Aircraft cabin thermal control strategy based on adaptive temperature and thermal sensation

被引:0
作者
Liu Dong [1 ]
Pang Liping [1 ]
Chen Yunpeng [1 ]
Zhou Yue [2 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Sch Aviat Sci & Engn, Beijing, Peoples R China
[2] Aviat Key Lab Sci & Technol Aero Electromech Syst, Nanjing, Jiangsu, Peoples R China
来源
2017 IEEE INTERNATIONAL CONFERENCE ON CYBERNETICS AND INTELLIGENT SYSTEMS (CIS) AND IEEE CONFERENCE ON ROBOTICS, AUTOMATION AND MECHATRONICS (RAM) | 2017年
关键词
aircraft cabin; air supply temperature; control strategy; thermal environment; dynamic simulation;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
An Environment Control System (ECS) in civil aircraft will control the cabin thermal environment with constant temperature control strategy. However, the passenger dress, heat loads will change with the flight process. This constant control strategy cannot satisfy these dynamic requirements and faces the challenge. An aircraft cabin thermal control strategy based on adaptive temperature and thermal sensation evaluation is presented in this paper to solve this question. The new thermal control strategy includes initial and accurate control strategies, which individually control the thermal environment. For the night flight mode, the initial control strategy with a constant supply air temperature is used to control the cabin thermal environment according to the adaptive temperature. For the day time, the accurate control strategy with a dynamic supply air temperature is used to control the cabin thermal environment according to the thermal sensation of passenger. This new control strategy can ensure passengers in the aircraft cabin to have a comfortable thermal sensation under different flight times and seasons.
引用
收藏
页码:183 / 187
页数:5
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