| 民用飞机客舱舱门区域温度控制研究 |
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| 引用本文： | 杨 智、程 湛. 民用飞机客舱舱门区域温度控制研究[J]. 民用飞机设计与研究, 2013, 0(3): 46-48 |
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| 作者姓名： | 杨 智、程 湛 |
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| 作者单位： | 上海飞机设计研究院,上海,201210 |
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| 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。
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| 关 键 词： | 舱门区域 温度控制 民用飞机 |
Research on the Temperature Control of the Cabin Door Area for Civil Aircraft |
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| Yang Zhi , Chen Zhan. Research on the Temperature Control of the Cabin Door Area for Civil Aircraft[J]. Civil Aircraft Design and Research, 2013, 0(3): 46-48 |
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| Authors: | Yang Zhi Chen Zhan |
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| Affiliation: | Shanghai Aircraft Design and Research Institute,Shanghai 201210,China |
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| Abstract: | 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. |
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| Keywords: | Door Area Temperature Control Civil Aircraft |
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