航空材料学报
航空材料學報
항공재료학보
JOURNAL OF AERONAUTICAL MATERIALS
2009年
6期
38-42
,共5页
王国军%熊柏青%张永安%聂波%丛福官
王國軍%熊柏青%張永安%聶波%叢福官
왕국군%웅백청%장영안%섭파%총복관
淬透性%大规格棒材%2D70铝合金%温度控制仪%冷却速率
淬透性%大規格棒材%2D70鋁閤金%溫度控製儀%冷卻速率
쉬투성%대규격봉재%2D70려합금%온도공제의%냉각속솔
hardenability%larger dimension bar%2D70 aluminum alloy%temperature monitoring instrument%cooling velocity
采用多路温度控制仪监测材料淬火过程不同部位的温度变化的试验方法,通过对材料硬度和力学性能指标的测试分析,描绘出大规格2D70铝合金棒材截面上距离边部不同距离的硬度和力学性能变化曲线,对比分析了该试验条件和工业化生产条件下合金的硬度和力学性能变化曲线, 探讨了本试验方法应用到工业化生产中检测材料淬透性的可能性.研究结果表明,淬火过程中2D70铝合金250mm×250mm的棒材边部和心部的温度基本均匀,淬火过程中总的冷却速率为4℃/s, 可满足合金充分固溶的要求, 工业化生产的250mm 棒材已经完全淬透.
採用多路溫度控製儀鑑測材料淬火過程不同部位的溫度變化的試驗方法,通過對材料硬度和力學性能指標的測試分析,描繪齣大規格2D70鋁閤金棒材截麵上距離邊部不同距離的硬度和力學性能變化麯線,對比分析瞭該試驗條件和工業化生產條件下閤金的硬度和力學性能變化麯線, 探討瞭本試驗方法應用到工業化生產中檢測材料淬透性的可能性.研究結果錶明,淬火過程中2D70鋁閤金250mm×250mm的棒材邊部和心部的溫度基本均勻,淬火過程中總的冷卻速率為4℃/s, 可滿足閤金充分固溶的要求, 工業化生產的250mm 棒材已經完全淬透.
채용다로온도공제의감측재료쉬화과정불동부위적온도변화적시험방법,통과대재료경도화역학성능지표적측시분석,묘회출대규격2D70려합금봉재절면상거리변부불동거리적경도화역학성능변화곡선,대비분석료해시험조건화공업화생산조건하합금적경도화역학성능변화곡선, 탐토료본시험방법응용도공업화생산중검측재료쉬투성적가능성.연구결과표명,쉬화과정중2D70려합금250mm×250mm적봉재변부화심부적온도기본균균,쉬화과정중총적냉각속솔위4℃/s, 가만족합금충분고용적요구, 공업화생산적250mm 봉재이경완전쉬투.
The variation curve of hardness and mechanical property with different distance from core of the 2D70 aluminum alloy larger dimension bar has been drawn by monitoring different site temperature changes on the same cross section during quenching process in lab ,and through testing and analyzing hardness and mechanical property of the materials. The same variation curve of the same specification material which produced by commercial process has been described. The curves of different material have been compared and analyzed. The feasibility of the experiment method applied to commercial process product has been discussed. The study shows that the temperature of core and edge on the cross section of the 2D70 aluminum alloy of 250mm×250mm during quenching process is uniform. The general cooling velocity during quenching process is 4℃/s, The sufficiency solution has been occurred. The quenched depth of the alloy is greater than 125mm.