发明名称 |
GEARED TURBINE ENGINE WITH RELATIVELY LIGHTWEIGHT PROPULSOR MODULE |
摘要 |
<p>An example gas turbine engine includes a propulsor assembly including at least a fan module and a fan drive turbine module; a gas generator assembly including at least a compressor section, a combustor in fluid communication with the compressor section, and a turbine in fluid communication with the combustor; and a geared architecture driven by the fan drive turbine module for rotating a fan of the fan module. A weight of the fan module and the fan drive turbine module is less than about 40% of a total weight of a gas turbine engine.</p> |
申请公布号 |
CA2886359(A1) |
申请公布日期 |
2014.04.17 |
申请号 |
CA20132886359 |
申请日期 |
2013.02.08 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SCHWARZ, FRED M.;SUCIU, GABRIEL L. |
分类号 |
F02C7/00;F02C7/20;F02C7/32 |
主分类号 |
F02C7/00 |
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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