Relative Fuel Ratio Unit Limiter for Gas Turbine Surge Recovery
AssigneePratt & Whitney Canada Corp.
InventorLouis DURANLEAU-HENDRICKX
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AssigneePratt & Whitney Canada Corp.
InventorLouis DURANLEAU-HENDRICKX
Estimating the term…
A method includes monitoring a fuel ratio unit (RU) of a gas turbine engine over time, where the RU is a ratio of a fuel flow to a compressor discharge pressure during operation of the gas turbine engine. The method also includes storing the RU in a memory. The method further includes, in response to identifying a surge detection time at which an engine surge is detected, retrieving, from the memory, a pre-surge RU before the surge detection time, where the pre-surge RU corresponds to a pre-surge time. The method also includes determining a relative RU limit based on the pre-surge RU such that the relative RU limit is less than the pre-surge RU by at least a bias value. In addition, the method includes limiting the fuel flow to the relative RU limit for a duration of the detected engine surge.
A method comprising:
A non-transitory machine-readable medium including instructions that when executed cause at least one processor to:
An electronic device comprising:
Dependencies are inferred from the claim text.