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US Patent 11326526 Deceleration of a gas turbine
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Is a
Patent
Current Assignee
Rolls-Royce
Date Filed
June 4, 2020
Date of Patent
May 10, 2022
Patent Applicant
Rolls-Royce
Patent Application Number
16892764
Patent Citations
US Patent 10196923 Operation of aircraft engines during transient conditions
US Patent 10293947 Aircraft heating system
US Patent 10436122 Fuel-air ratio control of gas turbine engines
US Patent 10583931 System and method for coordinated control of a power system
US Patent 10644630 Turbomachine with an electric machine assembly and method for operation
Patent Jurisdiction
United States Patent and Trademark Office
Patent Number
11326526
Patent Primary Examiner
Alain Chau
CPC Code
B64D 15/14
F01D 15/10
F02C 7/232
F02C 9/16
F02C 9/26
F02C 9/28
F02C 9/263
F02C 9/285
F02C 9/32
F02C 9/44
•••
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