航空活塞发动机电控硬件的模块化设计与实现
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昆明理工大学 民航与航空学院 昆明 650500

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TP216.1

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国家自然科学基金(61863017)资助项目


Modular design and implementation of electronic control hardware for the aero piston engine
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Faculty of Civil Aviation and Aeronautics, Kunming University of Science and Technology, Kunming 650500, China

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    摘要:

    针对高压共轨型航空活塞发动机的电控单元硬件电路,采用模块化设计方法有助于电控硬件系统适应功能化集成芯片的发展趋势。以英飞凌32位微控制器芯片为核心,从整体到细节对3.3 V和5 V电源供电稳压、MCU晶振供电、0 ~5 V传感器信号调理、执行器高低边功率驱动、PCB电路板布局等进行了模块化电路设计。经过PCB印刷电路制板和电子元器件的手工焊接,在发动机台架上进行了电路硬件系统的实验验证。实验结果中重点分析了曲轴凸轮轴传感器信号调理模块的0 ~3.3 V电压限幅和变频方波变换、高压泵油量计量电磁阀高边MOS管满足最大5 A的功率驱动和喷油器24~48 V混合半桥MOS管驱动Peak-Hold型瞬态电流。其整体实验效果好,符合应用要求。

    Abstract:

    The modular design method is adopted for the hardware circuit of electronic control unit on the high pressure common rail aero piston engine, which is helpful for the electronic control hardware system to adapt to the development trend of functional integrated chip. As the core of Infineon 32-bit microcontroller chip, it was modularly designed from the whole to the details by including the 3.3 V and 5 V power supply, MCU crystal oscillator power supply, 0 ~ 5 V sensor signal conditioning, high and low side power driving of the actuators, PCB layout and so on. After PCB printed circuit board and manual welding of electronic components, the circuit hardware system was verified on the engine bench. In the experimental results, it was analyzed that the 0 ~ 3.3 V voltage limiting and variable frequency square wave conversion of the signal conditioning module of crankshaft and camshaft sensor, the maximum 5 A power driving of the high-side MOS tube of the high pressure pump metering solenoid valve and the driving Peak-Hold transient current of the 24 ~ 48 V hybrid half-bridge MOS tube of the fuel injectors.

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徐劲松,黄国勇.航空活塞发动机电控硬件的模块化设计与实现[J].电子测量技术,2021,44(16):37-44

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  • 在线发布日期: 2024-08-22
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