Method and device for adjusting a threshold value of a fuel flow rate
AssigneeSafran Aircraft Engines
InventorsChristophe Javelot, Cedrik Djelassi, Bruno Robert Gaully, Ismail Sylla
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AssigneeSafran Aircraft Engines
InventorsChristophe Javelot, Cedrik Djelassi, Bruno Robert Gaully, Ismail Sylla
Estimating the term…
A method of adjusting a fuel flow rate in a turbine engine propelling an aircraft, including: obtaining a first estimate of a flow rate of fuel injected into a combustion chamber of the turbine engine propelling an aircraft and as delivered by a fuel metering device of the turbine engine; obtaining a second estimate of the fuel flow rate, which second estimate is more accurate than the first estimate for at least one range of fuel flow rate values and being delivered by an estimator device having a flow meter; and adjusting the fuel flow rate threshold value with help of a difference evaluated between the first estimate and the second estimate, the threshold value being for use in an open loop for regulating the turbine engine.
A method for regulating a turbine engine propelling an aircraft, the method comprising:
A non-transitory computer readable medium storing computer readable instructions thereon that when executed by a computer cause the computer to perform a method comprising:
A device for regulating a turbine engine propelling an aircraft, the device comprising:
Dependencies are inferred from the claim text.