首页> 外国专利> DUAL FLOW TURBOREACTOR WITH PUSH INVERSION GATES NOT SUBJECT TO THE SECONDARY FLOW IN THEIR INACTIVE POSITION

DUAL FLOW TURBOREACTOR WITH PUSH INVERSION GATES NOT SUBJECT TO THE SECONDARY FLOW IN THEIR INACTIVE POSITION

机译:带有推压换向阀的双流动涡轮机,在其非活动位置上不受二次流动的影响

摘要

P A turbofan (10) with double flow, preferably with separate flow or with a short basket (22), comprises two thrust reversing doors (24) normally received in housings (26) formed in the basket (22 ) and completely located outside of the inner envelope (20) thereof. When a thrust reversal effect is desired, the doors (24) are brought into the extension of the blower channel (16), behind the rear end of the nacelle. Thus, the doors (24) are not subjected to the secondary flow (F2) of the reactor when the airplane is in flight and the interior envelope (20) of the nacelle does not have any leakage or discontinuity and can be completely treated with noise reduction . /P
机译:具有双重流动,优选地具有单独流动或具有短的篮筐(22)的涡轮风扇(10)包括两个推力反向门(24),所述两个推力反向门(24)通常容纳在形成于篮筐(22)中的壳体(26)中并且完全定位在其内封套(20)的外侧。当需要反向推力时,门(24)进入机舱后端后方的鼓风机通道(16)的延伸部分。因此,当飞机在飞行中时,门(24)不会受到反应堆的二次流(F2)的影响,机舱的内部围护结构(20)不会有任何泄漏或不连续性,并且可以完全用噪音处理减少。

著录项

  • 公开/公告号FR2737256A1

    专利类型

  • 公开/公告日1997-01-31

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE;

    申请/专利号FR19950009082

  • 发明设计人 ALAIN PORTE;

    申请日1995-07-26

  • 分类号F02K1/70;

  • 国家 FR

  • 入库时间 2022-08-22 03:12:14

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