Gas Turbine Combustion System
A gas turbine and combustion system technology, applied in the direction of turbine/propulsion fuel delivery system, gas turbine device, combustion chamber, etc., can solve the problem of not providing service ability, improve maintainability, high maintainability, and reduce development time and cost effects
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[0061] figure 1 Shown is a can combustor 100 that allows individual combustion operations without deleterious interaction with other individual can combustors during combustion operations. The can burner 100 includes a number of removable premix burners 10 . Therefore, according to figure 1 The can architecture includes multiple premix furnaces 10 arranged on the can burner front 15, which allow individual combustion operations.
[0062] A premix furnace 10 (eg according to EP 0704657 A1) consists of the following devices: a swirl generator basically according to EP 0321809 A1 for the combustion air flow; means for fuel injection; and a mixing path formed by mixing tubes, which Located downstream of the swirl generator, wherein the mixing path includes a transition duct extending in the direction of flow within a first portion of the path for transferring the flow formed in the swirl generator to the junction In the cross-section of the flow of the mixing path downstream ...
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