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材料工程  2016, Vol. 44 Issue (8): 1-10    DOI: 10.11868/j.issn.1001-4381.2016.08.001
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航空发动机用先进高温钛合金材料技术研究与发展
蔡建明, 弭光宝, 高帆, 黄浩, 曹京霞, 黄旭, 曹春晓
北京航空材料研究院 先进钛合金航空科技重点实验室, 北京 100095
Research and Development of Some Advanced High Temperature Titanium Alloys for Aero-engine
CAI Jian-ming, MI Guang-bao, GAO Fan, HUANG Hao, CAO Jing-xia, HUANG Xu, CAO Chun-xiao
Aviation Key Laboratory of Science and Technology on Advanced Titanium Alloys, Beijing Institute of Aeronautical Materials, Beijing 100095, China
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摘要 新一代高推重比航空发动机压气机和涡轮系统高温环境使用的叶片、盘、机匣、整体叶盘和整体叶环等构件设计通常选用先进高温钛合金材料。本文综述近年来我国600℃高温钛合金、阻燃钛合金、TiAl合金、连续SiC纤维增强钛基复合材料及其应用技术取得的最新研究进展,并提出材料及构件设计、加工和使用亟待突破的关键技术,包括工业铸锭成分高纯化和均匀化控制技术、大规格棒材及特殊锻件制备技术、整体叶盘和整体叶环零件机械加工技术、材料性能评价及应用设计技术等。先进高温钛合金材料的不断应用将有力推动我国航空发动机技术发展。
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蔡建明
弭光宝
高帆
黄浩
曹京霞
黄旭
曹春晓
关键词 先进航空发动机600℃高温钛合金阻燃钛合金TiAl合金SiC纤维增强钛基复合材料钛火    
Abstract:Some advanced high temperature titanium alloys are usually selected to be manufactured into blade, disc, case, blisk and bling under high temperature environment in compressor and turbine system of a new generation high thrust-mass ratio aero-engine. The latest research progress of 600℃ high temperature titanium alloy, fireproof titanium alloy, TiAl alloy, continuous SiC fiber reinforced titanium matrix composite and their application technology in recent years in China were reviewed in this paper. The key technologies need to be broken through in design, processing and application of new material and component are put forward, including industrial ingot composition of high purified and homogeneous control technology, preparation technology of the large size bar and special forgings, machining technology of blisk and bling parts, material property evaluation and application design technique. The future with the continuous application of advanced high temperature titanium alloys, will be a strong impetus to the development of China's aero-engine technology.
Key wordsadvanced aero-engine    600℃ high temperature titanium alloy    fireproof titanium alloy    TiAl alloy    SiC fiber reinforced titanium matrix composite    titanium fire
收稿日期: 2016-04-15      出版日期: 2016-08-23
中图分类号:  TG146.2  
通讯作者: 弭光宝(1981-),男,高级工程师,博士,主要从事高温钛合金及阻燃性能等方面研究,联系地址:北京市海淀区温泉镇环山村8号北京航空材料研究院先进钛合金航空科技重点实验室(100095),miguangbao@163.com     E-mail: miguangbao@163.com
引用本文:   
蔡建明, 弭光宝, 高帆, 黄浩, 曹京霞, 黄旭, 曹春晓. 航空发动机用先进高温钛合金材料技术研究与发展[J]. 材料工程, 2016, 44(8): 1-10.
CAI Jian-ming, MI Guang-bao, GAO Fan, HUANG Hao, CAO Jing-xia, HUANG Xu, CAO Chun-xiao. Research and Development of Some Advanced High Temperature Titanium Alloys for Aero-engine. Journal of Materials Engineering, 2016, 44(8): 1-10.
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http://jme.biam.ac.cn/CN/10.11868/j.issn.1001-4381.2016.08.001      或      http://jme.biam.ac.cn/CN/Y2016/V44/I8/1
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