Assembly system of a thermocouple for a gas turbine

G - Physics – 01 – K

Patent

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Details

G01K 3/06 (2006.01) F01D 17/08 (2006.01) G01K 13/02 (2006.01)

Patent

CA 2549888

Assembly system (10) for a thermocouple (16) for a gas turbine equipped with a supporting element (12) in which the thermocouple (16) is housed, the supporting element (12) has a series of holes (45) for the inlet of the dis~charge gases of the gas turbine and a cavity (50) in which they are mixed before flowing through an opening (14) of the supporting element (12).

L'invention concerne un système d'assemblage (10) pour un thermocouple (16) pour une turbine à gaz comportant un élément de support (12) dans lequel le thermocouple (16) est logé. Selon l'invention, l'élément de support (12) comporte une série de trous (45) pour l'admission des gaz d'évacuation de la turbine à gaz, et une cavité (50) dans laquelle ils sont mélangés avant de s'écouler dans une ouverture (14) de l'élément de support (12).

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