Two stream tangential entry nozzle

Details Two stream tangential entry nozzle Two stream tangential entry nozzle

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/14 (2006.01) F23C 7/00 (2006.01) F23D 14/02 (2006.01) F23D 14/62 (2006.01) F23D 17/00 (2006.01)

Patent

CA 2225309

A tangential air entry fuel nozzle has a combustor inlet port to permit air and fuel to exit into a combustor. The port includes a convergent surface, a divergent surface, and a cylindrical surface extending therebetween. The convergent surface extends a first distance along the longitudinal axis of the nozzle, the cylindrical surface extends a second distance along the axis, and the second distance is at least 5% of the first distance.

Injecteur de carburant à entrée d'air tangentielle, comportant un orifice d'admission de chambre de combustion, pour permettre l'air et le carburant de sortir dans une chambre de combustion. L'orifice comporte une surface convergente, une surface divergente et une surface cylindrique entre les deux. La surface convergente se prolonge sur une première distance le long de l'axe longitudinal de l'injecteur, la surface cylindrique se prolonge sur une deuxième distance le long de l'axe et la deuxième distance équivaut à 5 %, au moins, de la première distance.

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