二筒体之间设置有第二绝缘件;且/或,
    所述电刷为弯折压缩于所述电刷孔中的弹性导电件,或者,所述电刷弹性压缩安装于所述电刷孔中。
  6. 根据权利要求5所述的旋转传输信号机构,其特征在于,所述旋转传输信号机构还包括两个分别套设于所述轴芯两端的第一轴承,所述第一筒体通过两个所述第一轴承与所述轴芯转动连接;且/或,
    所述旋转传输信号机构还包括第一垫圈,所述第一垫圈设置于所述第二筒体与所述第一端盖之间。
  7. 根据权利要求1所述的旋转传输信号机构,其特征在于,所述第一接线组件包括所述第一接线端子和与所述第二接线组件转动连接的顶盖,所述第一接线端子设置于所述顶盖之远离所述第二接线组件的一侧,所述顶盖朝向所述第二接线组件的一侧间隔设置有若干个间隔设置的第二环形凹槽,所述若干个第二环形凹槽同轴设置,每个所述第二环形凹槽中内嵌一个所述环状导电结构。
  8. 根据权利要求7所述的旋转传输信号机构,其特征在于,所述第二接线组件包括所述第二接线端子和与所述顶盖转动连接的底盖,所述第二接线端子设置于所述底盖之远离所述第一接线组件的一侧,所述底盖朝向所述顶盖的一侧由里向外间隔设置有若干个安装孔,每个安装孔中安装一个所述电刷。
  9. 根据权利要求8所述的旋转传输信号机构,其特征在于,所述旋转传输信号机构还包括连接轴和两个第二轴承,所述顶盖和所述底盖上分别贯穿开设一个轴承孔,每个所述轴承孔中安装一个所述第二轴承,所述连接轴穿设于 两个所述第二轴承中;且/或,
    所述旋转传输信号机构还包括第二垫圈,所述第二垫圈设置于所述顶盖和所述底盖之间。
  10. 一种无人机云台,其特征在于,包括用于供无人机机身安装的安装座、与所述安装座连接的第一轴臂、用于连接摄像头并与所述第一轴臂转动连接的第二轴臂、安装于所述第一轴臂上以用于驱动所述第二轴臂转动的电机以及如权利要求1-9任一项所述的旋转传输信号机构,所述第一接线组件与所述第二接线组件中的一者与所述第一轴臂固定连接、另一者与所述第二轴臂固定连接。
PCT/CN2020/102880 2019-07-18 2020-07-18 旋转传输信号机构以及无人机云台 WO2021008623A1 (zh)

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