Gas turbine exhaust device having a jet diffuser

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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172/22

F02C 7/00 (2006.01) F01D 25/30 (2006.01) F15D 1/04 (2006.01)

Patent

CA 1279580

PRECIS DE LA DIVULGATION: Dispositif d'échappement d'une turbine à gaz, installé entre la sortie de l'étage redresseur de cette turbine et une gaine d'échappement, constitué d'un diffuseur de jets dont l'axe est confondu avec celui de la turbine. La section des orifices de ce diffuseur varie de manière décroissante au fur et à mesure que l'on s'éloigne de la sortie turbine, caractérisé en ce que cette section varie logarithmiquement. L'invention trouve une application dans les turbines à gaz.

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