US 12,379,107 B2
Combustor nozzle, combustor and gas turbine including same
Afzal Pasha Mohammed, Palm Beach Gardens, FL (US); Jose Grana-Otero, Kent, WA (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. 18/527,025.
Prior Publication US 2025/0180211 A1, Jun. 5, 2025
Int. Cl. F23R 3/28 (2006.01); F23R 3/12 (2006.01)
CPC F23R 3/286 (2013.01) [F23D 2900/14021 (2013.01); F23R 3/12 (2013.01)] 19 Claims
OG exemplary drawing
 
1. A nozzle for a combustor that burns fuel, comprising:
a mixing tube through which air and fuel can flow;
the mixing tube having an inlet formed at a longitudinal end thereof for introduction of a first fluid into the mixing tube;
the mixing tube having one or more supply ports formed on an outer circumferential surface of the mixing tube for introduction of a second fluid into the mixing tube;
the mixing tube having at least one fuel/air separator disposed interior of the longitudinal end, the at least one fuel/air separator is operative to cause a flow of the second fluid to be enveloped by a flow of the first fluid before the first fluid and the second fluid subsequently mix inside the mixing tube;
wherein each of the one or more supply ports comprises a respective cylindrically-shaped tube that extends outwardly from the outer circumferential surface of the mixing tube, each cylindrically-shaped tube being configured to communicate the second fluid from outside the mixing tube to the at least one fuel/air separator.