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VARIABLE ALTITUDE DOUBLE-VGT TWO-STAGE ADJUSTABLE BOOST CONTROL METHOD

机译:可变高度双VGT两阶段可调升压控制方法

摘要

A variable altitude double-VGT two-stage adjustable boost control method comprises: a diesel engine ECU (31) querying and storing an initial boost pressure MAP according to an intake air temperature, a pressure and a diesel engine operating condition, and correcting the initial boost pressure MAP by means of an intake air temperature sensor (12) to obtain a target boost pressure MAP; and converting, by means of a driving circuit, digital signals into execution electrical signals of a low-pressure stage VGT actuator (14), a high-pressure stage VGT actuator (30) and a high-pressure stage turbine bypass valve actuator (32), and enabling the microcontrollers in the low-pressure stage VGT actuator (14), the high-pressure stage VGT actuator (30) and the high-pressure stage turbine bypass valve actuator (32) to adjust, according to the differences between the target boost pressure and the actual boost pressures fed back thereby, the opening position of a high-pressure stage compressor bypass valve (24), the opening position of a high-pressure stage turbine bypass valve (25), and the opening position of high-pressure stage VGT blades (18, 22) in real time.
机译:一种可变高度双VGT两级可调升压控制方法,包括:柴油机ECU(31)根据进气温度,压力和柴油机工况查询并存储初始升压压力MAP,并进行校正。借助于进气温度传感器(12)增压压力MAP,以获得目标增压压力MAP;并通过驱动电路将数字信号转换为低压级VGT执行器(14),高压级VGT执行器(30)和高压级涡轮旁通阀执行器(32)的执行电信号。 ),并使低压级VGT致动器(14),高压级VGT致动器(30)和高压级涡轮旁通阀致动器(32)中的微控制器根据两者之间的差异进行调节目标增压压力和反馈的实际增压压力,高压级压缩机旁通阀(24)的打开位置,高压级涡轮旁通阀(25)的打开位置以及压力级VGT叶片(18、22)实时。

著录项

  • 公开/公告号WO2019105080A1

    专利类型

  • 公开/公告日2019-06-06

    原文格式PDF

  • 申请/专利权人 ARMY MILITARY TRANSPORTATION UNIVERSITY;

    申请/专利号WO2018CN103190

  • 发明设计人 LIU RUILIN;ZHANG ZHONGJIE;

    申请日2018-08-30

  • 分类号F02D23;F02B37/24;

  • 国家 WO

  • 入库时间 2022-08-21 11:54:33

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