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    Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber
    3.
    发明申请
    Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber 有权
    用于将空气/燃料混合物注入涡轮机燃烧室的泡腾空气动力系统

    公开(公告)号：US20060059914A1

    公开(公告)日：2006-03-23

    申请号：US11230640

    申请日：2005-09-21

    申请人： Igor Mantchenkov ,  Thomas Noel ,  Alexander Novikov ,  Vladimir Orlov ,  Valery Pikalov ,  Gilles Rollin

    发明人： Igor Mantchenkov ,  Thomas Noel ,  Alexander Novikov ,  Vladimir Orlov ,  Valery Pikalov ,  Gilles Rollin

    IPC分类号： F02C7/22

    CPC分类号： F23D11/16

    摘要： An aerodynamic injection system for injecting an air/fuel mixture into a turbomachine combustion chamber comprises a tubular structure of axis XX′ that opens out at a downstream end for delivering the air/fuel mixture, at least one air feed channel that opens out into the structure so as to introduce air at a pressure PA therein, an annular fuel passage that is formed in the structure around its axis XX′, that is connected to at least one fuel feed channel in which there flows fuel at a pressure PC, and that opens out at a downstream end into the structure, and means for injecting gas into the at least one fuel feed channel, said gas being at a pressure PG that is greater than PA and greater than or equal to PC so as to create effervescence in the fuel on being introduced into the structure.

    摘要翻译： 用于将空气/燃料混合物喷射到涡轮机燃烧室中的空气动力注射系统包括：轴线XX'的管状结构，其在下游端开放以输送空气/燃料混合物;至少一个空气供给通道， 结构，以便在其中引入空气在其中的压力P A A;环形燃料通道，其形成在围绕其轴线XX'的结构中，其连接到至少一个燃料供给通道，在该燃料供给通道中流动 在压力P C C C下的燃料，并且在下游端开放到结构中，以及用于将气体注入至少一个燃料供给通道的装置，所述气体处于压力P < G>大于P＆lt; A＆gt;且大于或等于P C，以便在引入到结构中时在燃料中产生泡腾。

    Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber
    4.
    发明授权
    Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber 有权
    用于将空气/燃料混合物注入涡轮机燃烧室的泡腾空气动力系统

    公开(公告)号：US07506496B2

    公开(公告)日：2009-03-24

    申请号：US11230640

    申请日：2005-09-21

    申请人： Igor Mantchenkov ,  Thomas Noel ,  Alexander Novikov ,  Vladimir Orlov ,  Valery Pikalov ,  Gilles Rollin

    发明人： Igor Mantchenkov ,  Thomas Noel ,  Alexander Novikov ,  Vladimir Orlov ,  Valery Pikalov ,  Gilles Rollin

    IPC分类号： F23R3/28

    CPC分类号： F23D11/16

    摘要： An aerodynamic injection system for injecting an air/fuel mixture into a turbomachine combustion chamber comprises a tubular structure of axis XX′ that opens out at a downstream end for delivering the air/fuel mixture, at least one air feed channel that opens out into the structure so as to introduce air at a pressure PA therein, an annular fuel passage that is formed in the structure around its axis XX′, that is connected to at least one fuel feed channel in which there flows fuel at a pressure PC, and that opens out at a downstream end into the structure, and means for injecting gas into the at least one fuel feed channel, said gas being at a pressure PG that is greater than PA and greater than or equal to PC so as to create effervescence in the fuel on being introduced into the structure.

    摘要翻译： 用于将空气/燃料混合物喷射到涡轮机燃烧室中的空气动力注射系统包括：轴线XX'的管状结构，其在下游端开放以输送空气/燃料混合物;至少一个空气供给通道， 结构，以便以其中的压力PA引入空气;环形燃料通道，其形成在其轴线XX'周围的结构中，其连接到至少一个在压力PC处燃料的燃料供给通道，并且 在下游端开口进入结构，以及用于将气体注入至少一个燃料供给通道的装置，所述气体处于大于PA并且大于或等于PC的压力PG，以便在所述至少一个燃料供给通道中产生泡腾 被引入结构中的燃料。

    Effervescence injector for an aero-mechanical system for injecting air/fuel mixture into a turbomachine combustion chamber
    5.
    发明申请
    Effervescence injector for an aero-mechanical system for injecting air/fuel mixture into a turbomachine combustion chamber 有权
    用于将空气/燃料混合物喷射到涡轮机燃烧室中的航空机械系统的气泡注射器

    公开(公告)号：US20060059915A1

    公开(公告)日：2006-03-23

    申请号：US11232002

    申请日：2005-09-22

    申请人： Victor Furletov ,  Thomas Noel ,  Gilles Rollin ,  Alexander Vasilev ,  Victor Yagodkin

    发明人： Victor Furletov ,  Thomas Noel ,  Gilles Rollin ,  Alexander Vasilev ,  Victor Yagodkin

    IPC分类号： F02C7/22

    CPC分类号： F23R3/286 ,  F23D11/24 ,  F23R3/30

    摘要： A fuel injector for an aero-mechanical injection system for injecting an air/fuel mixture into a turbomachine combustion chamber, the injector comprising a main tubular structure of axis XX′ opening out at a downstream end for delivering the air/fuel mixture, a tubular fuel duct that is disposed inside the main structure and that opens out into the main structure via a fuel atomizer plug so as to introduce fuel into the main structure at a pressure PC into the main structure, at least one air feed channel that opens out into the main structure so as to introduce air at a pressure PA therein, and means for injecting into the fuel duct a gas at a pressure PG that is greater than PA and greater than or equal to PC so as to create effervescence in the fuel on being introduced into the main structure.

    摘要翻译： 一种用于将空气/燃料混合物喷射到涡轮机燃烧室中的航空机械喷射系统的燃料喷射器，所述喷射器包括在下游端开口用于输送空气/燃料混合物的轴线XX'的主管状结构，管状 燃料管道，其设置在主结构内部并且经由燃料雾化器塞打开到主结构中，以将燃料以压力P C C引入主结构中至少进入主结构 一个空气供给通道，其向主体结构开放，以便在其中引入空气，其中压力为P＆lt; A＆lt; A＆gt;;以及用于将气体以压力P＆lt; SUB>大于P＆lt; A＆gt;且大于或等于P C，以便在引入到主结构中时在燃料中产生泡腾。