Is a
Patent attributes
Patent Jurisdiction
Patent Number
Patent Inventor Names
Neil Terwilliger0
Christopher J. Hanlon0
Daniel Bernard Kupratis0
Date of Patent
May 25, 2021
0Patent Application Number
164312590
Date Filed
June 4, 2019
0Patent Citations Received
Patent Primary Examiner
Patent abstract
An aircraft gas turbine engine system comprises first and second gas turbine engines connected by an inter-engine gas path. The first gas turbine engine has a first spool with a first compressor section, and a second spool with a second compressor section downstream of and rotationally independent from the first compressor section. The second gas turbine engine is configured to provide power to at least one of the first and second spools of the first gas turbine engine. The inter-engine gas path is disposed to receive gas flow bled from a bleed location in the first gas turbine engine downstream of the first compressor section, and to supply this gas flow to an inlet of the second gas turbine engine.
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