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US Patent 10883424 Multi-spool gas turbine engine architecture

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Patent Citations Received
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US Patent 11879386 Modular multistage turbine system for gas turbine engines
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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. The LP pressure spool has an LP compressor and an LP turbine. The HP spool has an HP turbine and an HP compressor. An accessory gear box (AGB) is drivingly connected to the HP spool. The LP compressor is disposed axially between the HP compressor and the AGB. A gear train drivingly couples the LP compressor to the LP turbine. The gear train is integrated to the AGB.

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Patent Inventor Names
Guy Lefebvre0
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US Patent 11655757 Modular multistage compressor system for gas turbine engines
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10883424
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 US Patent 10883424 Multi-spool gas turbine engine architecture

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
10883424
Date of patent
January 5, 2021
Patent application number
15384959
Date Filed
December 20, 2016
Patent citations
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US Patent 10054001 V-shaped gearbox for driving turbomachine equipment
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US Patent 10072570 Reverse flow gas turbine engine core
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US Patent 10094295 Gas turbine engine with transmission
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US Patent 10125722 Turbine engine with a turbo-compressor
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US Patent 10132198 Support apparatus for disassembling and assembling gas turbine engine
Patent primary examiner
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Patrick Hamo

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