小型航空发动机测控系统设计  

Design of Measurement and Control System for Small Aero Engine

作　　者：鹿麟[1] 王少峰[1] 

机构地区：[1]中国电子科技集团第三十八研究所,安徽合肥230031

出　　处：《自动化技术与应用》2013年第1期114-118,共5页Techniques of Automation and Applications

摘　　要：发动机测控系统用于测试发动机的各项性能参数,以便更好的完成航空产品设计。文章提出一种基于PLC硬件和OPC接口技术的小型航空发动机测控系统,实现了发动机测试过程中参数数据的实时采集、处理、存储以及油门舵机的控制。经过调试运行证明,该系统可靠性高、界面友好、扩展性强,满足了小型航空发动机测试的需要。Measurement and control system for Engine is applied in detecting the performance parameters of engine, and accomplishes the better design of aeronautic product. A measurement and control system for small aero engine based on PLC hardware and OPC interface technology is put forward in this paper, and it achieves functions of real-time data acquisition, processing and storage and throttle servo control. The application shows that the system has high reliability, friendly interface and strong expansibility, and it meets the need of small aero engine test.

关 键 词：小型航空发动机 测控系统 PLC OPC接口技术 

分 类 号：TP274.2[自动化与计算机技术—检测技术与自动化装置]