METHOD FOR DETECTING A BLEED AIR SYSTEM FAULT

摘要

A method (100) of detecting a fault in a bleed air system (20) of an aircraft (10) having multiple engines (12) including transmitting a bleed air flow rate (102) from multiple engines, determining a difference (104) between the transmitted bleed air flow rates to define a difference value, determining (110), by a controller (50, 60), a fault condition with the bleed air system based on the difference value.