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US Patent 11041443 Multi-spool gas turbine engine architecture

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Is a

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Patent attributes

Patent Jurisdiction

United States Patent and Trademark Office

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Patent Number

Patent Inventor Names

Martin Poulin0

Jean Dubreuil0

Keith Morgan0

Lazar Mitrovic0

Eric Durocher0

Date of Patent

June 22, 2021

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Patent Application Number

165838960

Date Filed

September 26, 2019

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Patent Citations

US Patent 10113482 Gearbox for gas turbine engine

US Patent 10125722 Turbine engine with a turbo-compressor

US Patent 10054001 V-shaped gearbox for driving turbomachine equipment

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US Patent 10072570 Reverse flow gas turbine engine core

US Patent 10082080 Fan rotor for a turbo machine such as a multiple flow turbojet engine driven by a reduction gear

US Patent 10087761 Devices and methods for balancing a high-pressure spool of a gas turbine engine

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US Patent 10094295 Gas turbine engine with transmission

Patent Citations Received

US Patent 11668253 System and method for providing in-flight reverse thrust for an aircraft

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Patent Primary Examiner

Ehud Halberstam

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Patent abstract

A multi-spool gas turbine engine comprises a low pressure (LP) spool and a high pressure (HP) spool independently rotatable about a central axis extending through an accessory gear box (AGB). The LP spool has an LP compressor, which is axially positioned between the HP compressor of the HP spool and the AGB. A tower shaft drivingly connects the HP spool to the AGB.

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