| 发明名称 |
GEARED TURBOFAN ENGINE WITH OPTIMIZED DIFFUSER CASE FLANGE LOCATION |
| 摘要 |
A gas turbine engine has a compressor section, a compressor case substantially surrounding the compressor section, and a diffuser case attached at an attachment interface to the compressor case. The attachment interface is between a forward and an aft end of the compressor. A geared turbofan is also disclosed. |
| 申请公布号 |
WO2014058466(A1) |
申请公布日期 |
2014.04.17 |
| 申请号 |
WO2013US31301 |
申请日期 |
2013.03.14 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SCHWARZ, FREDERICK, M. |
| 分类号 |
F02K3/00;F02C3/04;F02C7/04;F02K99/00 |
主分类号 |
F02K3/00 |
| 代理机构 |
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代理人 |
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