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AN INFLATABLE AERODYNAMIC WING STRUCTURE

机译:充气式气动机翼结构

摘要

An inflatable aerodynamic wing structure comprising an aerodynamic skin, a first inflatable member positioned inside the skin such that it extends longitudinally of the wing structure adjacent a leading edge portion of the wing structure, a second inflatable member positioned inside the skin such that it extends longitudinally of the wing structure adjacent a trailing edge portion of the wing structure, and an inflatable chamber positioned between the first and the second inflatable members, the wing structure being such that the first and the second inflatable members are adapted to be inflated to a higher pressure than the inflatable chamber so that, in use of the wing structure, the first and the second inflatable members provide longitudinal rigidity and the inflatable chamber forms the skin into the aerodynamic shape required by the wing structure, and the inflatable chamber being such that it is inflatable at least primarily by dynamic pressure.
机译:一种可充气的空气动力学机翼结构,包括空气动力学表层;第一可充气构件,其定位在所述表皮内部,使得其沿所述机翼结构的纵向邻近所述机翼结构的前缘部分延伸;第二可充气构件,其定位在所述表皮内部,从而其纵向延伸邻近机翼结构的后缘部分的机翼结构,以及位于第一和第二可充气构件之间的可充气腔室,该机翼结构使得第一和第二可充气构件适于充气至更高的压力因此,在使用机翼结构时,第一和第二可充气部件提供纵向刚度,并且可充气室将皮肤形成为机翼结构所需的空气动力学形状,并且可充气室使得至少主要通过动压充气。

著录项

  • 公开/公告号GB2203113B

    专利类型

  • 公开/公告日1991-03-13

    原文格式PDF

  • 申请/专利权人 BARRY JOHN * JACOBSON;

    申请/专利号GB19880006059

  • 发明设计人 BARRY JOHN * JACOBSON;

    申请日1988-03-15

  • 分类号B64C3/30;B64C31/028;

  • 国家 GB

  • 入库时间 2022-08-22 05:48:13

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