航空发动机高温钛合金非等温氧化行为研究进展  

Research Progress of Non-Isothermal Oxidation Behavior of High Temperature Titanium Alloys for Aero-Engine

作　　者：弭光宝 欧阳佩旋 陈航 李培杰[3] 黄旭 曹春晓 MI Guangbao;OUYANG Peixuan;CHEN Hang;LI Peijie;HUANG Xu;CAO Chunxiao(Titanium Alloy Research Institute,AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China;Key Laboratory on Advanced Titanium Alloys of AECC,Beijing 100095,China;Department of Mechanical Engineering,Tsinghua University,Beijing 100084,China)

机构地区：[1]中国航发北京航空材料研究院钛合金研究所,北京100095 [2]中国航发先进钛合金重点实验室,北京100095 [3]清华大学机械工程系,北京100084

出　　处：《航空制造技术》2019年第15期88-92,共5页Aeronautical Manufacturing Technology

基　　金：国家自然科学基金(51471155);中国航发自主创新专项(CXPT–2018–36);国家科技重大专项(2017VII0012109)

摘　　要：阻燃性能是衡量航空发动机钛火安全的关键性能指标,通常采用钛合金材料/构件抵抗热自燃、点燃和扩展燃烧的能力进行综合评价。针对高性能航空发动机对先进高温钛合金的需求,在回顾近期抗点燃性能和抗燃烧性能试验技术研究基础上,重点从抗热自燃性能的层面介绍阻燃钛合金、高温钛合金及钛铝金属间化合物的非等温氧化行为及阻燃机理的研究进展,并对未来发展方向进行展望。Fireproof property is a key performance index to measure the safety of aero-engine titanium fire,which is generally evaluated by the abilities of titanium alloy materials/components to resist thermal spontaneous combustion,ignition and extended combustion.Aiming at the demand of advanced high-temperature titanium alloys for highperformance aero-engines,this paper reviews recent experimental studies on ignition resistance and combustion resistance and introduces the research progress of non-isothermal oxidation behavior and fireproof mechanism of fireproof titanium alloys,high temperature titanium alloys and intermetallic titanium aluminides from the aspect of thermal spontaneous combustion resistance.Finally,the future direction of development is prospected.

关 键 词：高温钛合金 阻燃钛合金 钛铝金属间化合物 非等温氧化 阻燃机理 

分 类 号：TG1[金属学及工艺—金属学]