发明名称 |
Turbomachine rotor assembly and method |
摘要 |
Disclosed is a rotor assembly for a turbomachine includes a disk having a first axial face and a second axial face. The disk includes at least one circumferential dovetail extending around an outer surface of the disk and a plurality of axial dovetails extending from the first axial face to the second axial face. Each blade of a plurality of blades is installed into an axial dovetail of the plurality of axial dovetails and each platform of a plurality of platforms is installed adjacent to a blade of the plurality of blades via the at least one circumferential dovetail. Further disclosed is a method of assembly of a rotor for a turbomachine.
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申请公布号 |
US8277190(B2) |
申请公布日期 |
2012.10.02 |
申请号 |
US20090412969 |
申请日期 |
2009.03.27 |
申请人 |
PIERSALL MATTHEW ROBERT;POTTER BRIAN DENVER;GENERAL ELECTRIC COMPANY |
发明人 |
PIERSALL MATTHEW ROBERT;POTTER BRIAN DENVER |
分类号 |
F01D5/30 |
主分类号 |
F01D5/30 |
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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