| 摘要 |
A condition measurement apparatus (10) is provided and includes a gas turbine engine combustor (20) having an end cover (210), a liner (22) defining a liner interior (220) and a fuel nozzle (23) communicative with the liner interior (220), the end cover (210) being formed to separate a cold side thereof, which is a relatively low temperature environment, from a hot side thereof, which is a relatively high temperature environment in which the liner (22) and the fuel nozzle (23) are disposed, the combustor (20) being formed to define a fuel flow path extending through piping (30) disposed at the cold side of the end cover (210) by which fuel is deliverable to the fuel nozzle (23), and a condition sensing device (40) operably mounted on the piping (30).
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