CN104451298A - 一种改进的2024铝合金 - Google Patents

一种改进的2024铝合金 Download PDF

Info

Publication number
CN104451298A
CN104451298A CN201410661936.9A CN201410661936A CN104451298A CN 104451298 A CN104451298 A CN 104451298A CN 201410661936 A CN201410661936 A CN 201410661936A CN 104451298 A CN104451298 A CN 104451298A
Authority
CN
China
Prior art keywords
aluminum alloy
improved
aluminium
present
weight
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201410661936.9A
Other languages
English (en)
Inventor
王洪初
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wuxi Hongsheng Aluminium Industry Co Ltd
Original Assignee
Wuxi Hongsheng Aluminium Industry Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wuxi Hongsheng Aluminium Industry Co Ltd filed Critical Wuxi Hongsheng Aluminium Industry Co Ltd
Priority to CN201410661936.9A priority Critical patent/CN104451298A/zh
Publication of CN104451298A publication Critical patent/CN104451298A/zh
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/12Alloys based on aluminium with copper as the next major constituent
    • C22C21/18Alloys based on aluminium with copper as the next major constituent with zinc
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/12Alloys based on aluminium with copper as the next major constituent
    • C22C21/14Alloys based on aluminium with copper as the next major constituent with silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/12Alloys based on aluminium with copper as the next major constituent
    • C22C21/16Alloys based on aluminium with copper as the next major constituent with magnesium

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Conductive Materials (AREA)

Abstract

本发明公开一种改进的2024铝合金,按重量计,该铝合金由如下组分组成:Cu3.8-4.9%,Mg1.2-1.8%,Mn0.3-0.9%,Si0.5%,Fe0.5%,Zn0.25%,Cr0.1%,Ti0.15%,In0.01-0.03%,余量为铝和不可避免的杂质,其中,Mn与Mg的重量比为1:(0.4-0.42)。与现有2024铝合金相比,本发明改进后的铝合金具有更为良好的综合性能。

Description

一种改进的2024铝合金
技术领域
本发明涉及一种改进的2024铝合金。
背景技术
2024铝合金是硬铝中用量最大的,具有强度高和耐热的特点,可用作150℃以下的工作零件,温度高于125℃时,2024铝合金的强度比7075铝合金的还高,被广泛应用于飞机结构(蒙皮、骨架、肋梁、隔框等)、铆钉、导弹构件、卡车轮毂、螺旋桨元件及其他各种结构件。
发明内容
本发明的目的是提供一种改进的2024铝合金。
为了解决上述技术问题,本发明提供了如下的技术方案:
一种改进的2024铝合金,按重量计,由如下组分组成:
Cu 3.8-4.9%,Mg 1.2-1.8%,Mn 0.3-0.9%,Si 0.5%,Fe 0.5%,Zn 0.25%,Cr 0.1%,Ti 0.15%,In 0.01-0.03%,余量为铝和不可避免的杂质,其中,Mn与Mg的重量比为1:(0.4-0.42)。
与现有2024铝合金相比,本发明改进后的铝合金的抗拉强度和屈服强度能提高10-15%左右,延伸率能提高15-20%,综合性能得到明显的改善。
具体实施方式
以下对本发明的优选实施例进行说明,应当理解,此处所描述的优选实施例仅用于说明和解释本发明,并不用于限定本发明。
实施例1
一种改进的2024铝合金,按重量计,其各组分含量如下:
Cu 3.8-4.9%,Mg 1.26%,Mn 0.51%,Si 0.5%,Fe 0.5%,Zn 0.25%,Cr 0.1%,Ti 0.15%,In 0.015%,余量为铝和不可避免的杂质(各杂质总量不大于0.15%,单个不大于0.05%)。在750℃熔炼,浇铸成厚度为11mm的铝板。抗拉强度:530MPa,屈服强度:386MPa,延伸率15.1%。
实施例2
一种改进的2024铝合金,按重量计,其各组分含量如下:
Cu 3.8-4.9%,Mg 1.5%,Mn 0.62%,Si 0.5%,Fe 0.5%,Zn 0.25%,Cr 0.1%,Ti 0.15%,In 0.03%,余量为铝和不可避免的杂质(各杂质总量不大于0.15%,单个不大于0.05%)。在750℃熔炼,浇铸成厚度为11mm的铝板。抗拉强度:525MPa,屈服强度:381MPa,延伸率14.5%。
最后应说明的是:以上所述仅为本发明的优选实施例而已,并不用于限制本发明,尽管参照前述实施例对本发明进行了详细的说明,对于本领域的技术人员来说,其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分技术特征进行等同替换。凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。

Claims (1)

1.一种改进的2024铝合金,按重量计,由如下组分组成:
Cu 3.8-4.9%,Mg 1.2-1.8%,Mn 0.3-0.9%,Si 0.5%,Fe 0.5%,Zn 0.25%,Cr 0.1%,Ti 0.15%,In 0.01-0.03%,余量为铝和不可避免的杂质,其中,Mn与Mg的重量比为1:(0.4-0.42)。
CN201410661936.9A 2014-11-19 2014-11-19 一种改进的2024铝合金 Pending CN104451298A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410661936.9A CN104451298A (zh) 2014-11-19 2014-11-19 一种改进的2024铝合金

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410661936.9A CN104451298A (zh) 2014-11-19 2014-11-19 一种改进的2024铝合金

Publications (1)

Publication Number Publication Date
CN104451298A true CN104451298A (zh) 2015-03-25

Family

ID=52898038

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410661936.9A Pending CN104451298A (zh) 2014-11-19 2014-11-19 一种改进的2024铝合金

Country Status (1)

Country Link
CN (1) CN104451298A (zh)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1332260A (zh) * 2001-07-26 2002-01-23 华南理工大学 高强韧和低热裂倾向的铸造铝基合金材料
CN1438346A (zh) * 2002-02-10 2003-08-27 江苏万里活塞轴瓦总厂 热精锻连杆铝合金配方
EP1382698A1 (fr) * 2002-07-11 2004-01-21 Pechiney Rhenalu Produit corroyé en alliage Al-Cu-Mg pour élément de structure d'avion
CN101631884A (zh) * 2007-03-20 2010-01-20 株式会社神户制钢所 铝合金材料及铝合金硬钎焊片材

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1332260A (zh) * 2001-07-26 2002-01-23 华南理工大学 高强韧和低热裂倾向的铸造铝基合金材料
CN1438346A (zh) * 2002-02-10 2003-08-27 江苏万里活塞轴瓦总厂 热精锻连杆铝合金配方
EP1382698A1 (fr) * 2002-07-11 2004-01-21 Pechiney Rhenalu Produit corroyé en alliage Al-Cu-Mg pour élément de structure d'avion
CN101631884A (zh) * 2007-03-20 2010-01-20 株式会社神户制钢所 铝合金材料及铝合金硬钎焊片材

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
中华人民共和国国家质量监督检验检疫总局,中国国家标准化管理委员会: "《变形铝及其铝合金,GB/T3190-2008》", 31 December 2008 *

Similar Documents

Publication Publication Date Title
KR102285212B1 (ko) 마그네슘 및 아연을 갖는 열처리성 알루미늄 합금 및 이의 제조 방법
ES2613857T3 (es) Cinta de aleación de aluminio resistente a la corrosión intercristalina y procedimiento para su fabricación
WO2008156532A3 (en) Aluminium alloy products having improved property combinations and method for their production
WO2007111634A3 (en) 2000 series aluminium alloys with enhanced damage tolerance performance for aerospace applications aluminium-legierungen der 2000er-serie mit verbesserter schadenstoleranzleistung fur luftfahrtanwendungen
BRPI0606957A2 (pt) ligas com base de alumìnio al-zn-cu-mg e métodos de produção e uso
NZ607854A (en) High strength alpha/beta titanium alloy fasteners and fastener stock
CN103131904A (zh) 一种铝合金材料及其热处理工艺
CA2519139A1 (en) Method for producing an integrated monolithic aluminium structure and aluminium product machined from that structure
JP6403290B2 (ja) アルミニウム不含のマグネシウム合金
CN103924136A (zh) 一种汽车轮毂用铝合金材料
CA2907807C (fr) Toles en alliage d'aluminium-cuivre-lithium pour la fabrication de fuselages d'avion
RU2015109148A (ru) Алюминий-литиевые сплавы серии 2ххх
JP2016520714A5 (zh)
Ma et al. Effect of Sc addition on microstructure and mechanical properties of 1460 alloy
CN109136697B (zh) 一种高强度铝铜系铝合金
CN101928865A (zh) 弹用超高强度铝合金
CN104611617A (zh) 一种液态模锻Al-Cu-Zn铝合金及其制备方法
CN103572106A (zh) 铝合金材料
MX2018011818A (es) Aleaciones de aluminio con propiedades tensoras mejoradas.
CN104313418A (zh) 一种高性能耐热铝合金材料
EP2942412B1 (en) Forged aerospace products from lithium-free aluminium alloy containing copper magnesium and silver
CN103572120A (zh) 铝镁硅合金
CA2729251A1 (en) High strength casting aluminum alloy material
CN104451298A (zh) 一种改进的2024铝合金
CN108531793A (zh) 一种铝合金金属材料

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20150325

RJ01 Rejection of invention patent application after publication