发明名称 GEARED TURBOFAN ENGINE WITH POWER DENSITY RANGE
摘要 A gas turbine engine (120) has a high pressure turbine (130) configured to rotate with a high pressure compressor (126) as a high pressure spool (132) in a first direction about a central axis (C) and a low pressure turbine (134) configured to rotate with a low pressure compressor (124) as a low pressure spool (136) in the first direction about the central axis (C). A power density is greater than or equal to about 1.5 and less than or equal to about 5.5 lbf/cubic inches. A fan (122) is connected to the low pressure spool (136) via a speed changing mechanism (48) and rotates in a second direction opposed to the first direction.
申请公布号 EP3043058(A1) 申请公布日期 2016.07.13
申请号 EP20160150651 申请日期 2016.01.08
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SCHWARZ, FREDERICK M.;KUPRATIS, DANIEL BERNARD
分类号 F02K3/06;F02C3/107 主分类号 F02K3/06
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