INDUCTION REGULATOR BLOCK
    4.
    发明授权
    INDUCTION REGULATOR BLOCK 有权
    感应调节器块

    公开(公告)号:EP1952009B1

    公开(公告)日:2011-04-06

    申请号:EP06808745.1

    申请日:2006-11-10

    申请人: Kennedy, Roger

    发明人: Kennedy, Roger

    IPC分类号: F02M35/10 F02M29/00

    摘要: The invention provides a manifold block (140) for improving the efficiency of an internal combustion engine. The manifold block is arranged to be located between an inlet manifold and a cylinder head of the engine (130), and comprises a block of material having at least one manifold channel (110) there through. The manifold channel has an input end and an output end, wherein the input end is connected to the inlet manifold (102), and the output end is connected to the cylinder. The manifold channel includes at least one injector head channel (132) located towards its input end and adapted to receive a fuel injector. The manifold block may also incorporate one or more induction regulators for improving the efficiency of fuel/air mixing in the manifold channels (104, 106, 108, 110).

    摘要翻译: 本发明提供了一种用于改善内燃机效率的歧管块(140)。 歧管块布置成位于发动机(130)的入口歧管和汽缸盖之间,并且包括具有穿过其中的至少一个歧管通道(110)的材料块。 歧管通道具有输入端和输出端,其中输入端连接到入口歧管(102),并且输出端连接到汽缸。 歧管通道包括至少一个朝向其输入端定位并适于接收燃料喷射器的喷射器头通道(132)。 歧管块还可以包含一个或多个感应调节器,用于提高歧管通道(104,106,108,110)中燃料/空气混合的效率。

    WING STRUCTURE OF AIR SWIRLING DEVICE FOR INTERNAL COMBUSTION ENGINE
    6.
    发明公开

    公开(公告)号:EP1478832A4

    公开(公告)日:2005-03-16

    申请号:EP03703400

    申请日:2003-01-22

    申请人: KIM SEI-YOUNG

    发明人: KIM SEI-YOUNG

    摘要: Disclosed is a wing structure of air swirling device for internal combustion engine, which has a swirling device body mounted in an air cleaner, a plurality of wings mounted slantingly and radially on the swirling device body for accelerating or increasing an airflow revolution, and one or more slits formed on prescribed positions of the plurality of wings for suppressing the formation of eddy in a negative pressure zone on the rear surface of each of the plurality of wings, includes a plurality of auxiliary wings protrudedly provided to the outside with reference to the surface of each of the wings, so that the airflow collided against the surface of each of said wings go straight ahead.

    摘要翻译: 公开了一种用于内燃机的空气涡流装置的机翼结构,其具有安装在空气滤清器中的涡流装置本体,多个安装在涡流装置本体上的用于加速或增加气流旋转的翼部, 形成在多个翼的规定位置上的更多狭缝用于抑制在多个翼的每一个的后表面上的负压区中形成涡流,所述多个翼包括多个辅助翼,所述辅助翼相对于表面突出地设置在外侧 ,使得与每个所述翼的表面碰撞的气流直线前进。

    INDUCTION AND FUEL DELIVERY SYSTEM FOR PISTON ENGINE
    7.
    发明公开
    INDUCTION AND FUEL DELIVERY SYSTEM FOR PISTON ENGINE 无效
    EINLASS- UND KRAFTSTOFFZUFUHYSYSTEMFÜRKOLBENMOTOR

    公开(公告)号:EP2078153A4

    公开(公告)日:2015-03-25

    申请号:EP06804475

    申请日:2006-11-06

    申请人: ENVIROTECH LTD

    摘要: Apparatus constituting part of an induction and fuel delivery system for a cylinder of a piston internal combustion engine comprising a small cyclone into which is tangentially discharged a flow of heated air to generate a sustained vortex of high rotational speed; a modulatable fuel injector delivering a flow of atomized fuel into said small cyclone wherein it underdoes flash evaporation and energetic mixing; a delivery duct connecting said small cyclone to the inlet tract of said cylinder wherein said vortex fuel-air mixture is mixed with heated induction air; and means to prevent overheating of said modulatable fuel injector.

    摘要翻译: 构成用于活塞内燃机的气缸的感应和燃料输送系统的一部分的装置,其包括小的旋风分离器,切向地排出热空气流以产生高转速的持续涡流; 一个可调节的燃料喷射器将雾化燃料流输送到所述小旋风分离器中,其中它发生闪蒸和高能混合; 将所述小旋风分离器连接到所述气缸的入口管道的输送管道,其中所述涡流燃料 - 空气混合物与加热的感应空气混合; 以及用于防止所述可调节燃料喷射器过热的装置。

    FLUID PROCESSING METHOD
    8.
    发明授权
    FLUID PROCESSING METHOD 有权
    VERFAHREN ZUR BEHANDLUNG VONFLÜSSIGKEITEN

    公开(公告)号:EP1064083B1

    公开(公告)日:2006-05-24

    申请号:EP99912381.3

    申请日:1999-03-11

    申请人: Lytesyde L.L.C.

    发明人: ROCK, Kelly

    IPC分类号: B01F5/00 F02M29/00

    摘要: This disclosure relates to a centrifugal vortex system for preparing a liquid, such as fuel and includes a chamber housing defining a vortex chamber. An array of tangential apertures are formed in the chamber housing to permit fluid to be turbulently introduced into the vortex chamber to create a vortical flow of fluid through the vortex chamber. In one embodiment, a plurality of vortex chambers are arranged in series to allow the fluid to pass through several vortex chambers. In other eombodiments, the chamber housing may be stepped, textured, or both to increase the turbulence of the flow through the chamber. In yet another embodiment, a pressure differential supply jacket is provided to normalize the amount of flow through the tangential apertures according to the location of the apertures. A centrifuge chamber is also disclosed which has a plurality of output conduits on a bottom surface and a tapered extension member downwardly extending from a top surface to enhance the centrigugal flow of the fluid. Additionally, a bypass conduit is provided to selectively permit the flow to bypass one or more chambers.

    摘要翻译: 本公开涉及一种用于制备诸如燃料的液体的离心涡流系统,并且包括限定涡流室的腔室。 在腔室壳体中形成切向孔阵列,以允许流体被湍流地引入涡流室中以产生通过涡流室的涡流涡流。 在一个实施例中,多个涡流室被串联布置以允许流体通过几个涡流室。 在其它实施例中,室室可以是阶梯状,纹理化的或两者的,以增加通过室的流动的紊流。 在另一个实施例中,提供压力差供应套管以根据孔的位置标准化通过切向孔的流量。 还公开了一种离心机室,其在底表面上具有多个输出导管,并且从顶表面向下延伸的锥形延伸构件以增强流体的离心流动。 另外,提供旁路管道以选择性地允许流动绕过一个或多个腔室。