Ring-shaped turbine engine combustion chamber with improved...

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

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F23R 3/46 (2006.01) F02C 3/14 (2006.01) F23R 3/50 (2006.01) F23R 3/60 (2006.01)

Patent

CA 2500762

Chambre de combustion annulaire de turbomachine, comportant des parois annulaires interne (4a) et externe réunies par une paroi transversale, les parois interne et externe se prolongeant à leur extrémité aval par des brides de fixation interne (18) et externe destinées à être fixées respectivement sur des enveloppes interne (2a) et externe d'un carter de la turbomachine pour le maintien en position de la chambre de combustion, la bride interne (18) étant munie d'une pluralité de trous destinés à alimenter en air de refroidissement une turbine haute-pression de la turbomachine, les trous d'alimentation en air de la bride interne (18) étant répartis circonférentiellement sur au moins deux rangées (26a, 26b) disposées en quinconce.

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