SECONDARY BURNER
    2.
    发明专利

    公开(公告)号:CA2098810A1

    公开(公告)日:1994-01-04

    申请号:CA2098810

    申请日:1993-06-18

    Inventor: KELLER JAKOB

    Abstract: 92/078 In a secondary burner for a gas turbine combustion chamber, a fuel feed (2, 3) arranged in a combustion chamber wall (1) is surrounded by an annular air duct (4). The air duct (4) communicates, by means of at least one supply tube (5), with a through-flow Helmholtz resonator (6). The outlet from the Helmholtz resonator damping tube (7), which is configured as an annular duct, is located in the region of the burner mouth (8) in the secondary combustion space (9). (Fig. 1)

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