期刊文献+

飞机地面积/除冰环境模拟与试验研究 被引量:5

Environmental Simulation and Experimental Study of Aircraft Icing and Deicing on Ground
下载PDF
导出
摘要 飞机地面积冰是飞机进入冬季安全飞行的重要隐患,很多飞行事故都是因为没有清除飞机表面的积冰而造成的。基于对飞机地面积/除冰的真实环境的分析,在低温湿热试验箱中模拟积/除冰时的大气条件,对机翼积/除冰进行试验研究。通过改变环境温度、除冰液温度、流量、浓度等影响因素,利用光纤式结冰传感器得到不同环境条件下,除冰液参数对除冰过程的影响数据,并对这些数据进行了分析。试验结果表明该装置能有效地模拟飞机地面积/除冰过程,数据分析显示飞机地面结冰过程主要受外界环境温度,湿度(空气的水含量)的影响;对飞机地面除冰来说,除冰液温度参数是除冰效果达到最佳的关键因素。 Aircraft icing on ground is a major danger for flight safety in winter,and numerous flight accidents could attribute to not having cleared the ice on the aircraft body before takeoff.An atmosphere icing weather condition was simulated in a low temperature cabin to imitate aircraft deicing on ground based on the study of aircraft ice mechanism on ground.Then several conditions,such as deicing fluids temperature,flow rate and scale,were changed to study the influencing factors on the aircraft deicing process using fiber-optic icing sensors.Experimental results show that the aircraft deicing simulation environment could effectively simulate the deicing/icing process.Moreover,analysis results reveal that the environment temperature,humidity are the main parameters for the aircraft icing process and the deicing fluids temperature is the key factor to obtain ideal deicing effect.
出处 《中国安全科学学报》 CAS CSCD 北大核心 2011年第11期97-102,共6页 China Safety Science Journal
基金 国家自然科学基金资助(60939001 60879020) 民航局重大科技项目(60932016)
关键词 结冰/除冰 除冰液参数 环境模拟 光纤式结冰传感器 飞机 ground icing and de-icing parameters of deicing fluid environmental simulation fiber-optic icing sensor aircraft
  • 相关文献

参考文献12

  • 1James T. Riley, Warren Underwood Edward, Pugacz. The FAA ground icing research program[A]. 45th AIAA Aerospace Sciences Meeting and Exhibit[C]. Reno, Nevada,2007:8-11.
  • 2M. Gaudreau. Guidelines for aircraft ground icing operations[ R]. Canada :Civil Aviation Communications Centre,2005.
  • 3李红琳.严格飞机除冰/防冰液适航审定[J].中国民用航空,2006(2):29-31. 被引量:11
  • 4Guilherme Araajo Lima da Silva, Otatvio de Mattos Silvares, Euryale Jorge Godoy de Jesus Zerbini. Numerical simulation of airfoil thermal anti-Ice operation part 1: mathematical modeling[J]. Journal of Aircraft ,2007, 44(2):627-634.
  • 5常士楠,艾素霄,陈余,袁修干.一种飞机机翼表面结冰过程仿真方法[J].系统仿真学报,2008,20(10):2538-2541. 被引量:13
  • 6周莉,徐浩军,龚胜科,李大伟.飞机结冰特性及防除冰技术研究[J].中国安全科学学报,2010,20(6):105-110. 被引量:65
  • 7刘根林,沈海军.飞机防冰与除冰技术综述[J].江苏航空,2003(4):18-20. 被引量:16
  • 8Charles Ryerson , Mary Wyderski , Donald Tarazano, et al. Objective evaluation of fluid, blower, and infrared ground deicing technologies[A]. 41st Aerospace Sciences Meeting and Exhibit[C] . Reno, Nevada, 2003:6-9.
  • 9Peter Dawson ,Medhat Hanna. Hot Water Deicing of Aircraft: Phase 2[R]. Canada:Transportation Development Centre on Behalf of Civil Aviation Safety and Security, 2000.
  • 10裘燮纲 韩凤华.飞机防冰系统[M].北京:航空专业教材编审组,1985..

二级参考文献35

共引文献160

同被引文献56

引证文献5

二级引证文献13

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部