Turbine engine combustion chamber with tangential slots

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

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F23R 3/60 (2006.01) F23R 3/46 (2006.01)

Patent

CA 2577527

L'invention concerne une chambre de combustion annulaire de turbomachine, comportant des parois longitudinales (6, 8) reliées par un fond de chambre transversal (10) et un carénage (12) monobloc, le fond de chambre (10) et le carénage (12) comprenant chacun une bride interne (16, 20) et une bride externe (18, 22) percées chacune d'une pluralité de trous pour le passage de systèmes de fixation (14a, 14b) pour la fixation du carénage sur le fond de chambre. A chaque système de fixation, est associée au moins une fente tangentielle (30) formée sur la bride (16, 18) correspondante du fond de chambre (10) et/ou sur la bride (20, 22) correspondante du carénage (12), chaque fente (30) étant formée au voisinage immédiat du système de fixation (14a, 14b) correspondant.

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