Turbine engine combustion chamber

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

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F23R 3/06 (2006.01) F23R 3/42 (2006.01)

Patent

CA 2577507

Chambre de combustion (10) d'une turbomachine, comprenant des orifices (52, 54) d'entrée d'air primaire et d'air de dilution formés par emboutissage et comprenant des bords (66) en saillie à l'intérieur de la chambre de combustion (10), et des moyens de réduction et/ou de relaxation des contraintes dans les bords ou au voisinage des bords de ces orifices (52, 54), ces moyens comprenant pour chaque orifice une, deux ou trois fentes formées dans le bord (66) ou autour d'une partie du bord dudit orifice (52, 54).

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