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Improvements in or relating to internal combustion engines employing liquid fuel injection and compression ignition

机译:使用液体燃料喷射和压燃的内燃机的改进或与之有关的改进

摘要

470,404. Oil engines. RICARDO, H. R. Feb. 13, 1936, No. 4367. [Class 7 (iii)] The spherical combustion chamber of a compression ignition engine communicates with the cylinder through similar parallel or slightly inclined cylindrical passages F, in a hot plug C. The axis of the fuel injector D lies in a particular plane and at a certain perpendicular distance from the centre X of the combustion chamber, the axis of the fuel jet meeting the wall of the combustion chamber at a point situated near the orifices of the passages in the plug. The passages are preferably arranged so that the air streams through them blend into a common stream before reaching the injector. The direction of the fuel jet may be such that the main portion of the fuel is carried by the rotating air agains t the hot plug. The combustion chamber may be arranged in the cylinder head or at the side of the cylinder and it may be offset from a radial plane containing the cylinder axis. The invention is applicable to engines in which the whole or only part of the combustion space is formed by the spherical chamber. For starting purposes, the combustion chamber is provided with a heating plug E. Specifications 371,025, 384,340, 431,345, and 439,426 are referred to.
机译:470,404。石油发动机。 RICARDO,HR,1936年2月13日,第4367号。[等级7(iii)]压燃式发动机的球形燃烧室通过热塞C中类似的平行或略微倾斜的圆柱形通道F与气缸连通。喷油器D的轴线位于特定平面内且距燃烧室中心X垂直一定距离,燃料射流的轴线在靠近燃烧室壁孔的位置与燃烧室壁相遇。插头。通道优选地布置成使得穿过它们的空气流在到达喷射器之前混合成共同的流。燃料射流的方向可以使得燃料的主要部分由旋转的空气再次通过热塞来携带。燃烧室可以布置在汽缸盖中或在汽缸的侧面,并且它可以偏离包含汽缸轴线的径向平面。本发明适用于其中全部或仅部分燃烧空间由球形腔形成的发动机。为了启动的目的,燃烧室设置有加热塞E。参考规格371,025、384,340、431,345和439,426。

著录项

  • 公开/公告号GB470404A

    专利类型

  • 公开/公告日1937-08-13

    原文格式PDF

  • 申请/专利权人 HARRY RALPH RICARDO;

    申请/专利号GB19360004367

  • 发明设计人

    申请日1936-02-13

  • 分类号F02B19/08;F02B19/14;

  • 国家 GB

  • 入库时间 2022-08-24 05:41:33

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