Hamilton Sundstrand Corporation

Diego Rocha

Glenn C Lemmers, Jr

Dhaval S Patel

Andreas C Koenig

Ted A Martin

Duane C Johnson

Derek R Hochstetler

Eric A Brust

Jonathan C Dell

John F Defenbaugh

A rotor for a permanent magnet generator includes a rotor body extending between a first end and a second end, having a cylindrical bore and a plurality of flats on an outer peripheral surface. Permanent magnets are positioned at the flats. An outer ring surrounds the permanent magnets and defines an outer diameter. A ratio of the outer diameter to an axial length between the first and second ends is between 3.2 and 3.4. An integrated drive generator and a method are also disclosed.

Permanent magnet generator rotor for integrated drive generator

An aircraft main power generation system includes a rotor shaft, a main power generator a permanent magnet, an exciter, an aircraft power bus, and a generator control unit. The generator control unit is configured to provide a control current to the exciter in response to a speed of the main power generator reaching a threshold speed and electrically couple the main power generator to the aircraft power bus in response to the speed of the main power generator reaching a minimum operating speed, the threshold speed being lower than the minimum operating speed; or provide a control current to the exciter in response to the speed of the main power generator reaching a predetermined speed and electrically coupling the main power generator to the aircraft power bus in response to a time period elapsing after the speed of the main power generator has reached the predetermined speed.

Wound field generator overvoltage prevention

Growing community of inventors

Rockford, IL, United States of America

Diego Rocha