发明名称 GAS TURBINE ENGINE WITH MODULAR CORES AND PROPULSION UNIT
摘要 <p>A separate propulsion unit incorporating a free turbine and a fan receives gases from a plurality of core engines. The core engines each include a compressor, a turbine and a combustion section. The core engines in combination pass gases across the free turbine. A method is also disclosed.</p>
申请公布号 SG11201404046P(A) 申请公布日期 2014.10.30
申请号 SG11201404046P 申请日期 2013.02.05
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SUCIU, GABRIEL L.;DYE, CHRISTOPHER;STAUBACH, JOSEPH B.
分类号 F02K3/12;F02C5/00;F02C7/00;F02K3/06 主分类号 F02K3/12
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