发明公开
EP2686650A1 A THERMOCOUPLE ON A CONTOURED GAS TURBINE ENGINE COMPONENT 有权
VEFAHREN于形成热电元件上的轮廓燃气轮机部件

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).
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