首页> 外国专利> For the propeller blade streamlined a high performance multi-blade propeller streamlined provided with such blades and arrangement of the tail rotor a helix for a rotary wing streamlined 371

For the propeller blade streamlined a high performance multi-blade propeller streamlined provided with such blades and arrangement of the tail rotor a helix for a rotary wing streamlined 371

机译:对于螺旋桨叶片流线型的高性能多叶片螺旋桨流线型,配备有此类叶片和尾部旋翼的布置,旋翼的螺旋线流线型371

摘要

Blade for shrouded propeller. / p & & p & according to the invention, this blade is characterized: - in that, in a plane, its aerodynamically active part has a rectangular shape; and - in that: / p & & p & gt. the maximal camber of the successive profiles constituting the active transport of the blade increases to a value close to 0 to a value close to 0,04; / p & & p & gt. — v of the cowling portion of the active blade decreases from a first value of about 12degre (s) to a second value close to 4degre (s), and then increases up to a third value close to 4,5degre (s); and / p & & p & gt. the relative maximum thickness of said successive profiles decreases to a value close to 13,5% to a value close to 9,5% / p & & p & embodiment of the faired propellers with high performance and in particular arrangement of the tail rotor for rotary wing aircraft.
机译:螺旋桨叶片。 & &根据本发明,该叶片的特征在于:-在平面上,其空气动力作用部分具有矩形形状;和-在于: & & —主动叶片的整流罩部分的v从大约12度的第一值减小到接近4度的第二值,然后增加到接近4度的第三值。和 & &所述连续轮廓的相对最大厚度减小到接近13.5%的值到接近9.5%的值。 & &具有高性能的整流罩螺旋桨的实施例,特别是用于旋转翼飞机的尾旋翼的布置。

著录项

  • 公开/公告号FR2628062B1

    专利类型

  • 公开/公告日1990-08-10

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE STE NATIONALE INDLE;

    申请/专利号FR19880002873

  • 发明设计人 ALAIN ERIC VUILLET;

    申请日1988-03-07

  • 分类号B64C11/18;

  • 国家 FR

  • 入库时间 2022-08-22 06:09:31

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