Premix fuel injector with low acoustics

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

Patent

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Details

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 2225393

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 combustor 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 30% of the first distance.

Injecteur de carburant avec entrée d'air tangentielle comportant un orifice d'admission de chambre de combustion afin de permettre au mélange air-carburant d'arriver dans une chambre de combustion. L'orifice comprend une surface convergente, une surface de chambre de combustion et une surface cylindrique comprise entre les deux. La surface convergente s'étend sur une première distance le long de l'axe longitudinal de l'injecteur, la surface cylindrique s'étend sur une deuxième distance le long de l'axe et la deuxième distance correspond à 30 %, au moins, de la première distance.

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