首页> 外国专利> Flow channel for e.g. aircraft engine, has slat whose floating bearing is adjusted under elastic deformation of slats in radial direction to extent and/or axial direction of flow channel relative to fixed wall portion

Flow channel for e.g. aircraft engine, has slat whose floating bearing is adjusted under elastic deformation of slats in radial direction to extent and/or axial direction of flow channel relative to fixed wall portion

机译:例如的流道飞机发动机具有板条,该板条的浮动轴承在板条沿径向方向弹性变形至相对于固定壁部分的流动通道的范围和/或轴向方向上进行调节

摘要

The channel (1) has an adjustable wall portion comprising an arrangement of slats (2) that is fixed in a floating bearing (5). The floating bearing is adjusted relative to a fixed wall portion (4) of the flow channel. The floating bearing of the slats is adjusted under elastic deformation of the slats in radial direction (R) to extent and/or axial directions, of the flow channel relative to the fixed wall portion. The floating bearing is arranged in upstream or downstream of a fixed bearing (3A). The slats are made of steel and/or fiber-reinforced plastic.
机译:通道(1)具有可调节的壁部分,该壁部分包括固定在浮动轴承(5)中的板条(2)的布置。浮动轴承相对于流动通道的固定壁部分(4)被调节。板条的浮动轴承在板条沿径向(R)的弹性变形下相对于固定壁部分在流动通道的范围和/或轴向上被调节。浮动轴承布置在固定轴承(3A)的上游或下游。板条由钢和/或纤维增强塑料制成。

著录项

  • 公开/公告号DE102010023998A1

    专利类型

  • 公开/公告日2011-12-22

    原文格式PDF

  • 申请/专利权人 MTU AERO ENGINES GMBH;

    申请/专利号DE20101023998

  • 发明设计人 RAMM GUENTER DR.;

    申请日2010-06-16

  • 分类号F02K1/08;

  • 国家 DE

  • 入库时间 2022-08-21 17:05:32

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