A gas turbine engine having three shafts connecting respective high, intermediate and low-pressure turbines and compressors is characterised by an intermediate pressure turbine that includes two rotor stages.
申请公布号
US2010089019(A1)
申请公布日期
2010.04.15
申请号
US20090468978
申请日期
2009.05.20
申请人
ROLLS-ROYCE PLC
发明人
KNIGHT GLENN ALEXANDER;RICHARDS MARTYN;TAYLOR MARK DAVID;MAGUIRE ALAN ROBERT
