首页> 外国专利> Bypass turbofan engine comprising a nacelle equipped with a translationally-mobile thrust-reversal system and with a fan case equipped with supports

Bypass turbofan engine comprising a nacelle equipped with a translationally-mobile thrust-reversal system and with a fan case equipped with supports

机译:旁路涡手机,包括配备有翻译 - 移动推力逆转系统的机舱和配备有支撑件的风扇盒

摘要

A bypass turbofan engine with a nacelle comprising a fan case and a thrust-reversal system. The fan case comprises an exterior wall, and the reversal system comprises a slider having an upstream frame, a downstream frame and a plurality of spars fixed between the upstream frame and the downstream frame, in which the slider is able to move between a forward position and a retracted position. The fan case comprises, at a rear edge of its exterior wall, a support. Each support comprises, for each spar, a shoe fixed to the exterior wall and positioned radially about the spar, and a skirt secured to the shoes and extending the rear edge, in which, in a forward position, the skirt bears around the downstream frame, and in which in a forward/retracted/intermediate position, the shoes are distant from the spars from the upstream frame.
机译:具有机舱的旁路涡扇发动机,包括风扇壳和推力翻转系统。 风扇盒包括外壁,并且反转系统包括滑块,滑块具有上游框架,下游框架和固定在上游框架和下游框架之间的多个翼梁,其中滑块能够在正向位置之间移动 和缩回的位置。 风扇壳在其外壁的后边缘包括支撑件。 每个支撑件包括固定到外壁上的鞋子并径向地定位在翼梁上,以及固定在鞋子上并延伸后边缘的裙部,其中裙部围绕下游框架围绕下游框架 并且在前进/缩回/中间位置,鞋子远离来自上游框架的翼梁。

著录项

  • 公开/公告号US11136938B2

    专利类型

  • 公开/公告日2021-10-05

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS SAS;

    申请/专利号US201916656632

  • 申请日2019-10-18

  • 分类号F02K1/72;B29C65/70;B29C65/78;B29C65;B29C65/48;B29L31/30;F02K1/54;F02K1/68;

  • 国家 US

  • 入库时间 2022-08-24 21:26:39

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