Rocket engine having guide vanes in the nozzle of the engine

Details Rocket engine having guide vanes in the nozzle of the engine Rocket engine having guide vanes in the nozzle of the engine

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 9/97 (2006.01) F42B 10/66 (2006.01)

Patent

CA 2539835

A rocket engine having guide vanes in the engine nozzle, the guide vanes (2) being mounted for turning at or near the rearmost ends of fixed vanes (1) being parallel to the axis of the nozzle and protruding into the combustion chamber of the engine. The foremost ends (4) of the guide vanes (2) may be shielded by the rearmost ends of the fixed vanes (1), and the guide vanes (2) may be individually turnable.

L'invention concerne un moteur-fusée comportant des aubes directrices dans sa tuyère, ces aubes directrices (2) étant montées de façon à pouvoir tourner au niveau ou à proximité des extrémités arrière d'aubes fixes (1) parallèles à l'axe de la tuyère et faisant saillie dans la chambre de combustion du moteur. Les extrémités avant (4) des aubes directrices (2) peuvent être protégées par les extrémités arrière des aubes fixes (1), et les aubes directrices (2) peuvent être tournées individuellement.

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