摘要
现代飞机性能不断提高,高功率集成电子电器设备的出现,使飞行器的总体性能得到发展,但同时产生了较大负荷。在这样情况下,亟需加强对蒸发循环制冷系统的分析和研究。以某型直升机为例,根据该机型对驾驶舱制冷的技术要求,确定蒸发循环制冷系统的各组件方案,并运用仿真系统对设计进行优化。
With the continuous improvement of modern aircraft performance and the emergence of high power integrated electronic and electrical equipment,the overall performance of the aircraft has been developed,but at the same time,it also produces a large load.In this case,it is urgent to strengthen the analysis and research of evaporative cycle refrigeration system.Based on the technical requirements of the model for cabin refrigeration,this paper determines the components of evaporative cycle refrigeration system,and optimizes the design by using simulation system.
作者
何予东
张毅
李志刚
HE Yudong;ZHANG Yi;LI Zhigang(Xinxiang Aviation Industry(Group)Co.,Ltd.,Xinxiang 450049;China Railway Engineering Equipment Group Tunnel Equipment Manufacturing Co.,Ltd.,Xinxiang 453000;Henan Henan Hydrogen Equipment Co.,Ltd.,Xinxiang 453000)
出处
《现代制造技术与装备》
2020年第6期83-85,共3页
Modern Manufacturing Technology and Equipment
关键词
蒸发循环制冷系统
控制规律
动态性能
性能参数
evaporation cycle refrigeration system
control law
dynamic performance
performance parameters