民用飞机客舱舱门区域温度控制研究  

Research on the Temperature Control of the Cabin Door Area for Civil Aircraft

作　　者：杨智[1] 程湛[1] 

机构地区：[1]上海飞机设计研究院,上海201210

出　　处：《民用飞机设计与研究》2013年第3期46-48,共3页Civil Aircraft Design & Research

摘　　要：对民用飞机客舱舱门区域温度控制进行了研究,建立了客舱舱门区域温度计算模型,并且提出了客舱舱门区域温度控制方法:即客舱舱门区域温度控制主要通过加热器来提高供入舱门区域的空气温度来实现;而舱门接触温度控制主要通过在舱门结构梁与内饰板之间布置绝热层或增加内饰板的热阻来实现。同时为避免在某些工况下舱门加热器出口空气温度太高舱门区域加热器需设置自动关断逻辑。The temperature control of cabin door area for civil aircraft is investigated, and the calculation model of cabin door area is established. The method of temperature control for cabin door area is also presented. It could be laid out a heater to improve the air temperature of cabin door area inlet for the temperature control of door area, and it could be laid out the insulation between structure and liner of the cabin door or enhanced the resistance of liner for the temperature control of door area. And at the same time, the logic of automatic shutting off has to be set in order to avoid that the outlet temperature of heater is too high in some operating condition.

关 键 词：舱门区域 温度控制 民用飞机 

分 类 号：V223.2[航空宇航科学与技术—飞行器设计]