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AIRCRAFT COMPARISON ENGINE INTRODUCTION AIRCRAFT MARKETING AUTHORISATION SCHEME

机译:飞机比较引擎介绍飞机营销授权方案

摘要

A fuel delivery system provided with at least a fuel delivery pump and a high pressure pump distributing fuel to individual injectors on the cylinders included with apparatus for preheating the intake air for air-compressing internal combustion engines. Communication therewith occurs through a header pipe. Components thereof include an injection valve provided at the end of all high pressure pipes leading to the engine cylinders and arranged to open at a predetermined pressure. Each of the high pressure pipes is provided with a branch off conduit arranged to be shut off by an isolating valve. All branch offs are brought together to a common header pipe supplying the preheating equipment with fuel.
机译:一种燃料输送系统,其至少具有燃料输送泵和高压泵,所述燃料输送系统将燃料分配至气缸上的各个喷射器,所述气缸包括用于对进气进行预热以对空气进行压缩的内燃机的设备。通过总管进行通信。其部件包括喷射阀,该喷射阀设置在通向发动机气缸的所有高压管的端部,并布置成以预定压力打开。每个高压管设置有分支导管,该分支导管被布置成由隔离阀关闭。所有分支都汇集到一个公共总管中,为预热设备提供燃料。

著录项

  • 公开/公告号SE7809992L

    专利类型

  • 公开/公告日1979-03-25

    原文格式PDF

  • 申请/专利权人 * MASCHINENFABRIK AUGSBURG-NURNBERG AG;

    申请/专利号SE19780009992

  • 发明设计人 N * DALFONSO;A * NEITZ;

    申请日1978-09-22

  • 分类号F02N17/02;

  • 国家 SE

  • 入库时间 2022-08-22 20:28:12

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