Gas turbine and its combustion chamber.
A combustion chamber and turbine technology, applied in the field of combustion chambers, can solve the problems of insufficient air volume, difficulty in obtaining combustion chambers, etc., and achieve the effect of effective cooling operation
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[0040] Embodiments of the present invention will be described below with reference to the accompanying drawings. first embodiment
[0041] figure 1 and figure 2 It is the first aspect of the combustion chamber of the present invention. More precisely, figure 1 is a cross-sectional view of the combustion chamber. figure 2 An important part of the combustion chamber for cooling operation. figure 1 The illustrated combustor combusts fuel to produce combustion gases that drive a turbine (not shown). The combustion chamber 10 has a nozzle portion 11 .
[0042] A pilot nozzle 12 and a main nozzle 13 are contained in the nozzle section 11 . Air compressed by an air compressor (not shown in the figure) is supplied to the nozzle portion 11 to be mixed with fuel supplied from the pilot nozzle 12 . Here the mixture of air and fuel is ignited; thereby forming a pilot flame there.
[0043] The main nozzle 13 injects fuel. Guide the flame to ignite the fuel. The ignited fuel r...
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