Methods and apparatus for supplying feed air to turbine...

Details Methods and apparatus for supplying feed air to turbine... Methods and apparatus for supplying feed air to turbine...

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/06 (2006.01) F02C 7/18 (2006.01) F23R 3/10 (2006.01) F23R 3/60 (2006.01)

Patent

CA 2472541

A combustor (16) for a gas turbine engine, including a liner (43) defining a combustion chamber (54) therein, and a casing (40) extending circumferentially around the combustor liner, the casing comprising an inlet (84) coupled in flow communication with a feed air source and a scroll duct (86) coupled in flow communication with the inlet and extending at least partially circumferentially around the liner.

Chambre de combustion (16) pour un moteur à turbine au gaz, comprenant une chemise de chambre de combustion (43) qui délimite la chambre de combustion (54) à l'intérieur, ainsi qu'un boîtier (40) qui fait le tour de la chemise de chambre de combustion. Ce boîtier comprend un orifice d'entrée (84) couplé pour assurer un passage pour une source d'alimentation en air et une conduite en spirale (86) couplée pour assurer un passage avec l'orifice d'entrée et qui s'étend au moins partiellement autour de la chemise de chambre de combustion.

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