Dual fuel nozzle tip assembly
AssigneeGeneral Electric Company
InventorsBorys Borysovych Shershnyov, Leonid Yulyevich Ginessin
Life of this patent
Estimating the term…
Loading patent…
AssigneeGeneral Electric Company
InventorsBorys Borysovych Shershnyov, Leonid Yulyevich Ginessin
Estimating the term…
A fuel nozzle for a combustor includes a burner tube and a center nozzle assembly disposed within the burner tube. The center nozzle assembly includes a center body that at least partially defines a cooling air flow passage through the center nozzle assembly. A premix flow passage is defined between the burner tube and the center nozzle assembly. A tip assembly is disposed at a downstream end of the center body. The tip assembly includes an impingement plate, and a cap that is disposed downstream from the impingement plate. The impingement plate and the cap at least partially define a cooling plenum therebetween. An insert passage extends through the impingement plate and a cooling flow outlet extends through the cap. A plurality of cooling ports extends through the impingement plate to provide for fluid communication between the cooling air flow passage and the cooling plenum.
A fuel nozzle for a combustor, the fuel nozzle comprising:
A tip assembly for a fuel nozzle, comprising:
A gas turbine comprising:
Dependencies are inferred from the claim text.