초록 ▼

The invention relates to an exhaust nozzle for a bypass turbomachine, the nozzle comprising a central body, a primary cowl surrounding the central body to define a primary channel, and a secondary cowl surrounding the primary cowl to define a secondary annular channel, the secondary cowl comprising

The invention relates to an exhaust nozzle for a bypass turbomachine, the nozzle comprising a central body, a primary cowl surrounding the central body to define a primary channel, and a secondary cowl surrounding the primary cowl to define a secondary annular channel, the secondary cowl comprising a stationary portion and a movable portion disposed to extend the stationary portion and capable of moving longitudinally upstream and downstream relative to the stationary portion and relative to the primary cowl so as to vary the exhaust section and/or the throat section of the nozzle, the stationary portion of the secondary cowl presenting a plurality of spaced-apart repetitive patterns disposed extending its trailing edge, and the movable portion of the secondary cowl including in its outside surface a plurality of indentations of shapes complementary to the patterns of the stationary portion.

대표청구항 ▼

What is claimed is: 1. A gas exhaust nozzle for a bypass turbomachine, the nozzle comprising an annular central body centered on a longitudinal axis of the nozzle, an annular primary cowl surrounding the central body coaxially so as to co-operate therewith to define a primary annular channel, and a

What is claimed is: 1. A gas exhaust nozzle for a bypass turbomachine, the nozzle comprising an annular central body centered on a longitudinal axis of the nozzle, an annular primary cowl surrounding the central body coaxially so as to co-operate therewith to define a primary annular channel, and an annular secondary cowl surrounding the primary cowl coaxially so as to co-operate therewith to define a secondary annular channel coaxial with the primary channel, wherein the secondary cowl comprises a stationary portion and a movable portion extending the stationary portion longitudinally and capable of moving longitudinally upstream and downstream relative to the stationary portion and relative to the primary cowl so as to vary the exhaust section and/or the throat section of the nozzle, the stationary portion of the secondary cowl presenting a plurality of repetitive patterns circumferentially spaced apart and longitudinally extending its trailing edge, and the moving portion of the secondary cowl having in its outside surface a plurality of indentations of shapes complementary to the patterns of the stationary portion. 2. A nozzle according to claim 1, in which the moving portion of the secondary cowl presents an inside diameter that decreases going downstream, and the primary cowl presents in its portion facing the movable portion of the secondary cowl, a downstream annular portion having an outside diameter that decreases going downstream, the moving portion of the secondary cowl being movable longitudinally between two extreme positions; a downstream extreme position corresponding to a nominal exhaust section or throat section, and an upstream extreme position corresponding to an exhaust section or throat section reduced to a minimum. 3. A nozzle according to claim 1, in which the secondary cowl includes at least one actuator for moving the movable portion of said cowl longitudinally. 4. A bypass turbomachine, including a gas exhaust nozzle according to claim 1.