发明名称 |
COMBUSTION TURBINE IN WHICH COMBUSTION IS INTERMITTENT |
摘要 |
Disclosed is a combustion turbine (1) for intermittent combustion with at least one combustion chamber (3) having inlet valves (2) and an ignition device (18), the at least one combustion chamber (3) having no shut-off devices on the off-gas side and being thus open on the off-gas side at all times. Downstream of the at least one combustion chamber (3), a turbine (4), which can be impinged with process gas obtained in the combustion chamber (3), is positioned, with a flow-through chamber (5) being positioned between the at least one combustion chamber (3) and the turbine (4) axially behind the at least one combustion chamber (3). The flow-through chamber (5) is separated from the at least one combustion chamber (3) by a guiding plate (6) or a further turbine (7) to generate a swirl flow. This permits improved acoustic decoupling of the flow noises and the pressure fluctuation in the combustion chamber (3). |
申请公布号 |
CA2734054(C) |
申请公布日期 |
2016.12.20 |
申请号 |
CA20092734054 |
申请日期 |
2009.08.05 |
申请人 |
GABL, HELMUTH;LORENZ, EDMUND;NIEDERL, FRANZ |
发明人 |
GABL, HELMUTH;LORENZ, EDMUND;NIEDERL, FRANZ |
分类号 |
F02C5/12;F02K7/06;F23R7/00 |
主分类号 |
F02C5/12 |
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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