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Gas Turbine Engine with Air/Fuel Heat ExchangerOne embodiment of the present invention is a unique aircraft propulsion gas turbine engine. Another embodiment is a unique gas turbine engine. Another embodiment is a unique gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines with heat exchange systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
Document ID
20170009534
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Karam, Michael Abraham
Donovan, Eric Sean
Krautheim, Michael Stephen
Vetters, Daniel Kent
Chouinard, Donald G.
Date Acquired
October 4, 2017
Publication Date
September 26, 2017
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-14/319,680
Patent Number: US-Patent-9,771,867
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,771,867
Patent Application
US-Patent-Appl-SN-14/319,680

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