The Boeing Company

Alan Thomas Bernier

Thomas A Campbell

Edward Zielinski

Charles Steven Meis

Warren Andrew Atkey

Jian Huang

Farhad Nozari

Charles J Fiterman

Michael D Bowman

Jonathan M Cruse

Casey Y K Ng

Ernest H Kanning

Jeffrey Joseph White

Thomas F Currier

Christopher Mark Severns

Casey Ng

Mark Dixon Ralston

Kent W Knechtel

Casey Y Ng

A transformer comprising a core and a plurality of conductor lines. Each conductor line in the plurality of conductor lines comprises at least three windings wound around the core such that a phase voltage at an output connection point associated with a corresponding conductor line of the plurality of conductor lines is substantially a selected percentage of a line voltage for the corresponding conductor line and such that harmonic currents are reduced to within selected tolerances.

Multi-phase autotransformer

A method and apparatus for transferring power to a load. An AC-to-DC converter output for an AC-to-DC converter is connected to a filter circuit input in a DC-to-DC converter via a connector such that a no-break power transfer occurs when transferring between providing power for the load by the AC-to-DC converter and providing power for the load by the DC-to-DC converter. The topology of the AC-to-DC converter needs only 21 windings for achieving a 24-pulse transformer rectifier unit.

No-break power transfer

A method and apparatus for forming a direct current power supply. An apparatus comprises a transformer and a rectifier. The transformer is figured to output a plurality of phase-shifted alternating currents in response to receiving a plurality of alternating currents. The plurality of alternating currents and the plurality of phase-shifted alternating currents form a plurality of input alternating currents that are offset relative to each other by one-twelfth of a cycle in phase. The rectifier is configured to form a direct current power supply having a common mode voltage reduced to zero within selected tolerances in response to receiving the plurality of input alternating currents.

Six-phase supplied transformer rectifier unit

Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet engine. The jet engine can be configured to provide propulsive thrust to the aircraft, and the electric generator can be configured to receive shaft power from the jet engine. The environmental control system can be configured to provide outside air to a passenger cabin of the aircraft in the absence of bleed air from the jet engine.

Electric-based secondary power system architectures for aircraft

Methods and systems for starting aircraft turbofan engines are disclosed. A system in accordance with one embodiment includes an electrically-powered starter motor coupled to a turbofan engine to provide power to the turbofan engine during an engine start procedure. The system can further include an on-board, deployable, ram air driven turbine coupled to an electrical generator, which is in turn coupled to the starter motor to provide electrical power to the starter motor. In other embodiments, the ram air driven turbine can be replaced with a fuel cell or a battery. In still further embodiments, a single controller can control operation of both the engine starter and other motors of the aircraft.

Systems and methods for starting aircraft engines

A data collection network and electrical power distribution network designed to reduce airplane wire weight and allow nearly complete wiring design and installation of wiring and equipment in the major structural sections of the airplane.

Aircraft electrical power distribution network

Growing community of inventors

Woodinville, WA, United States of America

Alan Thomas Bernier