ELECTRIC-BASED SECONDARY POWER SYSTEM ARCHITECTURES FOR AIRCRAFT
摘要
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.
申请公布号
EP1554174(B1)
申请公布日期
2016.08.10
申请号
EP20030796354
申请日期
2003.10.22
申请人
THE BOEING COMPANY
发明人
ATKEY, WARREN A.;BERNIER, ALAN T.;BOWMAN, MICHAEL D.;CAMPBELL, THOMAS A.;CRUSE, JONATHAN M.;FITERMAN, CHARLES J.;MEIS, CHARLES S.;NG, CASEY, Y. K.;NOZARI, FARHAD;ZIELINSKI, EDWARD