• 过程系统工程 •

飞机环控系统空气循环机仿真建模及试验校核

1. 1.南京机电液压工程研究中心航空机电系统综合航空科技重点试验室，江苏 南京 211106
2.南京机电科技有限公司，江苏 南京 211102
• 收稿日期:2019-10-07 修回日期:2019-11-13 出版日期:2020-04-25 发布日期:2020-05-22
• 通讯作者: 孟繁鑫 E-mail:sunsky170@163.com
• 作者简介:孟繁鑫（1983—），男，博士，高级工程师，sunsky170@163.com

Modeling and validating of air cycle machine in aircraft environmental control system

Fanxin MENG1(),Jianing SUN2,Yue ZHOU1,Zanjun GAO1,Dingbin CHENG1

1. 1.Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration in Nanjing Engineering Institute of Aircraft Systems, Nanjing 211106, Jiangsu, China
2.Nanjing Aircraft Systems Science and Technology Limited Company, Nanjing 211102, Jiangsu, China
• Received:2019-10-07 Revised:2019-11-13 Online:2020-04-25 Published:2020-05-22
• Contact: Fanxin MENG E-mail:sunsky170@163.com

Abstract:

Mathematical models of compressor-turbine-fan air cycle machine were established in aircraft environmental control system. The simulation models of air cycle machine were developed. The performance test principles and procedures are put forward for the product and performance tests are carried out to obtain the performance data under design conditions. By comparing simulation results and experimental data for compressor pressure ratio and efficiency characteristics, turbine temperature drop, fan pressure rise, the simulation model was corrected and validated. Results show that the modeling method provided in this paper can calculate the performance of the air cycle machine accurately with the ±10% simulation error. The simulation precision meets the requirements of aircraft environmental control system engineering design and it is helpful to develop environmental control system and its components.

• V 245.3
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