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AIRCRAFT APPLIED APPLICATION SYSTEMS AND CORRESPONDING METHODS

机译:飞机应用的应用系统及方法

摘要

Aerospace vehicle fairing systems and associated methods, including fairings that house flap surface drive mechanisms on aircraft, are disclosed herein. One aspect of the invention is directed toward a fairing system that includes a fairing mounted to an airfoil. The fairing can have a longitudinal axis and a fairing section extending along the longitudinal axis forward and aft of a trailing edge portion of an airfoil section. In one embodiment of the invention, the fairing section can have a wide portion located aft of the airfoil section with a single spanwise width that is greater than or equal to a spanwise width of any other portion of the fairing section. In another embodiment of the invention the fairing section can have a first side and a second side, each with a point of maximum curvature. At least one point of maximum curvature can be located aft of the airfoil section.
机译:本文公开了航空飞行器整流罩系统和相关方法,包括在飞机上容纳襟翼表面驱动机构的整流罩。本发明的一个方面针对一种整流罩系统,其包括安装在机翼上的整流罩。整流罩可具有纵轴和沿纵轴在机翼部分的后缘部分的后部前后延伸的整流器部分。在本发明的一个实施例中,整流罩部分可以具有位于机翼部分后方的较宽部分,其具有单个展向宽度,该单一展向宽度大于或等于整流罩部分的任何其他部分的展向宽度。在本发明的另一个实施例中,整流罩部分可以具有第一侧面和第二侧面,每个侧面具有最大弯曲点。最大曲率的至少一个点可以位于翼型部分的后部。

著录项

  • 公开/公告号AT442986T

    专利类型

  • 公开/公告日2009-10-15

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号AT20060758661T

  • 发明设计人 VOOGT NICOLAAS;

    申请日2006-04-26

  • 分类号B64C9/16;B64C7;

  • 国家 AT

  • 入库时间 2022-08-21 19:24:16

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