Gas turbine engine with stacked accessory components
摘要
An engine accessory system for a gas turbine engine includes a first accessory component (AC1) defined along an accessory axis (Z) and a second accessory component (AC2) mounted to the first accessory component (AC1) along the accessory axis (Z).
申请公布号
EP2239440(A1)
申请公布日期
2010.10.13
申请号
EP20100250338
申请日期
2010.02.25
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
CASS. MICHAEL F.;MERRY, BRIAN D.;ELDER, JAMES S.;SUCIU, GABRIEL L.;DYE, CHRISTOPHER M.
