发明名称 |
A THERMOCOUPLE ON A CONTOURED GAS TURBINE ENGINE COMPONENT |
摘要 |
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) |
申请公布号 |
WO2012145095(A1) |
申请公布日期 |
2012.10.26 |
申请号 |
WO2012US28858 |
申请日期 |
2012.03.13 |
申请人 |
SIEMENS ENERGY, INC.;SUBRAMANIAN, RAMESH;KULKARNI, ANAND A.;SHEEHAN, KEVIN C. |
发明人 |
SUBRAMANIAN, RAMESH;KULKARNI, ANAND A.;SHEEHAN, KEVIN C. |
分类号 |
G01K1/02;F01D17/08;G01K7/02;G01K11/12 |
主分类号 |
G01K1/02 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|