Method and apparatus for determining series arcing in a hybrid-electric propulsion system
AssigneePratt & Whitney Canada Corp.
InventorsAlireza Gharagozloo, Michael Hanna
Life of this patent
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AssigneePratt & Whitney Canada Corp.
InventorsAlireza Gharagozloo, Michael Hanna
Estimating the term…
A hybrid-electric propulsion system is provided that includes a thermal engine, an electric motor, a battery, a battery management unit (BMU), an electrical distribution bus, an artificial intelligence (AI) model, and a monitoring system (MS) controller. The electrical distribution bus electrically connects the electric motor and the BMU. The MS controller is in communication with the AI model, the electric motor, the BMU, and a memory storing instructions. The instructions when executed cause the MS controller to: receive a first operational parameter from the BMU unit; control the AI model to produce a predicted first operational parameter utilizing at least one electric motor operating parameter; and determine the presence of series arcing within the electrical distribution bus using the first operational parameter and the predicted first operational parameter.
A hybrid-electric propulsion (HEP) system, comprising:
A method for determining series arcing in an aircraft hybrid-electric propulsion (HEP) system, comprising:
Dependencies are inferred from the claim text.