Air swirl device arranged in spray nozzle of combustion chamber of gas turbine
A swirl device, gas turbine technology, applied in the combustion chamber, continuous combustion chamber, combustion method and other directions, can solve the problems of weak swirl intensity, small airflow deflection angle, poor fuel and air mixing effect, etc., to improve combustion Reliability, wide design space, effect of improved velocity distribution
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[0018] The principle, structure and specific implementation of the present invention will be further described below in conjunction with the accompanying drawings.
[0019] figure 1 , figure 2 and image 3 It is a schematic diagram of the structural principle of a gas turbine combustor nozzle equipped with an air swirl device. The air swirl device is arranged upstream of the central cone 3 in the peripheral annular air channel 2. The air swirl device 4 adopts an axial vane structure. It is best to adopt a hollow axial vane structure, which is evenly arranged along the peripheral annular air passage 2, and communicates with the central fuel passage 1 through the fuel injection hole 6, and the number of vanes is generally between 6 and 12.
[0020] The blade of the air swirl device 4 is provided with a notch 5, and the starting position is located at the bending angle change point 7 on the suction side of the blade. The intersection 8 of the cutting surface 13 of the notch 5 ...
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