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1. 发明授权

US06422481B1 Method of enhancing heat transfer in a heated tip fuel injector 有权
公开(公告)号：US06422481B1
公开(公告)日：2002-07-23
申请号：US09261408
申请日：1999-03-03
申请人： Wei-Min Ren , Frank Zimmermann , John F. Nally, Jr. , John Bright
发明人： Wei-Min Ren , Frank Zimmermann , John F. Nally, Jr. , John Bright
IPC分类号： B05B124
摘要： A method of heating fuel includes providing a fuel injector having an internal heater and a reciprocable needle valve; providing fuel to the fuel injector; passing the fuel through at least one flow-disturbing element; and heating the fuel.

2. 发明授权

US6135360A Heated tip fuel injector with enhanced heat transfer 失效
标题翻译：加热尖端燃油喷射器具有增强的热传递
公开(公告)号：US6135360A
公开(公告)日：2000-10-24
申请号：US261407
申请日：1999-03-03
申请人： Wei-Min Ren , Frank Zimmermann , John F. Nally, Jr. , John Bright
发明人： Wei-Min Ren , Frank Zimmermann , John F. Nally, Jr. , John Bright
IPC分类号： F02M51/00 , F02M51/06 , F02M53/06 , F02M61/16 , B05B1/24
CPC分类号： F02M51/005 , F02M51/0671 , F02M53/06 , F02M61/162
摘要： A heated tip fuel injector includes a housing having a bore formed therein for receiving fuel under pressure; a valve seat mounted at one end of the housing, the valve seat including an orifice; a needle valve having one end mounted to an armature and another end which contacts the valve seat to close off fuel outflow from the bore and which is lifted from the valve seat to inject fuel; a heater disposed in the housing upstream of the valve seat and extending around the needle valve; and at least one flow disturbing element disposed upstream of the heater. The flow-disturbing element enhances heat transfer from the heater to the fuel.
摘要翻译：加热尖端燃料喷射器包括其中形成有用于在压力下接收燃料的孔的壳体; 安装在所述壳体的一端的阀座，所述阀座包括孔口; 针阀，其一端安装到电枢，另一端接触阀座，以关闭从孔中燃料流出并从阀座提升以喷射燃料; 加热器，设置在所述壳体的上游并且围绕所述针阀延伸; 以及设置在加热器上游的至少一个流动干扰元件。流动干扰元件增强了从加热器到燃料的热传递。

3. 发明授权

US6109543A Method of preheating fuel with an internal heater 失效
标题翻译：用内部加热器预热燃料的方法
公开(公告)号：US6109543A
公开(公告)日：2000-08-29
申请号：US88126
申请日：1998-06-01
申请人： John S. Bright , Jerry E. Nines , Michael J. Frick , Frank Zimmermann , Christoph Kendlbacher , John F. Nally, Jr. , Wei-Min Ren
发明人： John S. Bright , Jerry E. Nines , Michael J. Frick , Frank Zimmermann , Christoph Kendlbacher , John F. Nally, Jr. , Wei-Min Ren
IPC分类号： F02M51/00 , F02M51/06 , F02M53/06 , F02M61/16 , F02M69/00 , B05B1/24
CPC分类号： F02M51/0671 , F02M51/005 , F02M53/06
摘要： A method of preheating fuel in a fuel injector with an internal heater energized to reduce emissions. The heater being a ceramic hollow cylinder disposed within a valve body just upstream of a valve seat where fuel is injected through an orifice into the engine. Conductors for energizing the heater extend into the valve body and are sealed against the escape of pressurized fuel. In one version, the conductors are extended through an O-ring to be sealed. In another version the conductors include pins extending through the valve body sidewall with glass seals fused to the valve body and the pins. The conductors may comprise flat foil strips clamped between the O-ring and an elastomeric washer. The conductors also may be molded into the magnetic coil bobbin and sealed where the conductors emerge into the fuel cavity. The heater has metallized surfaces to create current flow through its wall thickness, and the conductors are electrically connected respectively to the inner end and outer surfaces of the hollow cylinder by metallization patterns enabling both mechanical contacts to be made on the outside of the heater.
摘要翻译：一种用燃料喷射器预热燃料的方法，其中内部加热器通电以减少排放。加热器是陶瓷中空圆柱体，其位于阀体正好位于阀座上游的阀体内，其中燃料通过孔喷入发动机。用于激励加热器的导体延伸到阀体中并且被密封以抵抗加压燃料的逸出。在一个版本中，导体通过O形环延伸以进行密封。在另一种形式中，导体包括延伸穿过阀体侧壁的销，玻璃密封件与阀体和销钉熔合。导体可以包括夹在O形环和弹性垫圈之间的扁平箔带。导体也可以被模制到磁性线圈筒管中并且在导体出现到燃料腔中时被密封。加热器具有金属化表面以产生通过其壁厚度的电流，并且导体通过金属化图案分别电连接到中空圆柱体的内端和外表面，使得能够在加热器的外部形成机械接触。

4. 发明授权

US6102303A Fuel injector with internal heater 失效
标题翻译：带内部加热器的燃油喷射器
公开(公告)号：US6102303A
公开(公告)日：2000-08-15
申请号：US88127
申请日：1998-06-01
申请人： John S. Bright , Jerry E. Nines , Michael J. Frick , Frank Zimmermann , Christoph Kendlbacher , John F. Nally, Jr. , Wei-Min Ren
发明人： John S. Bright , Jerry E. Nines , Michael J. Frick , Frank Zimmermann , Christoph Kendlbacher , John F. Nally, Jr. , Wei-Min Ren
IPC分类号： F02M51/00 , F02M51/06 , F02M53/06 , B05B1/24
CPC分类号： F02M53/06 , F02M51/005 , F02M51/0671
摘要： A fuel injector has an internal heater energized during cold starting to reduce emissions, the heater being a ceramic hollow cylinder disposed within a valve body just upstream of a valve seat where fuel is injected through an orifice into the engine. Conductors for energizing the heater extend into the valve body and are sealed against the escape of pressurized fuel. In one version, the conductors extend through an O-ring to be sealed. In another version the conductors include pins extending through the valve body sidewall with glass seals fused to the valve body and the pins. The conductors may comprise flat foil strips clamped between the O-ring and an elastomeric washer. The conductors also may be molded into the magnetic coil bobbin and sealed where the conductors emerge into the fuel cavity. The heater has metallized surfaces to create current flow through its wall thickness, and the conductors are electrically connected respectively to the inner end and outer surfaces of the hollow cylinder by metallization patterns enabling both mechanical contacts on the outside of the heater.
摘要翻译：燃料喷射器在冷起动期间具有内部加热器通电以减少排放，该加热器是陶瓷中空圆柱体，其位于阀体正好位于阀座上游的阀体内，其中燃料通过孔喷射到发动机中。用于激励加热器的导体延伸到阀体中并且被密封以抵抗加压燃料的逸出。在一个版本中，导体延伸穿过O形圈进行密封。在另一种形式中，导体包括延伸穿过阀体侧壁的销，玻璃密封件与阀体和销钉熔合。导体可以包括夹在O形环和弹性垫圈之间的扁平箔带。导体也可以被模制到磁性线圈筒管中并且在导体出现到燃料腔中时被密封。加热器具有金属化表面以产生通过其壁厚度的电流，并且导体通过金属化图案分别电连接到中空圆柱体的内端和外表面，从而能够在加热器的外部实现机械接触。

5. 发明授权

US5996912A Flat needle for pressurized swirl fuel injector 失效
标题翻译：用于加压涡流燃油喷射器的平针
公开(公告)号：US5996912A
公开(公告)日：1999-12-07
申请号：US999411
申请日：1997-12-23
申请人： Wei-Min Ren , Jingming Jim Shen
发明人： Wei-Min Ren , Jingming Jim Shen
IPC分类号： F02M51/06 , F02M51/08 , F02M61/16 , F02M61/18
CPC分类号： F02M61/18 , F02M51/0667 , F02M51/0671 , F02M61/162 , F02M61/168
摘要： The injector nozzle includes a cylindrical needle which is axially reciprocated by an armature assembly. The needle has a needle tip terminating in a flat end surface with a spherical transition surface between the flat end surface and the side walls of the needle. Depending upon the diameter of the needle and the included angle of the valve seat, the diameter of the flat end surface may be less than the diameter of the orifice through the valve seat. The circular edge defined between the flat end surface and the spherical transition surface defines a location where the liquid fuel and air consistently separate from the needle in the valve-open condition whereby variations in the spray cone angle and the flow rate are minimized during steady-state and transient operating conditions.
摘要翻译：喷射器喷嘴包括由电枢组件轴向往复运动的圆柱形针。针头具有终端于扁平端面的针尖，在平坦端表面和针的侧壁之间具有球形过渡表面。根据针的直径和阀座的夹角，平坦端面的直径可以小于通过阀座的孔的直径。限定在平坦端表面和球形过渡表面之间的圆形边缘限定了液体燃料和空气在阀打开状态下与针头一致地分离的位置，从而在稳定状态期间喷雾锥角和流速的变化最小化，状态和瞬态操作条件。

6. 发明申请

US20100183439A1 Systems, Methods, and Apparatus for Controlling Gas Leakage in a Turbine 有权
标题翻译：用于控制涡轮机气体泄漏的系统，方法和装置
公开(公告)号：US20100183439A1
公开(公告)日：2010-07-22
申请号：US12357931
申请日：2009-01-22
申请人： Wei-Min Ren
发明人： Wei-Min Ren
IPC分类号： F01D11/00 , F16J15/40
CPC分类号： F01D3/04 , F01D11/003 , F01D11/04 , F02C7/28 , F05D2220/31 , F05D2240/61 , F05D2240/63
摘要： Systems, methods and apparatus for controlling gas leakage in a turbine are provided. A plurality of seals may be provided in series, where each of the plurality of seals may be operable to reduce gas backflow from an inlet of a turbine component. Further, one or more channels may be provided that are operable to direct at least a portion of the gas backflow from respective points within the plurality of seals to corresponding points within a gas flow path of the turbine. The at least a portion of the gas backflow may be directed to the points within the gas flow path through the one or more channels. Additionally, the diameters of the plurality of seals may be optimized to at least partially balance the net thrust generated by the gas flow path of the turbine.
摘要翻译：提供了一种用于控制涡轮机中的气体泄漏的系统，方法和装置。可以串联地设置多个密封件，其中多个密封件中的每一个可以是可操作的，以减少来自涡轮机部件的入口的气体回流。此外，可以提供一个或多个通道，其可操作以将来自多个密封件内的各个点的气体回流的至少一部分引导到涡轮机的气体流动路径内的对应点。气体回流的至少一部分可以通过一个或多个通道被引导到气体流动路径内的点。此外，可以优化多个密封件的直径以至少部分地平衡由涡轮机的气体流动路径产生的净推力。

7. 发明申请

US20080118350A1 Turbine seal guards 审中-公开
标题翻译：涡轮密封卫兵
公开(公告)号：US20080118350A1
公开(公告)日：2008-05-22
申请号：US11600539
申请日：2006-11-16
申请人： Sean Feeny , Michael Montgomery , Mark Bowen , Stephen Swan , David Caruso , Wei-Min Ren , Michael Hamlin , Jeffrey Simkins
发明人： Sean Feeny , Michael Montgomery , Mark Bowen , Stephen Swan , David Caruso , Wei-Min Ren , Michael Hamlin , Jeffrey Simkins
IPC分类号： F01D11/08 , F01D5/14
CPC分类号： F01D11/08
摘要： The application may further describe a seal guard in a turbine where the turbine include a plurality of circumferentially spaced nozzles, a plurality of circumferentially spaced turbine blades that each include a blade cover, and an opening defined by a trailing edge of the nozzles and a leading edge of the blade covers. The seal guard may include an upstream axial fin positioned at the trailing edge of the nozzles that extends in a downstream direction across at least part of the opening or a downstream axial fin positioned at a leading edge of a blade cover that extends in an upstream direction across at least part of the opening.
摘要翻译：该应用可以进一步描述涡轮机中的密封防护件，其中涡轮机包括多个周向间隔开的喷嘴，多个周向间隔开的涡轮机叶片，每个涡轮机叶片包括叶片盖和由喷嘴的后缘限定的开口，叶片边缘。密封防护件可以包括位于喷嘴的后缘处的上游轴向翅片，其沿下游方向跨过开口的至少一部分延伸，或者位于沿着上游方向延伸的叶片盖的前缘处的下游轴向翅片至少部分开放。

8. 发明授权

US06776353B2 Fuel injector valve seat assembly with radially outward leading fuel flow passages feeding multi-hole orifice disk 有权
标题翻译：燃料喷射器阀座组件，具有径向向外引导的燃料流动通道供给多孔孔盘
公开(公告)号：US06776353B2
公开(公告)日：2004-08-17
申请号：US10015941
申请日：2001-12-17
申请人： Jayashree Moorthy , Wei-Min Ren
发明人： Jayashree Moorthy , Wei-Min Ren
IPC分类号： F02D700
CPC分类号： F02M61/186 , F02M61/18 , F02M61/1806 , F02M61/188
摘要： A fuel injector for use in a fuel injection system of an internal combustion engine that includes a body, valve seat, closure member, orifice plate and metering device. The closure member and the valve seat define a sealing surface, located on a virtual circle defining a sealing diameter. The orifice plate includes a third surface, a fourth surface and at least one orifice, located on a virtual circle on the orifice plate defining a first radius and between the third and fourth surfaces. The metering device has first and second faces contiguous to a third face. At least one of the first and third faces are spaced from one of the first and second surfaces of the valve seat to define a plurality of passages. Each passage has an outlet located on a virtual circle defining a second diameter greater than at least one of the first and the sealing diameters.
摘要翻译：一种用于内燃机的燃料喷射系统的燃料喷射器，其包括主体，阀座，关闭构件，孔板和计量装置。闭合构件和阀座限定了密封表面，其位于限定密封直径的虚拟圆上。孔板包括位于孔板上的虚拟圆上的第三表面，第四表面和至少一个孔，限定第一半径，并且在第三和第四表面之间。计量装置具有与第三面邻接的第一和第二面。第一和第三面中的至少一个与阀座的第一和第二表面之一间隔开以限定多个通道。每个通道具有位于虚拟圆上的出口，限定第二直径大于第一密封直径和密封直径中的至少一个。

9. 发明授权

US06357677B1 Fuel injection valve with multiple nozzle plates 有权
标题翻译：具有多个喷嘴板的燃油喷射阀
公开(公告)号：US06357677B1
公开(公告)日：2002-03-19
申请号：US09538730
申请日：2000-03-30
申请人： Wei-Min Ren , David P. Wieczorek
发明人： Wei-Min Ren , David P. Wieczorek
IPC分类号： F02M5100
CPC分类号： F02M51/0671 , F02M51/0675 , F02M61/12 , F02M61/1853
摘要： A metering assembly for a fuel injector having multiple orifice plates is disclosed. The metering assembly includes a valve body, a seat, a needle and a multi-layer orifice plate assembly. The valve body has an inlet, an outlet and a longitudinal axis extending therethrough. The seat is disposed proximate the outlet and includes a passage having a sealing surface and an orifice. The needle is reciprocally located within the housing along the longitudinal axis between a first position wherein the needle is displaced from the seat, allowing fuel flow past the needle, and a second position wherein the needle is biased against the seat, precluding fuel flow past the needle. The multi-layer orifice plate assembly is located at the housing outlet and includes a first orifice plate having a plurality of first openings extending therethrough. The orifice plate assembly further includes a second orifice plate having a plurality of second openings extending therethrough. The plurality of first openings and the plurality of second openings are fluidly connected by at least one channel. A method of accelerating fuel through the injector is also disclosed.
摘要翻译：公开了一种用于具有多个孔板的燃料喷射器的计量组件。计量组件包括阀体，阀座，针和多层孔板组件。阀体具有从其延伸的入口，出口和纵向轴线。座椅靠近出口设置并且包括具有密封表面和孔口的通道。所述针沿着所述纵向轴线在所述壳体内沿所述纵向轴线相互位于所述第一位置之间，所述第一位置是所述针从所述座部移位，允许燃料流过所述针，以及第二位置，其中所述针被偏压抵靠所述座椅，针。多层孔板组件位于壳体出口处，并且包括具有延伸穿过其中的多个第一开口的第一孔板。孔板组件还包括具有延伸穿过其中的多个第二开口的第二孔板。多个第一开口和多个第二开口通过至少一个通道流体连接。还公开了一种通过喷射器加速燃料的方法。

10. 发明授权

US08147185B2 Systems, methods, and apparatus for controlling gas leakage in a turbine 有权
标题翻译：用于控制涡轮机中的气体泄漏的系统，方法和装置
公开(公告)号：US08147185B2
公开(公告)日：2012-04-03
申请号：US12357931
申请日：2009-01-22
申请人： Wei-Min Ren
发明人： Wei-Min Ren
IPC分类号： F01B25/00 , F01D13/02 , F01D17/00 , F03D7/00 , F04D27/00
CPC分类号： F01D3/04 , F01D11/003 , F01D11/04 , F02C7/28 , F05D2220/31 , F05D2240/61 , F05D2240/63
摘要： Systems, methods and apparatus for controlling gas leakage in a turbine are provided. A plurality of seals may be provided in series, where each of the plurality of seals may be operable to reduce gas backflow from an inlet of a turbine component. Further, one or more channels may be provided that are operable to direct at least a portion of the gas backflow from respective points within the plurality of seals to corresponding points within a gas flow path of the turbine. The at least a portion of the gas backflow may be directed to the points within the gas flow path through the one or more channels. Additionally, the diameters of the plurality of seals may be optimized to at least partially balance the net thrust generated by the gas flow path of the turbine.
摘要翻译：提供了一种用于控制涡轮机中的气体泄漏的系统，方法和装置。可以串联地设置多个密封件，其中多个密封件中的每一个可以是可操作的，以减少来自涡轮机部件的入口的气体回流。此外，可以提供一个或多个通道，其可操作以将来自多个密封件内的各个点的气体回流的至少一部分引导到涡轮机的气体流动路径内的对应点。气体回流的至少一部分可以通过一个或多个通道被引导到气体流动路径内的点。此外，可以优化多个密封件的直径以至少部分地平衡由涡轮机的气体流动路径产生的净推力。

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