发明名称 |
SYSTEM AND METHOD FOR A FUEL NOZZLE |
摘要 |
A system includes an oxidant compressor and a gas turbine engine turbine, which includes a turbine combustor, a turbine, and an exhaust gas compressor. The turbine combustor includes a plurality of diffusion fuel nozzles, each including a first oxidant conduit configured to inject a first oxidant through a plurality of first oxidant openings configured to impart swirling motion to the first oxidant in a first rotational direction, a first fuel conduit configured to inject a first fuel through a plurality of first fuel openings configured to impart swirling motion to the first fuel in a second rotational direction, and a second oxidant conduit configured to inject a second oxidant through a plurality of second oxidant openings configured to impart swirling motion to the second oxidant in a third rotational direction. The first fuel conduit surrounds the first oxidant conduit and the second oxidant conduit surrounds the first fuel conduit. |
申请公布号 |
EP3014087(A1) |
申请公布日期 |
2016.05.04 |
申请号 |
EP20140736246 |
申请日期 |
2014.06.16 |
申请人 |
EXXONMOBIL UPSTREAM RESEARCH COMPANY |
发明人 |
ZUO, BAIFANG;ZIMINSKY, WILLY STEVE;STEVENSON, CHRISTIAN XAVIER;SLOBODYANSKIY, ILYA ALEKSANDROVICH |
分类号 |
F02C3/34;F02C7/22 |
主分类号 |
F02C3/34 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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