POWER DISTRIBUTION SYSTEM AND METHOD OF OPERATING
Applicants
GE Aviation Systems LLC
Inventors
DALAL, Manish Ashvinkumar
Abstract
A power distribution system (11), (111) for an aircraft (10), and method (400) of operating includes, including determining, by a supplemental electrical power system (30), an operating mode of the aircraft (10), selecting, by the supplemental electrical power system (30), at least one supplementary power source (34a), (34b), (34c) of a set of at least two supplementary power sources (34), and at least one of receiving, by the selected at least one supplementary power source (34a), (34b), (34c), a first current (51) from the primary power bus (23), or selectively providing a second current (52) to the primary power bus (23) from the selected at least one supplementary power source (34a), (34b), (34c).
IPC Classifications
Designated States
AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LI, LT, LU, LV, MC, ME, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR