发明名称 Turbofan engine including improved fan blade lining
摘要 An improved rotary engine, engine lining and engine casing and lining combination are disclosed. The engine is preferable a turbofan engine and includes a fan blade, rotatably mounted within a generally cylindrical casing for rotation about a lengthwise extending central axis. An annular lining is mounted within the casing between a tip of the fan blade and the casing. The lining seals the tip of the fan blade within the casing. The lining includes a brush seal that extends around an inner circumference of the casing, and has a plurality of bristles that extend radially inward from the seal. A retaining membrane extends around the brush seal, preventing the bristles from extending substantially in a radial direction from the brush seal. The retaining membrane is adapted to release the bristles to extend radially inward to occupy a region between the tip of the fan blade and the casing upon a radial excursion of the fan blade. The bristles, once released, at least partially seal the tip of the fan blade and the casing reducing air recirculation at the blade tip.
申请公布号 US6217277(B1) 申请公布日期 2001.04.17
申请号 US19990412642 申请日期 1999.10.05
申请人 PRATT & WHITNEY CANADA CORP. 发明人 LIU XIAOLIU;RAW JOHN ANGUS
分类号 F01D11/02;F01D11/08;F01D11/12;F01D21/04;F02K3/06;F04D29/08;F04D29/52;(IPC1-7):F01B25/16 主分类号 F01D11/02
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