CPC F02C 9/28 (2013.01) [F02C 9/40 (2013.01); F05D 2260/80 (2013.01); F05D 2270/303 (2013.01); F05D 2270/304 (2013.01); F05D 2270/708 (2013.01); F23N 2221/10 (2020.01)] | 15 Claims |
1. A method of operating an aircraft including a gas turbine engine, the method comprising:
passing UV-visual spectrum light through an aviation fuel suitable for powering the gas turbine engine of the aircraft;
measuring a transmittance parameter indicating the transmittance of light through the aviation fuel;
determining one or more fuel characteristics of the aviation fuel based on the transmittance parameter, the one or more fuel characteristics including one or more of:
a percentage of sustainable aviation fuel in the aviation fuel; and
an indication as to whether the aviation fuel is fossil fuel;
communicating the one or more fuel characteristics to a controller of the gas turbine engine or the aircraft, and
operating the aircraft according to the one or more fuel characteristics including:
a) modifying a control parameter of the aircraft in response to the one or more fuel characteristics; and/or
b) providing a second fuel during refuelling of the aircraft, wherein one or more fuel characteristics of the second fuel are different than the one or more fuel characteristics of the aviation fuel.
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