(57) ABSTRACT A system for estimating flight range of an electric aircraft. The system
generally includes at least a sensor and a flight controller. The at least a sensor is …

A decentralized electrical power allocation system is provided. The system includes a power
bus, electric power consumers, and at least two power source assemblies. Each power …

Abstract Systems and methods including a plurality of reformer stacks extended around the
combustion chamber. The reformer stacks are distributed along a length of the combustion …

Abstract Systems and methods of aircraft thrust management are provided. For example, a
propulsion system for an aircraft comprises a fuel cell assembly comprising a fuel cell, a …

A method of operating a fuel cell assembly for an aircraft is provided. The method includes:
receiving flight load predictor data for a scheduled flight of the aircraft prior to initiation of the …

A combustion section defines an axial direction, a radial direction, and a circumferential
direction. The combustion section includes a casing that defines a diffusion chamber. A …

A gas turbine engine includes a fuel cell assembly including a fuel cell stack and defining a
fuel cell assembly operating parameter, a fuel source, and a turbomachine. The …

A propulsion system for an aircraft, the aircraft including an aircraft fuel supply, the
propulsion system including: a turbomachine including a compressor section, a combustion …

A propulsion system is provided including: a gas turbine engine including a combustion
section having a combustor; and a modular fuel cell assembly. The modular fuel cell …

A method for operating a propulsion system for an aircraft, the propulsion system including a
gas turbine engine and a fuel cell assembly, the fuel cell assembly comprising a fuel cell …