摘要
在对国外飞机环境控制与热能综合管理技术进行分析的基础上,以某飞机为背景,开展环境控制系统与热能综合管理系统的初步研究。提出某飞机环境控制与热能综合管理系统方案,初步完成各子系统能量的合理匹配,以期为民用飞机综合热能管理技术的预研发展提供依据。
Based on the analysis of foreign aircraft ECS and T/EMS made, the preliminary research of the ECS and T/EMS is developed for some aircraft. The ECS and T/EMS system scheme for some aircraft is presented and the parameters'matching is finished, aiming at supply the reference to the preliminary research of civil aircraft T/EMS.
出处
《民用飞机设计与研究》
2013年第2期13-17,共5页
Civil Aircraft Design & Research
关键词
环境控制系统
综合热能管理系统
民用飞机
Environmental Control System (ECS)
Integration Thermal and Energy Management System (T! EMS)
Civil Aircraft