首页> 外国专利> Dual cam control mechanism for coordinated deployment and retraction of an air-craft's leading and trailing edge wing flaps

Dual cam control mechanism for coordinated deployment and retraction of an air-craft's leading and trailing edge wing flaps

机译:双凸轮控制机构可协调部署和收回飞机的前缘和后缘机翼襟翼

摘要

In the disclosed mechanism a primary position control cam has first and second camming surfaces for cooperating with separate followers that in turn act through a hydraulic subsystem to position the leading and trailing edge wing flaps in response to a single, pilot operated control lever. A secondary cam also having first and second camming surfaces correspondingly shaped to those of the primary cam, is slaved to the actual, hydraulically effected movement of the trailing edge flaps. Cooperating with the first surface of the secondary cam is a feedback follower for providing a mechanical feedback signal that assists the primary cam and the associated hydraulics in positioning the trailing edge flaps. An override follower cooperates with the second camming surface on the secondary cam and mechanically overrides the ability of the primary cam's second surface follower to position the leading edge flaps under certain conditions, so as to ensure a predetermined, aerodynamically critical sequencing of the hydraulically effected movements of the leading and trailing edge flaps as they seek the positions commanded by the single, pilot operated lever.
机译:在公开的机构中,主位置控制凸轮具有第一凸轮表面和第二凸轮表面,用于与单独的从动件配合,所述从动件又通过液压子系统起作用,以响应于单个飞行员操作的控制杆来定位前缘和后缘机翼襟翼。辅助凸轮也具有对应于主凸轮的形状的第一和第二凸轮表面,该从动凸轮是由后缘襟翼的实际液压作用引起的。反馈从动件与辅助凸轮的第一表面配合,用于提供机械反馈信号,该信号有助于主凸轮和相关的液压装置定位后缘襟翼。超驰从动件与辅助凸轮上的第二凸轮表面协作,并在一定条件下机械地超越主凸轮的第二从动件定位前缘襟翼的能力,从而确保对液压影响的运动进行预定的,对空气动力学至关重要的排序前缘和后缘襟翼寻找单个飞行员操纵杆所指示的位置时的位置。

著录项

  • 公开/公告号US4244541A

    专利类型

  • 公开/公告日1981-01-13

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US19790000064

  • 发明设计人 RUPERT I. DORN;

    申请日1979-01-02

  • 分类号B64C13/32;

  • 国家 US

  • 入库时间 2022-08-22 14:50:21

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