Wall for combustion chamber in a turbine engine with single...

Details Wall for combustion chamber in a turbine engine with single... Wall for combustion chamber in a turbine engine with single...

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/06 (2006.01) F23R 3/10 (2006.01) F23R 3/50 (2006.01)

Patent

CA 2749632

The invention relates to a combustion chamber for a turbine engine that comprises coaxial revolution walls (14, 16) with intake openings for primary air and dilution air into the chamber, the openings in each being substantially aligned with each other about a longitudinal axis of the chamber and defining a single annular row of openings (66).

Chambre de combustion d'une turbomachine, comprenant des parois de révolution (14, 16) coaxiales comportant des orifices d'entrée d'air primaire et d'air de dilution dans la chambre, les orifices de chaque paroi étant sensiblement alignés les uns avec les autres autour de l'axe longitudinal de la chambre et formant une seule rangée annulaire d'orifices (66).

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