FIELD: transport.
SUBSTANCE: thrust reverser for a dual-flow turbojet engine gondola includes a static part, a downstream moveable cowl, driving means and means for directional movement of the moveable cowl, relative to the static part, as well as air foil lattices. The cowl is made capable to move between the forward thrust position and thrust reversion position. Air foil lattices are oriented at an angle relative to the moveable cowl movement. Driving means and means for directional movement of the moveable cowl are located between the adjacent lattices, and a covering wall is provided which connects the said adjacent lattices bypassing the driving and directional movement means. The covering wall is formed by an additional air foil lattice made in such a way that it intensifies deviation of the said secondary flow forward along the flow. The second invention in the set relates to the dual-flow turbojet engine gondola including the above-mentioned thrust reverser. One more invention in the set relates to an aircraft with such gondola.
EFFECT: set of inventions permits to increase efficiency of the secondary flow deviations during reversing the thrust of the dual-flow turbojet engine.
9 cl, 14 dwg
