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2650-T8铝合金材料耐热性能的研究进展
引用本文:王国军,熊柏青,陶志民,李锡武,刘科研. 2650-T8铝合金材料耐热性能的研究进展[J]. 金属功能材料, 2009, 16(3): 73-80
作者姓名:王国军  熊柏青  陶志民  李锡武  刘科研
作者单位:北京有色金属研究总院,有色金属材料制备加工国家重点实验室,北京,100088;东北轻合金有限责任公司,黑龙江,哈尔滨,150060;北京有色金属研究总院,有色金属材料制备加工国家重点实验室,北京,100088;东北轻合金有限责任公司,黑龙江,哈尔滨,150060
摘    要:2650铝合金作为一种新型耐热变形铝合金,主要应用于超音速运输飞机蒙皮。它具有良好的耐热性能,在100~130℃温度范围,150MPa负荷下服役6000h,其变形量不超过0.1%。该材料在国内尚没有公开发表的文献作详细介绍。本文从蠕变及断裂行为、蠕变和热暴露对沉淀强化的影响、热驱动对材料滑移的作用和蠕变物理模型的建立等几个方面,介绍了对2650-T8材料的高温性能方面的研究进展。对耐热铝合金的研究提出了自己的看法和建议。

关 键 词:2650铝合金  耐热材料  蠕变行为  热暴露  热驱动  物理模型

Recent Development on Resistance to High Temperature of 2650-T8 Aluminum Alloy Material
WANG Guo-jun,XIONG Bai-qing,TAO Zhi-min,LI Xi-wu,LIU Ke-yan. Recent Development on Resistance to High Temperature of 2650-T8 Aluminum Alloy Material[J]. Metallic Functional Materials, 2009, 16(3): 73-80
Authors:WANG Guo-jun  XIONG Bai-qing  TAO Zhi-min  LI Xi-wu  LIU Ke-yan
Affiliation:1.State key Laboratory for Fabrication and Processing of Nonferrous Metals;General Research Institute for Nonferrous Metals;Beijing 100088;China;2.Northeast Light Alloy Co.Ltd.;Harbin 150060;Heilongjiang;China
Abstract:2650 aluminum alloy , as a new type of heat-resistant aluminum alloy,is used mainly for the fuselage skin of the future supersonic civil transport aircraft. It exhibits a high resistance to heat and a strong resistance to long- term creep. Exposed to temperatures ranging from 100 to 130 ℃ during the supersonic flying phase, the material does not deform by more than 0.1% under a 150 MPa load during the 60,000 h service life. In this paper, in terms of creep and fracture behavior, effect of thermal exposure or creep on precipitation hardening, recent development on heat resistant property of 2650-T8 aluminum alloy is introduced. At last, the views and suggestions on heat-resistant aluminum alloy research are put forward.
Keywords:2650 aluminum alloy  heat resistant material  creep behavior  heat exposure  thermal activation  physics-based modeling  
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