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A guiding system of the movable fairing of a turbojet engine thrust reverser system comprising two guide pieces mounted on an upper frame fixed to a mast and pieces to be guided attached to the movable fairing. The guide pieces are provided with a groove of a circular cross section and the piece to

A guiding system of the movable fairing of a turbojet engine thrust reverser system comprising two guide pieces mounted on an upper frame fixed to a mast and pieces to be guided attached to the movable fairing. The guide pieces are provided with a groove of a circular cross section and the piece to be guided is a cylindrical body having, on a generatrix and in a radial plane, a flange, the end of which has means to fasten it to a fitting on the movable fairing.

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In a thrust reverser system of a jet engine having a stationary casing attached to a mast and a section of a nacelle fairing movable between a deployed position, wherein the thrust of the jet engine is reversed, and a stowed position, the improved means for slidably mounting the movable section of t

In a thrust reverser system of a jet engine having a stationary casing attached to a mast and a section of a nacelle fairing movable between a deployed position, wherein the thrust of the jet engine is reversed, and a stowed position, the improved means for slidably mounting the movable section of the nacelle fairing comprising: (a) a pair of upper guide pieces, each guide piece defining a longitudinal groove having a generally circular cross-section and a slot extending through a wall along the length of the upper guide piece, the plane of the slot being approximately perpendicular to a median vertical plane of the nacelle; (b) first means to attach the upper guide pieces to an upper portion of the stationary casing such that the slots open in opposite directions; (c) a pair of lower guide pieces, each guide piece defining a longitudinal groove having a generally circular cross-section and a slot extending through a wall along the length of the lower guide pieces, the plane of the slot being approximately pependicular to a median vertical plane of the nacelle; (d) second means to attach the lower guide pieces to a lower portion of the stationary casing such that the slots open in opposite directions; (e) a pair of upper guided elements having generally circular cross-sections, one of the upper guided elements slidably disposed in each of the grooves in the upper guide pieces, each of the upper guided elements having a radial flange extending from its periphery through the slot in the upper guide piece; (f) means to attach the flanges of the upper guided elements to an upper portion of the movable nacelle portion; (g) a pair of lower guided elements having generally circular cross-sections, one of the lower guided elements slidably disposed in each of the grooves in the lower guide pieces, each of the lower guided elements having a radial flange extending from its periphery through the slot in the lower guide piece; (h) means to attach the flanges of the lower guided elements to a lower portion of the movable nacelle portion; and, (i) friction reducing means interposed between the upper and lower guided elements and the surfaces of the grooves in the upper and lower guide pieces to reduce the sliding friction therebetween.