A gas turbine engine includes a turbomachine and a thermal management system. The
thermal management system includes a heat source heat exchanger configured to collect …

A combustion engine includes a combustion section; a fuel delivery system for providing a
fuel flow to the combustion section, the fuel delivery system including an oxygen reduction …

An apparatus and method of cooling a gas turbine engine including a core with a
compressor section in which the compressor section includes a closed loop cooling circuit …

A method of operating a thermal management system for a gas turbine engine includes
determining the gas turbine engine is in a first operating mode; transferring heat from a first …

US10941706B2 - Closed cycle heat engine for a gas turbine engine - Google Patents
US10941706B2 - Closed cycle heat engine for a gas turbine engine - Google Patents Closed …

A thermal management system includes a first heat source assembly including a first heat
source exchanger, a first thermal fluid inlet line extending to the first heat source exchanger …

A fuel system for an aircraft includes a fuel source and a fuel oxygen reduction unit defining
a liquid fuel supply path, a stripping gas supply path, a liquid fuel outlet path, and a stripping …

An engine includes a combustion section and a fuel delivery system in fluid communication
with the combustion section for providing fuel to the combustion section. The fuel delivery …

A fuel oxygen conversion unit includes a stripping gas flowpath for a vehicle or an engine of
the vehicle. The fuel oxygen conversion unit includes a stripping gas boost pump positioned …

A gas turbine engine includes a turbomachine including a compressor section, a
combustion section, a turbine section, and an exhaust section arranged in serial flow order …