WO2018040893A1 - 一种摇杆装置及遥控器 - Google Patents
一种摇杆装置及遥控器 Download PDFInfo
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- WO2018040893A1 WO2018040893A1 PCT/CN2017/097160 CN2017097160W WO2018040893A1 WO 2018040893 A1 WO2018040893 A1 WO 2018040893A1 CN 2017097160 W CN2017097160 W CN 2017097160W WO 2018040893 A1 WO2018040893 A1 WO 2018040893A1
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- rotating shaft
- rocker
- rotating
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- swing arm
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- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
Definitions
- the embodiments of the present application relate to the field of remote control technologies, and in particular, to a rocker device and a remote controller.
- a drone is a non-manned aerial vehicle that is operated by a radio remote control device or an onboard computer program control system.
- the drone has a simple structure and low cost of use. It can not only perform the tasks performed by manned aircraft, but also be suitable for tasks that are not suitable for manned aircraft, such as geological disaster investigation in dangerous areas, air rescue command and environmental remote sensing monitoring.
- the drone is usually controlled by the remote controller when performing the task, and the moving direction of the drone is controlled by detecting the moving direction of the remote control operating the joystick, and the rocker of the existing drone remote control rocker device moves in the direction.
- the reset operation is required manually, which is time-consuming and labor-intensive and the reset is not accurate enough, how to design a rocker device capable of automatically resetting is a problem to be solved in the prior art.
- the technical problem that is mainly solved by the embodiment of the present application is that the rocker of the existing drone remote control rocker device needs to manually perform a reset operation after the moving direction operation, which is time-consuming and labor-intensive and the reset is not accurate enough.
- a technical solution adopted by the embodiment of the present application is to provide a rocker device, comprising: a base; a first rotating shaft, the first rotating shaft is rotatably connected with the base; and a rocker Fixed to the first rotating shaft; a reset mechanism, and the first a rotating shaft connection for placing the rocker in an original position opposite to the base, and the reset mechanism acts on the first rotating shaft when the rocker is biased by the external force to the original position The restoring force to return the rocker to its original position.
- the reset mechanism includes: a first swing arm, a second swing arm, and a first elastic deformation member; and the first rotating shaft further includes a first rotating piece extending from one end of the first rotating shaft, One end of the first swing arm is provided with a first rotating hole and a first limiting slot communicating with the first rotating hole, and one end of the second swinging arm is provided with a second rotating hole and the second a second limiting slot communicating with the rotating hole, wherein one end of the first rotating shaft disposed with the first rotating piece sequentially passes through the first rotating hole and the second rotating hole, and the first rotating piece is located
- the first limiting slot and the second limiting slot are respectively connected; the two ends of the first elastic deformation member are respectively connected with the other end of the first swing arm and the other end of the second swing arm, and the first An elastic deformation member is in a stretched state.
- the rocker device further includes: a second rotating shaft sleeve, the second rotating shaft sleeve is disposed on the first rotating shaft and is rotatably connected with the base, and the second rotating shaft is The rocker runs through.
- the reset mechanism further includes: a third swing arm, a fourth swing arm and a second elastic deformation; the second rotating shaft is further provided with a second rotating piece extending from one end of the second rotating shaft
- One end of the third swing arm is provided with a third rotating hole and a third limiting slot communicating with the third rotating hole
- one end of the fourth swinging arm is provided with a fourth rotating hole and a fourth limiting slot communicating with the four rotating holes
- the second rotating shaft is provided with one end of the second rotating piece sequentially passing through the third rotating hole and the fourth rotating hole, and the second rotating piece Located in the third limiting slot and the fourth limiting slot; two ends of the second elastic deformation member are respectively connected to the other end of the third swing arm and the other end of the fourth swing arm, and The second elastic deformation member is in a stretched state.
- the rocker device further comprises a fixing mechanism for fixing the first rotating shaft and the second rotating shaft, the fixing mechanism comprising at least one of the following: a bearing, a collar.
- another technical solution adopted by the embodiment of the present application is to provide a remote controller including the rocker device described in the present application and a device for sensing the rocker Sensor for moving position.
- the senor is a magnetic sensor
- the magnetic sensor comprises a magnet and a magnetic induction chip
- the magnet is disposed at a bottom of the rocker
- the magnetic induction chip is disposed inside the base.
- the rocker device includes: a second rotating shaft sleeve, the second rotating shaft sleeve is disposed on the first rotating shaft and is rotatably connected with the base, and the second rotating shaft is shaken
- the rod is penetrating;
- the sensor is a potentiometer, and the potentiometer is disposed on the first rotating shaft and the second rotating shaft, respectively.
- the remote controller further comprises a printed circuit board assembly, and the magnetic induction chip is disposed on the printed circuit board assembly.
- the remote controller further comprises a casing; the casing is provided with a perforation, the casing covers the rocker device and the rocker is pierced from the perforation.
- the beneficial effect of the embodiment of the present application is that the rocker device provided by the embodiment of the present application is provided with a reset mechanism on the rotating shaft, and after the rocking lever is oscillated in any direction, the rocker will be under the action of the resetting force of the reset mechanism. Re-reset makes the remote control more flexible and the reset faster and more accurate.
- FIG. 1 is a schematic structural view of a rocker device according to an embodiment of the present application.
- FIG. 2 is a schematic cross-sectional view of a rocker device provided by an embodiment of the present application.
- FIG. 3 is an exploded view of a remote controller according to an embodiment of the present application.
- FIG. 4 is a schematic cross-sectional view of a remote controller according to an embodiment of the present application.
- FIG. 5 is a schematic structural diagram of a remote controller according to an embodiment of the present application.
- a rocker device provided by the embodiment of the present invention includes: a base 10; a first rotating shaft 20, the first rotating shaft 20 is rotatably connected with the base 10;
- the rocker 30 is fixed to the first rotating shaft 20, and in the embodiment, the rocker 30 is provided with a circular hole at the bottom thereof, and the rocker 30 is fixed in the circular hole by inserting the pin into the circular hole.
- a first rotating shaft 20 a reset mechanism 40 coupled to the first rotating shaft 20 for placing the rocker 30 in an original position opposite to the base 10, and subjecting the rocker 30 to an external force
- the reset mechanism 40 When the home position is moved, the reset mechanism 40 generates a restoring force acting on the first rotating shaft 20 to return the rocker 30 to the original position by providing a reset mechanism on the first rotating shaft 20. 40.
- the rocker 30 After the rocker 30 is oscillated in the X-axis direction, the rocker 30 will be reset again under the resetting force of the reset mechanism 40, so that the remote control operation is more flexible and the reset is faster and more accurate.
- the reset mechanism 40 includes: a first swing arm 41, a second swing arm 42 and a first elastic deformation member 43; the first rotation shaft 20 is further provided with one end from the first rotation shaft 20 An extended first rotating piece 21 is disposed at one end of the first swinging arm 41 and a first rotating hole 411 and a first limiting slot 412 communicating with the first rotating hole 411, the second swinging arm 42 a second rotating hole 421 and a second limiting slot 422 communicating with the second rotating hole 421 are disposed at one end, and one end of the first rotating shaft 20 provided with the first rotating piece 21 sequentially passes through the a first rotating hole 411 and a second rotating hole 421, and the first A rotating piece 21 is located in the first limiting slot 412 and the second limiting slot 422; two ends of the first elastic deformation member 43 are respectively opposite to the other end of the first swing arm 41 and the second swing arm The other end of the 42 is connected, and the first elastic deformation member 43 is in a stretched state, and can be accurately controlled by controlling the first rotating
- the relative position of the first rotating piece 21 and the first limiting slot 412 and the second limiting slot 422 can be flexibly changed according to requirements, first in FIG.
- the rotating piece 21 is a convex rotating piece and the concave first limiting groove 412 and the second limiting groove 422 are matched with each other.
- the concave rotating piece and the protruding limiting groove can also cooperate with each other.
- FIG. 1 is only one embodiment, and is not intended to limit the present application.
- the first elastic deformation member 43 in FIG. 1 is a tension spring. In practical applications, it may also be a rubber band or other elastic object capable of generating a restoring force. .
- the rocker device further includes: a second rotating shaft 50, the second rotating shaft 50 is sleeved on the first rotating shaft 20 and is rotatably connected with the base 10, and the second rotating shaft It is penetrated by the rocker 30.
- the rocking lever 30 is reset again under the resetting force of the reset mechanism 40, so that the remote control operation is more flexible. The reset is faster and more accurate.
- the reset mechanism 40 further includes: a third swing arm 44, a fourth swing arm 45, and a second elastic deformation member 46; the second rotation shaft 50 is further provided with the second rotation shaft 50 a second rotating piece 51 extending from one end of the third swinging arm 44 is provided with a third rotating hole 441 and a third limiting slot 442 communicating with the third rotating hole 441, the fourth swinging arm 45 One end of the second rotating shaft 50 is disposed with a fourth rotating hole 451 and a fourth limiting slot 452 communicating with the fourth rotating hole 451.
- the third rotating hole 441 and the fourth rotating hole 451 are located, and the second rotating piece 51 is located in the third limiting groove 442 and the fourth limiting groove 452; both ends of the second elastic deformation piece 46 Connected to the other end of the third swing arm 44 and the other end of the fourth swing arm 45, respectively, and the second elastic deformation member 46 is in a stretched state, by controlling the second rotating piece 51 at the
- the rotation of the three limiting slots 442 and the fourth limiting slot 452 can accurately control the angle of rotation, and it is worth noting that The relative position of the second rotating piece 51 and the third limiting slot 442 and the fourth limiting slot 452 can be flexibly changed according to requirements.
- the second rotating piece 51 is a convex rotating piece and the third limiting groove 442 and the fourth limiting groove 452 are matched with each other.
- the rotating piece and the convex piece may be concave.
- the limiting slots are matched with each other.
- FIG. 1 is only one embodiment, and is not intended to limit the present application.
- the second elastic deformation member 46 of FIG. 1 is the same as the first elastic deformation member 43. In the application, it can also be an elastic body such as a rubber band that can generate a restoring force.
- the rocker device further includes a fixing mechanism 60 for fixing the first rotating shaft 20 and the second rotating shaft 50, in order to make the first rotating shaft 20 and the second rotating shaft 50
- a fixing mechanism 60 for fixing the first rotating shaft 20 and the second rotating shaft 50, in order to make the first rotating shaft 20 and the second rotating shaft 50
- the structure is more compact, and the relative position of the first rotating shaft 20 and the second rotating shaft 50 needs to be fixed by using the fixing mechanism 60 to avoid relative displacement during the rotation of the rocker 30, which affects the reset of the reset mechanism. Precision.
- the fixing mechanism 60 used in the embodiment is four bearings having the same size and shape, and the four bearings are respectively fitted at the two ends of the first rotating shaft 20 and the second rotating shaft 50, thereby The first rotating shaft 20 and the second rotating shaft 50 are fixed.
- the securing mechanism 60 can employ a collar or the like.
- a remote controller includes the rocker device described in Embodiment 1 and a sensor for sensing a moving position of the rocker device.
- the sensor includes a magnetic sensor 71.
- the magnetic sensor 71 includes a magnet 711 and a magnetic induction chip 712.
- the magnet 711 is disposed at the bottom of the rocker 30, and the magnetic induction chip 712 is disposed at Inside the base 10, the operation principle of the remote controller is to control the displacement of the aircraft by measuring the relative displacement of the magnet 711 and the magnetic induction chip 712.
- the rocker 30 is not operated, the magnet 711 is located at the magnetic induction chip 712. Directly below, the rocker 30 is swayed back and forth, and the relative displacement of the magnet 711 and the magnetic induction chip 712 is generated.
- the displacement determines the displacement of the aircraft in the front, rear, left and right directions.
- the remote controller further includes a printed circuit board assembly 80 disposed on the printed circuit board assembly 80 for calculating the magnet 711 and the magnetic sensor chip 712.
- the relative displacement transmits the data to the aircraft.
- the remote controller further includes a housing 90 provided with a through hole 91 covering the rocker device and the rocker 30 passing through the through hole 91, the housing 90
- a housing 90 provided with a through hole 91 covering the rocker device and the rocker 30 passing through the through hole 91, the housing 90
- the outer casing 90, and the outer casing 90 is provided with perforations 91 to allow the rocker 30 to pass out for convenient operation.
- the magnetic sensor 71 in the sensor can be replaced with a potentiometer, that is, the sensor includes a potentiometer 72, and the potentiometers are respectively disposed at the On the first rotating shaft 20 and the second rotating shaft 50, the operating principle of the remote controller is to change the resistance change in the potentiometer by operating the rocker 30 before and after shaking, so that the current or voltage in the circuit Changes occur to control the displacement of the aircraft.
- the magnetic sensor 71 provided in FIG. 4 and the potentiometer 72 provided in FIG. 5 are all examples of the sensors in the remote controller. In practical applications, the sensor may also be an infrared sensor, a Hall sensor, or the like.
- a remote controller is provided, and a sensor capable of sensing a moving position of the rocker device is disposed on the rocker device, and the control station is controlled by controlling the movement of the rocker in the rocker device.
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- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
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- Transmission And Conversion Of Sensor Element Output (AREA)
- Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)
- Mechanical Control Devices (AREA)
Abstract
一种摇杆(30)装置及遥控器,其包括:底座(10);第一转动轴(20),第一转动轴(20)与底座(10)转动连接;摇杆(30),与第一转动轴(20)固定;复位机构(40),与第一转动轴(20)连接,用于使摇杆(30)处于与底座(10)相对的原位置,并且在摇杆(30)受到外力偏移原位置时,复位机构(40)产生作用于第一转动轴(20)的复位力,以使摇杆(30)回复至原位置。摇杆(30)装置通过在转动轴上设置复位机构(40),操作摇杆(30)在任意方向进行摆动后,摇杆(30)均会在复位机构(40)复位力的作用下重新复位,使得遥控复位精准。
Description
相关申请的交叉参考
本申请要求于2016年8月31日提交中国专利局、申请号为201610797121.2、发明名称为“一种摇杆装置及遥控器”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。
本申请实施方式涉及遥控技术领域,特别是涉及一种摇杆装置及遥控器。
无人机是通过无线电遥控设备或机载计算机程控系统进行操控的不载人飞行器。无人机结构简单、使用成本低,不但能完成有人驾驶飞机执行的任务,更适用于有人飞机不宜执行的任务,如危险区域的地质灾害调查、空中救援指挥和环境遥感监测。
无人机在执行任务时通常使用遥控器进行控制,通过检测遥控器操作摇杆的移动方向控制无人机的移动方向,现有的无人机遥控器摇杆装置的摇杆进行方向移动操作后需要手动进行复位操作,耗时耗力且复位不够精准,如何设计一种可自动实现复位的摇杆装置是现有技术有待解决的问题。
发明内容
本申请实施方式主要解决的技术问题是现有的无人机遥控器摇杆装置的摇杆进行方向移动操作后需要手动进行复位操作,耗时耗力且复位不够精准。
为解决上述技术问题,本申请实施方式采用的一个技术方案是:提供一种摇杆装置,包括:底座;第一转动轴,所述第一转动轴与所述底座转动连接;摇杆,其固定于所述第一转动轴;复位机构,与所述第一
转动轴连接,用于使所述摇杆处于与所述底座相对的原位置,并且在所述摇杆受到外力偏移所述原位置时,所述复位机构产生作用于所述第一转动轴的复位力,以使所述摇杆回复至原位置。
其中,所述复位机构包括:第一摆动臂、第二摆动臂和第一弹性形变件;所述第一转动轴上还设置有从所述第一转动轴的一端延伸的第一转动片,所述第一摆动臂的一端设置有第一转动孔以及与所述第一转动孔连通的第一限位槽,所述第二摆动臂的一端设置有第二转动孔以及与所述第二转动孔连通的第二限位槽,所述第一转动轴的设置有所述第一转动片的一端依次穿过所述第一转动孔和第二转动孔,并且所述第一转动片位于所述第一限位槽和第二限位槽内;所述第一弹性形变件的两端分别与所述第一摆动臂的另一端和第二摆动臂的另一端连接,并且所述第一弹性形变件处于拉伸状态。
其中,所述摇杆装置还包括:第二转动轴,所述第二转动轴套接设置于所述第一转动轴上并与所述底座转动连接,并且所述第二转动轴被所述摇杆贯穿。
其中,所述复位机构还包括:第三摆动臂、第四摆动臂和第二弹性形变件;所述第二转动轴上还设置有从所述第二转动轴的一端延伸的第二转动片,所述第三摆动臂的一端设置有第三转动孔以及与所述第三转动孔连通的第三限位槽,所述第四摆动臂的一端设置有第四转动孔以及与所述第四转动孔连通的第四限位槽,所述第二转动轴的设置有所述第二转动片的一端依次穿过所述第三转动孔和第四转动孔,并且所述第二转动片位于所述第三限位槽和第四限位槽内;所述第二弹性形变件的两端分别与所述第三摆动臂的另一端和第四摆动臂的另一端连接,并且所述第二弹性形变件处于拉伸状态。
其中,所述摇杆装置还包括用于固定所述第一转动轴和所述第二转动轴的固定机构,所述固定机构包括如下至少一种:轴承,轴环。
为解决上述技术问题,本申请实施方式采用的另一个技术方案是:提供一种遥控器,包括本申请所述的摇杆装置和用于感测所述摇杆装置
移动位置的传感器。
其中,所述传感器为磁感应器,所述磁感应器包括磁铁和磁感应芯片,所述磁铁设置于所述摇杆底部,所述磁感应芯片设置于所述底座内部。
其中,所述摇杆装置包括:第二转动轴,所述第二转动轴套接设置于所述第一转动轴上并与所述底座转动连接,并且所述第二转动轴被所述摇杆贯穿;所述传感器为电位器,所述电位器分别设置于所述第一转动轴和所述第二转动轴上。
其中,所述遥控器还包括印刷电路板组件,所述磁感应芯片设置于所述印刷电路板组件上。
其中,所述遥控器还包括外壳;所述外壳设有穿孔,所述外壳覆盖所述摇杆装置且所述摇杆从所述穿孔穿出。
本申请实施方式的有益效果是:本申请实施方式提供的摇杆装置通过在转动轴上设置一复位机构,操作摇杆在任意方向进行摆动后,摇杆均会在复位机构复位力的作用下重新复位,使得遥控操作更加灵活,复位更加快速精准。
为了更清楚地说明本申请实施例的技术方案,下面将对本申请实施例中所需要使用的附图作简单地介绍。显而易见地,下面所描述的附图仅仅是本申请的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。
图1是本申请实施例提供的一种摇杆装置的结构示意图;
图2是本申请实施例提供的一种摇杆装置的截面示意图;
图3是本申请实施例提供的一种遥控器的部件分解图;
图4是本申请实施例提供的一种遥控器的截面示意图;
图5是本申请实施例提供的一种遥控器的结构示意图。
为了使本申请的目的、技术方案及优点更加清楚明白,以下结合附图及实施例,对本申请进行进一步详细说明。应当理解,此处所描述的具体实施例仅用以解释本申请,并不用于限定本申请。
需要说明的是,如果不冲突,本申请实施例中的各个特征可以相互结合,均在本申请的保护范围之内。另外,虽然在装置示意图中进行了功能模块划分,在流程图中示出了逻辑顺序,但是在某些情况下,可以以不同于装置示意图中的模块划分,或流程图中的顺序执行所示出或描述的步骤。
具体地,下面结合附图,对本申请实施例作进一步阐述。
实施例1
如图1-3所示,本申请实施例提供的一种摇杆装置,包括:底座10;第一转动轴20,所述第一转动轴20与所述底座10转动连接;摇杆30,其固定于所述第一转动轴20,在本实施例中,所述摇杆30底部设有一圆形孔洞,通过将销轴插入所述圆形孔洞而将所述摇杆30固定在所述第一转动轴20上;复位机构40,与所述第一转动轴20连接,用于使所述摇杆30处于与所述底座10相对的原位置,并且在所述摇杆30受到外力偏移所述原位置时,所述复位机构40产生作用于所述第一转动轴20的复位力,以使所述摇杆30回复至原位置,通过在第一转动轴20上设置一复位机构40,操作摇杆30在X轴方向进行摆动后,摇杆30均会在复位机构40复位力的作用下重新复位,使得遥控操作更加灵活,复位更加快速精准。
具体地,所述复位机构40包括:第一摆动臂41、第二摆动臂42和第一弹性形变件43;所述第一转动轴20上还设置有从所述第一转动轴20的一端延伸的第一转动片21,所述第一摆动臂41的一端设置有第一转动孔411以及与所述第一转动孔411连通的第一限位槽412,所述第二摆动臂42的一端设置有第二转动孔421以及与所述第二转动孔421连通的第二限位槽422,所述第一转动轴20的设置有所述第一转动片21的一端依次穿过所述第一转动孔411和第二转动孔421,并且所述第
一转动片21位于所述第一限位槽412和第二限位槽422内;所述第一弹性形变件43的两端分别与所述第一摆动臂41的另一端和第二摆动臂42的另一端连接,并且所述第一弹性形变件43处于拉伸状态,通过控制所述第一转动片21在所述第一限位槽412和第二限位槽422内转动,能够精准的控制转动的角度,值得说明的是,所述第一转动片21与所述第一限位槽412和第二限位槽422的相对位置是可以根据需要灵活改变的,图1中第一转动片21为凸起的转动片与凹陷的第一限位槽412和第二限位槽422相互配合,在实际应用中,也可以为凹陷的转动片与凸起的限位槽相互配合,图1仅为实施例一种,并不用于限定本申请,同时图1中第一弹性形变件43为一拉簧,在实际应用中,也可以是橡皮筋等其他可以产生回复力的弹性物体。
具体地,所述摇杆装置还包括:第二转动轴50,所述第二转动轴50套接设置于所述第一转动轴20上并与所述底座10转动连接,并且第二转动轴被所述摇杆30贯穿。通过在所述摇杆装置上设置第二转动轴50,操作摇杆30在Z轴方向进行摆动后,摇杆30均会在复位机构40复位力的作用下重新复位,使得遥控操作更加灵活,复位更加快速精准。
具体地,所述复位机构40还包括:第三摆动臂44、第四摆动臂45和第二弹性形变件46;所述第二转动轴50上还设置有从所述第二转动轴50的一端延伸的第二转动片51,所述第三摆动臂44的一端设置有第三转动孔441以及与所述第三转动孔441连通的第三限位槽442,所述第四摆动臂45的一端设置有第四转动孔451以及与所述第四转动孔451连通的第四限位槽452,所述第二转动轴50的设置有所述第二转动片51的一端依次穿过所述第三转动孔441和第四转动孔451,并且所述第二转动片51位于所述第三限位槽442和第四限位槽452内;所述第二弹性形变件46的两端分别与所述第三摆动臂44的另一端和第四摆动臂45的另一端连接,并且所述第二弹性形变件46处于拉伸状态,通过控制所述第二转动片51在所述第三限位槽442和第四限位槽452内转动,能够精准的控制转动的角度,值得说明的是,所述第二转动片51与所述第三限位槽442和第四限位槽452的相对位置是可以根据需要灵活改
变的,图1中第二转动片51为凸起的转动片与凹陷的第三限位槽442和第四限位槽452相互配合,在实际应用中,也可以为凹陷的转动片与凸起的限位槽相互配合,图1仅为实施例一种,并不用于限定本申请,同时图1中第二弹性形变件46与所述第一弹性形变件43相同的拉簧,在实际应用中,也可以是橡皮筋等其他可以产生回复力的弹性物体。
具体地,所述摇杆装置还包括用于固定所述第一转动轴20和所述第二转动轴50的固定机构60,为了使所述第一转动轴20和所述第二转动轴50结构更加紧凑,需要使用固定机构60将所述第一转动轴20和所述第二转动轴50的相对位置进行固定,避免在所述摇杆30转动过程中发生相对位移,影响复位机构的复位精度。
在本实施例中所采用的固定机构60为四个大小形状均相同的轴承,所述四个轴承分别套装在所述第一转动轴20和所述第二转动轴50的两端,从而对所述第一转动轴20和所述第二转动轴50进行固定。在另一些实现方式中,所述固定机构60可以采用轴环等类似的部件。
在本申请实施例中所提供的摇杆装置,通过在转动轴上设置一复位机构,操作摇杆在任意方向进行摆动后,摇杆均会在复位机构复位力的作用下重新复位,使得遥控操作更加灵活,复位更加快速精准。
实施例2
如图3-4所示,本申请另一实施例提供的一种遥控器,包括实施例1所述的摇杆装置和用于感测所述摇杆装置移动位置的传感器。
如图4所示,具体地,所述传感器包括磁感应器71,所述磁感应器71包括磁铁711和磁感应芯片712,所述磁铁711设置于所述摇杆30底部,所述磁感应芯片712设置于所述底座10内部,该遥控器的操作原理在于通过测量磁体711和磁感应芯片712的相对位移从而控制飞行器的位移,在不操作所述摇杆30时,所述磁铁711位于所述磁感应芯片712的正下方,操作所述摇杆30前后左右摇晃将带动所述磁体711与所述磁感应芯片712产生前后左右的相对位移,该位移量决定着飞行器的前后左右方向上的位移。
具体地,所述遥控器还包括印刷电路板组件80,所述磁感应芯片712设置于所述印刷电路板组件80上,所述印刷电路板组件80用于计算所述磁体711和磁感应芯片712的相对位移将数据传输至飞行器。
具体地,所述遥控器还包括外壳90,所述外壳90设有穿孔91,所述外壳90覆盖所述摇杆装置且所述摇杆30从所述穿孔91穿出,所述外壳90用于保护所述摇杆装置,由于所述摇杆装置部件较多,且需要反复操作摇杆的位置,若长期裸露在外面容易使操作部件老化或丢失,因此在所述摇杆装置外部设置保护外壳90,且外壳90设有穿孔91可使摇杆30穿出方便操作。
可以理解的是,在一些其它实施中,如图5所示,所述传感器中的可磁感应器71可替换成电位器,也即所述传感器包括电位器72,所述电位器分别设置于所述第一转动轴20和所述第二转动轴50上,该遥控器的操作原理在于通过操作所述摇杆30前后左右摇晃改变所述电位器内的电阻变化,使得电路内的电流或者电压发生变化从而控制飞行器的位移变化。
值得说明的是,图4提供的磁感应器71和图5提供的电位器72均为所述遥控器内传感器的举例说明,在实际应用中,该传感器还可以为红外传感器、霍尔传感器等。
在本申请实施例中,提供一种遥控器,在摇杆装置上设置能够感测所述摇杆装置移动位置的传感器,通过控制所述摇杆装置内摇杆的前后左右的移动达到控制所述飞行器前后左右方向上的位移。
以上所述仅为本申请的实施方式,并非因此限制本申请的专利范围,凡是利用本申请说明书及附图内容所作的等效结构或等效流程变换,或直接或间接运用在其他相关的技术领域,均同理包括在本申请的专利保护范围内。
Claims (10)
- 一种摇杆装置,其特征在于,包括:底座;第一转动轴,所述第一转动轴与所述底座转动连接;摇杆,其固定于所述第一转动轴;复位机构,与所述第一转动轴连接,用于使所述摇杆处于与所述底座相对的原位置,并且在所述摇杆受到外力偏移所述原位置时,所述复位机构产生作用于所述第一转动轴的复位力,以使所述摇杆回复至原位置。
- 根据权利要求1所述的摇杆装置,其特征在于,所述复位机构包括:第一摆动臂、第二摆动臂和第一弹性形变件;所述第一转动轴上还设置有从所述第一转动轴的一端延伸的第一转动片,所述第一摆动臂的一端设置有第一转动孔以及与所述第一转动孔连通的第一限位槽,所述第二摆动臂的一端设置有第二转动孔以及与所述第二转动孔连通的第二限位槽,所述第一转动轴的设置有所述第一转动片的一端依次穿过所述第一转动孔和第二转动孔,并且所述第一转动片位于所述第一限位槽和第二限位槽内;所述第一弹性形变件的两端分别与所述第一摆动臂的另一端和第二摆动臂的另一端连接,并且所述第一弹性形变件处于拉伸状态。
- 根据权利要求1所述的摇杆装置,其特征在于,所述摇杆装置还包括:第二转动轴,所述第二转动轴套接设置于所述第一转动轴上并与所述底座转动连接,并且所述第二转动轴被所述摇杆贯穿。
- 根据权利要求3所述的摇杆装置,其特征在于,所述复位机构还包括:第三摆动臂、第四摆动臂和第二弹性形变件;所述第二转动轴上还设置有从所述第二转动轴的一端延伸的第二 转动片,所述第三摆动臂的一端设置有第三转动孔以及与所述第三转动孔连通的第三限位槽,所述第四摆动臂的一端设置有第四转动孔以及与所述第四转动孔连通的第四限位槽,所述第二转动轴的设置有所述第二转动片的一端依次穿过所述第三转动孔和第四转动孔,并且所述第二转动片位于所述第三限位槽和第四限位槽内;所述第二弹性形变件的两端分别与所述第三摆动臂的另一端和第四摆动臂的另一端连接,并且所述第二弹性形变件处于拉伸状态。
- 根据权利要求3所述的摇杆装置,其特征在于,所述摇杆装置还包括用于固定所述第一转动轴和所述第二转动轴的固定机构,所述固定机构包括如下至少一种:轴承,轴环。
- 一种遥控器,其特征在于,包括如权利要求1-2任一项所述的摇杆装置和用于感测所述摇杆装置移动位置的传感器。
- 根据权利要求6所述的遥控器,其特征在于,所述传感器为磁感应器,所述磁感应器包括磁铁和磁感应芯片,所述磁铁设置于所述摇杆底部,所述磁感应芯片设置于所述底座内部。
- 根据权利要求7所述的遥控器,其特征在于,所述摇杆装置包括:第二转动轴,所述第二转动轴套接设置于所述第一转动轴上并与所述底座转动连接,并且所述第二转动轴被所述摇杆贯穿;所述传感器为电位器,所述电位器分别设置于所述第一转动轴和所述第二转动轴上。
- 根据权利要求7或8所述的遥控器,其特征在于,所述遥控器还包括印刷电路板组件,所述磁感应芯片设置于所述印刷电路板组件上。
- 根据权利要求9所述的遥控器,其特征在于,所述遥控器还包 括外壳;所述外壳设有穿孔,所述外壳覆盖所述摇杆装置且所述摇杆从所述穿孔穿出。
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| CN111346368A (zh) | 2020-02-28 | 2020-06-30 | 歌尔科技有限公司 | 一种游戏手柄及其摇杆反馈力装置 |
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| CN115077362B (zh) * | 2022-08-19 | 2022-11-22 | 泉州市以色工业设计有限公司 | 平面移动位置检测装置及方法、输入设备 |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204143294U (zh) * | 2014-09-30 | 2015-02-04 | 深圳市大疆创新科技有限公司 | 摇杆装置及遥控器 |
| CN204614719U (zh) * | 2015-04-21 | 2015-09-02 | 东莞福哥电子有限公司 | 一种改进复位机构的3d旋转输入装置 |
| CN204792582U (zh) * | 2015-07-27 | 2015-11-18 | 东莞市凯华电子有限公司 | 新型游戏摇杆开关 |
| CN105161345A (zh) * | 2015-09-18 | 2015-12-16 | 东莞福哥电子有限公司 | 一种3d旋转摇杆控制装置 |
| US20160031554A1 (en) * | 2014-07-30 | 2016-02-04 | Siniger LLC | Control system for an aircraft |
| CN105517656A (zh) * | 2014-09-30 | 2016-04-20 | 深圳市大疆创新科技有限公司 | 拨轮组件、遥控器以及无人机控制方法 |
| CN106297247A (zh) * | 2016-08-31 | 2017-01-04 | 深圳市道通智能航空技术有限公司 | 一种摇杆装置及遥控器 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN200944200Y (zh) * | 2006-08-04 | 2007-09-05 | 东莞福哥电子有限公司 | 一种电磁感应式摇杆 |
| CN201035441Y (zh) * | 2007-04-19 | 2008-03-12 | 浙江红苹果电子有限公司 | 高精度的三维摇杆 |
| CN203674055U (zh) * | 2014-01-06 | 2014-06-25 | 东莞福哥电子有限公司 | 一种操作性良好的3d旋转输入装置 |
| CN203916083U (zh) * | 2014-06-03 | 2014-11-05 | 深圳市大疆创新科技有限公司 | 摇杆装置 |
| CN204143295U (zh) * | 2014-09-30 | 2015-02-04 | 深圳市大疆创新科技有限公司 | 拨轮组件和具有该拨轮组件的遥控器 |
| CN204833173U (zh) * | 2015-08-10 | 2015-12-02 | 深圳市大疆创新科技有限公司 | 动作感测结构及使用该动作感测结构的运动器件 |
-
2016
- 2016-08-31 CN CN201610797121.2A patent/CN106297247B/zh active Active
-
2017
- 2017-08-11 WO PCT/CN2017/097160 patent/WO2018040893A1/zh not_active Ceased
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160031554A1 (en) * | 2014-07-30 | 2016-02-04 | Siniger LLC | Control system for an aircraft |
| CN204143294U (zh) * | 2014-09-30 | 2015-02-04 | 深圳市大疆创新科技有限公司 | 摇杆装置及遥控器 |
| CN105517656A (zh) * | 2014-09-30 | 2016-04-20 | 深圳市大疆创新科技有限公司 | 拨轮组件、遥控器以及无人机控制方法 |
| CN204614719U (zh) * | 2015-04-21 | 2015-09-02 | 东莞福哥电子有限公司 | 一种改进复位机构的3d旋转输入装置 |
| CN204792582U (zh) * | 2015-07-27 | 2015-11-18 | 东莞市凯华电子有限公司 | 新型游戏摇杆开关 |
| CN105161345A (zh) * | 2015-09-18 | 2015-12-16 | 东莞福哥电子有限公司 | 一种3d旋转摇杆控制装置 |
| CN106297247A (zh) * | 2016-08-31 | 2017-01-04 | 深圳市道通智能航空技术有限公司 | 一种摇杆装置及遥控器 |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110347172A (zh) * | 2019-08-16 | 2019-10-18 | 珠海市双捷科技有限公司 | 一种地面角度检测装置、地面控制装置、系留无人机的控制系统 |
| CN110347172B (zh) * | 2019-08-16 | 2024-05-03 | 珠海市双捷科技有限公司 | 一种地面角度检测装置、地面控制装置、系留无人机的控制系统 |
| CN111054063A (zh) * | 2020-01-17 | 2020-04-24 | 深圳市七熊科技有限公司 | 及时检测摇杆感应数据的摇杆模块、摇杆系统、游戏手柄 |
| CN111540189A (zh) * | 2020-05-18 | 2020-08-14 | 安徽新盾消防设备有限公司 | 一种多功能单手持遥控器 |
| CN114156028A (zh) * | 2021-10-26 | 2022-03-08 | 东莞福哥电子有限公司 | 一种回弹力可调的摇杆电位器 |
| CN114156028B (zh) * | 2021-10-26 | 2023-11-14 | 东莞福哥电子有限公司 | 一种回弹力可调的摇杆电位器 |
| CN118466280A (zh) * | 2024-04-28 | 2024-08-09 | 广东控银实业有限公司 | 电容摇杆装置和遥控器 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106297247B (zh) | 2020-05-12 |
| CN106297247A (zh) | 2017-01-04 |
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