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ACTIVE CLEARANCE CONTROL APPARATUS

机译:主动间隙控制装置

摘要

The bore of the compressor for a gas turbine engine is heated by selectively bleeding compressor air from downstream stages so that heating only occurs at discreet times during the engine operating envelope. The bled air is admitted into the bore at the mid-stage station of the compressor wherein the compressor disks are scrubbed so as to expand and close the gap between the outer air seal and tips of the compressor blades during cruise of the aircraft and prevented from heating the disks during the high powered operations of the engine.
机译:用于燃气涡轮发动机的压缩机的孔通过选择性地从下游级放气压缩空气而被加热,使得加热仅在发动机工作范围内的离散时间发生。排出的空气在压缩机的中级工位处进入孔中,在此压缩机盘被擦洗,以便在飞机巡航期间扩大和封闭外部空气密封件与压缩机叶片的尖端之间的间隙,并防止在发动机大功率运行期间加热磁盘。

著录项

  • 公开/公告号JPH0472051B2

    专利类型

  • 公开/公告日1992-11-17

    原文格式PDF

  • 申请/专利权人 YUNAITETSUDO TEKUNOROJIIZU CORP;

    申请/专利号JP19840233041

  • 发明设计人 HAAUEI AAUIN UEINAA;KENESU RII ARAADO;

    申请日1984-11-05

  • 分类号F01D11/08;F01D11/24;F02C7/18;F02C7/28;F04D29/52;

  • 国家 JP

  • 入库时间 2022-08-22 05:13:13

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