首页> 外国专利> DIESEL ENGINE OPERATED BY FUEL INFERIOR TO IGNITION PROPERTYAND FUEL JET VALVE USED IN SAID ENGINE

DIESEL ENGINE OPERATED BY FUEL INFERIOR TO IGNITION PROPERTYAND FUEL JET VALVE USED IN SAID ENGINE

机译:汽油发动机劣质点火用柴油发动机和通用发动机燃料喷射阀

摘要

The fuel system of a motor features injectors with separate inlets (8, 21) for main fuel and pilot fuel. Each injector has a single set of side nozzle holes (5) and an axially shiftable glider (10), which in a foremost extreme position closes off the nozzle holes. The main fuel can flow to the nozzle holes (5) through an internal glider hole (11, 13), which open into the wall of the slider and after a certain backwards movement of the glider stand opposite the nozzle holes. The pilot fuel can flow through a non-return valve (22) to a chamber (14) in front of the glider's foremost end face. A narrow hole (15) leads from the chamber to the glider hole. When the injection period ends upon the forward movement of the glider, this pumps the pilot fuel from the chamber (14) in to the glider hole (11, 13). As a consequence the main fuel which is injected in the first phase of each injection period contains a high amount of pilot fuel. Problem free ignition is hereby assured with minimal use of pilot fuel and with an uncomplicated assembly and direction of the fuel system.IMAGE
机译:发动机的燃油系统的喷射器带有分别用于主燃料和引燃燃料的单独入口(8、21)。每个喷油器都有一套侧喷嘴孔(5)和一个可轴向移动的滑杆(10),滑杆在最重要的位置将喷嘴孔封闭。主燃料可以通过内部滑孔(11、13)流向喷嘴孔(5),该滑孔通向滑块的壁,并且在滑阀经过一定的向后移动后,与喷嘴孔相对。引燃燃料可以通过止回阀(22)流到滑翔机最前端端面前面的腔室(14)。狭窄的孔(15)从腔室通向滑翔机孔。当滑行器向前运动时喷射周期结束时,这会将引燃燃料从燃烧室(14)泵入滑行器孔(11、13)。结果,在每个喷射周期的第一阶段中喷射的主燃料包含大量的引燃燃料。因此,通过最少使用引燃燃料以及燃料系统的组装和方向不复杂,可以确保无故障点火。

著录项

  • 公开/公告号JPH059633B2

    专利类型

  • 公开/公告日1993-02-05

    原文格式PDF

  • 申请/专利权人 MAN B & W DIESEL AS;

    申请/专利号JP19850074167

  • 发明设计人 PEDERSEN PETER SUNN;

    申请日1985-04-08

  • 分类号F02M43/04;F02B3/06;F02M61/10;F02M61/18;

  • 国家 JP

  • 入库时间 2022-08-22 05:19:20

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