某型航空发动机综合电子调节器测控系统设计  

Design of measurement and control system for EEC of a type of aero-engine

作　　者：李洪栋 王雷涛 杨全廷 

机构地区：[1]空军95927部队

出　　处：《传感器与微系统》2012年第1期114-116,共3页Transducer and Microsystem Technologies

摘　　要：基于虚拟仪器技术研制了某型航空发动机综合电子调节器测试系统,进行了传感器的虚拟和硬件部分的设计以及软件的开发与调试。实验测试证明:测控系统能够实现相关传感器的模拟和所有信号的模拟发送与采集,测试精度高,性能稳定,在研究综合电子调节器内部结构和控制规律,以及发动机数字控制系统设计中具有重要的工程应用价值。Based on the virtual instrument technology, a test system for electronic engine controller（EEC） of an aero-engine is designed. The signals of the sensors is simulated. The hardware of the system is established. The program is designed. The test experiments show that all needed signals can be simulated, sent, and collected. The test system is reliable, stable and has high precision. It has important value in studying EEC inside structural and control rule, and designing digital electronical controller for aero-engine.

关 键 词：航空发动机 传感器 测控系统 电子发动机调节器 

分 类 号：TP212[自动化与计算机技术—检测技术与自动化装置]