发明名称 |
COMBUSTION BURNER, COMBUSTOR, AND GAS TURBINE |
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 |
US2016298845(A1) |
申请公布日期 |
2016.10.13 |
申请号 |
US201514897814 |
申请日期 |
2015.01.23 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
NAGAI Naonori;TADA Katsuyoshi;INOUE Kei;SAITO Keijiro |
分类号 |
F23R3/14;F23R3/00;F23R3/28 |
主分类号 |
F23R3/14 |
代理机构 |
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代理人 |
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主权项 |
1. A combustion burner comprising:
a nozzle; and a swirl vane disposed in an axial flow path extending along an axial direction of the nozzle around the nozzle, wherein the swirl vane includes
a tip portion for swirling gas in a swirl direction, the gas flowing through a radially-outer region of the axial flow path, anda root portion disposed on an inner side in a radial direction of the nozzle as seen from the tip portion, the root portion having a cutout on a side of a trailing edge, wherein the radially-outer region and a radially-inner region of the axial flow path communicate with each other without being partitioned, at least in a range in the axial direction in which the swirl vane is disposed, wherein 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, wherein the pressure surface of the swirl vane at the tip portion has a curved surface curving in the swirl direction toward the trailing edge, and wherein the pressure surface of the swirl vane has a stepped portion between the curved surface of the tip portion and the curved surface of the root portion. |
地址 |
Tokyo JP |