Invention Grant
US09127596B2 Gas turbine engine fuel control system 有权
燃气轮机发动机燃油控制系统

Gas turbine engine fuel control system
Abstract:
A fuel control system having a combustive energy value evaluator determining a combustive energy value of the fuel, and a controller calculating a desired flow rate based at least on the combustive energy value and controlling a fuel metering device such that the fuel flow rate corresponds to the desired fuel flow rate.
Public/Granted literature
Information query
Patent Agency Ranking
0/0