Damper for gas turbines
A gas turbine and damper technology, applied in combustion chambers, combustion methods, combustion equipment, etc., can solve problems such as hindering dampers, and achieve the effect of extending operating life
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[0045] figure 1 A schematic cross-sectional view of a damper 100 with a portion of a combustor 200 of a gas turbine is shown according to an embodiment of the invention, with some portions cut away for clarity. The damper 100 includes a resonant cavity 110 having a box shape or a cylindrical shape as defined by the peripheral wall 102 and the inlet 104 . Such as figure 1 As shown, the main part of the resonant cavity 110 is cut away, because this will not hinder a complete and complete understanding of the technical solution of the present invention. Also, for clarity and conciseness, figure 1 Only those parts of the combustion chamber 200 that are closely relevant to the invention are shown. Resonant cavity 110 consists of figure 1 Fasteners, not shown, are hermetically attached to the structure 106 of the combustion chamber 200 . In an exemplary embodiment of the invention, the structure 106 of the combustor 200 may be a shell of the combustor 200 . Those skilled in th...
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