Patent ID: 9548639
Date: 2017-01-17
CPC Classifications: F01D,F02C,F02N,F05D,H02K

Claim:
1. A power generation unit for an aircraft engine, which unit is connected with an engine rotary shaft of the aircraft engine via an accessory gearbox, the power generation unit comprising: a rotor extending through the accessory gearbox and having an intermediate portion positioned longitudinally intermediate of the rotor, and opposite side portions with the intermediate portion intervening therebetween; a drive gear mounted on the intermediate portion of the rotor to drive the rotor; permanent magnet elements respectively mounted on outer peripheries of the opposite side portions of the rotor; and stator coils disposed separately from each other so as to respectively confront outer peripheries of the permanent magnet elements and the outer periphery of the rotor on which the permanent magnet elements are mounted, the stator coils being electrically connected with each other.