Pre-mixed fuel spray nozzle for gas turbine and combustor
A technology of fuel nozzles, gas turbines, applied in the field of combustion chambers
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[0040] The present invention will be described in more detail with reference to the following examples, but it should be understood that the present invention is not considered limited to these examples.
[0041] Referring now to the drawings, the same reference numerals refer to the same elements throughout the multiple figures, figure 1 Shown therein is a combustion chamber 10 with premix nozzles 12, 22 according to a first exemplary embodiment of the present invention. The main components of the combustion chamber 10 include a combustion chamber shell 14, an end cover 16, a cap 18, a reaction zone 20, a central premix fuel nozzle 12 and a plurality of peripheral premix fuel nozzles 22. The nozzles 12 and 22 are used to inject the air-fuel mixture 21 into the reaction zone 20.
[0042] Such as Figure 2 to Figure 9 As can be best seen in, the premixed fuel nozzles 12, 22 generally include a fuel and air premixer 23, a nozzle head 24, and a burner tube 25. It is worth noting that...
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