AIRCRAFT DEICING SYSTEM

摘要

A deicing system (10) for preventing ice accumulation on an airfoil surface (14) of an aircraft (12). The system (10) can comprise a control module (66) which controls a valve (64) based on pressure conditions within the deicer chambers (30), a reservoir (60) for providing pressurized inflation fluid to the deicer chambers (30), and/or a line (62) for providing the deflation suction for the airfoil's low-pressure side (18).