首页> 外国专利> MITIGATION OF SURFACE DISCONTINUITIES BETWEEN FLIGHT CONTROL SURFACES AND AN AIRFRAME OF AN AIRCRAFT

MITIGATION OF SURFACE DISCONTINUITIES BETWEEN FLIGHT CONTROL SURFACES AND AN AIRFRAME OF AN AIRCRAFT

机译:飞机飞行控制面与飞机机体之间表面不连续性的缓解

摘要

Embodiments provide a transitional element that bridges a gap between an edgeof a flightcontrol surface and an edge of a non-movable portion of an airframe. In oneembodiment, atransitional element bridges a gap between an edge of a flight control surfaceand an edge ofa non-movable portion of an airframe. The transitional element includes aplurality of ribsthat span the gap. Each of the plurality of ribs has a contour thatcorresponds to the flightcontrol surface and is configured to pivot a portion of a rotated angle of theflight controlsurface to generate a transitional surface across the gap.
机译:实施例提供了过渡元件,其过渡了边缘之间的间隙。一次飞行控制面和机身不可移动部分的边缘。合而为一实施例,一个过渡元件弥合了飞行控制面边缘之间的间隙和一个边缘机身的不可移动部分。过渡元素包括多个肋骨跨越差距。多个肋中的每一个具有的轮廓对应航班控制表面,并配置为使飞行控制表面产生跨间隙的过渡表面。

著录项

  • 公开/公告号CA2935181A1

    专利类型

  • 公开/公告日2017-02-20

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号CA20162935181

  • 发明设计人 LOYET JESSICA;PITT DALE M.;

    申请日2016-07-05

  • 分类号B64C9;B64C3/18;B64C3/38;B64C9/02;

  • 国家 CA

  • 入库时间 2022-08-21 13:34:38

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