Device for supplying oxidizing agent to a gas turbine engine...

F - Mech Eng,Light,Heat,Weapons – 23 – R

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F23R 3/28 (2006.01) F23R 3/26 (2006.01)

Patent

CA 2218459

L'invention concerne un dispositif d'alimentation en comburant d'une chambre de combustion (1) d'une turbine à gaz. Ce dispositif comprend une pluralité de diaphragme de réglage (11a, 11b) commandés par paires au moyen d'un organe de commande (21). Chaque diaphragme de réglage (11) comporte un ensemble d'aubes (12a, 12b), une couronne (16a, 16b) et un organe de réglage (27a, 27b) pour assurer le pivotement relatif de la couronne par rapport à l'ensemble d'aubes. Dans chaque paire de diaphragmes (11a, 11b), l'organe de réglage (27a) d'un diaphragme (11a) agit sur l'ensemble d'aubes (12a) tandis que l'organe de réglage (27b) de l'autre diaphragme (11b) agit suc la couronne (16b). Les circuits d'air des deux diaphragmes (16a, 16b) ont ainsi des géométries identiques.

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