Systems and methods for multi-module control of a hydrogen powered hybrid electric powertrain

1. A thermally managed hydrogen-powered hybrid electric powertrain system for a hydrogen-powered vehicle, the system comprising:

one or more fuel cell stacks comprising a plurality of hydrogen fuel cells configured to process hydrogen fuel to generate electricity, first thermal energy, and exhaust water;

one or more primary electric power units that receive the electricity generated by the one or more fuel cell stacks, wherein the electricity is provided from the one or more fuel cell stacks to the one or more primary electric power units without passing through a DC-to-DC converter and/or being stored in a battery, and wherein the one or more primary electric power units generates second thermal energy;

one or more radiators configured to receive and thermally dissipate the first and second thermal energy tranmitted from the one or more fuel cell stacks and the one or more primary electric power units, respectively;

one or more pumps configured to transmit coolant to the one or more radiators;

a turbine configured to receive mechanical power from the one or more fuel cell stacks;

a second compressor configured to receive the mechanical power from the turbine and to direct first compressed air to the turbine and the one or more fuel cell stacks;

a first compressor configured to provide second compressed air to the second compressor; and

a water distribution system configured to receive the exhaust water generated by the one or more fuel cell stacks and to direct the exhaust water to an exhaust outlet.

2. The system of claim 1 , further comprising 1) a speed reducer coupled to the primary electric power unit and configured to transmit thermal energy to the one or more pumps and receive mechanical power from the primary electric power unit; and 2) a peripheral electric power unit configured to transmit the thermal energy to the one or more pumps, wherein the first compressor receives power from the peripheral electric power unit.

3. The system of claim 1 , further comprising a peripheral electric power unit configured to provide electrical power to the first compressor, and comprising a battery configured to receive the electrical power generated from the one or more fuel cell stacks and transmit the electrical power to the peripheral electric power unit, wherein the battery does not provide electrical power to the primary electrical power unit.

4. The system of claim 1 wherein at least a portion of the exhaust water generated by the at least one fuel cell stack passes through the turbine, and the turbine is configured to direct the exhaust water to the water distribution system.

5. The system of claim 4 wherein the turbine is configured to further transmit a fluid to an exhaust.

6. The system of claim 1 , further comprising a deicing system configured to receive a fluid from the turbine.

7. The system of claim 1 wherein the water distribution system comprises a spray bar forming the exhaust outlet and configured to direct the exhaust water onto the radiator.

8. The system of claim 1 , further comprising a hydrogen-powered powertrain and hydro-electro-aero-thermal management system (HEATMS) configured to control and manage thermal energy generated by the hydrogen-powered powertrain.

9. The system of claim 8 wherein the HEATMS is configured to:

predict one or more changes in an electrical power demand of the hydrogen-powered powertrain during operation of the primary electrical power unit;

controlling an amount of air mass flow rate to the one or more fuel cell stacks to direct an amount of air to the one or more fuel cell stacks based at least in part on the one or more predicted changes in the electrical power demand of the powertrain; and

providing the amount of air to the one or more fuel cell stacks before occurrence of the predicted electrical power demand for generation of an output of electrical power by the one or more fuel cell stacks at or before occurrence of the predicted electrical power demand of the powertrain, wherein the output of electrical power is timed to reduce a transient period for delivery of the electrical power to the primary electrical power unit.

10. An aircraft comprising at least one hydrogen-powered powerplant having a thermally managed hybrid electric powertrain system, the system comprising:

one or more fuel cell stacks comprising a plurality of hydrogen fuel cells configured to process hydrogen fuel to generate electricity, first thermal energy, and exhaust water;

one or more primary electric power units that received the electricity generated by the one or more fuel cell stacks, wherein the electricity is provided from the one or more fuel cell stacks to the one or more primary electric power units without passing through a DC-to-DC converter and/or being stored in a battery, and wherein the one or more primary electric power units generates second thermal energy;

one or more radiators configured to receive and thermally dissipate the first and second thermal energy tranmitted from the one or more fuel cell stacks and the one or more primary electric power units, respectively;

one or more pumps configured to transmit coolant to the one or more radiators;

a speed reducer configured to transmit the thermal energy to the one or more pumps and receive mechanical power from the primary electric power unit;

a peripheral electric power unit configured to transmit the thermal energy to the one or more pumps;

a turbine configured to receive mechanical power from the one or more fuel cell stacks;

a second compressor configured to receive the mechanical power from the turbine and to direct first compressed air to the turbine and the one or more fuel cell stacks;

a first compressor configured to provide second compressed air to the second compressor; and

a water distribution system configured to receive the exhaust water generated by the one or more fuel cell stacks and to direct the exhaust water to an exhaust outlet.

11. The system of claim 8 , further comprising a plurality of sensors onboard the vehicle, and wherein the HEATMS comprises:

a first module coupled to the sensors and configured to receive sensor data;

a second module coupled to the first module and configured to determine, based on the sensor data:

a peripheral electric power output;

a primary electric power output;

a battery power output; and

a pump power, a pump fluid flowrate, or both.

12. The system of claim 11 , wherein the plurality of sensors are configured to receive the sensed data that comprises ambient air temperature, ambient air pressure, aircraft velocity, aircraft altitude, aircraft GPS position, peripheral electric power unit output voltage, peripheral electric power unit output current, air inlet flow rate, air inlet temperature, air inlet pressure, air/water outlet flow rate, air/water outlet temperature, air/water outlet pressure, hydrogen inlet flow rate, hydrogen inlet temperature, hydrogen inlet pressure, speed reducer temperature, compressor inlet flow rate, compressor inlet temperature, compressor inlet pressure, compressor outlet flow rate, compressor outlet temperature, compressor outlet pressure, turbine inlet flow rate, turbine inlet temperature, turbine inlet pressure, turbine outlet flow rate, turbine outlet temperature, turbine outlet pressure, propeller rotational speed, radiator cooling fluid inlet temperature, radiator cooling fluid outlet temperature, a pilot control, or any combination thereof.