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Pat. 10801414 United States, Int. Cl.22 F02C 7/266, F02P 3/00, F02P 3/08, F02P 3/12, F02P 9/00, F02P 15/00, H02M 1/00, H02M 7/00, H02M 7/06. Gas turbine engine including a rectifierless electronic control unit and method for supplying power to same : Appl. N 15/413681 : Filed 24.01.2017 : Pub. 13.10.2020 : / Jeff M. Kelly ; Assignee Honeywell International Inc ; NN p. : patents.google.com : URL: https://patents.google.com/patent/US10801414/en?oq=US10801414.html (дата обращения: ДД.ММ.ГГГГ).