Gas turbine engine sensor probe

Power plants – Combustion products used as motive fluid

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Details

60 3933, 415118, 374144, F02G 300, F01B 2526, F01D 2500, G01K 108

Patent

active

051859963

ABSTRACT:
A high temperature thermocouple sensing apparatus is readily removable from a gas turbine engine. The thermocouple extends through aligned openings in inner and outer housings and seals both openings through use of a pair of spherical sealing elements and a spring seal bellows urging a seat into sealing engagement with one sealing element and urging the other sealing element into engagement with the inner housing.

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