首页> 外国专利> PROCESS FOR AIR CIRCULATION IN A TURBINE ENGINE COMPRESSOR, COMPRESSOR ARRANGEMENT PUTTING IT INTO PLAY, STAGE OF COMPRESSION AND COMPRESSOR COMPRISING SUCH AN ARRANGEMENT, AND AIRCRAFT ENGINE EQUIPPED WITH SUCH A COMPRESSOR

PROCESS FOR AIR CIRCULATION IN A TURBINE ENGINE COMPRESSOR, COMPRESSOR ARRANGEMENT PUTTING IT INTO PLAY, STAGE OF COMPRESSION AND COMPRESSOR COMPRISING SUCH AN ARRANGEMENT, AND AIRCRAFT ENGINE EQUIPPED WITH SUCH A COMPRESSOR

机译:涡轮发动机压缩机中的空气循环过程,将其投入使用的压缩机布置,压缩阶段和包含这种布置的压缩机以及装有这种压缩机的飞机发动机

摘要

For a compression stage of a compressor comprising a plurality of compression stages (28) having: movable (14) and fixed (26) wheels, outer (8) and inner (4) casings delimiting a stream (10) having an outer vein (34) and an inner vein (36), the method comprises an operation where air is sucked into the inner vein, and is sent into a fixed blade of said fixed wheel, and an operation where withdraws air in said fixed blade, and is sent outside the compressor. The compressor arrangement for carrying out the method comprises suction means (42, 44) and sampling means (48, 50).
机译:对于包括多个压缩级(28)的压缩机的压缩级,该压缩级(28)具有:可移动(14)和固定(26)轮,外罩(8)和内罩(4)界定了具有外静脉(10)的气流(10) 34)和内静脉(36),该方法包括将空气吸入内静脉并送入所述固定轮的固定叶片的操作,以及在所述固定叶片中抽出空气并发送的操作。在压缩机外面。用于执行该方法的压缩机装置包括抽吸装置(42、44)和采样装置(48、50)。

著录项

  • 公开/公告号CA2521983C

    专利类型

  • 公开/公告日2013-06-18

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号CA20052521983

  • 发明设计人 LARDELLIER ALAIN;

    申请日2005-09-29

  • 分类号F02C3/13;F01D9/06;F02C7;F02K3;

  • 国家 CA

  • 入库时间 2022-08-21 16:38:26

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