热力机械复合式除冰技术浅析
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- 英文论文题名：Discuss on Thermo-Mechanical Expulsion De-icing Technology
- 论文作者：马庆林
- 英文论文作者：Ma Qinglin ; The First Aircraft Institute of AVIC
- 年：2016
- 作者机构：中航工业第一飞机设计研究院;
- 论文关键词：飞机结冰 ; 结冰防护 ; 热力机械复合式除冰
- 英文论文关键词：aircraft Icing ; ice protection ; thermo-mechanical expulsion de-icing
- 会议召开时间：2016-10-31
- 会议录名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛文集（下册）
- 英文会议录名称：Discovery,Innovation and Communication——Proceedings of 7th CSAA Science and Technology Youth Forum
- 语种：中文
- 分类号：V244.15
- 学会代码：ZGHU
- 会议名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛
- 会议地点：中国广东中山
- 主办单位：中国航空学会
- 学会名称：中国航空学会
- 页数：4
- 文件大小：1354k
- 原文格式：O
- 会议级别：全国
摘要
飞机结冰严重危及飞行安全,结冰防护系统是保证结冰气象条件下安全飞行的重要保障之一。本文探讨的力机械复合式除冰技术由脉冲式电加热除冰和电磁排斥式除冰组成,其典型特点是能量消耗低,除冰效率高,可以盖更大的防护区域,满足严酷结冰条件下安全飞行的需求。最后介绍了一种热力机械复合式除冰系统的技术方案,与传统的电加热除冰技术比较说明其优越性。
In-flight icing has seriously hazardous effects on aircraft safety.Ice protection system is employed to ensure aircraft flight safety during icing conditions.A hybrid ice protection technology discussed here is developed to meet the requirements of high performance efficiency and low power consumption,named Thermo-Mechanical Expulsion De-icing System(TMEDS).TMEDS combines pulse electro-thermal de-icing technology and electro-magnetic expulsion de-icing technology together.TMEDS can extend the protected surfaces to a larger area and ensure flight safety in more serious icing condition.A solution of TMEDS Architecture is introduced.Comparison with traditional electro-thermal de-icing technology shows that TMEDS has obvious advantage on high performance efficiency and low power consumption.
In-flight icing has seriously hazardous effects on aircraft safety.Ice protection system is employed to ensure aircraft flight safety during icing conditions.A hybrid ice protection technology discussed here is developed to meet the requirements of high performance efficiency and low power consumption,named Thermo-Mechanical Expulsion De-icing System(TMEDS).TMEDS combines pulse electro-thermal de-icing technology and electro-magnetic expulsion de-icing technology together.TMEDS can extend the protected surfaces to a larger area and ensure flight safety in more serious icing condition.A solution of TMEDS Architecture is introduced.Comparison with traditional electro-thermal de-icing technology shows that TMEDS has obvious advantage on high performance efficiency and low power consumption.
引文
[1]Transportation Safety Board.Aircraft Accident Report:Inflight Icing Encounter and Loss of Control Simmons Airlines,American Eagle Flight 4184,1996.
[2]Petrenko V F,Higa M,Starostin M,et al.Pulse Electrothermal De-icing[C]//Proceedings of the Thirteenth(2003)International Offshore and Polar Engineering Conference.2003:435-438.
[3]Joseph J Gerardi,Richard B Ingram.Electro-Magnetic Expulsion De-icing System.United States Patent,2000.
[4]Cox&Company,Inc.Low Power Ice Protection Systems.2010.
[5]Kamel Al-Khalil.Thermo-Mechanical Expulsion Deicing System-TMEDS.AIAA,2007-0692,2007.
[6]Qinglin Ma.Aircraft Icing and Thermo-Mechanical Expulsion De-icing Technology.Cranfield University,Msc.Thesis,2010.
[2]Petrenko V F,Higa M,Starostin M,et al.Pulse Electrothermal De-icing[C]//Proceedings of the Thirteenth(2003)International Offshore and Polar Engineering Conference.2003:435-438.
[3]Joseph J Gerardi,Richard B Ingram.Electro-Magnetic Expulsion De-icing System.United States Patent,2000.
[4]Cox&Company,Inc.Low Power Ice Protection Systems.2010.
[5]Kamel Al-Khalil.Thermo-Mechanical Expulsion Deicing System-TMEDS.AIAA,2007-0692,2007.
[6]Qinglin Ma.Aircraft Icing and Thermo-Mechanical Expulsion De-icing Technology.Cranfield University,Msc.Thesis,2010.