首页> 外国专利> fahrzeugsteuerungssystem and procedures using a steuerflu00e4che and hilfssteuerflu00e4che with translation

fahrzeugsteuerungssystem and procedures using a steuerflu00e4che and hilfssteuerflu00e4che with translation

机译:使用税区和辅助控制区并进行翻译的车辆控制系统和程序

摘要

Control systems and methods for a vehicle such as an aircraft or watercraft employ a trailing edge control surface that is pivotal about a pivot axis fixed relative to the vehicle and is deflected to create control forces, and a tab pivotally mounted to an aft end of the control surface. An aft end of a linkage is connected to the tab spaced from the tab pivot axis, and the linkage extends forward to a forward end that is coupled to fixed vehicle structure, such that deflection of the control surface causes a deflection of the tab as long as the forward end of the linkage does not lie in line with the control surface pivot axis, the in-line position defining a neutral position of the linkage. A gearing control actuator is coupled to the linkage and is operable to position the forward end of the linkage at selectively variable distances on one or the other side of the neutral position, thus providing variable gearing ratios between the control surface and the tab. Tab gearing ratio can be varied as a function of vehicle operating condition. An alternative control system includes a backup tab actuator for providing tab deflection upon failure of the actuator system that deflects the control surface. The tab can be used as a control tab for providing the motive force for moving the control surface, or the tab can be used as a mini control surface by locking the control surface in a fixed position.
机译:用于诸如飞机或水上飞机的车辆的控制系统和方法采用后缘控制表面,该后缘控制表面绕相对于车辆固定的枢转轴线枢转并且被偏转以产生控制力,并且翼片枢转地安装至发动机的后端。控制面。连杆机构的后端连接到与凸舌枢转轴线间隔开的凸舌,并且连杆向前延伸到与固定车辆结构相连的前端,这样控制面的挠曲会导致凸舌偏向因为联动装置的前端不与控制表面枢转轴线成一直线,所以直列位置限定联动装置的中性位置。齿轮控制致动器联接到连杆,并且可操作以将连杆的前端定位在空档位置的一侧或另一侧上的选择性可变距离处,从而在控制表面和凸片之间提供可变的传动比。翼片传动比可以根据车辆的运行状况而变化。一种可选的控制系统包括备用翼片致动器,用于在致动器系统发生故障时使翼片偏转,该致动器系统使控制表面偏转。所述凸片可以用作控制凸片,以提供用于移动所述控制表面的原动力,或者所述凸片可以通过将所述控制表面锁定在固定位置而用作微型控制表面。

著录项

  • 公开/公告号DE60023896D1

    专利类型

  • 公开/公告日2005-12-15

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY SEATTLE;

    申请/专利号DE2000623896T

  • 发明设计人 BRISLAWN G.;

    申请日2000-07-05

  • 分类号B64C9/04;B64C9/10;B63H25/38;

  • 国家 DE

  • 入库时间 2022-08-21 21:19:07

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