Thermocouple probe
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United States of America Patent
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Jun 13, 1995
Grant Date -
N/A
app pub date -
Oct 26, 1993
filing date -
Oct 30, 1992
priority date (Note) -
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Abstract
A thermocouple probe 10 suitable for use in a gas turbine engine comprises a thermocouple element 12 which is coaxially arranged inside a protective sheath 16. The thermocouple element 12 is resiliently supported by a helical member 18 which insulates the element 12 from deleterious vibrations induced in the sheath 16 by alternately contacting the protective sheath (16) and the thermocouple element (12).
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