GAS TURBINE BURNER ASSEMBLY EQUIPPED WITH A HELMHOLTZ RESONATOR
    7.
    发明公开
    GAS TURBINE BURNER ASSEMBLY EQUIPPED WITH A HELMHOLTZ RESONATOR 审中-公开
    有亥姆霍兹共振器燃气轮机燃烧器装置

    公开(公告)号:EP2938927A1

    公开(公告)日:2015-11-04

    申请号:EP13831874.6

    申请日:2013-12-27

    CPC classification number: F23R3/286 F23R3/343 F23R2900/00014

    Abstract: A burner assembly for a gas turbine includes a main burner (20), extending about an axis (B), and a Helmholtz resonator (22) having a resonant chamber (35) and passages (36, 37) for fluidic connection of the resonant chamber (35) to the outside. The main burner (20) further includes an inner body (25) and an outer body (26), which extend about the axis (B), and a swirler (23), arranged between the inner body (25) and the outer body (26) and defining mixing channels (30). The resonant chamber (35) is arranged about the outer body (26) adjacent to an inlet (31) of the swirler (23). The outer body (26) delimits a portion of the resonant chamber (35) and is shaped so as to prevent direct fluidic connections between the Helmholtz resonator (22) and the mixing channels (30).

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