#MRA SYSTEMS INC [US]

THRUST REVERSER ASSEMBLY AND METHOD OF OPERATION

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…

DRIVE·Nov 6·2 min read

F02K1/70 MRA SYSTEMS INC [US]

Turbomachine Nacelle And Anti-Icing System And Method Therefor

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-sectiona…

DRIVE·Aug 10·1 min read

B64D15/12 MRA SYSTEMS INC [US]

Turbomachine Nacelle And Anti-Icing System And Method Therefor

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…

DRIVE·Aug 10·1 min read

F02C7/047 MRA SYSTEMS INC [US]