公开(公告)号：US20240007025A1

公开(公告)日：2024-01-04

申请号：US17827188

申请日：2022-05-27

Applicant: Rolls-Royce Corporation

Inventor： David R. Trawick ,  Matthew Hill ,  Chandana J. Gajanayake

IPC: H02P3/06 ,  B64D31/00 ,  H02K1/12 ,  H02K1/27 ,  H02K7/00 ,  H02K11/33 ,  B64D27/10 ,  B64D27/24 ,  B64D35/08

CPC classification number: H02P3/06 ,  B64D31/00 ,  H02K1/12 ,  H02K1/27 ,  B64D2027/026 ,  H02K11/33 ,  B64D27/10 ,  B64D27/24 ,  B64D35/08 ,  H02K7/003

Abstract: An aircraft includes an internal combustion engine and an electrical power system. The electrical power system includes a permanent magnet machine and an inverter coupled to the permanent magnet machine. The permanent magnet machine includes a stator and a rotor configured to rotate relative to the stator.