发明名称 GEARED TURBOFAN ARCHITECTURE FOR IMPROVED THRUST DENSITY
摘要 A turbine engine includes a fan, a compressor section having a low pressure compressor section and a high pressure compressor section, a combustor in fluid communication with the compressor section and a turbine section in fluid communication with the combustor. The turbine section includes a low pressure turbine section and a high pressure turbine section. The low pressure compressor section, the low pressure turbine section and the fan rotate in a first direction whereas the high pressure compressor section and the high pressure turbine section rotate in a second direction opposite the first direction.
申请公布号 US2013219908(A1) 申请公布日期 2013.08.29
申请号 US201213483406 申请日期 2012.05.30
申请人 SCHWARZ FREDERICK M.;KUPRATIS DANIEL BERNARD;SUCIU GABRIEL L. 发明人 SCHWARZ FREDERICK M.;KUPRATIS DANIEL BERNARD;SUCIU GABRIEL L.
分类号 F02C3/10 主分类号 F02C3/10
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