Invention Application
US20140013759A1 PREMIX BURNER OF THE MULTI-CONE TYPE FOR A GAS TURBINE 有权
用于气体涡轮机的多种类型的PREMIX燃烧器

PREMIX BURNER OF THE MULTI-CONE TYPE FOR A GAS TURBINE
Abstract:
The invention relates to a premix burner of the multi-cone type for a gas turbine that includes a plurality of shells which are arranged around a central burner axis and are parts of a virtual, axially extending common cone, which opens in a downstream direction, whereby said parts are displaced perpendicular to said burner axis such that a tangential slot is defined between each pair of adjacent shells. The flame front of such a burner is stabilized by providing a virtual common cone with a cone angle, which varies in axial direction.
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