发明名称 |
Turbomachine rotor assembly and method |
摘要 |
<p>Disclosed is a rotor assembly (10) for a turbomachine includes a disk (12) having a first axial face (20) and a second axial face (22). The disk (12) includes at least one circumferential dovetail (30) extending around an outer surface (32) of the disk (12) and a plurality of axial dovetails (18) extending from the first axial face (20) to the second axial face (22). Each blade (14) of a plurality of blades (14) is installed into an axial dovetail (30) of the plurality of axial dovetails (30) and each platform (16) of a plurality of platforms (16) is installed adjacent to a blade (14) of the plurality of blades (14) via the at least one circumferential dovetail (30). Further disclosed is a method of assembly of a rotor for a turbomachine.</p> |
申请公布号 |
EP2233696(A3) |
申请公布日期 |
2013.03.06 |
申请号 |
EP20100156684 |
申请日期 |
2010.03.16 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
PIERSALL, MATTHEW ROBERT;POTTER, BRIAN DENVER |
分类号 |
F01D5/30;F01D11/00 |
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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