Invention Grant
US09528898B2 Probe for measuring pressure oscillations in the combustor of a gas turbine 有权
用于测量燃气轮机燃烧器中的压力振荡的探头

Probe for measuring pressure oscillations in the combustor of a gas turbine
Abstract:
A probe is provided for measuring high frequent pressure oscillations of hot gases that combines redundancy of the output signals with high quality of the output signals.
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