TURBINE NOZZLE SEGMENT AND METHOD FOR REPAIRING A TURBINE NOZZLE SEGMENT
摘要
A turbine nozzle segment includes a first band, an airfoil extending from the first band and a support attached to the first band. The support may have a plurality of circumferentially spaced apart tabs.
申请公布号
WO2009085580(A2)
申请公布日期
2009.07.09
申请号
WO2008US85886
申请日期
2008.12.08
申请人
GENERAL ELECTRIC COMPANY;MORGAN, CLIVE, ANDREW;HEFFRON, TODD, STEPHEN;FONSEKA, SANJEEWA, THUSITHA;GRIFFITHS, PETER, ROBERT
发明人
MORGAN, CLIVE, ANDREW;HEFFRON, TODD, STEPHEN;FONSEKA, SANJEEWA, THUSITHA;GRIFFITHS, PETER, ROBERT
