An exhaust assembly (52) for a gas turbine engine (40) which includes a turbine rear frame (75). The exhaust assembly comprises an engine exhaust nozzle (76) extending downstream from the turbine rear frame and an infrared suppression system (72) coupled i...

An engine nozzle (21, 31, 41, 51, 61) is described in which the nozzle is deformable from a first state, typically a round shape, to a second state which may approach a polygon or have a fluted edge. The first and the second state defining different nozzle...

An acoustically treated bullnose fairing assembly for a thrust reverser of an aircraft, the thrust reverser having an outer fixed structure and a stowable blocker door. The bullnose fairing assembly includes a back sheet, a face sheet and a honeycomb struc...

Device for reducing the IR target signature of aircraft threatened by guided missiles with IR seeker heads comprises a high pressure tank (1) containing a piston (4) dividing the inner chamber of the tank into a gas chamber (3) and a liquid chamber (2) and...