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    • 5. 发明申请
    • FUEL-STRATIFIED COMBUSTION CHAMBER IN A DIRECT-INJECTED INTERNAL COMBUSTION ENGINE
    • 直喷式内燃机燃油分离室
    • US20140123934A1
    • 2014-05-08
    • US14072369
    • 2013-11-05
    • David J. Schouweiler, JR.
    • David J. Schouweiler, JR.
    • F02B17/00
    • F02B17/005F02B23/101F02B23/105F02B25/14Y02T10/125
    • A combustion chamber is provided within an internal combustion engine, the chamber bounded by a cylinder bore, a primary end, and a secondary end. The secondary end reciprocates between a TDC position nearest the primary end and a BDC position. Induction and exhaust ports are timed to open and close to transfer air into, and gasses from, the chamber. The chamber becomes fuel stratified when the secondary end is positioned within a stratified distance of the primary end. When stratified, the chamber is comprised of a central region, a perimeter region, and a transfer passageway between regions. A fuel injector at the primary end injects fuel only into the central region and only prior to ignition. The perimeter region pumps air into the central region prior to ignition, creating tumble turbulence. Combustion is initiated near TDC in the central region and concluded near TDC in the transfer passageway.
    • 燃烧室设置在内燃机内,该室由气缸孔,主端和次端限定。 次级端在最接近主端的TDC位置与BDC位置之间往复运动。 感应和排气口定时打开和关闭,以将空气转移到室内并从腔室中吸入气体。 当第二端位于主端的分层距离内时,室变成燃料分层。 当分层时,室由中心区域,周边区域和区域之间的传输通道组成。 主燃料喷射器仅将燃料仅喷射到中心区域,仅在点燃之前。 周边区域在点燃之前将空气泵入中心区域,产生翻滚紊流。 在中部地区,TDC附近发起燃烧,并在TDC的传输通道附近完成燃烧。
    • 7. 发明授权
    • Multi-zone gaseous fuel high efficiency engine
    • 多区气体燃料高效发动机
    • US08291884B2
    • 2012-10-23
    • US13248652
    • 2011-09-29
    • Brad Alan BoyerMatthew Aaron Younkins
    • Brad Alan BoyerMatthew Aaron Younkins
    • F02B43/00
    • F02B23/105F02D41/0027F02D41/401F02D2041/389F02P5/045F02P15/02Y02T10/125Y02T10/44
    • An engine having cylinders capable of combusting gaseous fuel includes at least one spark plug per cylinder, a gaseous fuel injector extending into each cylinder and having at least one nozzle cluster containing a one or more nozzles positioned to direct gaseous fuel only toward a spark gap of an associated spark plug, and a control system operating each spark plug and each injector to deliver gaseous fuel directly to the cylinder and initiate combustion. A method for controlling an engine capable of operating with gaseous fuel includes injecting the gaseous fuel directly into each cylinder through a centrally located injector having a plurality of clusters of nozzles, each cluster associated with one of at least two spark plugs positioned closer to a cylinder wall than to the injector, each cluster directing the gaseous fuel toward an associated spark plug gap.
    • 具有能够燃烧气体燃料的气缸的发动机包括每个气缸至少一个火花塞,延伸到每个气缸中的气体燃料喷射器,并且具有至少一个喷嘴组,其包含一个或多个喷嘴,其定位成将气态燃料仅引导到火花隙 相关联的火花塞,以及操作每个火花塞和每个喷射器的控制系统,以将气体燃料直接输送到气缸并开始燃烧。 一种用于控制能够用气体燃料操作的发动机的方法包括通过具有多个喷嘴群的中心位置的喷射器将气体燃料直接喷射到每个气缸中,每个喷射器与位于更靠近气缸的至少两个火花塞中的一个相关联 每个簇将气体燃料引导到相关联的火花塞间隙。
    • 9. 发明申请
    • Cylinder injection engine
    • 气缸喷射发动机
    • US20110146620A1
    • 2011-06-23
    • US12926926
    • 2010-12-17
    • Makoto Kaneko
    • Makoto Kaneko
    • F02D43/00
    • F02B23/105F02B2023/102F02B2023/106F02D13/0215F02D13/0246F02D13/0261Y02T10/125Y02T10/18
    • A mask portion is provided at a partial area of an intake port at a side opposite to an exhaust port. The mask portion prevents a part of the intake port from being opened when the intake valve is in a low lift state. A top surface of a piston includes a smooth surface. An ECU sets the maximum lift of the intake valve for a variable valve mechanism to an intermediate lift and sets a fuel injection timing for an injector to a compression stroke when an operating range of the engine is a fast idle range. The intermediate lift is an amount of lift at which the intake valve is moved beyond the mask portion and a flow rate of intake air in the partial area is limited relative to a flow rate of the intake air in other areas owing to the mask portion.
    • 在与排气口相反的一侧的进气口的局部区域设置有掩模部。 当进气门处于低提升状态时,掩模部分防止进气口的一部分打开。 活塞的顶面包括光滑的表面。 ECU将可变气门机构的进气门的最大升程设定为中间升程,并且当发动机的运行范围为快速空转范围时,将喷射器的燃料喷射正时设定为压缩冲程。 中间升程是进气门移动超过掩模部分的升程量,并且部分区域中的进气的流量相对于由于掩模部分在其它区域中的进气的流量而被限制。