Aircraft secondary electric load controlling system

Details Aircraft secondary electric load controlling system Aircraft secondary electric load controlling system

B - Operations, Transporting

64

D

B64D 31/00 (2006.01) B60L 1/00 (2006.01) B64D 41/00 (2006.01) H02J 3/00 (2006.01)

Patent

CA 2472409

A method of controlling electrical load power consumption during operation of an aircraft (12) includes determining current operating conditions of the aircraft (12). An engine secondary power extraction limit is determined in response to the current operating conditions. Engine secondary power extraction is determined. Multiple secondary loads (18) are operated in response to the engine secondary power extraction limit and the engine secondary power extraction.

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