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Conferences > LACSEA > 2016 > LT4F > LT4F.4

Optical sensing of turbine inlet temperature in a pressurized gas turbine combustor

S. Buerkle, M. Greifenstein, S. Wagner, A. Dreizler, and V. Ebert

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Abstract

A probe-based, fiber-coupled TDLAS sensor, operating at 1.4 µm for the measurement of gas turbine inlet temperatures using two line thermometry is developed and validated in a pressurized generic single-sector combustor.

© 2016 Optical Society of America

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