Ignition-supplementing combustion chamber and gas turbine system
A gas turbine and combustor technology, which is applied in the direction of using various fuel combustion, combustion methods, combustion types, etc., can solve the problems of the maximum state drop of flue gas temperature, large gap between peak and valley electricity prices, and limited adjustment range, etc., to achieve structural and Ease of control, reduced emissions, and improved regulation range
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[0020] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0021] Such as figure 1 with figure 2 As shown, a post-combustion combustor 1 provided by the embodiment of the present invention includes a combustor casing 11, a flame tube 12, a fuel nozzle 13 and an igniter 14, and the combustor casing 11 is arranged behind the gas turbine 2. In the gas flue, the flame tube 12 is located in the combustion chamber casing 11, including the main combustion zone A and the middle zone B arranged in sequence from the front end...
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