Rtx Corporation

Milos Ilak

Neil J Terwilliger

Abbas A Alahyari

Pratyush Kumar

Yasir Al-Nadawi

Daniel T Pollock

A propulsion system for an aircraft includes at least two steam generation assemblies that each include a condenser where water is extracted from the gas flow and an evaporator where the extracted water is heated to generate a portion of a total steam flow for injection into the core flow path. A monitoring system is configured to gather information indicative of operation of each of the at least two steam generation assemblies. A control system is configured to independently adjust operation of each of the at least two steam generation assemblies.

Steam injected turbine engine steam generation control

A method for a hybrid electric propulsion (HEP) system includes utilizing a soft actor-critic agent, which includes at least one neural network, and a control barrier function (CBF) filter to obtain a power splitting profile for an HEP system. The power splitting profile includes an electric motor power for an electric motor of the HEP system and a gas turbine power for a gas turbine of the HEP system. The electric motor power and gas turbine power collectively provide a combined HEP output power. The method also includes, during a flight of an aircraft that includes the HEP system, performing an output action for the HEP system based on the power splitting profile. The utilizing is performed based on a predefined fuel consumption objective and a state of charge of at least one battery that powers the electric motor. A system for a HEP system is also disclosed.

System and methods for power split algorithm design for aircraft hybrid electric propulsion based on combined actor-critic RL agent and control barrier function filter

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Milos Ilak