兵器材料科学与工程
兵器材料科學與工程
병기재료과학여공정
Ordnance Material Science and Engineering
2013年
6期
18-21
,共4页
侯立群%陈小辉%邢志媛%李素梅%王旭东%徐瑛
侯立群%陳小輝%邢誌媛%李素梅%王旭東%徐瑛
후립군%진소휘%형지원%리소매%왕욱동%서영
Al-Si-Cu-Mg系合金%固溶处理%时效处理%差热分析
Al-Si-Cu-Mg繫閤金%固溶處理%時效處理%差熱分析
Al-Si-Cu-Mg계합금%고용처리%시효처리%차열분석
Al-Si-Cu-Mg alloy%solution treatment%aging treatment%differential thermal analysis
为进一步提高ZL111合金的力学特性,满足更高功率发动机缸盖和机体的使用要求,在完成新型Al-Si-Cu-Mg系合金化学成分设计的基础上,采用差热分析、电阻测量、微观组织观察和力学特性测试等研究手段,对新型Al-Si-Cu-Mg系合金热处理工艺进行了深入研究。结果表明,当热处理工艺为490℃×4 h+500℃×6 h+520℃×8 h固溶处理和165℃×9 h时效处理,新型Al-Si-Cu-Mg系合金室温抗拉强度和伸长率分别为340 MPa和2.5%。
為進一步提高ZL111閤金的力學特性,滿足更高功率髮動機缸蓋和機體的使用要求,在完成新型Al-Si-Cu-Mg繫閤金化學成分設計的基礎上,採用差熱分析、電阻測量、微觀組織觀察和力學特性測試等研究手段,對新型Al-Si-Cu-Mg繫閤金熱處理工藝進行瞭深入研究。結果錶明,噹熱處理工藝為490℃×4 h+500℃×6 h+520℃×8 h固溶處理和165℃×9 h時效處理,新型Al-Si-Cu-Mg繫閤金室溫抗拉彊度和伸長率分彆為340 MPa和2.5%。
위진일보제고ZL111합금적역학특성,만족경고공솔발동궤항개화궤체적사용요구,재완성신형Al-Si-Cu-Mg계합금화학성분설계적기출상,채용차열분석、전조측량、미관조직관찰화역학특성측시등연구수단,대신형Al-Si-Cu-Mg계합금열처리공예진행료심입연구。결과표명,당열처리공예위490℃×4 h+500℃×6 h+520℃×8 h고용처리화165℃×9 h시효처리,신형Al-Si-Cu-Mg계합금실온항랍강도화신장솔분별위340 MPa화2.5%。
In order to further improve mechanical properties of ZL111 alloy and satisfy operating requirements of higher power engine cylinder heads and cylinder blocks,the heat treatment processes based on chemical composition design of a new Al-Si-Cu-Mg alloy were studied using differential thermal analysis(DTA),microstructure observation,electric resistance and mechanical property measurements. The results show that the optimized heat treatment process of the new Al-Si-Cu-Mg alloy is 490℃×4 h+500℃×6 h+520℃×8 h solution treatment and 165℃×9 h aging treatment,the ambient ultimate tensile strength and elongation of the heat-treated alloy are 340 MPa and 2.5%,respectively.