TURBINE NOZZLE SEGMENT AND METHOD OF REPAIRING SAME
摘要
<p>A method is provided for repairing a metallic turbine component which includes at least two airfoils interconnected by a mid-span shroud. The method includes: (a) applying a reinforcement plate to the mid-span shroud; (b) applying braze material to at least a portion of a perimeter of the reinforcement plate; (c) heating the component to melt and flow the braze material between the reinforcement plate and the mid-span shroud; and (d) allowing the braze material to cool and solidify so as to bond the reinforcement plate to the mid-span shroud.</p>
申请公布号
CA2746275(A1)
申请公布日期
2012.01.28
申请号
CA20112746275
申请日期
2011.07.14
申请人
GENERAL ELECTRIC COMPANY
发明人
GARZA, JOSE ABIEL;GRADY, WAYNE RAY;MANKOWSKI, PAWEL;ZAK, MARCIN;TRAJER, MARCIN