发明名称 |
CIRCUMFERENTIALLY AND AXIALLY STAGED ANNULAR COMBUSTOR FOR GAS TURBINE ENGINE COMBUSTOR |
摘要 |
A combustor section for a gas turbine engine includes an outer wall assembly and an inner wall assembly inboard of the outer wall assembly to define an annular combustion chamber therebetween. A forward fuel injection system is in communication with the combustion chamber. A downstream fuel injection system is in communication with the combustion chamber through the outer wall assembly and a swirl mixer system in communication with the combustion chamber through the inner wall assembly. |
申请公布号 |
EP3060850(A4) |
申请公布日期 |
2016.12.21 |
申请号 |
EP20140878606 |
申请日期 |
2014.10.21 |
申请人 |
United Technologies Corporation |
发明人 |
SNYDER, Timothy S. |
分类号 |
F23R3/28;F02C7/22;F23R3/00;F23R3/06;F23R3/14;F23R3/34;F23R3/42;F23R3/50 |
主分类号 |
F23R3/28 |
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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