发明名称 |
GAS TURBINE ENGINE SHAFT MEMBERS AND MAINTENANCE METHOD |
摘要 |
A gas turbine engine includes first and second shaft members in an interference fit relationship with one another at an interface. The first and second shaft members respectively include first and second flanges that are arranged adjacent to the interface. The first and second flanges respectively include first and second threads that are configured to cooperate with a tool during disassembly of the first and second shaft members. |
申请公布号 |
US2016146103(A1) |
申请公布日期 |
2016.05.26 |
申请号 |
US201514937153 |
申请日期 |
2015.11.10 |
申请人 |
United Technologies Corporation |
发明人 |
Muldoon Marc J. |
分类号 |
F02C3/107 |
主分类号 |
F02C3/107 |
代理机构 |
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代理人 |
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主权项 |
1. A gas turbine engine comprising:
first and second shaft members in an interference fit relationship with one another at an interface, the first and second shaft members respectively include first and second flanges arranged adjacent to the interface, the first and second flanges respectively include first and second threads configured to cooperate with a tool during disassembly of the first and second shaft members. |
地址 |
Hartford CT US |