Effervescence injector for an aero-mechanical system for injecting air/fuel mixture into a turbomachine combustion chamber
    1.
    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

    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< A< A>;以及用于将气体以压力P< SUB>大于P< A>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。

    Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber
    2.
    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

    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
    3.
    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

    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。

    Method for allocating of at least one access point to a mobile terminal in a cellular network, corresponding terminal, mobile server and programs
    5.
    发明授权
    Method for allocating of at least one access point to a mobile terminal in a cellular network, corresponding terminal, mobile server and programs 有权
    用于将蜂窝网络,对应终端,移动服务器和节目中的至少一个接入点分配给移动终端的方法

    公开(公告)号:US08948763B2

    公开(公告)日:2015-02-03

    申请号:US12279293

    申请日:2007-02-13

    IPC分类号: H04W36/32 H04W48/08 H04W36/08

    CPC分类号: H04W48/08 H04W36/08 H04W36/32

    摘要: A method is provided for allocating at least one access point to a mobile terminal in a cellular network formed by multiple cells each controlled by an access point, wherein the mobile terminals move about. The method includes the following steps: locating a mobile terminal inside a current cell; identifying, using the locating, a target cell with which the terminal is likely to be connected; transmitting in advance to the terminal a target context, comprising at least one identifier of the access point of the target cell; implementing a procedure for connecting said terminal to the access point of the target cell, based on predetermined cell modification criterion.

    摘要翻译: 提供了一种方法,用于将蜂窝网络中的至少一个接入点分配给由接入点控制的多个小区形成的移动终端,其中移动终端移动。 该方法包括以下步骤:将移动终端定位在当前小区内; 使用所述定位来识别所述终端可能连接的目标小区; 预先向终端发送目标上下文,其包括目标小区的接入点的至少一个标识符; 基于预定的小区修改标准,实现用于将所述终端连接到目标小区的接入点的过程。

    ANTI-COKING INJECTOR ARM
    6.
    发明申请
    ANTI-COKING INJECTOR ARM 审中-公开
    防伪注射器ARM

    公开(公告)号:US20070068164A1

    公开(公告)日:2007-03-29

    申请号:US11535667

    申请日:2006-09-27

    IPC分类号: F02C7/22

    摘要: According to the invention, the injector arms comprise a peripheral duct forming part of a primary fuel circuit that delivers fuel continuously, and a central duct forming part of a secondary fuel circuit that delivers fuel at an essentially variable rate.

    摘要翻译: 根据本发明,喷射器臂包括形成连续输送燃料的主燃料回路的一部分的周边管道,以及形成以基本上可变速率输送燃料的二次燃料回路的一部分的中心管道。

    METHOD FOR ALLOCATING OF AT LEAST ONE ACCESS POINT TO A MOBILE TERMINAL IN A CELLULAR NETWORK, CORRESPONDING TERMINAL, MOBILE SERVER AND PROGRAMS
    7.
    发明申请
    METHOD FOR ALLOCATING OF AT LEAST ONE ACCESS POINT TO A MOBILE TERMINAL IN A CELLULAR NETWORK, CORRESPONDING TERMINAL, MOBILE SERVER AND PROGRAMS 有权
    在细胞网络,对应终端,移动服务器和程序中分配至少一个接入点到移动终端的方法

    公开(公告)号:US20090017825A1

    公开(公告)日:2009-01-15

    申请号:US12279293

    申请日:2007-02-13

    IPC分类号: H04Q7/38 H04L12/28

    CPC分类号: H04W48/08 H04W36/08 H04W36/32

    摘要: A method is provided for allocating at least one access point to a mobile terminal in a cellular network formed by multiple cells each controlled by an access point, wherein the mobile terminals move about. The method includes the following steps: locating a mobile terminal inside a current cell; identifying, using the locating, a target cell with which the terminal is likely to be connected; transmitting in advance to the terminal a target context, comprising at least one identifier of the access point of the target cell; implementing a procedure for connecting said terminal to the access point of the target cell, based on predetermined cell modification criterion.

    摘要翻译: 提供了一种方法,用于将蜂窝网络中的至少一个接入点分配给由接入点控制的多个小区形成的移动终端,其中移动终端移动。 该方法包括以下步骤:将移动终端定位在当前小区内; 使用所述定位来识别所述终端可能连接的目标小区; 预先向终端发送目标上下文,其包括目标小区的接入点的至少一个标识符; 基于预定的小区修改标准,实现用于将所述终端连接到目标小区的接入点的过程。

    MULTIMODE FUEL INJECTOR FOR COMBUSTION CHAMBERS, IN PARTICULAR OF A JET ENGINE
    8.
    发明申请
    MULTIMODE FUEL INJECTOR FOR COMBUSTION CHAMBERS, IN PARTICULAR OF A JET ENGINE 有权
    喷气发动机特别是燃料燃烧器的多模燃料喷射器

    公开(公告)号:US20070169486A1

    公开(公告)日:2007-07-26

    申请号:US11620314

    申请日:2007-01-05

    IPC分类号: F02C7/26

    摘要: A fuel injector comprises a peripheral atomisation system having a plurality of fuel ejection orifices distributed at regular intervals along the circumference and an annular air eddy deflector, comprising air ejection channels such that, for each fuel ejection axis defined by an ejection orifice, there is a corresponding air ejection channel of which at least the radially most internal part has a median substantially intersecting this fuel ejection axis.

    摘要翻译: 燃料喷射器包括具有沿着圆周以规则间隔分布的多个燃料喷射孔的周边雾化系统和环形空气涡流偏转器,包括空气喷射通道,使得对于由喷射孔限定的每个燃料喷射轴线, 相应的空气喷射通道至少具有径向最内部的中间部分大致与该燃料喷射轴线相交。