发明名称 |
Integral nozzle and shroud |
摘要 |
A gas turbine engine component including a nozzle outer band, a plurality of nozzle vanes extending inward from the outer band, and an inner band extending circumferentially around inner ends of the vanes. Further, the component has a shroud integral with the outer band adapted for surrounding a plurality of blades mounted in the engine for rotation about a centerline thereof.
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申请公布号 |
US2002182057(A1) |
申请公布日期 |
2002.12.05 |
申请号 |
US20010867294 |
申请日期 |
2001.05.29 |
申请人 |
LIOTTA GARY CHARLES;MANNING ROBERT FRANCIS |
发明人 |
LIOTTA GARY CHARLES;MANNING ROBERT FRANCIS |
分类号 |
F01D9/02;F01D9/04;F01D25/12;F01D25/24;(IPC1-7):F01D9/04;F01D9/06 |
主分类号 |
F01D9/02 |
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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