发明名称 Method of repairing a turbine engine component
摘要 <p>A method of repairing a turbine engine component (10) involves offering two repair options (14,18) to a customer. A first repair option (14) is based on an operating environment of the turbine engine component (10) and the second repair option (18) is based on cost. The first repair option (14) is priced higher than the second repair option (18). The turbine engine component (10) is examined. The turbine engine component (10) is then repaired according to the selected repair option (14,18).</p>
申请公布号 EP2036657(A2) 申请公布日期 2009.03.18
申请号 EP20080252930 申请日期 2008.09.03
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MCCALL, THOMAS;BOLAND, ROBERT M.;PELLET, PAUL M.;QUINN, DANIEL E.
分类号 B23P6/00;C23C14/06;F01D5/00;G06Q10/00 主分类号 B23P6/00
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