GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
摘要
A gas turbine engine includes a spool along an engine centerline axis which drives a gear train, said spool includes a low stage count low pressure turbine.
申请公布号
EP2776318(A4)
申请公布日期
2014.11.26
申请号
EP20120863186
申请日期
2012.12.31
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
SUCIU, GABRIEL L.;MERRY, BRIAN D.;DYE, CHRISTOPHER, M.;JOHNSON, STEVEN B.;SCHWARZ, FREDERICK M.
