航空发动机分布式控制系统技术分析及系统方案

宋军强; 潘慕绚; 黄金泉

航空发动机分布式控制系统技术分析及系统方案

1.
南京航空航天大学能源与动力学院, 南京 210016
2.
中国航空工业集团公司航空动力控制系统研究所, 江苏无锡 214063

基金项目: 航空科学基金(2011ZB52021);中央高校基本科研业务费青年科技创新基金(NZ2012112);江苏省高校优势学科建设工程

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出版历程
- 收稿日期: 2012-08-09
- 刊出日期: 2013-10-28

Technology analysis and system scheme for aero-engine distributed control system

1.
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2.
Aviation Motor Control System Institute, Aviation Industry Corporation of China, Wuxi Jiangsu 214063, China

摘要

摘要: 分析了航空发动机分布式控制系统的系统结构、通讯总线、智能元件、高温电子元器件及分布式电源总线等领域的研究现状,并进行技术成熟度评估.结果表明:航空发动机分布式控制系统研究处于基础研究阶段,各项技术成熟度(TRL)主要处于TRL1~TRL2.针对某涡扇发动机提出基于TTCAN(时间触发控制器局域网协议)总线的过渡分布式和部分分布式两种控制系统方案,分析了各方案中系统结构、控制功能和信号交互特点,以期为航空发动机分布式控制系统进一步研究提供参考.
- 航空发动机 /
- 分布式控制系统构架 /
- 通讯总线 /
- 智能元件 /
- 高温电子元器件 /
- 电源总线
Abstract: The status, progress and technology readiness level of the system architecture, communication bus, smart components, high temperature electronic components and power bus for aero-engine distributed control system were analyzed and evaluated. The results show that the studies for aero-engine distributed control system are at fundamental phase and the technology readiness level (TRL) is TRL 1 to TRL 2. According to the analysis and evaluation aforementioned, two potential schemes of distributed control system for a turbofan were proposed, including transitionally distributed control and partially distributed control based on TTCAN bus, and the system architectures, control functions and communication traits were discussed, providing a reference for future development of the aero-engine distributed control system.
- aero-engine /
- architecture of distributed control system /
- communication bus /
- smart components /
- high temperature electronic components /
- power bus

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参考文献(36)

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