Turbulent jet ignition pre-chamber combustion system for spark ignition engines
    1.
    发明授权
    Turbulent jet ignition pre-chamber combustion system for spark ignition engines 有权
    用于火花点火发动机的湍流喷射点火预燃室燃烧系统

    公开(公告)号:US08857405B2

    公开(公告)日:2014-10-14

    申请号:US13286638

    申请日:2011-11-01

    Applicant: William Attard

    Inventor: William Attard

    Abstract: An ignition system for an internal combustion engine having at least one combustion chamber where the ignition system includes a housing, an ignition device, an injector, and a pre-chamber having a nozzle disposed spaced from the proximal portion of the pre-chamber. The igniter portion of the ignition device and the nozzle of the injector are operatively supported in the proximal portion of the pre-chamber and disposed flush therewith. The igniter portion ignites the fuel in pre-chamber such that partially combusted pre-chamber products are forced through orifices in the pre-chamber nozzle and extinguish, but dispersed through the combustion chamber so as to ignite the main fuel charge therein.

    Abstract translation: 一种用于具有至少一个燃烧室的内燃机的点火系统,其中所述点火系统包括壳体,点火装置,喷射器和具有与所述预制室的近侧部分间隔开的喷嘴的预制室。 点火装置的点火器部分和喷射器的喷嘴可操作地支撑在预燃室的近侧部分中并且与其齐平地设置。 点火器部分点燃预燃室中的燃料,使得部分燃烧的预制室产物被迫通过预喷室喷嘴中的孔并熄灭,但是通过燃烧室分散以便点燃其中的主要燃料电荷。

    FUEL INJECTION SYSTEM FOR AN ENGINE
    3.
    发明申请
    FUEL INJECTION SYSTEM FOR AN ENGINE 审中-公开
    发动机燃油喷射系统

    公开(公告)号:US20160061095A1

    公开(公告)日:2016-03-03

    申请号:US14934188

    申请日:2015-11-06

    CPC classification number: F02B19/12 F02B19/1057 F02D41/3017 Y02T10/125

    Abstract: A fuel injection system for an engine is described. The fuel injection system includes a prechamber assembly mounted on a cylinder head of the engine. The prechamber assembly includes a prechamber located upstream of a combustion chamber of the engine and configured to receive air-fuel mixture. Further, the prechamber assembly includes a fuel injector to controllably supply fuel into the prechamber, where the supplied fuel mixes with the air-fuel mixture to form a homogeneous mixture of air and fuel at a predefined stoichiometric ratio. The prechamber assembly also includes a spark plug disposed at a downstream region of the prechamber, the downstream region being proximal to the combustion chamber of the engine. The fuel injection system also includes a controller operably coupled to the fuel injector, where the controller is configured to control the predefined stoichiometric ratio of air to fuel in in the prechamber.

    Abstract translation: 描述了用于发动机的燃料喷射系统。 燃料喷射系统包括安装在发动机的气缸盖上的预燃室组件。 前置机组件包括位于发动机的燃烧室的上游并被配置为接收空气 - 燃料混合物的预燃室。 此外,前室组件包括燃料喷射器以可控地将燃料供应到预燃室中,其中供应的燃料与空气 - 燃料混合物混合以以预定的化学计量比形成空气和燃料的均匀混合物。 预制室组件还包括设置在预室的下游区域处的火花塞,下游区域靠近发动机的燃烧室。 燃料喷射系统还包括可操作地耦合到燃料喷射器的控制器,其中控制器配置成控制预燃室中空气与燃料的预定化学计量比。

    TURBULENT JET IGNITION PRE-CHAMBER COMBUSTION SYSTEM FOR SPARK IGNITION ENGINES
    4.
    发明申请
    TURBULENT JET IGNITION PRE-CHAMBER COMBUSTION SYSTEM FOR SPARK IGNITION ENGINES 有权
    用于火花点火发动机的涡轮喷嘴预燃室燃烧系统

    公开(公告)号:US20120103302A1

    公开(公告)日:2012-05-03

    申请号:US13286638

    申请日:2011-11-01

    Applicant: William Attard

    Inventor: William Attard

    Abstract: An ignition system for an internal combustion engine having at least one combustion chamber where the ignition system includes a housing, an ignition device, an injector, and a pre-chamber having a nozzle disposed spaced from the proximal portion of the pre-chamber. The igniter portion of the ignition device and the nozzle of the injector are operatively supported in the proximal portion of the pre-chamber and disposed flush therewith. The igniter portion ignites the fuel in pre-chamber such that partially combusted pre-chamber products are forced through orifices in the pre-chamber nozzle and extinguish, but dispersed through the combustion chamber so as to ignite the main fuel charge therein.

    Abstract translation: 一种用于具有至少一个燃烧室的内燃机的点火系统,其中所述点火系统包括壳体,点火装置,喷射器和具有与所述预制室的近侧部分间隔开的喷嘴的预制室。 点火装置的点火器部分和喷射器的喷嘴可操作地支撑在预燃室的近侧部分中并且与其齐平地设置。 点火器部分点燃预燃室中的燃料,使得部分燃烧的预制室产物被迫通过预喷室喷嘴中的孔并熄灭,但是通过燃烧室分散以便点燃其中的主要燃料电荷。

    Ignition combustion pre-chamber for internal combustion engines with
constant stoichiometric air-fuel mixture at ignition
    5.
    发明授权
    Ignition combustion pre-chamber for internal combustion engines with constant stoichiometric air-fuel mixture at ignition 失效
    用于点火时具有恒定化学计量空气燃料混合物的内燃机的点火燃烧预燃室

    公开(公告)号:US5081969A

    公开(公告)日:1992-01-21

    申请号:US480170

    申请日:1990-02-14

    Abstract: An ignition combustion pre-chamber for igniting an air-fuel mixture in an internal combustion engine which operates in conjunction with an engine management system to maintain an ideal stoichiometric air-fuel ratio in the pre-chamber throughout the complete operating range of the engine. A one-way check valve admits a separate air-fuel mixture into the pre-chamber which, after mixing with the portion of the air-fuel mixture of the main combustion chamber which necessarily enters the pre-chamber during the compression stroke of the engine, results in an ideal stoichiometric mixture receptive to quick ignition and faster flame front propagation throughout the main combustion chamber. In a second embodiment, the pre-chamber is separated from the main combustion chamber by a second one-way check valve which prevents mixing of the separate air-fuel mixtures during the compression stroke, allowing a constant stoichiometric air-fuel ratio to be introduced into the pre-chamber and ignited. Alternate gaseous fuels can also be used with the pre-chamber.

    Abstract translation: 一种用于点燃内燃机中的空气燃料混合物的点火燃烧预燃烧室,其与发动机管理系统相结合,以在发动机的整个工作范围内在预燃室中保持理想的理论空燃比。 单向止回阀允许单独的空气 - 燃料混合物进入预制室,在与发动机的压缩冲程期间必须进入预制室的主燃烧室的空气 - 燃料混合物的部分混合之后 导致理想的化学计量混合物,其接受快速点火并且在整个主燃烧室中快速的火焰前传播。 在第二实施例中,预燃室通过第二单向止回阀与主燃烧室分离,其防止在压缩冲程期间混合分离的空气 - 燃料混合物,从而允许引入恒定的理论空燃比 进入前房并点燃。 替代气体燃料也可以与预燃室一起使用。

    Turbulent jet ignition pre-chamber combustion system for spark ignition engines
    6.
    发明授权
    Turbulent jet ignition pre-chamber combustion system for spark ignition engines 有权
    用于火花点火发动机的湍流喷射点火预燃室燃烧系统

    公开(公告)号:US09353674B2

    公开(公告)日:2016-05-31

    申请号:US14496824

    申请日:2014-09-25

    Abstract: An ignition system for an internal combustion engine having at least one combustion chamber where the ignition system includes a housing, an ignition device, an injector, and a pre-chamber having a nozzle disposed spaced from the proximal portion of the pre-chamber. The igniter portion of the ignition device and the nozzle of the injector are operatively supported in the proximal portion of the pre-chamber and disposed flush therewith. The igniter portion ignites the fuel in pre-chamber such that partially combusted pre-chamber products are forced through orifices in the pre-chamber nozzle and extinguish, but dispersed through the combustion chamber so as to ignite the main fuel charge therein.

    Abstract translation: 一种用于具有至少一个燃烧室的内燃机的点火系统,其中所述点火系统包括壳体,点火装置,喷射器和具有与所述预制室的近侧部分间隔开的喷嘴的预制室。 点火装置的点火器部分和喷射器的喷嘴可操作地支撑在预燃室的近侧部分中并且与其齐平地设置。 点火器部分点燃预燃室中的燃料,使得部分燃烧的预制室产物被迫通过预喷室喷嘴中的孔并熄灭,但是通过燃烧室分散以便点燃其中的主要燃料电荷。

    PRECHAMBER ASSEMBLY FOR AN ENGINE
    7.
    发明申请
    PRECHAMBER ASSEMBLY FOR AN ENGINE 审中-公开
    前置发动机总成

    公开(公告)号:US20160053667A1

    公开(公告)日:2016-02-25

    申请号:US14929438

    申请日:2015-11-02

    Abstract: A prechamber assembly for an engine is disclosed. The prechamber assembly includes an air-fuel chamber and a prechamber in fluid communication with the air-fuel chamber via a conduit. The conduit includes a first end disposed in the air-fuel chamber and a second end disposed in the prechamber to allow premixed air-fuel mixture to flow from the air-fuel chamber to the prechamber. The prechamber is to receive a lean air-fuel mixture during a compression stroke of the engine. Further, the prechamber assembly also includes a valve disposed at the first end of the conduit, the valve configured to allow the premixed air-fuel mixture to flow from the air-fuel chamber to the prechamber. The premixed air-fuel mixture entering the prechamber mixes with the lean air-fuel mixture to form a stoichiometric ratio of a rich air-fuel mixture.

    Abstract translation: 公开了一种用于发动机的前室组件。 前置机组件包括空气燃料室和经由导管与空气 - 燃料室流体连通的预制室。 导管包括设置在空气燃料室中的第一端和设置在预燃室中的第二端,以使预混合的空气 - 燃料混合物从空气 - 燃料室流动到预燃室。 预燃机是在发动机的压缩冲程期间接收稀薄的空气 - 燃料混合物。 此外,前室组件还包括设置在管道的第一端处的阀,阀构造成允许预混合的空气 - 燃料混合物从空气燃料室流动到预燃室。 进入预燃室的预混合空气 - 燃料混合物与贫空气混合物混合以形成浓空气混合物的化学计量比。

    TURBULENT JET IGNITION PRE-CHAMBER COMBUSTION SYSTEM FOR SPARK IGNITION ENGINES
    9.
    发明申请
    TURBULENT JET IGNITION PRE-CHAMBER COMBUSTION SYSTEM FOR SPARK IGNITION ENGINES 有权
    用于火花点火发动机的涡轮喷嘴预燃室燃烧系统

    公开(公告)号:US20150068489A1

    公开(公告)日:2015-03-12

    申请号:US14496824

    申请日:2014-09-25

    Abstract: An ignition system for an internal combustion engine having at least one combustion chamber where the ignition system includes a housing, an ignition device, an injector, and a pre-chamber having a nozzle disposed spaced from the proximal portion of the pre-chamber. The igniter portion of the ignition device and the nozzle of the injector are operatively supported in the proximal portion of the pre-chamber and disposed flush therewith. The igniter portion ignites the fuel in pre-chamber such that partially combusted pre-chamber products are forced through orifices in the pre-chamber nozzle and extinguish, but dispersed through the combustion chamber so as to ignite the main fuel charge therein.

    Abstract translation: 一种用于具有至少一个燃烧室的内燃机的点火系统,其中所述点火系统包括壳体,点火装置,喷射器和具有与所述预制室的近侧部分间隔开的喷嘴的预制室。 点火装置的点火器部分和喷射器的喷嘴可操作地支撑在预燃室的近侧部分中并且与其齐平地设置。 点火器部分点燃预燃室中的燃料,使得部分燃烧的预制室产物被迫通过预喷室喷嘴中的孔并熄灭,但是通过燃烧室分散以便点燃其中的主要燃料电荷。

Patent Agency Ranking