Patent ID: 11970282
Assignee: GENERAL ELECTRIC COMPANY
Field: Transport (Mechanical engineering)
Classification: CPC B  Y | IPC B

Claim 12:
13. A method of operating a propulsion system for an aircraft, the propulsion system comprising a fuel cell assembly comprising a fuel cell and a turbomachine, the method comprising:
receiving data indicative of a propulsion system thrust discrepancy, wherein receiving data indicative of the propulsion system thrust discrepancy includes receiving data indicative of a thrust imbalance between a first propulsion assembly and a second propulsion assembly; and
modifying an output of the fuel cell in response to receiving data indicative of the propulsion system thrust discrepancy, wherein modifying the output of the fuel cell in response to receiving data indicative of the propulsion system thrust discrepancy comprises modifying an electrical power output to the second propulsion assembly.