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

Abstract

The present disclosure provides systems and methods for a hydrogen-powered hybrid electric powertrain and the associated hydro-electro-aero-thermal management system (HEATMS).

1 .- 10 . (canceled) 
     
     
         11 . A thermally managed hydrogen-powered hybrid electric powertrain system for a hydrogen-powered vehicle, the system comprising:
 hydrogen fuel cells configured to generate electricity;   A first electric power unit that receive the electricity from the hydrogen fuel cells, wherein the one or more first electric power units generates thermal energy;   one or more radiators configured to receive and thermally dissipate the thermal energy from the first electric power unit;   a turbine configured to receive mechanical power from the fuel cells;   a second compressor configured to receive the mechanical power from the turbine and to direct first compressed air to the turbine and the fuel cells; and   a first compressor configured to provide second compressed air to the second compressor; and   a hydrogen-powered powertrain and hydro-electro-aero-thermal management system (HEATMS) configured to control and manage thermal energy generated b the hydrogen-powered powertrain, 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 first electrical power unit; 
 controlling an amount of air mass flow rate to the fuel cells to direct an amount of air to the fuel cells 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 fuel cells before occurrence of the predicted electrical power demand for generation of an output of electrical power by the fuel cells 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. 
   
     
     
         12 . The system of  claim 11 , further comprising 1) a speed reducer coupled to the first electric power unit and configured to receive mechanical power from the first electric power unit; and 2) a peripheral electric power unit, wherein the first compressor receives power from the peripheral electric power unit. 
     
     
         13 . The system of  claim 11 , 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 fuel cells and transmit the electrical power to the peripheral electric power unit, wherein the battery does not provide electrical power to the first electrical power unit. 
     
     
         14 . The system of  claim 11 , further comprising a water distribution system configured to receive the exhaust water generated by the fuel cells and to direct the exhaust water an exhaust outlet, wherein at least a portion of the exhaust water passes through the turbine, and the turbine is configured to direct the exhaust water to the water distribution system. 
     
     
         15 . The system of  claim 14  wherein the turbine is configured to further transmit a fluid to an exhaust. 
     
     
         16 . The system of  claim 11 , further comprising a deicing system configured to receive a fluid from the turbine. 
     
     
         17 . The system of  claim 14  wherein the water distribution system comprises a spray bar forming the exhaust outlet and configured to direct the exhaust water onto the radiator. 
     
     
         18 . (canceled) 
     
     
         19 . (canceled) 
     
     
         20 . 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 heat;   one or more pumps configured to transmit coolant to the one or more radiators;   one or more fuel cell stacks configured to transmit thermal energy to the one or more radiators;   a primary electric power unit configured to transmit the thermal energy to the one or more radiators and receive electrical power from the one or more fuel cell stacks;   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 first 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 an exhaust outlet.   
     
     
         21 . The system of  claim 11 , further comprising a plurality of sensors onboard the vehicle, and wherein the HEATMS comprises:
 a first module configured to receive sensor data;   a second module 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.   
     
     
         22 . The system of  claim 20 , wherein the plurality of sensors are configures 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. 
     
     
         23 . The system of  claim 21 , wherein the second module is configured to determine the peripheral electric power output, the primary electric power output, the battery power output, the pump power, the pump fluid flow rate, or any combination thereof from the sensor data using a machine learning algorithm.