A system and method for repairing a gas turbine engine component
摘要
<p>A method of repairing a defect (18) in a component (10) includes forming a slot (30; 78) in the component (10), thereby removing at least a substantial part of the defect (18) from the component (10), where the slot (30; 78) has a predetermined geometry.</p>
申请公布号
EP1743731(B2)
申请公布日期
2013.04.10
申请号
EP20060253713
申请日期
2006.07.14
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
LEIBFRIED, PETER E.;DUNNE, PHILIP J.;ARRIGONI, JOHN P.;SORVILLO, WILLIAM G. SR.;SIMARD, DALE A.
