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WING STRUCTURE WITH SELF-INDUCED CAMBER

机译:机翼结构自感应弯度

摘要

ABSTRACT OF THE DISCLOSUREAn improved wing structure is provided having a self-inducedcamber. The wing comprises an aerodynamic dihedral sailstructure having a fabric sail tensioned on a supporting framecomprised of lateral brace members and a longitudinal memberintermediate the ends of the lateral braces. The tensioning ofthe sail and the configuration of the supporting frame is suchthat the sail assumes a dihedral shape, with the sail beingcaused to assume a tensioned or stressed condition along aportion of the leading edge of the sail intermediate therespective lateral ends of the sail resulting in the formation ofa self-induced camber at that location.-1-
机译:披露摘要提供了一种具有自感应的改进的机翼结构外倾机翼包括空气动力二面帆具有在支撑框架上张紧的织物风帆的结构由侧向支撑构件和纵向构件组成在侧支架的两端之间。张紧帆和支撑架的配置是这样的帆呈二面角的形状,导致沿着风帆前缘中间的部分帆的各个横向端导致形成该位置处的自生弧度。-1-

著录项

  • 公开/公告号CA1257856A

    专利类型

  • 公开/公告日1989-07-25

    原文格式PDF

  • 申请/专利权人 CROWELL ROBERT L.;

    申请/专利号CA19870552795

  • 发明设计人 CROWELL ROBERT L.;

    申请日1987-11-25

  • 分类号B64C3/22;B64C31/06;

  • 国家 CA

  • 入库时间 2022-08-22 06:36:18

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