Burner, in particular for gas turbines
A burner and combustion air technology, applied in the direction of burner, combustion chamber, combustion method, etc., can solve the problem of changing the design of the burner
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[0028] The burner according to the invention is shown in a clearly schematic schematic diagram below with reference to figure 1 Describe the scheme that is the basis for the burner.
[0029] A burner according to the invention can optionally be arranged in combination with several burners of the same type in the combustion chamber of a gas turbine plant, the burner comprising an inner pilot burner system and a main combustion chamber concentrically surrounding the pilot burner system device system. Both the pilot burner system and the main burner system can optionally be operated with gaseous and / or liquid fuels such as natural gas or fuel oil.
[0030] The pilot burner system comprises an inner oil delivery channel 1 which is concentrically surrounded by an inner annular gas delivery channel 3 . This gas delivery channel is in turn surrounded concentrically by the inner air delivery channel or inert gas delivery channel 5 . Furthermore, a suitable ignition system (not show...
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