DEVICE TO MEASURE GAS TURBINE BLADE TEMPERATURE Russian patent published in 2008 - IPC G01J5/14 

Abstract RU 2332646 C1

FIELD: radiation pyrometry.

SUBSTANCE: device incorporates a micro processor system and AD converter. The photoelectric converter output is connected to the AD converter input, in its turn, connected to the said micro processor system with a feedback with the AD converter. The eddy-current blade position pickup is also connected, via a rectangular pulse shaper, with the said micro processor system.

EFFECT: reducing the errors caused by unburnt fuel particle radiation to tolerable values.

1 dwg

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RU 2 332 646 C1

Authors

Skudnov Evgenij Mikhajlovich

Tokarev Vladimir Petrovich

Dates

2008-08-27Published

2007-03-20Filed