航空工程进展2012，Vol.3Issue(1)：120-124,5.
浅析过冷大水滴规章对防冰系统设计的影响
Design Affect on Anti-icing System in Super-cooled Large Droplet Regulation
刘鹏 1史献林1
作者信息
- 1. 上海飞机设计研究院环控氧气系统设计研究部,上海200232
- 折叠
摘要
Abstract
The background of super-cooled large droplet（SLD） icing condition regulation is introduced,and the new Sec.25.1420 SLD icing conditions regulations are analyzed in this paper.Compared with 14CFR appendix C icing condition,the wing usually has the large droplet impingement region,and can easily be resulted in runback ice after the ice protection region under SLD icing condition.So it is necessary to extend the chord of upper surface of ice protection region.In the supplement of typically icing condition system,installing the flush-mounted ice detector in the runback ice area is an effective means to detect SLD icing condition.The category of SLD icing condition is also analyzed,and the translation of FAR25.1093.（b） regulation is presented.关键词
过冷大水滴结冰条件/后溜冰/防冰系统/结冰探测系统Key words
super-cooled large droplet icing condition/runback ice/anti-icing system/icing detection system引用本文复制引用
刘鹏,史献林..浅析过冷大水滴规章对防冰系统设计的影响[J].航空工程进展,2012,3(1):120-124,5.
