Engine mounting configuration for a turbofan gas turbine engine
摘要
An engine mounting configuration reacts engine thrust at an aft mount (84). The engine mounting configuration reduces backbone bending of the engine, intermediate case distortion and frees-up space within the core nacelle.
申请公布号
EP2025898(A3)
申请公布日期
2013.08.28
申请号
EP20080252476
申请日期
2008.07.21
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
SUCIU, GABRIEL L.;MERRY, BRIAN D.;MARX, JON A.;NORDEEN, CRAIG A.;DYE, CHRISTOPHER M.