A thrust reverser comprises a translating sleeve panel (130). A first articulating slider (170) and a second articulating slider (171) are located at a circumferential end of the translating sleeve panel (130). Each of the first articulating slider (170) a...

A thrust reverser cascade flow directing element (28) for a gas turbine engine (10) comprises a plurality of plates (30) and a plurality of flow directing vanes (40). At least one vane (40) extends between each pair of plates (30), the plurality of plates ...