WO2017181492A1 - 一种扰流板手柄 - Google Patents

一种扰流板手柄 Download PDF

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Publication number
WO2017181492A1
WO2017181492A1 PCT/CN2016/084148 CN2016084148W WO2017181492A1 WO 2017181492 A1 WO2017181492 A1 WO 2017181492A1 CN 2016084148 W CN2016084148 W CN 2016084148W WO 2017181492 A1 WO2017181492 A1 WO 2017181492A1
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WO
WIPO (PCT)
Prior art keywords
handle
rotating shaft
hole
spoiler
vertical plate
Prior art date
Application number
PCT/CN2016/084148
Other languages
English (en)
French (fr)
Inventor
吴晶
吴斌
Original Assignee
成都艾尔伯特科技有限责任公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication of WO2017181492A1 publication Critical patent/WO2017181492A1/zh

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Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
    • G06F3/01—Input arrangements or combined input and output arrangements for interaction between user and computer
    • G06F3/03—Arrangements for converting the position or the displacement of a member into a coded form
    • G06F3/033—Pointing devices displaced or positioned by the user, e.g. mice, trackballs, pens or joysticks; Accessories therefor
    • G06F3/0338—Pointing devices displaced or positioned by the user, e.g. mice, trackballs, pens or joysticks; Accessories therefor with detection of limited linear or angular displacement of an operating part of the device from a neutral position, e.g. isotonic or isometric joysticks
    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer

Definitions

  • the present invention relates to the technical field of simulating a spoiler handle structure in a flight cockpit system, and more particularly to a spoiler handle.
  • Virtual reality technology is a computer simulation system that can create and experience a virtual world. It uses a computer to generate a simulation environment. It is a multi-source information fusion interactive system simulation of three-dimensional dynamic vision and entity behavior. Immerse yourself in the environment.
  • the simulated flight cockpit system is operated by the cockpit operating system, H
  • the UD system consists of two subsystems, among which the operating system mainly consists of a steering column, an ankle, a throttle lever, a flap control handle, a front wheel turning hand wheel, a top control board, a top control board mounting bracket, a rear electronic board, and a supporting I. 0 acquisition system composition, HUD system is mainly composed of HUD main body, HUD mounting bracket and so on. In the cockpit of the simulated flight, the interior of the cockpit is mainly composed of the operating system and the man-machine interface. The various signals, analog signals and control signals collected on the operating system are mainly handled by the I/O acquisition board. The 1/0 acquisition board is connected to the I/O computer, and then the relevant data is sent to other processing systems via Ethernet. The internal system data exchange relationship of the cockpit frame component is shown in Fig. 1.
  • the spoiler handle in the operating system is used to detect the corresponding position information of the handle and send the collected signal to the I/O computer.
  • the existing spoiler handle has a complicated structure and is expensive to manufacture, and cannot detect the corresponding position information of the handle, and the handle is easy to fall under the action of no external force.
  • the object of the present invention is to overcome the shortcomings of the prior art, and to provide a spoiler handle that is compact in structure, avoids the phenomenon that the handle is tilted under the action of no external force, can realize the position information of the detection handle, and is simple to operate.
  • a spoiler handle comprising a handle, an encoder, a base, a platform disposed above the base, and a vertical plate disposed perpendicular to the platform, Vertical board
  • the lower end portion is rotatably mounted with a rotating shaft, and the rotating shaft is disposed through the vertical plate.
  • the front end surface of the vertical plate is uniformly distributed with a plurality of limiting slots around the rotating shaft.
  • the limiting groove is disposed above the rotating shaft, and the lower end portion of the handle is fixed on the rotating shaft.
  • a through hole A is arranged in the middle of the handle, a cylinder is inserted into the through hole A, a baffle is arranged on the rear end surface of the handle, and a through hole B communicating with the through hole A is disposed on the baffle, and the inside of the cylinder is provided with a spring, one end of the spring is fixed to the bottom of the cylinder, the other end of the spring is fixed with a ball, the ball is disposed in the through hole B, the ball is in contact with the vertical plate, and the synchronous pulley A is mounted on the rotating shaft, the input of the encoder A timing pulley B is mounted on the shaft, and a timing belt is installed between the timing pulley A and the timing pulley B.
  • the upper end of the handle is provided with a handle.
  • the encoder is fixedly mounted on the base.
  • a plurality of uprights are disposed between the base and the platform.
  • the timing belt is disposed through the platform.
  • the lower end portion of the handle is fixed to the front end portion of the rotating shaft, and the timing pulley A is attached to the rear end portion of the rotating shaft.
  • the present invention has the following advantages:
  • the present invention has a compact structure, avoids the phenomenon that the handle is tilted without external force, can realize the position information of the detection handle, and is simple to operate.
  • FIG. 1 is an internal system data exchange relationship of a cockpit frame assembly
  • Figure 3 is a rear elevational view of the present invention.
  • FIG. 4 is a schematic view showing a connection structure of a ball and a handle according to the present invention.
  • Figure 5 is a full cross-sectional view of Figure 4.
  • a spoiler handle includes a handle 1, an encoder 2, a base 3, a platform 4 disposed above the base 3, and a vertical plate 5 disposed perpendicular to the platform 4.
  • a plurality of uprights 18 are disposed between the base 3 and the platform 4, and the lower end of the vertical plate 5 is rotatably mounted with a rotating shaft 6, and the rotating shaft 6 is disposed through the vertical plate 5, and the front end surface of the vertical plate 5 is wound around the rotating shaft 6
  • a plurality of limiting slots 7 are evenly distributed for the center of the circle.
  • the limiting slot 7 has a hemispherical shape.
  • the limiting slot 7 is disposed above the rotating shaft 6, and the lower end of the handle 1 is fixed to the rotating shaft 6.
  • a middle portion of the handle 1 is provided with a through hole A8, a through hole A8 is inserted into the cylindrical body 9, and a rear end surface of the handle 1 is provided with a baffle 10, and the baffle 10 is provided with a communication.
  • a through hole B1 l of the through hole A8, a spring 12 is disposed in the cylindrical body 9, one end of the spring 12 is fixed to the bottom of the cylindrical body 9, the other end of the spring 12 is fixed with a ball 13, and the ball 13 is disposed at the through hole B11 Inside, the ball 13 is in contact with the vertical plate 5, and the spring 12 is in a compressed state.
  • the rotating shaft 6 is mounted with a timing pulley A14, and the encoder 2 is fixedly mounted on the base 3, and the input pulley of the encoder 2 is mounted with a timing pulley B15, a synchronous pulley A14 and synchronization.
  • a timing belt 16 is mounted between the pulleys B15, and the timing belt 16 is disposed through the platform 4.
  • the upper end portion of the handle 1 is provided with a handlebar 1; the lower end portion of the handle 1 is fixed to the front end portion of the rotating shaft 6, and the timing pulley A14 is attached to the rear end portion of the rotating shaft 6.
  • the working process of the present invention is as follows: In the flight simulation, the user rotates the handle 1 by hand, the handle 1 drives the rotating shaft 6 to rotate, the rotating shaft 6 drives the synchronous pulley A14 to rotate, and the synchronous pulley A14 drives the synchronous belt through the synchronous belt 16
  • the wheel B15 rotates
  • the timing pulley B15 drives the input shaft of the encoder 2 to rotate
  • the encoder 2 captures the position information of the handle 1
  • the encoder 2 transmits the position information of the handle 1 to the I/O computer, thereby realizing the actual detection handle 1 location information.
  • the handle 1 is rotated again, and the ball 13 on the handle 1 is slid into the limiting slot 7. Under the action of the spring restoring force, the ball 13 is pressed against the limiting slot 7, thereby realizing
  • the positioning of the handle 1 means that the handle 1 will not fall off after the hand is released, which is convenient for the user to operate.

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  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Human Computer Interaction (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Educational Administration (AREA)
  • Educational Technology (AREA)
  • Mechanical Control Devices (AREA)
  • Steering Devices For Bicycles And Motorcycles (AREA)

Abstract

一种扰流板手柄，它包括手柄（1）、编码器（2）、机座（3）、设置于机座（3）上方的平台（4）以及垂直于平台（4）设置的立板（5），限位槽（7）设置于转轴（6）的上方，手柄（1）的下端部固定于转轴（6）上，通孔A（8）内插装有筒体（9），手柄（1）的后端面设置有挡板（10），挡板（10）上设置有连通通孔A（8）的通孔B（11），弹簧（12）的另一端固定有滚珠（13），滚珠（13）设置于通孔B（11）内，滚珠（13）与立板（5）接触，同步带轮A（14）和同步带轮B（15）之间安装有同步带（16）。所述扰流板手柄结构紧凑、避免了手柄在没有外力作用下出现倾倒的现象、能够实现检测手柄位置信息。

Description

一种扰流板手柄
技术领域
[0001] 本发明涉及模拟飞行座舱系统中扰流板手柄结构的技术领域， 特别是一种扰流 板手柄。
背景技术
[0002] 虚拟现实技术是一种可以创建和体验虚拟世界的计算机仿真系统它利用计算机 生成一种模拟环境是一种多源信息融合的交互式的三维动态视景和实体行为的 系统仿真使用户沉浸到该环境中。 目前， 模拟飞行座舱系统由座舱操作系统、 H
UD系统两个子系统组成， 其中操作系统主要由驾驶杆、 脚蹬、 油门操纵杆、 襟 翼操纵手柄、 前轮转弯手轮、 顶控板、 顶控板安装支架、 后电子板以及配套的 I 0采集系统组成， HUD系统主要由 HUD主体、 HUD安装支架等组成。 而在模拟 飞行的座舱内， 座舱的内部主要由操作系统和人机操作界面组成， 在操作系统 上采集的各种幵关信号、 模拟信号和控制信号主要由 I/O采集板卡负责处理， 而 1/ 0采集板卡又与 I/O计算机连接， 然后通过以太网把相关数据发送给其它处理系 统， 座舱机架组件内部系统数据交换关系如图 1所示。
[0003] 操作系统中的扰流板手柄用于检测手柄的相应位置信息， 并将采集的信号实吋 发送到 I/O计算机。 然而现有的扰流板手柄结构复杂， 造价昂贵， 不能够实吋检 测手柄相应位置信息， 此外手柄在没有外力把持的作用下容易倾倒。
技术问题
[0004] 本发明的目的在于克服现有技术的缺点， 提供一种结构紧凑、 避免了手柄在没 有外力作用下出现倾倒的现象、 能够实现检测手柄位置信息、 操作简单的扰流 板手柄。
问题的解决方案
技术解决方案
[0005] 本发明的目的通过以下技术方案来实现： 一种扰流板手柄， 它包括手柄、 编码 器、 机座、 设置于机座上方的平台以及垂直于平台设置的立板， 所述的立板的 下端部旋转安装有转轴， 转轴贯穿立板设置， 立板的前端面上且绕转轴为圆心 均匀分布有多个限位槽， 限位槽设置于转轴的上方， 手柄的下端部固定于转轴 上， 手柄的中部设置有通孔 A， 通孔 A内插装有筒体， 手柄的后端面设置有挡板 ， 挡板上设置有连通通孔 A的通孔 B， 所述的筒体内设置有弹簧， 弹簧的一端固 定于筒体的底部， 弹簧的另一端固定有滚珠， 滚珠设置于通孔 B内， 滚珠与立板 接触， 所述的转轴上安装有同步带轮 A， 编码器的输入轴上安装有同步带轮 B， 同步带轮 A和同步带轮 B之间安装有同步带。
[0006] 所述的手柄的上端部设置有手把。
[0007] 所述的编码器固定安装于机座上。
[0008] 所述的机座与平台之间设置有多根立柱。
[0009] 所述的同步带贯穿平台设置。
[0010] 所述的手柄的下端部固定于转轴的前端部， 所述的同步带轮 A安装于转轴的后 端部。
发明的有益效果
有益效果
[0011] 本发明具有以下优点： 本发明结构紧凑、 避免了手柄在没有外力作用下出现倾 倒的现象、 能够实现检测手柄位置信息、 操作简单。
对附图的简要说明
附图说明
[0012] 图 1为座舱机架组件内部系统数据交换关系；
[0013] 图 2为本发明的主视图；
[0014] 图 3为本发明的后视图；
[0015] 图 4为本发明的滚珠与手柄的连接结构示意图；
[0016] 图 5为图 4的全剖视图；
[0017] 图中， 1-手柄， 2-编码器， 3-机座， 4-平台， 5-立板， 6-转轴， 7-限位槽， 8-通 孔 A， 9-筒体， 10-挡板， 11-通孔 B， 12-弹簧， 13-滚珠， 14-同步带轮 A， 15-同步 带轮 B， 16-同步带， 17-手把， 18-立柱。 本发明的实施方式
[0018] 下面结合附图对本发明做进一步的描述， 本发明的保护范围不局限于以下所述
[0019] 如图 2-5所示， 一种扰流板手柄， 它包括手柄 1、 编码器 2、 机座 3、 设置于机座 3上方的平台 4以及垂直于平台 4设置的立板 5， 机座 3与平台 4之间设置有多根立 柱 18， 所述的立板 5的下端部旋转安装有转轴 6， 转轴 6贯穿立板 5设置， 立板 5的 前端面上且绕转轴 6为圆心均匀分布有多个限位槽 7， 限位槽 7呈半球形状， 限位 槽 7设置于转轴 6的上方， 手柄 1的下端部固定于转轴 6上。
[0020] 如图 2-5所示， 手柄 1的中部设置有通孔 A8， 通孔 A8内插装有筒体 9， 手柄 1的 后端面设置有挡板 10， 挡板 10上设置有连通通孔 A8的通孔 Bl l， 所述的筒体 9内 设置有弹簧 12， 弹簧 12的一端固定于筒体 9的底部， 弹簧 12的另一端固定有滚珠 13， 滚珠 13设置于通孔 B11内， 滚珠 13与立板 5接触， 弹簧 12处于压缩状态。 如 图 2和图 3所示， 转轴 6上安装有同步带轮 A14， 编码器 2固定安装于机座 3上， 编 码器 2的输入轴上安装有同步带轮 B15， 同步带轮 A14和同步带轮 B15之间安装有 同步带 16， 同步带 16贯穿平台 4设置。
[0021] 所述的手柄 1的上端部设置有手把 1 ; 所述的手柄 1的下端部固定于转轴 6的前端 部， 所述的同步带轮 A14安装于转轴 6的后端部。
[0022] 本发明的工作过程如下： 在进行飞行模拟吋， 用户经手把转动手柄 1， 手柄 1带 动转轴 6转动， 转轴 6带动同步带轮 A14转动， 同步带轮 A14经同步带 16带动同步 带轮 B15转动， 同步带轮 B15带动编码器 2的输入轴转动， 编码器 2采集手柄 1位置 信息， 编码器 2并将手柄 1位置信息传递给 I/O计算机， 从而实现了实吋检测手柄 1 位置信息。 当要搁置手柄 1吋， 只需再次转动手柄 1， 使手柄 1上的滚珠 13滑入限 位槽 7内， 在弹簧恢复力的作用下， 滚珠 13抵压于限位槽 7内， 从而实现了手柄 1 的定位， 即吋松手后手柄 1也不会脱落， 方便用户的操作。
[0023] 以上所述仅是本发明的优选实施方式， 应当理解本发明并非局限于本文所披露 的形式， 不应看作是对其他实施例的排除， 而可用于各种其他组合、 修改和环 境， 并能够在本文所述构想范围内， 通过上述教导或相关领域的技术或知识进 行改动。 而本领域人员所进行的改动和变化不脱离本发明的精神和范围， 则都 应在本发明所附权利要求的保护范围内。

Claims

权利要求书
一种扰流板手柄， 其特征在于： 它包括手柄 （1) 、 编码器 （2) 、 机 座 （3) 、 设置于机座 （3) 上方的平台 （4) 以及垂直于平台 （4) 设 置的立板 （5) ， 所述的立板 （5) 的下端部旋转安装有转轴 （6) ， 转轴 （6) 贯穿立板 （5) 设置， 立板 （5) 的前端面上且绕转轴 （6) 为圆心均匀分布有多个限位槽 （7) ， 限位槽 （7) 设置于转轴 （6) 的上方， 手柄 （1) 的下端部固定于转轴 （6) 上， 手柄 （1) 的中部 设置有通孔 A (8) ， 通孔 A (8) 内插装有筒体 （9) ， 手柄 （1) 的 后端面设置有挡板 （10) ， 挡板 （10) 上设置有连通通孔 A (8) 的 通孔 B (11) ， 所述的筒体 （9) 内设置有弹簧 （12) ， 弹簧 （12) 的一端固定于筒体 （9) 的底部， 弹簧 （12) 的另一端固定有滚珠 （1 3) ， 滚珠 （13) 设置于通孔 B (11) 内， 滚珠 （13) 与立板 （5) 接 触， 所述的转轴 （6) 上安装有同步带轮 A (14) ， 编码器 （2) 的输 入轴上安装有同步带轮 B (15) ， 同步带轮 A (14) 和同步带轮 B (15 ) 之间安装有同步带 （16) 。
根据权利要求 1所述的一种扰流板手柄， 其特征在于： 所述的手柄 （1 ) 的上端部设置有手把 （17) 。
根据权利要求 1所述的一种扰流板手柄， 其特征在于： 所述的编码器
(2) 固定安装于机座 （3) 上。
根据权利要求 1所述的一种扰流板手柄， 其特征在于： 所述的机座 （3 ) 与平台 （4) 之间设置有多根立柱 （18) 。
根据权利要求 1所述的一种扰流板手柄， 其特征在于： 所述的同步带
(16) 贯穿平台 （4) 设置。
根据权利要求 1所述的一种扰流板手柄， 其特征在于： 所述的手柄 （1 ) 的下端部固定于转轴 （6) 的前端部， 所述的同步带轮 A (14) 安 装于转轴 （6) 的后端部。
PCT/CN2016/084148 2016-04-20 2016-05-31 一种扰流板手柄 WO2017181492A1 (zh)

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CN201620331744.6 2016-04-20

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2424457Y (zh) * 2000-04-21 2001-03-21 陈德才 操纵杆位置检测装置
US20120187940A1 (en) * 2009-11-20 2012-07-26 Ecs Engineered Control Systems Ag Device for detecting the position of a shift and/or selector lever for a transmission and shift device for the transmission of a motor vehicle
CN103794104A (zh) * 2012-12-03 2014-05-14 天津工业大学 飞行模拟机自动油门系统
CN105160961A (zh) * 2015-09-29 2015-12-16 哈尔滨莱特兄弟科技开发有限公司 仿真飞机起落架模拟装置

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2424457Y (zh) * 2000-04-21 2001-03-21 陈德才 操纵杆位置检测装置
US20120187940A1 (en) * 2009-11-20 2012-07-26 Ecs Engineered Control Systems Ag Device for detecting the position of a shift and/or selector lever for a transmission and shift device for the transmission of a motor vehicle
CN103794104A (zh) * 2012-12-03 2014-05-14 天津工业大学 飞行模拟机自动油门系统
CN105160961A (zh) * 2015-09-29 2015-12-16 哈尔滨莱特兄弟科技开发有限公司 仿真飞机起落架模拟装置

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