发明名称 Combustor assembly with trapped vortex cavity
摘要 A combustor assembly is disclosed. The combustor assembly may include an annular trapped vortex cavity located adjacent to a downstream end of a bundle of air/fuel premixing injection tubes. The annular trapped vortex cavity may include an opening at a radially inner portion of the annular trapped vortex cavity adjacent to the head end of the bundle of premixing tubes. The annular trapped vortex cavity may also include one or more air injection holes and one or more fuel sources disposed about the annular trapped vortex cavity such that the one or more air injection holes and the one or more fuel sources are configured to drive a vortex within the annular trapped vortex cavity.
申请公布号 US9074773(B2) 申请公布日期 2015.07.07
申请号 US201213367686 申请日期 2012.02.07
申请人 General Electric Company 发明人 Boardman Gregory Allen;Chila Ronald;McConnaughhay Johnie F.
分类号 F23R3/30;F23R3/28;F23R3/58;F23C5/00 主分类号 F23R3/30
代理机构 Sutherland Asbill & Brennan LLP 代理人 Sutherland Asbill & Brennan LLP
主权项 1. A combustor assembly, comprising: an annular trapped vortex cavity located adjacent to a downstream end of a bundle of air/fuel premixing injection tubes; the annular trapped vortex cavity comprising an opening at a radially inner portion adjacent to a head end of the bundle of premixing tubes; one or more air injection holes disposed about the annular trapped vortex cavity; one or more fuel sources disposed about the annular trapped vortex cavity, wherein the one or more fuel sources comprise: at least one air/fuel premixing injection tube disposed on an annular aft wall of the annular trapped vortex cavity; andat least one air/fuel premixing injection tube disposed on a forward wall of the annular trapped vortex cavity; and wherein the one or more air injection holes and the one or more fuel sources are configured to drive a vortex within the annular trapped vortex cavity.
地址 Schenectady NY US
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