发明名称 |
Rotor blades for turbine engines |
摘要 |
A tip shroud that includes a plurality of damping fins, each damping fin including a substantially non-radially-aligned surface that is configured to make contact with a tip shroud of a neighboring rotor blade. At least one damping fin may include a leading edge damping fin and at least one damping fin may include a trailing edge damping fin. The leading edge damping fin may be configured to correspond to the trailing edge damping fin.
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申请公布号 |
US8371816(B2) |
申请公布日期 |
2013.02.12 |
申请号 |
US20090533378 |
申请日期 |
2009.07.31 |
申请人 |
GENERAL ELECTRIC COMPANY;PIERSALL MATTHEW R.;POTTER BRIAN D. |
发明人 |
PIERSALL MATTHEW R.;POTTER BRIAN D. |
分类号 |
F01D1/00 |
主分类号 |
F01D1/00 |
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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