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REQUIREMENTS FOR THE MEASUREMENT OF THE AIRCRAFT STRUCTURE INTO A FIRE-RAFT MACHINE WITH A GAS-RAFT SYSTEM

机译:在具有气浮系统的气浮机中测量飞机结构的要求

摘要

The invention concerns a elongation valve for controlling the flow rate of exhaust gases recycled in intake manifold (1) of the engine (1, 2, 3). The invention is characterised in that it consists in: calculating the air flow rate (Q0) with closed control valve (5), on the basis of the engine speed (Nmot), the pressure (Pco1) in the intake manifold (1), the temperature of the air (Tair) sucked in by the engine, and a filling rate (C0) of the engine cylinders, and calculating the air flow rate (Qair) with open control valve (5) from the expression: Qair = Qo f1f2/1 + C4.f2, wherein (f1) and (f2) are correcting factors and (C4) a calibrating factor based on the engine speed (Nmot). The invention is applicable to diesel engines supercharged with air.
机译:本发明涉及一种用于控制在发动机(1、2、3)的进气歧管(1)中再循环的废气的流量的伸长阀。本发明的特征在于:基于发动机转速(Nmot),进气歧管(1)中的压力(Pco1),以关闭的控制阀(5)计算空气流量(Q0),发动机吸入的空气(Tair)的温度和发动机气缸的填充率(C0),并根据以下表达式计算控制阀(5)打开时的空气流量(Qair):Qair = Qo f1f2 / 1 + C4.f2,其中(f1)和(f2)是校正因子,(C4)是基于发动机转速(Nmot)的校准因子。本发明适用于增压空气的柴油机。

著录项

  • 公开/公告号DE60006359D1

    专利类型

  • 公开/公告日2003-12-11

    原文格式PDF

  • 申请/专利权人 RENAULT S.A.S. BOULOGNE BILLANCOURT;

    申请/专利号DE20006006359T

  • 发明设计人 ABIDA JAMIL;

    申请日2000-02-10

  • 分类号F02D41/18;F02D21/08;

  • 国家 DE

  • 入库时间 2022-08-21 22:41:43

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