Early pilot lean burn strategy in dual fuel engine using targeted pilot flames

    公开(公告)号:US10823106B1

    公开(公告)日:2020-11-03

    申请号:US16410269

    申请日:2019-05-13

    Abstract: Operating a dual fuel engine system includes injecting an early shot and a second shot of a liquid fuel into a cylinder after a late closing timing of an intake valve, and producing a first and a second pilot flame based on ignition of the early shot and the second shot of liquid fuel. The early shot of liquid fuel is targeted such that a distribution of ignition points of the first pilot flame is biased outwardly of a combustion bowl in the piston. Propagation of the first and second pilot flames from geometrically distinct ignition locations rapidly increases pressure and temperature in the cylinder to provide fast combustion of a lean mixture of a gaseous fuel and air in a main charge in the cylinder.

    Ducted Combustion Systems Utilizing Tubular Ducts
    7.
    发明申请
    Ducted Combustion Systems Utilizing Tubular Ducts 有权
    使用管道的管道燃烧系统

    公开(公告)号:US20160298583A1

    公开(公告)日:2016-10-13

    申请号:US14685264

    申请日:2015-04-13

    Abstract: A ducted combustion system is disclosed. The ducted combustion system includes a combustion chamber bound by a flame deck surface of a cylinder head of an internal combustion engine and by a piston top surface of a piston disposed within the internal combustion engine. The system includes a fuel injector including one or more orifices, the one or more orifices injecting fuel into the combustion chamber as one or more fuel jets. The system includes one or more ducts disposed within the combustion chamber between the flame deck surface and the piston top surface, the one or more ducts being generally tubular shaped structures and being disposed such that each of the one or more fuel jets at least partially enters one of the one or more ducts upon being injected into the combustion chamber.

    Abstract translation: 公开了管道燃烧系统。 管道燃烧系统包括由内燃机的气缸盖的火焰甲板表面和设置在内燃机内的活塞的活塞顶表面结合的燃烧室。 该系统包括一个燃料喷射器,该燃料喷射器包括一个或多个喷孔,一个或多个喷嘴将燃料喷射到燃烧室中作为一个或多个燃料喷射。 该系统包括设置在火焰甲板表面和活塞顶表面之间的燃烧室内的一个或多个管道,一个或多个管道通常是管状结构,并且被布置成使得一个或多个燃料喷嘴中的每一个至少部分地进入 一个或多个管道中的一个被注入到燃烧室中。

    REACTIVITY CONTROLLED COMPRESSION IGNITION ENGINE AND METHOD OF COMBUSTION PHASING CONTROL
    8.
    发明申请
    REACTIVITY CONTROLLED COMPRESSION IGNITION ENGINE AND METHOD OF COMBUSTION PHASING CONTROL 审中-公开
    反应控制压缩点火发动机和燃烧相位控制方法

    公开(公告)号:US20150285178A1

    公开(公告)日:2015-10-08

    申请号:US14243181

    申请日:2014-04-02

    Inventor: Bobby John

    Abstract: A reactivity controlled compression ignition engine compression ignites a stratified reactivity charge mixture, of recirculated exhaust gas, air, a low reactivity fuel and a high reactivity fuel. During steady state operating conditions, combustion phasing control includes adjusting an exhaust gas recirculation (EGR) rate relative to a base EGR rate associated with the steady speed and load. When transitioning to a new speed and load during a transient condition, combustion phasing control does not utilize EGR rate control, but does include adjustments to quantities and timings of at least three injection sequences of the high reactivity fuel.

    Abstract translation: 反应性控制的压缩点火发动机压缩点燃分层反应性电荷混合物,再循环废气,空气,低反应性燃料和高反应性燃料。 在稳态运行条件下,燃烧定相控制包括相对于与稳定速度和负载相关联的基本EGR率来调节废气再循环(EGR)速率。 当在瞬态条件下转变到新的速度和负载时,燃烧定相控制不利用EGR率控制,而是包括对高反应性燃料的至少三个喷射序列的量和定时的调整。

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