US Patent 11976589 Gas turbine engine system wear reduction
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US Patent 11976589 Gas turbine engine system wear reduction
Article
Patent abstract
An engine system for an aircraft includes a first gas turbine engine, a second gas turbine engine, and a control system. The control system is configured to operate the first gas turbine engine with a sub-idle fuel burn schedule based on detecting landing of the aircraft, where the sub-idle fuel burn schedule includes a reduction of an idle fuel burn schedule. The control system is configured to operate the second gas turbine engine with the idle fuel burn schedule based on detecting landing of the aircraft.
Infobox
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Patent Jurisdiction
Patent Number
Patent Inventor Names
Ramesh Rajagopalan0
Stephen A. Witalis0
Subhradeep Chowdhury0
Date of Patent
May 7, 2024
0Patent Application Number
177209000
Date Filed
April 14, 2022
0Patent Citations
Patent Primary Examiner
CPC Code
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