US 12,339,007 B2
Combustor nozzle, combustor and gas turbine including same
Afzal Pasha Mohammed, Palm Beach Gardens, FL (US); Brian Connolly, San Antonio, TX (US); Prabhat Jha, San Antonio, TX (US); Griffin C. Beck, San Antonio, TX (US); Dong Sik Han, Changwon-si (KR); Ho Keun Kim, Daejeon (KR); and Young Jun Shin, Seongnam-si (KR)
Assigned to Doosan Enerbility Co., Ltd., Changwon-si (KR)
Filed by DOOSAN ENERBILITY CO., LTD., Changwon-si (KR)
Filed on Dec. 1, 2023, as Appl. No. 18/527,072.
Prior Publication US 2025/0180212 A1, Jun. 5, 2025
Int. Cl. F23R 3/28 (2006.01); F23R 3/12 (2006.01)
CPC F23R 3/286 (2013.01) [F23R 3/12 (2013.01); F23D 2900/14021 (2013.01)] 18 Claims
OG exemplary drawing
 
1. A nozzle for a combustor that burns fuel, comprising:
a central nozzle,
one or more outer nozzles arranged radially around the central nozzle, comprising:
a housing coupled to one or more of an adjacent housing or the central nozzle,
a plurality of mixing tubes through which air and fuel can flow;
wherein each mixing tube in the plurality of mixing tubes comprises:
a first opening formed at a longitudinal end thereof for introduction of a first fluid into the mixing tube;
one or more intermediate openings formed on an outer circumferential surface of the mixing tube for introduction of a second fluid into the mixing tube; and
a plurality of fluid vortex generators disposed on an inner circumferential surface of the mixing tube between the longitudinal end and the one or more intermediate openings;
wherein the plurality of fluid vortex generators is disposed as a pair of fluid vortex generators, and wherein a first vortex generator of the pair of fluid vortex generators is positioned at a first distance from the first opening formed at the longitudinal end of the mixing tube and a second vortex generator of the pair of fluid vortex generators is positioned at a second distance from the first opening formed at the longitudinal end of the mixing tube, the second distance being greater than the first distance.