burner
A technology of combustion device and combustion chamber, which is applied in the direction of gas turbine device, combustion chamber, combustion type, etc.
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[0018] Reference is now made to the drawings; the drawings include like reference numerals for like or similar parts throughout the several views.
[0019] Preferably, the combustion device is part of a gas turbine, such as a continuous combustion gas turbine 1 .
[0020] The continuous combustion gas turbine 1 comprises a compressor 2, a first combustion device 3, a first turbine 4 (high pressure turbine), a second combustion device 5 and a second turbine 6 (low pressure turbine). These gas turbines are well known in the art.
[0021] During operation, the compressor 2 compresses oxidant and supplies it to the first combustion device 3 . The oxidizing agent is usually air and is referred to below as air. The first combustion device 3 receives compressed air and fuel and burns them to produce hot gases which are partially expanded in the first turbine 4 . Exhaust gases from the first turbine 4 enter the second combustion unit 5 , where additional fuel is supplied and burned...
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