发明名称 |
GAS TURBINE ENGINE COMPRESSOR ROTOR ASSEMBLY AND BALANCING SYSTEM |
摘要 |
A method for balancing a compressor rotor assembly including a forward weldment (211) and an aft weldment (212) includes pre-balancing the aft weldment (212) of the compressor rotor assembly (210) with compressor disks (220) prior to populating the compressor disks (220) with circumferentially installed compressor rotor blades (230). Pre-balancing the aft weldment (212) includes measuring a rotational balance of the aft weldment (212). Pre-balancing the aft weldment (212) also includes determining a number of underplatform weights (260) needed and a location for each underplatform weight (260) within a circumferential slot (236) of one the compressor disks (220). Pre-balancing the aft weldment (212) further includes mounting each underplatform weight (260) in the determined location. |
申请公布号 |
US2014140849(A1) |
申请公布日期 |
2014.05.22 |
申请号 |
US201213684056 |
申请日期 |
2012.11.21 |
申请人 |
SOLAR TURBINES INCORPORATED |
发明人 |
MUSCAT CORY PATRICK;MCDONALD LAURA ELIZABETH;MILLER JAMES ERIC;VAVREK GARY PAUL |
分类号 |
F01D5/02 |
主分类号 |
F01D5/02 |
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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