发明名称 |
Tip sealing method for compressors |
摘要 |
A recirculation passageway 52 for a turbine engine 10 provides stall protection in a booster 40 by directing high pressure airflow from a flow path 50 of the booster 40 and into the passageway 52. The high pressure airflow loses energy and decreases in pressure while traveling through the passageway 52 until re-entry into the booster 40 flow path 50. The airflow recirculates in the passageway 52 until the airflow may be steadily discharged through a high pressure compressor. <IMAGE> |
申请公布号 |
EP1052376(A3) |
申请公布日期 |
2003.06.04 |
申请号 |
EP20000303941 |
申请日期 |
2000.05.10 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
HAUSER, AMBROSE ANDREAS;SEDA, JORGE FRANCISCO;SZUCS, PETER NICHOLAS |
分类号 |
F02C7/00;F01D5/14;F04D27/02;F04D29/16;F04D29/54;F04D29/68 |
主分类号 |
F02C7/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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