发明名称 |
Turbofan engine for combustion chamber of turbine, has fuel-air-mixture that is introduced in flow direction towards compressor in core flow, where combustion chamber is supplied with core flow and is combusted in explosive manner |
摘要 |
<p>The turbofan engine has a fuel-air-mixture that is introduced in flow direction towards a compressor (05) in a core flow, where a combustion chamber (16) is supplied with the core flow and is combusted in an explosive manner. The combustion chamber is arranged in a boiler (22) in a sectional manner and has an evaporation space, in which the water mist is generated and is vaporized to cool the wall of the combustion chamber.</p> |
申请公布号 |
DE102013112506(A1) |
申请公布日期 |
2014.04.03 |
申请号 |
DE201310112506 |
申请日期 |
2013.11.13 |
申请人 |
GRAETZER, MARCO |
发明人 |
GRAETZER, MARCO |
分类号 |
F02C3/30;F02C7/16;F02K3/04;F02K7/02;F23R7/00 |
主分类号 |
F02C3/30 |
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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