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    • 2. 发明申请
    • DUAL FUEL INJECTOR WITH HYDRAULIC LOCK SEAL
    • 双燃油喷射器与液压锁紧密封
    • WO2013033140A1
    • 2013-03-07
    • PCT/US2012/052760
    • 2012-08-29
    • CATERPILLAR INC.KIM, HoisanSOMMARS, Mark, F.
    • KIM, HoisanSOMMARS, Mark, F.
    • F02M43/04F02D19/06F02M37/00F02M61/16
    • F02M43/04F02D19/0694F02D19/10Y02T10/36
    • A dual fuel injector (12) includes an injector body (70) that defines a liquid fuel inlet (57) fluidly connected to a liquid nozzle chamber (99), a gas fuel inlet (48) fluidly connected to a gas nozzle chamber (91), and a tip component (71) that defines a liquid nozzle outlet set (96) and a gas nozzle outlet set (90). A liquid needle valve member (78) is guided in the injector body (70) to move between positions in and out of contact with a first valve seat (180) positioned between the liquid nozzle chamber (99) and the liquid nozzle outlet set (96). A gas needle valve member (73) is guided in the injector body (70) to move between positions in and out of contact with a second valve seat (181) positioned between the gas nozzle chamber (91) and the gas nozzle outlet set (90). A hydraulic lock seal (93) for inhibiting migration of gas fuel from the gas nozzle chamber (91) into the first fuel includes an annular volume (191) surrounding a guide segment (74) of the gas needle valve member (73). The annular volume (191) is fluidly connected to the liquid nozzle volume (99) by a seal passage (190). A check valve (200) is positioned in the seal passage (190) and is movable to a closed positioned responsive to a pressure differential between liquid fuel in the liquid nozzle chamber (99) and gas fuel in the gas nozzle chamber (91) in the tip component (71). The check valve (200) may close when a gas fuel supply is exhausted and an engine (5) utilizing the dual fuel injector (12) operates in a limp home single fueling mode.
    • 双燃料喷射器(12)包括喷射器主体(70),其限定与液体喷嘴室(99)流体连接的液体燃料入口(57),与气体喷嘴室(91)流体连接的气体燃料入口 )和限定液体喷嘴出口组(96)和气体喷嘴出口组(90)的尖端部件(71)。 液体针阀构件(78)在喷射器主体(70)中被引导以在与位于液体喷嘴室(99)和液体喷嘴出口组(100)之间的第一阀座(180)接触和不接触的位置之间移动 96)。 气体针阀构件(73)在喷射器主体(70)中被引导以在与位于气体喷嘴室(91)和气体喷嘴出口组(21)之间的第二阀座(181)接触和不接触的位置之间移动 90)。 用于抑制气体燃料从气体喷嘴室(91)向第一燃料的迁移的液压锁紧密封件(93)包括围绕气针阀构件(73)的引导段(74)的环形容积(191)。 环形体积(191)通过密封通道(190)与液体喷嘴体积(99)流体连接。 止回阀(200)定位在密封通道(190)中,并且可响应于液体喷嘴室(99)中的液体燃料与气体喷嘴室(91)中的气体燃料之间的压差而移动到闭合位置 尖端部件(71)。 当气体燃料供应被排出时,止回阀(200)可以关闭,并且利用双重燃料喷射器(12)的发动机(5)以跛脚的单次燃料供给模式运行。
    • 3. 发明申请
    • PIEZO INTENSIFIER FUEL INJECTOR AND ENGINE USING SAME
    • PIEZO INTENSIFIER燃油喷射器和使用它的发动机
    • WO2009051675A1
    • 2009-04-23
    • PCT/US2008/011681
    • 2008-10-10
    • CATERPILLAR INC.KIM, HoisanGIBSON, DennisSOMMARS, Mark
    • KIM, HoisanGIBSON, DennisSOMMARS, Mark
    • F02M47/02F02M57/02F02M59/36F02M63/00
    • F02M59/366F02M47/027F02M57/025F02M63/0026F02M63/0064
    • A common rail (18) fuel injection system includes a piezo intensifier fuel injector (14) that includes a plurality of components. Among these are a needle valve member (60), an intensifier piston (80), a first piezo stack electrical actuator (50) and a second piezo stack electrical actuator (51). These components have a first configuration at which the needle valve member (60) blocks a nozzle outlet (16) of the fuel injector (14), and a shoulder (87) of the intensifier piston (80) is exposed to fluid pressure in a common rail (18). The components have a second configuration at which the nozzle outlet (16) is fluidly connected to the common rail (18) for a low pressure injection event (A). The components have a third configuration at which the nozzle outlet (16) is fluidly blocked from the common rail (18), but movement of the intensifier displaces fluid through the nozzle outlet (16) for a high pressure injection event.
    • 共轨(18)燃料喷射系统包括包括多个部件的压电增强器燃料喷射器(14)。 其中包括针阀构件(60),增压器活塞(80),第一压电叠层电致动器(50)和第二压电叠层电致动器(51)。 这些部件具有第一构造,针阀构件(60)阻挡燃料喷射器(14)的喷嘴出口(16),并且增压器活塞(80)的肩部(87)暴露于流体压力 共轨(18)。 这些部件具有第二配置,在该第二配置处喷嘴出口(16)流体地连接到用于低压喷射事件(A)的共轨(18)。 这些部件具有第三构型,在该第三构型处,喷嘴出口16从共轨(18)流体地阻挡,但是增压器的运动使流体通过喷嘴出口(16)移动,用于高压注射事件。
    • 4. 发明申请
    • DUAL FUEL INJECTOR, ENGINE USING THE SAME AND METHOD OF OPERATING THE ENGINE
    • 双燃料喷射器,使用它的发动机和操作发动机的方法
    • WO2012155030A3
    • 2013-01-03
    • PCT/US2012037483
    • 2012-05-11
    • CATERPILLAR INCKIM HOISANDING XIANGDONGSOMMARS MARK F
    • KIM HOISANDING XIANGDONGSOMMARS MARK F
    • F02D19/06F02M43/04F02M45/08F02M47/02F02M63/02
    • F02D19/0615F02D19/0684F02D19/0694F02D19/10F02M43/04F02M45/086F02M47/027F02M51/06F02M51/0625F02M63/029F02M2200/44F02M2200/46Y02T10/36
    • A dual fuel injector (100) may be used to inject both gas and liquid fuel into a cylinder (7) of a compression ignition engine (5). An injector body (12) defines a first set of nozzle outlets (90), a second set of nozzle outlets (90), a first fuel inlet (33) and a second fuel inlet (36). A dual solenoid actuator (100) includes a first armature (110), a first coil (102), a second armature (103) and a second coil (104) that share a common centerline (54). The dual solenoid actuator (100) has a non-injection configuration at which the first armature (110) is at an un-energized position and the second armature (103) is at an un-energized position. The dual solenoid actuator (100) has a first fuel injection configuration at which the first fuel inlet (48) is fluidly connected to the first set of nozzle outlets (90), the first armature (110) is at an energized position and the second armature (103) is at the un-energized position. The dual solenoid actuator (100) has a second fuel injection configuration at which the second fuel inlet (57) is fluidly connected to the second set of nozzle outlets (96), the first armature (110) is at the un-energized position and the second armature (103) is at an energized position. The dual solenoid actuator (100) may also include a combined fuel injection configuration.
    • 双燃料喷射器(100)可用于将气体和液体燃料喷射到压缩点火发动机(5)的气缸(7)中。 喷射器主体(12)限定第一组喷嘴出口(90),第二组喷嘴出口(90),第一燃料入口(33)和第二燃料入口(36)。 双螺线管致动器(100)包括共享公共中心线(54)的第一电枢(110),第一线圈(102),第二电枢(103)和第二线圈(104)。 双螺线管致动器(100)具有非注入构造,第一电枢(110)处于非激励位置,第二电枢(103)处于未通电位置。 双螺线管致动器(100)具有第一燃料喷射构造,第一燃料入口(48)在该第一燃料喷射构造处流体地连接到第一组喷嘴出口(90),第一电枢(110)处于通电位置,第二燃料入口 电枢(103)处于未通电位置。 双螺线管致动器(100)具有第二燃料喷射构造,第二燃料入口(57)在该第二燃料喷射构造处流体地连接到第二组喷嘴出口(96),第一电枢(110)处于未通电位置,并且 第二电枢(103)处于通电位置。 双螺线管致动器(100)还可以包括组合的燃料喷射构造。
    • 9. 发明申请
    • FUEL INJECTOR FOR DUAL FUEL COMMON RAIL SYSTEM
    • 双燃料通用铁路系统燃油喷射器
    • WO2013033136A1
    • 2013-03-07
    • PCT/US2012/052756
    • 2012-08-29
    • CATERPILLAR INC.KIM, Hoisan
    • KIM, Hoisan
    • F02M43/04F02D19/06F02D19/08F02M55/02F02M61/18
    • F02M43/04F02D19/0647F02D19/0694F02D19/10F02M47/027F02M55/02F02M63/0019F02M63/0035F02M63/0064F02M63/008F02M2200/44Y02T10/36
    • A duel fuel system (10) includes a plurality of fuel injectors (12) that have a non-injection configuration, a liquid fuel injection configuration, a gaseous fuel injection configuration and a combined fuel injection configuration. Each of the fuel injectors (12) is fluidly connected to a gaseous fuel common rail (14) and a liquid fuel common rail (16). Each of the fuel injectors (12) includes a three way gas control valve (28) and a three way liquid control valve (29) that move along a common centerline (19). A gas control chamber (92) of each fuel injector (12) is fluidly connected to the liquid fuel common rail (16) by two passages (152, 154) in parallel when the gas control valve member (105) is in a first position corresponding to the non-injection configuration. The liquid control chamber (95) of each fuel injector (12) is also fluidly connected to the liquid fuel common rail (16) by two passages (150, 151) in parallel when the liquid control valve (29) is in a first position, again corresponding to the non-injection configuration.
    • 决斗燃料系统(10)包括具有非喷射构造,液体燃料喷射构造,气体燃料喷射构造和组合燃料喷射构造的多个燃料喷射器(12)。 每个燃料喷射器(12)流体地连接到气体燃料共轨(14)和液体燃料公共轨道(16)。 每个燃料喷射器(12)包括沿公共中心线(19)移动的三通气体控制阀(28)和三通液体控制阀(29)。 当气体控制阀构件(105)处于第一位置时,每个燃料喷射器(12)的气体控制室(92)通过两个通道(152,154)流体连接到液体燃料共轨(16) 对应于非注入配置。 当液体控制阀(29)处于第一位置时,每个燃料喷射器(12)的液体控制室(95)也通过两个通道(150,151)流体地连接到液体燃料公共轨道(16) ,再次对应于非注入配置。
    • 10. 发明申请
    • DUAL FUEL INJECTOR AND ENGINE USING SAME
    • 双燃料喷射器和发动机使用相同
    • WO2012155030A2
    • 2012-11-15
    • PCT/US2012/037483
    • 2012-05-11
    • CATERPILLAR INC.KIM, HoisanDING, XiangdongSOMMARS, Mark, F.
    • KIM, HoisanDING, XiangdongSOMMARS, Mark, F.
    • F02D19/06F02M43/04F02M47/02F02M63/02F02M45/08
    • F02D19/0615F02D19/0684F02D19/0694F02D19/10F02M43/04F02M45/086F02M47/027F02M51/06F02M51/0625F02M63/029F02M2200/44F02M2200/46Y02T10/36
    • A dual fuel injector (100) may be used to injector both gas and liquid fuel into a cylinder (7) of a compression ignition engine (5). An injector body (12) defines a first set of nozzle outlets (90), a second set of nozzle outlets (90), a first fuel inlet (33) and a second fuel inlet (36). A dual solenoid actuator (100) includes a first armature (110), a first coil (102), a second armature (103) and a second coil (104) that share a common centerline (54). The dual solenoid actuator (100) has a non-injection configuration at which the first armature (110) is at an un-energized position and the second armature (103) is at an un-energized position. The dual solenoid actuator (100) has a first fuel injection configuration at which the first fuel inlet (48) is fluidly connected to the first set of nozzle outlets (90), the first armature (110) is at an energized position and the second armature (103) is at the un-energized position. The dual solenoid actuator (100) has a second fuel injection configuration at which the second fuel inlet (57) is fluidly connected to the second set of nozzle outlets (96), the first armature (110) is at the un-energized position and the second armature (103) is at an energized position. The dual solenoid actuator (100) may also include a combined fuel injection configuration.
    • 双燃料喷射器(100)可用于将气体和液体燃料喷射到压缩点火发动机(5)的气缸(7)中。 喷射器主体(12)限定第一组喷嘴出口(90),第二组喷嘴出口(90),第一燃料入口(33)和第二燃料入口(36)。 双螺线管致动器(100)包括共享公共中心线(54)的第一电枢(110),第一线圈(102),第二电枢(103)和第二线圈(104)。 双螺线管致动器(100)具有非注入构造,第一电枢(110)处于非激励位置,第二电枢(103)处于未通电位置。 双螺线管致动器(100)具有第一燃料喷射构造,第一燃料入口(48)在该第一燃料喷射构造处流体地连接到第一组喷嘴出口(90),第一电枢(110)处于通电位置,第二燃料入口 电枢(103)处于未通电位置。 双螺线管致动器(100)具有第二燃料喷射构造,第二燃料入口(57)在该第二燃料喷射构造处流体地连接到第二组喷嘴出口(96),第一电枢(110)处于未通电位置,并且 第二电枢(103)处于通电位置。 双螺线管致动器(100)还可以包括组合的燃料喷射构造。