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AssigneeSociete Nationale d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
InventorsXavier Jean Michel Andr{acute over (e)} Guyonnet, Pascal Claude Wurniestky
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A rear mixer ejector of a turbomachine for a supersonic aircraft has an ejector casing of rectangular cross-section fitted with movable flaps defining a variable geometry exhaust nozzle, and cold air mixing devices mounted on the casing side walls upstream of the nozzle. The mixing devices comprise a plurality of U-section chutes extending into the casing from apertures in the casing side walls, each chute being formed by a pair of lateral walls and a transverse wall disposed between them. The chutes are adjustable between a deployed position and an inoperative position, either by pivoting the chutes about axes at the downstream edges of the apertures or by pivoting only the transverse walls about the upstream edges of the apertures. In each case the lateral walls of the chutes remain in the gas flow path through the casing, parallel to the casing axis, in both the deployed and the inoperative positions, and the transverse walls are parallel to the casing axis in the inoperative position.
A rear mixer ejector of a turbomachine for supersonic aircraft, comprising a casing having opposed top and bottom walls and opposed side walls defining a substantially rectangular cross-section, said casing having a central axis and defining a flow path for the gases exhausted from the gas generator of said turbomachine, movable variable geometry flaps in said top and bottom walls of said casing forming a variable geometry gas exhaust nozzle, air inlet apertures provided in said side walls of said casing upstream of said exhaust nozzle, and mixer means which are mounted on said side walls adjacent said air inlet apertures and are adjustable between an inoperative position and a deployed position wherein said mixer means are operative to channel into said gas flow path cold air which enters said casing from outside through said air inlet apertures, said mixer means on each of said side walls comprising a plurality of spaced apart chutes each mounted adjacent a respective air inlet aperture, each chute comprising two spaced lateral walls of substantially triangular shape and a transverse wall extending between said lateral walls to define a chute bottom which extends angularly into said gas flow path in the downstream direction when said mixer means are in the deployed position, said chutes on each of said side walls being of unitary construction and mounted to pivot between said inoperative position and said deployed position about an axis which is disposed at the downstream edge of the respective air inlet apertures and remote from said chute bottoms, whereby said chutes are disposed in said gas flow path in both said inoperative and deployed positions with said chute bottoms extending parallel to said central axis in said inoperative position, means being provided for closing said air inlet apertures when said chutes are in said inoperative position.
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