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
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