COMPRESSED CHOPPED FIBER COMPOSITE FAN BLADE PLATFORM
摘要
The present disclosure relates generally to the field of fan blade platforms for gas turbine engines. More specifically, the present disclosure relates to a compressed chopped fiber fan blade platform for a gas turbine engine.
申请公布号
EP3102791(A2)
申请公布日期
2016.12.14
申请号
EP20140886052
申请日期
2014.12.15
申请人
United Technologies Corporation
发明人
ALARCON, Andrew G.;TATTON, Royce E.;FORD, Barry M.;LI, Linda S.;TURNER, Matthew A.
