首页> 外国专利> FUSELAGE PROFILES, WINGS, AIRLINES OF AIRCRAFT CAPABLE TO TRAP AND ATTACH STABILIZED AIR VOLUMES AND ISOLATIONS OF FLOW THROUGH THE FORCES OF THE FIELD

FUSELAGE PROFILES, WINGS, AIRLINES OF AIRCRAFT CAPABLE TO TRAP AND ATTACH STABILIZED AIR VOLUMES AND ISOLATIONS OF FLOW THROUGH THE FORCES OF THE FIELD

机译:机身外形,机翼,可捕捉和附着稳定气流的飞机的机翼,以及通过场力的流动隔离

摘要

A design for the shapes of leading and trailing surfaces of an aircraft fuselage (1), wings or fins makes use of surfaces (2, 3) which trap and annexe volumes of air to produce turbulence at a rate four times greater than that of existing shapes. The leading or trailing surfaces are truncated to produce planes lying perpendicular to the air flow and having concave surfaces which deflect air forwards to form a wedge (V/2) of air ahead of the surface.
机译:飞机机身(1)的前,后表面,机翼或鳍片的形状设计利用表面(2、3)捕获并吞并大量的空气,从而以比现有飞机大四倍的速度产生湍流形状。前表面或后表面被截断以产生垂直于气流的平面,并具有凹入表面,该凹入表面使空气向前偏转以在表面之前形成空气的楔形(V / 2)。

著录项

  • 公开/公告号FR2794718B3

    专利类型

  • 公开/公告日2001-08-17

    原文格式PDF

  • 申请/专利权人 BUTTAZZONI GINO;

    申请/专利号FR19990007470

  • 发明设计人 BUTTAZZONI GINO;

    申请日1999-06-10

  • 分类号B64C23/00;

  • 国家 FR

  • 入库时间 2022-08-22 01:07:57

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