民用飞机设计与研究
民用飛機設計與研究
민용비궤설계여연구
CIVIL AIRCRAFT DESIGN AND RESEARCH
2013年
3期
46-48
,共3页
舱门区域%温度控制%民用飞机
艙門區域%溫度控製%民用飛機
창문구역%온도공제%민용비궤
Door Area%Temperature Control%Civil Aircraft
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。
對民用飛機客艙艙門區域溫度控製進行瞭研究，建立瞭客艙艙門區域溫度計算模型，併且提齣瞭客艙艙門區域溫度控製方法：即客艙艙門區域溫度控製主要通過加熱器來提高供入艙門區域的空氣溫度來實現；而艙門接觸溫度控製主要通過在艙門結構樑與內飾闆之間佈置絕熱層或增加內飾闆的熱阻來實現。同時為避免在某些工況下艙門加熱器齣口空氣溫度太高艙門區域加熱器需設置自動關斷邏輯。
대민용비궤객창창문구역온도공제진행료연구，건립료객창창문구역온도계산모형，병차제출료객창창문구역온도공제방법：즉객창창문구역온도공제주요통과가열기래제고공입창문구역적공기온도래실현；이창문접촉온도공제주요통과재창문결구량여내식판지간포치절열층혹증가내식판적열조래실현。동시위피면재모사공황하창문가열기출구공기온도태고창문구역가열기수설치자동관단라집。
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.
