Rtx Corporation

Daniel T Pollock

Neil J Terwilliger

Abbas A Alahyari

Milos Ilak

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.

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West Hartford, CT, United States of America

Daniel T Pollock