A thrust reverser assembly (12C) and operation suitable for high-bypass turbofan engines (10). The thrust reverser assembly includes a translating cowl (34A) mounted to a nacelle (12) of an engine and adapted to translate in an aft direction of the engine....

An anti-icing system (60,80) and method for an aircraft engine nacelle (50,70). The nacelle (50,70) has an inlet lip (56,76) that defines a leading edge of the nacelle (50,70) and has a cross-sectional shape and oppositely-disposed exterior and interior su...

An anti-icing system for a nacelle (50) of an aircraft engine (10). The nacelle (50) has an inlet lip (56) that defines a leading edge of the nacelle (50), and further has an annular-shaped cavity (58) adjacent and delimited in part by an interior surface ...