发明名称 |
DIFFERENTIAL GEARED ARCHITECTURE FOR GAS TURBINE ENGINE |
摘要 |
A gas turbine engine includes first and second shafts rotatable about a common axis. A first turbine section is supported on the first shaft. Second compressor and turbine sections are supported on the second shaft. The gas turbine engine includes a fan, a first compressor section, and a differential gear train that couples the fan and the first compressor section to the first shaft.
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申请公布号 |
US2013259651(A1) |
申请公布日期 |
2013.10.03 |
申请号 |
US201213437363 |
申请日期 |
2012.04.02 |
申请人 |
KUPRATIS DANIEL BERNARD;SCHWARZ FREDERICK M. |
发明人 |
KUPRATIS DANIEL BERNARD;SCHWARZ FREDERICK M. |
分类号 |
F01D15/12 |
主分类号 |
F01D15/12 |
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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