发明名称 燃焼バーナ及び燃焼器、並びにガスタービン
摘要 A combustion burner includes a nozzle and a swirl vane disposed in an axial flow path extending along an axial direction of the nozzle. The swirl vane includes a tip portion for swirling gas, the gas flowing through a radially-outer region of the axial flow path, and a root portion disposed on an inner side in a radial direction of the nozzle, the root portion having a cutout on a side of a trailing edge. The radially-outer region and a radially-inner region of the axial flow path communicate with each other, at least in a range in the axial direction in which the swirl vane is disposed. The swirl vane has a pressure surface, a downstream region of the pressure surface of the root portion being defined by the cutout as a curved surface which curves in a direction opposite to the swirl direction toward the trailing edge.
申请公布号 JP5913503(B2) 申请公布日期 2016.04.27
申请号 JP20140192017 申请日期 2014.09.19
申请人 三菱重工業株式会社 发明人 永井 尚教;多田 勝義;井上 慶;斉藤 圭司郎
分类号 F23R3/14 主分类号 F23R3/14
代理机构 代理人
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