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US Patent 10196923 Operation of aircraft engines during transient conditions

Patent 10196923 was granted and assigned to Pratt & Whitney Canada on February, 2019 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributors
Is a
Patent
Patent
1
Current Assignee
Pratt & Whitney Canada
Pratt & Whitney Canada
1
Date Filed
August 28, 2014
1
Date of Patent
February 5, 2019
1
Patent Applicant
Pratt & Whitney Canada
Pratt & Whitney Canada
1
Patent Application Number
14471130
1
Patent Citations Received
‌
US Patent 11415065 Material fatigue improvement for hybrid propulsion systems
1
‌
US Patent 11867069 Hybrid electric variable area turbine
2
‌
US Patent 11428171 Electric machine assistance for multi-spool turbomachine operation and control
‌
US Patent 11542872 Hybrid gas turbine engine system powered warm-up
‌
US Patent 11557995 Aircraft engine power-assist start stability control
‌
US Patent 11326526 Deceleration of a gas turbine
Patent Inventor Names
Jean Thomassin
1
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
1
Patent Number
10196923
1
Patent Primary Examiner
‌
Richard A. Edgar
1

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