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Double decker wing for aircraft - has upper and lower surfaces connected by vertical ribs

机译:飞机双层机翼-上下表面通过垂直肋连接

摘要

The double decker or biplane wing is for an aircraft. The upper and lower surfaces of the wing form part of a common aerofoil contour. The two surface (2,3) are connected to each other by a number of vertical ribs which extend from the leading edge to the trailing edge. The leading edge of the upper surface(2) projects beyond the leading edge of the lower surface (1) by an angle of 55 deg. The trailing edge of the lower surface (1) projects beyond the trailing edge of the upper surface by an angle of 45 deg. USE/ADVANTAGE - Increased lift with consequent shorter take-off for the aircraft.
机译:双层或双翼机翼用于飞机。机翼的上表面和下表面形成共同的机翼轮廓的一部分。这两个表面(2,3)通过许多从前缘延伸到后缘的垂直肋相互连接。上表面(2)的前缘伸出下表面(1)的前缘超过55度。下表面(1)的后缘突出超过上表面的后缘45度。使用/优势-增加升力,从而缩短飞机起飞时间。

著录项

  • 公开/公告号DE3917973A1

    专利类型

  • 公开/公告日1990-12-06

    原文格式PDF

  • 申请/专利权人 HORVATH ISTVAN 6482 BAD ORB DE;

    申请/专利号DE19893917973

  • 发明设计人 HORVATH ISTVAN 6482 BAD ORB DE;

    申请日1989-06-02

  • 分类号B64C3/00;

  • 国家 DE

  • 入库时间 2022-08-22 05:49:36

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