Mass flow metering system for aircraft applications

G - Physics – 01 – F

Patent

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G01F 9/00 (2006.01) B64D 37/00 (2006.01) B64D 43/00 (2006.01)

Patent

CA 2742333

A method of calculating fuel flow across an aircraft flight cycle includes the steps of providing a flow meter, and an alternative method of measuring fuel flow. The flow meter is used to calculate fuel flow over a portion of a flight cycle of an aircraft equipped with the system. Fuel flow is calculated with the alternative measurement system at least during maximum power flow portions of the flight cycle. A system is configured for performing this method. A method of calculating mass flow across a fuel metering unit uses fuel flow volume measurements and information about the fuel to reach a mass flow measurement.

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