期刊文献+

直升机结冰强度设计标准研究 被引量:3

Research of Icing Severity Standards for Helicopter
下载PDF
导出
摘要 介绍了影响直升机结冰特性的主要因素。针对国内直升机防/除冰系统设计标准中关于结冰强度划分没有明确界定的问题,通过引用适航规章要求并借鉴国外直升机结冰条件的设计标准,对直升机的结冰强度设计标准进行了分析和阐述,并提出了国内标准划分的建议以及在民用直升机防/除冰系统设计中的应用问题。 This article introduced the main conditions of helicopter icing characteristic.For the problem that no clear limit of the icing severity in the design standards of internal helicopter icing protection system,the article gave the analytical result and dissertation according to the requirements of airworthiness standard and icing design conditions of overseas helicopters.The article also gave the proposal of the standards of icing condition,and its application on the design of civil helicopter rotor icing protection.
出处 《直升机技术》 2011年第2期30-33,共4页 Helicopter Technique
关键词 直升机 结冰条件 结冰强度 防/除冰系统 设计标准 helicopter icing condition icing severity icing protection system standard
  • 相关文献

参考文献5

  • 1Design and Airworthness Require-ments for Service Aircraft,Volume 2-Rotorcraft. DEF-STAN00-970 .
  • 2Robert J Flemming,Philip J.Alldridge.Sikorsky S-92A and S-76D Rotor Ice Protection System[].SAE Aircraft and Engine Icing International Conference.2007
  • 3Leschi R.Certification/Qualification of an Aircraft forFlight in Known Icing Conditions[].SAE Air-craft and Engine Icing International Conference.2007
  • 4Ramage A I.Artifical Icing Flight Trials on The EH101[].th European Rotorcraft Forum.
  • 5Flemming R J,Hanks K W,Hanks M Lynn.US ArmyUH-60M Helicopter Main Rotor Ice Protection System[].SEA Aircraft&Engine icing International Confer-ence Seville.2007

同被引文献27

引证文献3

二级引证文献2

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