发明名称 A THERMOCOUPLE ON A CONTOURED GAS TURBINE ENGINE COMPONENT.
摘要 <p>A method of forming a thermocouple (12), including: depositing a first material on a component (10) to form a first leg (14); depositing a second material through a mask (30) to form a pattern (50) on the component (10), the pattern (50) forming a plurality of discrete second leg junction ends (20) and a continuous patch (52) of the second material comprising indiscrete lead ends of the second legs (16), each second leg junction end (20) spanning from a respective junction (18) with the first leg (14) to the continuous patch (52); and laser-ablating the continuous patch (52) to form discrete lead ends (22) of the second legs (16), each lead end (22) electrically connected to a respective junction end (20), thereby forming discrete second legs (16).</p>
申请公布号 MX2013010514(A) 申请公布日期 2014.02.27
申请号 MX20130010514 申请日期 2012.03.13
申请人 SIEMENS ENERGY, INC. 发明人 RAMESH SUBRAMANIAN;ANAND A. KULKARNI;KEVIN C. SHEEHAN
分类号 G01K1/02;F01D17/08;G01K7/02;G01K11/12 主分类号 G01K1/02
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