发明名称 |
Methods and apparatus for assembling gas turbine nozzles |
摘要 |
A method facilitates assembling a turbine nozzle for a gas turbine engine. The method includes providing a turbine nozzle including a plurality of airfoil vanes that extend between an inner band and an outer band, and forming a compound radii fillet that extends between a first of the airfoil vanes and the outer band, such that at least a second of the airfoil vanes is coupled to the outer band only by a single radii fillet.
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申请公布号 |
US2004120810(A1) |
申请公布日期 |
2004.06.24 |
申请号 |
US20020325035 |
申请日期 |
2002.12.20 |
申请人 |
BRAINCH GULCHARAN S.;MILLER WILLIAM;ALBRECHT RICHARD W.;STEWART DAVID B.;HEFFRON TODD STEPHEN |
发明人 |
BRAINCH GULCHARAN S.;MILLER WILLIAM;ALBRECHT RICHARD W.;STEWART DAVID B.;HEFFRON TODD STEPHEN |
分类号 |
F01D9/02;F01D5/14;F01D9/04;F02C7/00;(IPC1-7):F01D1/02 |
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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