Turbomachine airflow temperature sensor

Rotary kinetic fluid motors or pumps – With control means responsive to non-cyclic condition... – Temperature or fluid force responsive member

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Details

415118, 374138, 374148, F01D 1708

Patent

active

047100958

ABSTRACT:
A temperature sensor, for measuring the temperature of air flowing in a substantially annular path into a compressor stage of a gas turbine engine, is positioned in proximity to the inner diameter of the annular flow path forward of the compressor stage where the measured temperature of the compressor inlet air is reliable during periods of water ingestion as well as during dry operation.

REFERENCES:
patent: 2928279 (1960-03-01), Schober
patent: 3167960 (1965-02-01), Miesiak
patent: 3673870 (1972-07-01), Jalbert
patent: 4403872 (1983-09-01), DeLeo

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