An engine arrangement (14) comprises a gas turbine engine unit (16) and first and second support members (18, 20). The support members (18, 20) extend from a structural component (24) of the engine casing (22) to support the engine unit in a position spaced from the body or airframe of the aircraft.
申请公布号
WO0158759(A1)
申请公布日期
2001.08.16
申请号
WO2001GB00473
申请日期
2001.02.07
申请人
ROLLS-ROYCE PLC;EL HAMEL, KARIM;NEWTON, ARNOLD, CHARLES
