首页> 外国专利> AERODYNAMIC FAIRING OF THE FLANGE TO DRAINAGE DUCT (S) ON AIRCRAFT JET SUSPENSION PYLON

AERODYNAMIC FAIRING OF THE FLANGE TO DRAINAGE DUCT (S) ON AIRCRAFT JET SUSPENSION PYLON

机译:飞机射流悬挂塔上法兰对排水管道的气动动力学特性

摘要

The streamlining of the flange (5) of the drainage ducts (6) on the suspension pylon (2) of an aircraft engine comprises an aerodynamically shaped body. The rear face of the flange is not shaped and is transverse to the drainage duct in the direction of air flow along the pylon. The aerodynamic body which is fitted on the rear of the flange has a front face (9a) of complementary shape to that of the flange rear face. The body is tapered towards the rear between two lateral faces which join at the trailing edge of the body and extend the flange lateral faces from its front face. The body has a longitudinal bore (11) emerging in its front face and housing part of the rear end of the drainage duct.
机译:飞机发动机的悬挂吊架(2)上的排水管(6)的凸缘(5)的流线型包括空气动力学成形的主体。法兰的背面未定形,并且在沿塔架的气流方向上垂直于排水管。装配在凸缘后部上的空气动力学本体具有与凸缘后表面互补的形状的前表面(9a)。主体在两个侧面之间向后逐渐变细,两个侧面在主体的后缘处接合,并从其正面延伸凸缘侧面。该主体在其前表面和排水管后端的外壳部分中露出一个纵向孔(11)。

著录项

  • 公开/公告号FR2735444B3

    专利类型

  • 公开/公告日1997-05-09

    原文格式PDF

  • 申请/专利权人 MAIER SIMON;

    申请/专利号FR19960006748

  • 发明设计人

    申请日1996-05-31

  • 分类号B64D29/00;B64C23/00;

  • 国家 FR

  • 入库时间 2022-08-22 03:12:18

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