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WING FOR CREATING LIFT FORCES FROM A MULTI FLOW

机译:从多重流动中提升提升力的翅膀

摘要

The invention relates to a wing for generating a lifting force that has a trailing edge, a leading edge, an inner edge, an outer edge, an upper surface and a lower surface. The wing has a chord profile and a span direction. The leading edge includes a kink between the inner edge and the outer edge. The leading edge includes a reverse swept portion between the inner edge and the fracture, leading to the fracture, forming an angle with the direction of the span. The leading edge includes a straight swept portion between the kink and the outer edge, extending from the kink, forming an angle with the direction of the span. The upper surface has flow control means for controlling the lifting force, which are at least partially located between the leading and trailing edges behind the portion of the leading edge located between the kink and the outer edge.
机译:本发明涉及一种用于产生升力的机翼,该机翼具有后缘,前缘,内缘,外缘,上表面和下表面。机翼具有和弦轮廓和跨度方向。前缘包括在内边缘和外边缘之间的纽结。前缘包括在内边缘和裂缝之间的反向扫掠部分,其导致裂缝,与跨度的方向形成角度。前缘包括在扭结和外边缘之间的直的扫掠部分,该笔直的扫掠部分从扭结延伸,与跨度的方向形成角度。上表面具有用于控制提升力的流量控制装置,该流量控制装置至少部分地位于前缘和后缘之间,位于位于扭结和外缘之间的前缘部分的后面。

著录项

  • 公开/公告号EA201291027A1

    专利类型

  • 公开/公告日2013-04-30

    原文格式PDF

  • 申请/专利权人 Б.В. ГРИН ЭКС;

    申请/专利号EA20120091027

  • 发明设计人 РОБЕРТ ЯН;

    申请日2011-04-14

  • 分类号B64C3/10;B64C23;

  • 国家 EA

  • 入库时间 2022-08-21 16:41:48

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