中国材料进展
中國材料進展
중국재료진전
MATERIALS CHINA
2014年
8期
506-508
,共3页
侯智敏%赵永庆%张鹏省%毛小南%尹雁飞%李思兰
侯智敏%趙永慶%張鵬省%毛小南%尹雁飛%李思蘭
후지민%조영경%장붕성%모소남%윤안비%리사란
Ti12LC 合金%双重固溶%强韧化
Ti12LC 閤金%雙重固溶%彊韌化
Ti12LC 합금%쌍중고용%강인화
Ti12LC alloy%duplex solution treatment%strengthen and toughen
Ti12LC 合金是西北有色金属研究院研制的一种低成本钛合金,用于取代 TC11合金进行推广应用。本文对420mm Ti12LC 合金铸锭进行常规锻造,得到等轴组织的170mm Ti12LC 合金棒材。采用单重固溶+时效、双重固溶+时效两种不同的工艺对 Ti12LC 合金进行热处理,分析不同固溶工艺对 Ti12LC 合金显微组织及室温拉伸、室温冲击性能的影响。研究表明,在相同的固溶冷却速率下,增加单重固溶温度,初生等轴α相含量减少,合金强度增加、塑性减小、冲击韧性减小。单重固溶+时效热处理后合金冲击韧性低、强韧性匹配差。与单重低温固溶+时效相比,合金经高温预固溶慢冷+低温固溶处理后,初生α相尺寸及相含量变化不明显,但可以获得更大尺寸的次生α相,合金的塑性稍有降低、强度增加、冲击韧性改善明显,综合力学性能匹配良好。
Ti12LC 閤金是西北有色金屬研究院研製的一種低成本鈦閤金,用于取代 TC11閤金進行推廣應用。本文對420mm Ti12LC 閤金鑄錠進行常規鍛造,得到等軸組織的170mm Ti12LC 閤金棒材。採用單重固溶+時效、雙重固溶+時效兩種不同的工藝對 Ti12LC 閤金進行熱處理,分析不同固溶工藝對 Ti12LC 閤金顯微組織及室溫拉伸、室溫遲擊性能的影響。研究錶明,在相同的固溶冷卻速率下,增加單重固溶溫度,初生等軸α相含量減少,閤金彊度增加、塑性減小、遲擊韌性減小。單重固溶+時效熱處理後閤金遲擊韌性低、彊韌性匹配差。與單重低溫固溶+時效相比,閤金經高溫預固溶慢冷+低溫固溶處理後,初生α相呎吋及相含量變化不明顯,但可以穫得更大呎吋的次生α相,閤金的塑性稍有降低、彊度增加、遲擊韌性改善明顯,綜閤力學性能匹配良好。
Ti12LC 합금시서북유색금속연구원연제적일충저성본태합금,용우취대 TC11합금진행추엄응용。본문대420mm Ti12LC 합금주정진행상규단조,득도등축조직적170mm Ti12LC 합금봉재。채용단중고용+시효、쌍중고용+시효량충불동적공예대 Ti12LC 합금진행열처리,분석불동고용공예대 Ti12LC 합금현미조직급실온랍신、실온충격성능적영향。연구표명,재상동적고용냉각속솔하,증가단중고용온도,초생등축α상함량감소,합금강도증가、소성감소、충격인성감소。단중고용+시효열처리후합금충격인성저、강인성필배차。여단중저온고용+시효상비,합금경고온예고용만랭+저온고용처리후,초생α상척촌급상함량변화불명현,단가이획득경대척촌적차생α상,합금적소성초유강저、강도증가、충격인성개선명현,종합역학성능필배량호。
The low cost Ti12LC titanium alloy was developed by Northwest Institute for Non-ferrous Metal Research to re-place TC1 1 titanium alloy.The Ti12LC cast ingot of 420 mm was forged by conventional process,and worked in170mm equiaxed bars finally.The equiaxed Ti12LC alloys were single and duplex solution treated separately,and then aged at 540 ℃ for 6 h.The effects of different solution processes on the morphology and mechanical properties,especially the impact toughness were analyzed.The results show that the content of primary equiaxed αphase,the plasticity and the impact toughness decrease,but the strength of the alloy increases,when the solution temperature of α+βphase field sin-gle solution +aging heat treatments increases,for which the solution cooling rate is constant.The single solution +aging heat treated alloys have low impact toughness,which means that the impact toughness and strength are mismatched.Com-pared with single solution at low temperature,pre-solution at the upper α+βphase field followed by furnace cooling,and then re-solution at low temperature can result in larger dimension secondary αphase,higher strength and impact tough-ness,while the plasticity decreases in acceptable range,the content and dimension of primary αphase change little.The combined mechanical properties of the Ti12LC alloys heat treated by duplex solution +ageing match well.