A spinner (80) for a gas turbine engine (20) comprises an outer shell (82) for defining an airflow path when mounted in a gas turbine engine (20). An inner surface (84) is provided with a plurality of webs (86). A gas turbine engine (20) and a fan section (22) for a gas turbine engine (20) are also disclosed.
申请公布号
EP2915742(A1)
申请公布日期
2015.09.09
申请号
EP20150157399
申请日期
2015.03.03
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
ROACH, JAMES T.;COOK, III, GRANT O.;KLING, COLIN J.;O'BRIEN, JAMES F.;BUGAJ, SHARI L.
