Temperature sensor arrangement in combination with a gas turbine

Thermal measuring and testing – Temperature measurement – Combined with diverse art device

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Details

374137, 374147, 374148, 60 3933, G01K 114

Patent

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061426652

ABSTRACT:
In a temperature-measuring device, in particular for measuring the flame temperature in a gas turbine combustion chamber, a number of optical measuring sensors (7) are arranged directly upstream of a flame front (8) in a premixing zone (3) of a burner (1). Each optical measuring sensor (7) is aligned essentially parallel to and/or coaxial with a fuel flow (5) directed into the gas turbine combustion chamber.

REFERENCES:
patent: 4865416 (1989-09-01), Pratt
patent: 5361586 (1994-11-01), McWhirter et al.
patent: 5384467 (1995-01-01), Plimon et al.
patent: 5857320 (1999-01-01), Amos et al.

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