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1. 发明申请

WO2005075891A1 PRE-HEATING UNIT FOR A TURBINE AND TURBINE COMPRISING SAID PRE-HEATING UNIT 审中-公开
标题翻译：用于包括预热单元的涡轮机和涡轮机的预热单元
公开(公告)号：WO2005075891A1
公开(公告)日：2005-08-18
申请号：PCT/IT2004/000043
申请日：2004-02-06
申请人： GENOVESE, Santino
发明人： GENOVESE, Santino
IPC分类号： F23R3/32
CPC分类号： F02C7/266 , A63H27/02 , F01N2610/107 , F23D11/448 , F23D2900/00015 , F23R3/32
摘要： A pre-heating unit for a liquid fuel turbine for model aircraft comprises: - a body (14) which can be inserted by at least one of its ends in a combustion chamber of a turbine, and in which there is determined a fuel path which is determined between a fuel intake aperture (5) and a fuel outlet aperture (16), the said fuel intake aperture being in fluid communication with means to feed pressurized liquid fuel, and the said outlet aperture being positioned inside the combustion chamber of the turbine; - glow means (18) which are positioned along the said fuel path in order to heat the fuel to above its ignition temperature; and - nebulisation means (19) which are positioned along the said fuel path in order to obtain discharge of nebulised fuel from the said outlet aperture. Advantageously, the said preheating unit makes it possible to carry out starting of the turbine without requiring the use of gas or another fuel, other than that used for normal functioning of the turbine.
摘要翻译：用于模型飞行器的液体燃料涡轮机的预热单元包括： - 主体（14），其可以由其端部中的至少一个端部插入到涡轮机的燃烧室中，并且其中确定燃料路径，在燃料进入孔（5）和燃料出口孔（16）之间确定，所述燃料进入孔与供给加压液体燃料的装置流体连通，并且所述出口孔位于涡轮机的燃烧室内 ; - 发光装置（18），其沿着所述燃料路径定位，以便将燃料加热到高于其点火温度; 和 - 雾化装置（19），其沿着所述燃料路径定位，以便从所述出口孔排出雾化的燃料。有利地，所述预热单元使得除了用于涡轮机的正常功能之外，不需要使用气体或另一种燃料，可以执行涡轮机的启动。

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