Gas turbine engine temperature measurement system

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United States of America Patent

PATENT NO 12203379
APP PUB NO 20240309777A1
SERIAL NO

18594226

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Abstract

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A temperature measurement system for a gas turbine engine, the gas turbine engine including, in axial flow sequence, a compressor section, a combustor section having plural fuel spray nozzles, and a turbine section. The temperature measurement system includes one or more optical thermometers, each optical thermometer configured to measure the temperature of a component washed by the working gas of the engine, the or each component being in the combustor section or the turbine section at a first position along the axis of the engine.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE PLC62 BUCKINGHAM GATE LONDON SW1E 6AT

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Stevenson, Guy Derby, GB 2 0

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