Controlling hybrid-electric or all-electric powertrains and propulsion systems
AssigneesGeneral Electric Company, GE Avio S.r.l.
InventorsGregory L. Detweiler, Stefano Ettorre, Thomas William Brown
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AssigneesGeneral Electric Company, GE Avio S.r.l.
InventorsGregory L. Detweiler, Stefano Ettorre, Thomas William Brown
Estimating the term…
A hybrid-electric or all-electric powertrain may include a power control unit electrically coupled to an energy storage system. The power control unit may determine a power level command based at least in part on a power level request for the powertrain, and a power level-UCL and/or a power level-LCL. The power level-UCL and/or the power level-LCL may be based at least in part on an aggregate obverse power level request representing a requested power level for one or more obverse powertrains electrically coupled to the energy storage system. The power level commands may be limited by the power level-UCL and/or the power level-LCL. The power level-UCL may be set equal to either an available discharge power capacity or an apportionate discharge power capacity. The power level-LCL may be set equal to either an available storage power capacity or an apportionate storage power capacity.
A powertrain for an aircraft, the powertrain comprising:
A method of controlling a powertrain of an aircraft, the method comprising:
A non-transitory computer-readable medium comprising computer-executable instructions, which when executed by a processor associated with an electronic controller for a powertrain for an aircraft, cause the electronic controller to perform a method comprising:
Dependencies are inferred from the claim text.