发明名称 Turbine nozzle segment and method for repairing a turbine nozzle segment
摘要 <p>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.</p>
申请公布号 GB201010138(D0) 申请公布日期 2010.07.21
申请号 GB20100010138 申请日期 2008.12.08
申请人 GENERAL ELECTRIC COMPANY 发明人
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