Patent ID: 8950187
Filing Date: 2015-02-10
Classification: F23C,F23R

Abstract:
1. A premix burner of a multi-cone type for a gas turbine, said premix burner comprising: a plurality of shells which are arranged around a central burner axis and are sections of a virtual, axially extending common cone, which opens in a downstream direction, wherein the plurality of shells are displaced perpendicular to said burner axis such that a tangential slot is defined between each pair of adjacent shells, and wherein downstream ends of the shells are bordered by intersecting planes, which are defined by intersecting said shells with a virtual coaxial cylinder of a predetermined radius; and a cylindrical burner ring with an inner radius similar to said predetermined radius, the downstream ends of the shells are directly attached to an inner surface of the cylindrical burner ring, said premix burner with the attached burner ring is mounted within a coaxial burner sleeve, and the cylindrical burner ring is slideable in the axial direction of the premix burner.