常用铝合金成分对照
5052.5083.5754铝合金成分及质量分数
5052、5083、5754铝合金是常用的铝合金材料，具有良好的耐腐蚀性和可焊性，广泛用于船舶制造、航空航天、汽车零部件等领域。
在实际应用中，了解铝合金的成分及质量分数对于材料的选择和加工具有重要意义。
本文将针对5052、5083、5754铝合金的成分及质量分数进行详细介绍。
一、5052铝合金的成分及质量分数5052铝合金是一种具有优良加工性能和耐腐蚀性的铝镁合金，其主要成分和质量分数如下：1. 铝（Al）：余量2. 镁（Mg）：2.2~2.83. 锰（Mn）：0.15~0.354. 铜（Cu）：≤0.15. 锌（Zn）：≤0.16. 铬（Cr）：0.15~0.357. 钛（Ti）：≤0.18. 硅（Si）：≤0.259. 铁（Fe）：≤0.410. 其他单一杂质总量：≤0.0511. 其他总量：≤0.15从上述成分及质量分数可以看出，5052铝合金中镁的含量较高，使其具有较好的抗腐蚀性能和焊接性能，适用于湿气环境下的应用。
二、5083铝合金的成分及质量分数5083铝合金是一种具有良好耐腐蚀性和强度的铝镁合金，其主要成分和质量分数如下：1. 铝（Al）：余量2. 镁（Mg）：4.0~4.93. 锰（Mn）：0.4~1.04. 铁（Fe）：≤0.45. 硅（Si）：≤0.46. 铜（Cu）：≤0.17. 锌（Zn）：≤0.258. 钛（Ti）：≤0.159. 铬（Cr）：0.05~0.2510. 其他单一杂质总量：≤0.0511. 其他总量：≤0.155083铝合金中镁的含量较高，使其具有良好的耐腐蚀性能和焊接性能，适用于船舶制造和海洋工程等领域。
三、5754铝合金的成分及质量分数5754铝合金是一种具有优良强度和耐腐蚀性的铝镁合金，其主要成分和质量分数如下：1. 铝（Al）：余量2. 镁（Mg）：2.6~3.63. 锰（Mn）：0.54. 铁（Fe）：≤0.45. 硅（Si）：≤0.46. 铜（Cu）：≤0.17. 锌（Zn）：≤0.258. 钛（Ti）：≤0.29. 钒（V）：≤0.110. 其他单一杂质总量：≤0.0511. 其他总量：≤0.155754铝合金具有中等强度和良好的耐腐蚀性能，适用于用于罐体、车身板和船舶构造等领域。
各种牌号铝合金成分及性能
各种牌号铝合金成分及性能铝合金，这个听起来有点生涩的名词，其实在我们的生活中无处不在。
想想你手里的手机壳，或是你骑的那辆轻巧的自行车，里面或多或少都含有铝合金的成分。
它的牌号成分各有千秋，今天我们就来聊聊这些铝合金的成分和性能。
一、铝合金的基本分类铝合金一般分为铸造铝合金和锻造铝合金。
前者是通过铸造工艺制成，后者则是通过锻压来成型。
简单说，铸造铝合金通常用于大型的部件，比如汽车发动机外壳。
而锻造铝合金则常见于航空航天、运动器材等领域。
1.1 铸造铝合金的成分铸造铝合金常用的牌号有A356、A380等。
A356的主要成分是铝和硅，硅的含量能达到7%左右，这让它在铸造时流动性更好。
想象一下，铸造工艺就像是在做蛋糕，好的配方能让蛋糕更加松软。
A380则更注重强度，含有铜、镁等元素，适合做一些高强度的零部件。
1.2 锻造铝合金的成分锻造铝合金则以2024、7075为代表。
2024铝合金中，铜的含量高达4.9%。
这使得它具有超强的抗拉强度。
7075铝合金则是“天之骄子”，镁和锌的组合让它在航空领域大放异彩。
你想象一下，7075铝合金的强度甚至超过一些钢材，真是让人惊叹。
二、铝合金的性能铝合金的性能多种多样，但最重要的无非就是轻、强、耐腐蚀。
这几条都紧密联系着我们的生活。
2.1 轻便性铝合金的密度很低，大约是钢的三分之一。
这使得各种产品在保证强度的同时，又能做到轻便灵活。
比如你在登山时背的铝合金水壶，不仅不重，还能经受风吹雨打，真是一举两得。
2.2 强度不同牌号的铝合金，强度差异大。
像7075那种高强度的铝合金，广泛应用于飞机和赛车，承受着巨大压力和冲击。
而像3003铝合金，虽然强度较低，但却极其耐用，适合做一些家用器具。
2.3 耐腐蚀性铝合金表面可以形成一层致密的氧化膜，防止氧化。
想想你用的铝制厨房用品，不怕油烟，不怕水，清洗起来轻松简单。
这种特性让铝合金在海洋环境中也能发挥作用，很多船只的结构就采用了铝合金。
铝合金成分对照表
International Alloy DesignationsandChemical Composition LimitsforWrought Aluminum andWrought Aluminum Alloys1525 Wilson Boulevard, Arlington, VA 22209With Support for On-line Access From:A luminum E xtruders C ouncilA luminium F ederation of S outh A fricaA ustralian A luminium C ouncil L td.E uropean A luminium A ssociationJ apan A luminium A ssociationA lro S.A, R omaniaRevised: February 2009Supersedes: April 2006© Copyright 2009, The Aluminum Association, Inc.Unauthorized reproduction and sale by photocopy or any other method is illegal.Use of the InformationThe Aluminum Association has used its best efforts in compiling the information contained in this publication. Although the Association believes that its compilation procedures are reliable, it does not warrant, either expressly or impliedly, the accuracy or completeness of this information. The Aluminum Association assumes no responsibility or liability for the use of the information herein.All Aluminum Association published standards, data, specifications and other material are reviewed at least every five years and revised, reaffirmed or withdrawn. Users are advised to contact The Aluminum Association to ascertain whether the information in this publication has been superseded in the interim between publication and proposed use.CONTENTSPage FOREWORD (i)SIGNATORIES TO THE DECLARATION OF ACCORD ..................................... ii-iii REGISTERED DESIGNATIONS AND CHEMICAL COMPOSITION LIMITS .... 1-13 Footnotes .. (14)TABLE OF NOMINAL DENSITIES FOR ACTIVE ALLOYS ............................. 15-20 TABLE OF INACTIVE ALLOY DESIGNATIONS ............................................. 21-22 Table of Chemical Composition Limits for Inactive Original Alloys (23)CROSS REFERENCES OF INTERNATIONAL DESIGNATIONS— DECLARATION OF ACCORD (DOA) TO ISO (24)RECOMMENDATION TO THE DECLARATION OF ACCORD (25)Footnotes (26)Appendix A—Use of Designations (27)Appendix B—Deactivation of Registered Alloys (27)Appendix C—General Guidelines for Determining Compliancewith "Sale of Alloy" and "Commercial Quantity" forPurposes of Registering Wrought Aluminum andWrought Aluminum Alloys (27)DECLARATION OF ACCORD (28)FOREWORDL isted herein are designations and chemical composition limits for wrought aluminum and wrought aluminum alloys registered with The Aluminum Association. Numerical designations are assigned in accordance with the Recommendation—International Designation System for Wrought Aluminum and Wrought Aluminum Alloys, which is printed on pages 25 through 27. Additions may be made in accordance with the rules outlined in the Declaration of Accord printed on page 28, and alloys will be deleted when no longer in commercial use (see table of inactive alloys printed on pages 21-22).S ince the International Designation System for Wrought Aluminum and Wrought Aluminum Alloys is based on USA's national standard "American National Standard Alloy and Temper Designation System for Aluminum ANSI H35.1," the system limits introduction of experimental alloy compositions to USA registrations. An experimental alloy registered by USA under this system is indicated by the prefix "X" and is subject to the following rules:1. A composition shall not be designated as experimental ("X") for more than five years.2. During its experimental status, the registering organization may request changes in thecomposition limit of the alloy, provided that it does not invalidate any assigned designation.3. The "X" is dropped when the alloy is no longer experimental.4. An experimental composition that is inactivated shall retain the prefix "X" for the duration ofits inactive status. If reactivated, the "X" shall be removed.S ome of the registered alloys may be the subject of patent or patent applications, and their listing herein is not to be construed in any way as the granting of a license under such patent right.A list of the organizations that are signatories to the Declaration of Accord on the Recommendation is printed on pages ii-iii.SIGNATORIES TO THE DECLARATION OF ACCORDThe following organizations are signatories to the Declaration of Accord on an International Alloy Designation System for Wrought Aluminum and Wrought Aluminum Alloys which is printed on page 28 of this publication.The Aluminum Association Inc. USA 1525 Wilson BoulevardSuite 600Arlington, VA 22209USAAFA Association Francaise de l’Aluminium FRANCE 17, rue Hamelin75016 ParisFRANCEAll-Russian Institute of Aviation Materials (VIAM) RUSSIA 17 Radio Ulitza105005 MoscowRUSSIAwww.viam.ruAlro S.A. ROMANIA 116 Pitesti Street230048 SlatinaROMANIAwww.alro.roAluminium Association of Canada CANADA 1010 Sherbrooke Street West, Suite 1600Montreal, Quebec H3A2R7CANADAwww.aac.aluminium.qc.caAluminium Center Belgium BELGIUM Z.I. Research Park 3101731 ZellikBELGIUMwww.aluminiumcenter.beAluminium Federation Limited UK National Metalforming Centre47 Birmingham RoadWest Bromwich B70 6PYUNITED KINGDOMAluminium Federation of South Africa SOUTH AFRICA P. O. Box 423Isando, 1600REPUBLIC OF SOUTH AFRICA.zaAluminium – Verband Schweiz SWITZERLAND Hallenstrasse 15PostfachCH-8024 ZurichSWITZERLANDwww.alu.chAssociacão Brasileira do Aluminio—ABAL BRAZIL Rua Humberto 1, No. 220-4o.AndarSao Pãulo-SPCEP 04018-030BRAZIL.brAssociation for the Dutch NETHERLANDS Metallurgic Industry (VNMI)P.O. Box 190NL-2700 AD ZoetermeerNETHERLANDSwww.vnmi.nlAssomet - Associazione Nazionale ITALY Industrie Metalli non FerrosiVia dei Missaglia, 97I-20142 MilanoITALYwww.assomet.itAustralian Aluminium Council Limited AUSTRALIA Level 1, Dickson SquareP. O. Box 63Dickson, ACT 2602AUSTRALIA.auAustrian Non-Ferrous Metals Federation AUSTRIA Wiedner Hauptstrasse 63/3317Postfach 338A-1045 ViennaAUSTRIAwww.nemetall.atCentro Nacional de Investigaciones SPAIN Metalurgicas (CENIM)Avenida Gregorio del Amo, 8Ciudad Universitaria28040 MadridSPAINwww.cenim.csic.esChina Nonferrous Metals Techno-Economic CHINA Research InstituteNo. 9 Xizhang Hutong, Xizhimennei StreetBejing, 100035PEOPLES REPUBLIC OF CHINAEuropean Aluminium Association EAA Avenue de Broqueville, 12B-1150 BrusselsBELGIUMiiEuropean Organization for ASD-STAN Aerospace Standardization270, Avenue de Tervuren1150, BrusselsBELGIUMGesamtverband der Aluminium- GERMANY industrie e.V. (GDA)Am Bonneshof 5D-40474 DusseldorfGERMANYwww.aluinfo.deInstitute of Non-Ferrous Metals POLAND Light Metals Divison32-050 SkawinaUl. Pilsudskiego 19POLANDwww.imn.gliwice.plInstituto Mexicano del Alumino, A.C. MEXICO Francisco PetrarcaNo. 133 Piso 9MEXICO, 11560, DF.mx IRAM-Instituto Argentino De ARGENTINA NormalizacionPeru 556C1068AABBuenos AiresARGENTINA.arJapan Aluminium Association JAPAN Tsukamoto-Sozan Building2-15, Ginza 4-ChomeChuo-ku, Tokyo 104-0061JAPANwww.aluminum.or.jpSwedish Aluminium Association SWEDEN Aluminiumriket SverigeFramtidsvagen 21ASE-351 96 VaxjoSWEDENSignatories (Continued)iiiCALCULATED NOMINAL DENSITIES FOR ACTIVEWROUGHT ALUMINUM AND WROUGHT ALUMINUM ALLOYSDensity is dependent upon composition and nominal density is determined by computation rather than by a weight method. The values shown below have been computed in accordance with the Aluminum and Aluminum Alloy Density Calculation Procedure appearing on pages 2-12 and 2-13 of Aluminum Standards and Data. These calculated densities are nominal values and should not be specified as engineering requirements but may be used in calculating nominal values for weight per unit length, weight per unit area, covering area, etc.Limiting the expression of nominal density to the number of decimal places indicated is based on the fact that composition variations are discernible from one cast to another for most alloys. The expression of nominal density to more decimal places than allowed by the following implies higher precision than is justified and should not be used.1. Alloys listed below which have a minimum aluminum content of 99.35% or greater have nominal densityvalues which are rounded in the US customary system (lbs/in3) to the nearest multiple of 0.0005 and in the metric system [(kg/m3) x 103] to the nearest multiple of 0.005.2. Alloys listed below which have a minimum aluminum content of less than 99.35% have nominal densityvalues which are rounded in the US customary system (lbs/in3) to the nearest multiple of 0.001 and in the metric system [(kg/m3) x 103] to the nearest multiple of 0.01.The US customary (lbs/in3) unit values are derived from metric values and subsequently rounded and are not to be back-converted to metric values.Density Designation lbs/in.3(kg/m3) x 103 1050 0.0975 2.7051050A 0.0975 2.7051060 0.0975 2.7051065 0.0975 2.7001070 0.0975 2.7001070A 0.0975 2.7001080 0.0975 2.7001080A 0.0975 2.7001085 0.0975 2.7001090 0.0975 2.7001098 0.0975 2.7001100 0.098 2.711100A 0.098 2.711200 0.098 2.701200A 0.098 2.711300 0.098 2.711110 0.098 2.701120 0.098 2.711230 0.098 2.701230A 0.098 2.701235 0.0975 2.7051435 0.0980 2.7101145 0.0975 2.7001345 0.0975 2.7051445 0.0975 2.7001150 0.0975 2.7051350 0.0975 2.7051350A 0.0975 2.7001450 0.0975 2.7051370 0.0975 2.7001275 0.0975 2.7051185 0.0975 2.700Density Designation lbs/in.3(kg/m3) x 103 1285 0.0975 2.7001385 0.0975 2.7001188 0.0975 2.7001190 0.0975 2.7001290 0.0975 2.7001193 0.0975 2.7001198 0.0975 2.7001199 0.0975 2.7002001 0.102 2.822002 0.099 2.732004 0.102 2.822005 0.102 2.832006 0.099 2.742007 0.102 2.822007A 0.102 2.81+2007B 0.102 2.81 2008 0.098 2.722009 0.099 2.752010 0.098 2.722011 0.102 2.832011A 0.102 2.822111 0.102 2.832111A 0.102 2.832111B 0.102 2.832012 0.102 2.822013 0.099 2.732014 0.101 2.802014A 0.101 2.802214 0.101 2.802015 0.102 2.832016 0.101 2.792017 0.101 2.79Density Designation lbs/in.3(kg/m3) x 103 2017A 0.101 2.792117 0.099 2.752018 0.102 2.822218 0.101 2.812618 0.100 2.762618A 0.100 2.772219 0.103 2.842319 0.103 2.842419 0.102 2.842519 0.102 2.822021 0.103 2.842022 0.101 2.802023 0.100 2.772024 0.100 2.782024A 0.100 2.772124 0.100 2.782224 0.100 2.772224A 0.100 2.782324 0.100 2.772424 0.100 2.772524 0.100 2.782025 0.101 2.812026 0.100 2.772027 0.101 2.792028 0.102 2.83+2028A 0.101 2.80+2028B 0.102 2.81+2028C 0.102 2.82 2030 0.102 2.812031 0.100 2.772032 0.100 2.762034 0.101 2.792036 0.100 2.752037 0.099 2.742038 0.099 2.732039 0.101 2.812139 0.102 2.812040 0.102 2.81+2041 0.103 2.84+2044 0.102 2.81+2045 0.102 2.82 2050 0.098 2.702056 0.100 2.782090 0.093 2.592091 0.093 2.582094 0.098 2.722095 0.098 2.702195 0.098 2.712196 0.095 2.632097 0.096 2.652197 0.095 2.642297 0.096 2.65Density Designation lbs/in.3(kg/m3) x 103 2397 0.096 2.652098 0.097 2.702198 0.097 2.692099 0.095 2.632199 0.095 2.643002 0.098 2.703102 0.098 2.713003 0.099 2.733103 0.099 2.733103A 0.098 2.723103B 0.098 2.733203 0.098 2.733403 0.099 2.733004 0.098 2.723004A 0.098 2.713104 0.098 2.723204 0.098 2.713304 0.098 2.723005 0.098 2.733005A 0.099 2.733105 0.098 2.723105A 0.098 2.713105B 0.098 2.723007 0.098 2.723107 0.098 2.723207 0.098 2.713207A 0.098 2.723307 0.098 2.723009 0.099 2.733010 0.098 2.723110 0.098 2.723011 0.099 2.733012 0.098 2.72+3012A 0.098 2.72 3013 0.099 2.743014 0.099 2.753015 0.098 2.723016 0.098 2.723017 0.099 2.733019 0.099 2.733020 0.099 2.733025 0.098 2.723026 0.098 2.723030 0.098 2.723130 0.098 2.714004 0.096 2.654104 0.096 2.654006 0.098 2.714007 0.099 2.744008 0.096 2.674009 0.097 2.704010 0.096 2.67Density Designation lbs/in.3(kg/m3) x 103 4013 0.098 2.714014 0.097 2.704015 0.098 2.71+4015A 0.098 2.71+4115 0.098 2.72 4016 0.099 2.734017 0.098 2.724018 0.096 2.674019 0.099 2.744020 0.098 2.714026 0.099 2.734032 0.097 2.684043 0.097 2.694043A 0.097 2.694343 0.097 2.684643 0.097 2.694044 0.097 2.674045 0.096 2.674145 0.099 2.744145A 0.099 2.744046 0.096 2.664047 0.096 2.664047A 0.096 2.664147 0.096 2.665005 0.098 2.705005A 0.097 2.695205 0.097 2.705305 0.097 2.695505 0.097 2.695605 0.097 2.695006 0.098 2.715106 0.098 2.715010 0.098 2.715110 0.097 2.695110A 0.098 2.705210 0.097 2.695310 0.097 2.695016 0.097 2.705017 0.097 2.695018 0.096 2.675018A 0.097 2.675019 0.096 2.655019A 0.096 2.655119 0.096 2.655119A 0.096 2.655021 0.097 2.685022 0.096 2.665023 0.095 2.64+ 5024 0.096 2.65 5026 0.097 2.695027 0.096 2.655040 0.098 2.72Density Designation lbs/in.3(kg/m3) x 103 5140 0.098 2.715041 0.097 2.675042 0.096 2.675043 0.098 2.725049 0.097 2.705149 0.097 2.695249 0.097 2.705349 0.097 2.705449 0.097 2.705050 0.097 2.695050A 0.097 2.695150 0.097 2.685051 0.097 2.695051A 0.097 2.695151 0.097 2.685251 0.097 2.695251A 0.097 2.695351 0.097 2.685451 0.097 2.685052 0.097 2.685252 0.096 2.675352 0.097 2.675154 0.096 2.665154A 0.096 2.675154B 0.096 2.67+ 5154C 0.096 2.66 5254 0.096 2.665354 0.097 2.695454 0.097 2.695554 0.097 2.695654 0.096 2.665654A 0.096 2.665754 0.097 2.675954 0.096 2.665056 0.095 2.645356 0.096 2.645356A 0.096 2.645456 0.096 2.665456A 0.096 2.665456B 0.096 2.665556 0.096 2.665556A 0.096 2.655556B 0.096 2.655556C 0.096 2.665257 0.097 2.705457 0.097 2.695557 0.097 2.705657 0.097 2.695058 0.097 2.675059 0.096 2.665070 0.097 2.685180 0.097 2.70Density Designation lbs/in.3(kg/m3) x 103 5180A 0.097 2.705082 0.096 2.655182 0.096 2.655083 0.096 2.665183 0.096 2.665183A 0.096 2.665283 0.096 2.655283A 0.096 2.655283B 0.096 2.665383 0.096 2.665483 0.096 2.665086 0.096 2.665186 0.096 2.665087 0.096 2.665187 0.096 2.665088 0.096 2.656101 0.097 2.706101A 0.097 2.696101B 0.097 2.706201 0.097 2.696201A 0.097 2.696401 0.097 2.696501 0.098 2.706002 0.097 2.706003 0.097 2.706103 0.098 2.706005 0.097 2.706005A 0.098 2.706005B 0.097 2.706005C 0.098 2.706105 0.097 2.706205 0.098 2.716006 0.098 2.706106 0.098 2.706206 0.098 2.716306 0.097 2.706008 0.098 2.706009 0.098 2.716010 0.098 2.716110 0.098 2.716110A 0.098 2.716011 0.099 2.736111 0.098 2.716012 0.099 2.746012A 0.099 2.746013 0.098 2.716113 0.098 2.716014 0.098 2.706015 0.097 2.696016 0.098 2.706016A 0.098 2.706116 0.097 2.70Density Designation lbs/in.3(kg/m3) x 103 6018 0.099 2.746019 0.098 2.716020 0.099 2.736021 0.098 2.726022 0.097 2.696023 0.099 2.736024 0.098 2.726025 0.097 2.706026 0.099 2.74+6028 0.099 2.74 6033 0.099 2.736040 0.099 2.73+6041 0.099 2.73+6042 0.098 2.72+6043 0.098 2.72 6151 0.098 2.716351 0.098 2.716351A 0.098 2.716451 0.098 2.706951 0.098 2.706053 0.097 2.696056 0.098 2.726156 0.098 2.726060 0.097 2.706160 0.097 2.706260 0.098 2.706360 0.098 2.706460 0.097 2.706560 0.098 2.706061 0.098 2.706061A 0.098 2.706261 0.098 2.706162 0.097 2.706262 0.098 2.726262A 0.098 2.726063 0.097 2.706063A 0.097 2.706463 0.097 2.696463A 0.097 2.696763 0.097 2.696963 0.097 2.70+6064 0.098 2.72+6064A 0.098 2.72 6065 0.098 2.726066 0.098 2.726069 0.098 2.706070 0.098 2.716081 0.097 2.706181 0.097 2.696181A 0.098 2.706082 0.098 2.706082A 0.098 2.70Density Designation lbs/in.3(kg/m3) x 103 6182 0.098 2.716091 0.097 2.706092 0.098 2.707003 0.101 2.807004 0.100 2.777204 0.100 2.787005 0.100 2.777108 0.100 2.787108A 0.101 2.787009 0.101 2.807010 0.102 2.827012 0.101 2.817014 0.101 2.797015 0.100 2.777016 0.100 2.787116 0.101 2.787017 0.100 2.767018 0.101 2.797019 0.100 2.767019A 0.100 2.757020 0.100 2.787021 0.101 2.787022 0.100 2.777122 0.100 2.767023 0.100 2.787024 0.100 2.777025 0.100 2.777026 0.100 2.787028 0.100 2.777029 0.100 2.777129 0.100 2.787229 0.100 2.777030 0.101 2.797031 0.099 2.747032 0.102 2.827033 0.101 2.797034 0.105 2.907035 0.099 2.75+7035A 0.099 2.75 7036 0.104 2.887136 0.104 2.88+7037 0.103 2.85 7039 0.099 2.747040 0.102 2.827140 0.102 2.83+7041 0.101 2.80 7046 0.102 2.827046A 0.102 2.817049 0.103 2.847049A 0.103 2.847149 0.103 2.847249 0.103 2.84Density Designation lbs/in.3(kg/m3) x 103 7349 0.103 2.857449 0.103 2.857050 0.102 2.837050A 0.102 2.827150 0.102 2.837250 0.102 2.827055 0.103 2.86+7155 0.104 2.87 7056 0.104 2.877060 0.103 2.857064 0.103 2.857068 0.103 2.857168 0.103 2.867072 0.098 2.727075 0.101 2.817175 0.101 2.807475 0.101 2.817076 0.102 2.847178 0.102 2.837278 0.102 2.837278A 0.102 2.827081 0.102 2.837085 0.103 2.857090 0.103 2.857093 0.103 2.867095 0.104 2.898005 0.098 2.718006 0.099 2.748007 0.100 2.768008 0.099 2.748010 0.098 2.728011 0.098 2.718011A 0.098 2.718111 0.098 2.718211 0.098 2.728112 0.098 2.728014 0.099 2.738015 0.098 2.728016 0.098 2.728017 0.098 2.718018 0.098 2.728019 0.106 2.928021 0.098 2.738021A 0.098 2.728021B 0.098 2.728022 0.102 2.838023 0.099 2.748024 0.088 2.438025 0.098 2.71+8026 0.099 2.73 8030 0.098 2.718130 0.098 2.71Density Designation lbs/in.3(kg/m3) x 103 8040 0.098 2.718050 0.099 2.738150 0.098 2.738076A 0.098 2.718176 0.098 2.718077 0.098 2.708079 0.098 2.728090 0.092 2.548091 0.092 2.548093 0.092 2.55Density Designation lbs/in.3(kg/m3) x 103PREVIOUSLY ASSIGNED BUT PRESENTLY INACTIVE ALLOY DESIGNATIONS12DATEDESIGNATION RECLASSIFIED103081988-05-23103582005-04-13104082005-04-13104582005-04-131130 1966-09-091330 1964-12-181135 1997-02-031335 1966-09-091245 1966-09-091250 1988-05-231055 1988-05-231160 1958-04-22(Superseded by 1060)1260 2005-04-131360 1965-12-091165 1966-07-121170 1997-02-031270 1966-07-12107581988-05-231175 1997-02-031180 1997-02-031187 1958-09-10(Superseded by 1188)1095 1988-05-231197 1958-09-10(Superseded by 1199)109981965-12-09200381997-11-28X231681965-03-31X2119 1966-03-072020 1974-11-012225 1966-07-12204882005-04-132053 1983-11-09208082005-06-02X209682000-12-083303 1997-02-033205 1965-11-05300682005-04-133008 1996-03-153018 1998-01-164001 1965-11-054101 1965-11-054002 1981-05-29X4003 1975-01-27X4005 1977-06-01401182005-06-024012 1965-11-054543 1997-02-03DATEDESIGNATION RECLASSIFIED4245 1968-08-19(Redesignated 4048)404882005-04-13X5002 1963-06-035004 1967-04-265105 1960-04-285405 1966-07-125007 1968-05-135008 1968-05-135009 1968-05-135011 1967-04-26X5012 1970-06-305013 1996-10-02501481997-11-28X5015 1968-08-19X5020 1977-08-04X5220 1962-01-11502582005-06-025034 1973-08-095039 1975-11-245250 2005-04-135050B 1996-03-155152 1963-06-03X5452 1971-06-175552 1997-02-035652 2005-04-135053 1968-08-19X5153 1967-04-265854 1996-10-02X5055 1956-10-195155 1971-07-145056A141992-02-215357 2005-04-135757 1963-05-145857 1963-06-105957 1963-06-03X508081963-10-225280 1996-10-02X5084 1965-04-27X5184 1965-04-27X5085 1977-08-04X5090 1977-07-18509182000-04-26600181955-07-086301 2005-04-13600482005-04-13600782005-04-13601781997-02-03PREVIOUSLY ASSIGNED BUT PRESENTLY INACTIVE ALLOY DESIGNATIONS12 (continued)DATE DESIGNATION RECLASSIFIED605181963-12-12X6251 1965-03-316253 2002-05-22X6161 1963-06-03606281964-09-04X6163 1964-12-186263 1955-07-126363 1964-12-186563 1967-04-266663 1967-04-266863 1996-10-02X6064181965-03-31X6067 1974-11-016071 1966-07-126090 1992-06-01700181997-02-037002 1966-07-127104 1988-05-23X7006 1963-09-10X710681980-04-16X7007 1972-02-16700882005-04-13 7109 1996-03-15701181999-06-17701381997-02-037027 1996-06-26X7038 1967-04-267139 1966-09-097146 1997-02-037051 1996-10-027070 1988-05-23X7272 1965-03-317472 1997-02-03X7275 1963-06-03727782000-11-067079 1989-03-22 7179 1989-06-06X7279 1963-06-03X7080 1971-01-04709181997-02-03 800181997-02-03X8002 1964-12-18X8003 1964-12-188004 1996-10-02800982000-06-198212 1967-04-268013 1971-11-01802082005-04-138DATE DESIGNATION RECLASSIFIED8177 1997-02-03828082005-04-13X8380 1964-12-18X8480 1964-12-18808181997-02-03X8090A 1989-01-13X8092 1991-10-24X8192 1991-10-24CROSS REFERENCE OF INTERNATIONAL DESIGNATIONS DECLARATION OF ACCORD (DOA) TO ISO*DOA DESIGNATIONFORMER ISODESIGNATIONDOADESIGNATIONFORMER ISODESIGNATIONDOADESIGNATIONFORMER ISODESIGNATION1050A Al99.5 3105 AlMn0.5Mg0.5 6101 E-AlMgSi1350 E-Al99.5 4043 AlSi5 6101A E-AlMgSi(A) 1060 Al99.6 4043A AlSi5(A) 6005 AlSiMg1070A Al99.7 4047 AlSi12 6005A AlSiMg(A)1370 E-Al99.7 4047A AlSi12(A) 6351 AlSi1Mg0.5Mn 1080A Al99.8(A) 5005 AlMg1(B) 6060 AlMgSi1100 Al99.0Cu 5019 AlMg5 6061 AlMg1SiCu1200 Al99.0 5050 AlMg1.5(C) 6262 AlMg1SiPb2011 AlCu6BiPb 5251 AlMg2 6063 AlMg0.7Si2014 AlCu4SiMg 5052 AlMg2.5 6063A AlMg0.7Si(A) 2014A AlCu4SiMg(A) 5154 AlMg3.5 6181 AlSi1Mg0.82017 AlCu4MgSi 5154A AlMg3.5(A) 6082 AlSi1MgMn2017A AlCu4MgSi(A) 5454 AlMg3Mn 7005 AlZn4.5Mg1.5Mn 2117 AlCu2.5Mg 5554 AlMg3Mn(A) 7010 AlZn6MgCu2219 AlCu6Mn 5754 AlMg3 7020 AlZn4.5Mg1 2024 AlCu4Mg1 5056 AlMg5Cr 7049A AlZn8MgCu2030 AlCu4PbMg 5356 AlMg5Cr(A) 7050 AlZn6CuMgZr 3003 AlMn1Cu 5456 AlMg5Mn1 7075 AlZn5.5MgCu 3103 AlMn1 5083 AlMg4.5Mn0.7 7475 AlZn5.5MgCu(A) 3004 AlMn1Mg1 5183 AlMg4.5Mn0.7(A) 7178 AlZn7MgCu3005 AlMn1Mg0.5 5086 AlMg4*Source: ISO 209-1.NOTE: This table is included for informational purposes only. ISO 209-1 has been withdrawn and replaced by ISO 209 which references the Teal Sheets as the normative reference and the source for international alloy designations.The Aluminum Association RECOMMENDATION 15 December 1970 1525 Wilson Boulevard INTERNATIONAL DESIGNATION SYSTEM Revised March 2008 Arlington, VA 22209 FOR WROUGHT ALUMINUM AND WROUGHT ALUMINUM ALLOYSU.S.A.This Recommendation is based on the numerical designation system for wrought aluminum and wrought aluminum alloys which was adopted in the U.S.A. in 1954, andbecame its national standard in 1957. This Recommendation was officially adopted by the International Signatories of the Declaration of Accord on December 15, 1970.Designations in accordance with this Recommendation may be used by any country, but there is no obligation to use them. For use, see Appendixes A, B, and C.A numerical designation assigned in conformance with this Recommendation should only be used to indicate an aluminum or an aluminum alloy having chemicalcomposition limits identical to those registered with the Signatories to the Declaration of Accord on an International Alloy Designation System for Wrought Aluminum andWrought Aluminum Alloys.1. ScopeThis recommendation describes a four-digit numerical system for designating wroughtaluminum and wrought aluminum alloys.2. Alloy GroupsThe first of the four digits in the designation indicates the alloy group as follows:Aluminum, 99.00 percent and greater (1xxx)Aluminum alloys grouped by major alloying elements1,2,3Copper (2xxx)Manganese (3xxx)Silicon (4xxx)Magnesium (5xxx)Magnesium and Silicon (6xxx)Zinc (7xxx)Other elements (8xxx)Unused series (9xxx)3. 1xxx GroupThe designation assigned shall be in the 1xxx group whenever the minimum aluminumcontent is specified as 99.00 percent and greater. In the 1xxx group, the last two of the fourdigits in the designation indicate the minimum aluminum percentage4. These digits are thesame as the two digits to the right of the decimal point in minimum aluminum percentagewhen it is expressed to the nearest 0.01 percent. The second digit in the alloy designationindicates alloy modifications in impurity limits or alloying elements. If the second digit in thedesignation is zero, it indicates unalloyed aluminum having natural impurity limits; integers 1through 9, which are assigned consecutively as needed, indicate special control of one ormore individual impurities or alloying elements.4. 2xxx-8xxx GroupsThe alloy designation in the 2xxx through 8xxx groups is determined by the alloying element(Mg2Si for 6xxx alloys) present in the greatest mean percentage. If the greatest meanpercentage is common to more than one alloying element, choice of group will be in order ofgroup sequence Cu, Mn, Si, Mg, Mg2Si, Zn or Others. In the 2xxx through 8xxx alloy groupsthe last two of the four digits in the designation have no special significance but serve only toidentify the different aluminum alloys in the group. The second digit in the alloy designationindicates the original alloy5 and alloy modifications; integers 1 through 9, which are assignedconsecutively, indicate alloy modifications.5. ModificationsA modification of the original alloy 5 is limited to any one or a combination of the following:(a) Change of not more than the following amounts in the arithmetic mean of thelimits for an individual alloying element or combination of elements expressedas an alloying element or both:Arithmetic Mean of Limits for Alloying Elements in Original Alloy Maximum ChangeUp through 1.0 percent 0.15Over 1.0 through 2.0 percent 0.20Over 2.0 through 3.0 percent 0.25Over 3.0 through 4.0 percent 0.30Over 4.0 through 5.0 percent 0.35Over 5.0 through 6.0 percent 0.40Over 6.0 percent 0.50To determine compliance when maximum and minimum limits are specified for a combination of two or more elements in one alloy composition, the arithmetic mean of such combination is compared to the sum of the mean values of the same individual elements, or any combination thereof, in another alloy composition.(b) Addition or deletion of not more than one alloying element with limits having anarithmetic mean of not more than 0.30 percent, or addition or deletion of not morethan one combination of elements expressed as an alloying element with limitshaving a combined arithmetic mean of not more than 0.40 percent.(c) Substitution of one alloying element for another element serving the samepurpose.(d) Change in limits for impurities expressed singly or as a combination.(e) Change in limits for grain refining elements.(f) Maximum iron or silicon limits of 0.12 percent and 0.10 percent, or less,respectively, reflecting high purity base metal.An alloy should not be registered as a modification if it meets the requirements for a national variation.6. National VariationsNational variations of wrought aluminum and wrought aluminum alloys registered by another country in accordance with this Recommendation are identified by a serial letter after the numerical designation. The serial letters are assigned in alphabetical sequence starting withA for the first national variation registered, but omitting I, O, and Q.A national variation has composition limits which are similar but not identical to a modificationor an original alloy registered by another country, with differences such as:(a) Differences in arithmetic mean of limits for an individual alloying element orcombination of elements expressed as an alloying element, or both, notexceeding the following amounts:Arithmetic Mean of Limits for AlloyingElements in Original Alloy or ModificationMaximumDifferenceUp through 1.0 percent 0.15Over 1.0 through 2.0 percent 0.20Over 2.0 through 3.0 percent 0.25Over 3.0 through 4.0 percent 0.30Over 4.0 through 5.0 percent 0.35Over 5.0 through 6.0 percent 0.40Over 6.0 percent 0.50To determine compliance when maximum and minimum limits are specified for acombination of two or more elements in one alloy composition, the arithmetic mean ofsuch combination is compared to the sum of the mean values of the same individualelements, or any combination thereof, in another alloy composition.(b) Substitution of one alloying element for another element serving the samepurpose.(c) Different limits of impurities except for low iron. Iron maximum of 0.12 percent orless, reflecting high purity base metal, should be considered an alloy modification.See 5(f).(d) Different limits on grain refining elements.(e) Inclusion of a minimum limit for iron or silicon, or both.An alloy meeting these requirements should not be registered as a new alloy or alloymodification.See footnotes on page 2625See footnotes on page 14.。
常用压铸用铝合金材料名称对照表
主要工业国家压铸铝合金标准美国标准ASTM B85-96美国压铸铝合金化学成分表合金牌号成分ANSI ASTM UNS Si Fe Cu Mn Mg Ni Zn Sn Ti杂质(总量)铝AI 360.0SG100B A036009.0-10.0 2.00.60.350.40-0.600.500.500.150.25余量A360.0SG100A A136009.0-10.0 1.30.60.350.40-0.600.500.500.150.25余量380.0SC84B A038007.5-9.5 2.0 3.0-4.00.500.100.50 3.00.350.50余量A380.0E SC84A A138007.5-9.5 1.3 3.0-4.00.500.100.50 3.00.350.50余量383.0E SC102A A038309.5-11.5 1.3 2.0-3.00.500.100.30 3.00.150.50余量384.0E SC114A A0384010.5-12.0 1.3 3.0-4.50.500.100.50 3.00.350.50余量390.0SC174A A0390016.0-18.0 1.3 4.0-5.00.100.45-0.650.100.200.20余量B390.0SC174B A2390016.0-18.0 1.3 4.0-5.00.500.45-0.650.10 1.50.100.20余量392.0S19A0392018.0-20.0 1.50.40-0.800.20-0.600.80-1.200.500.500.300.200.50余量413.0S12B A0413011.0-13.0 2.0 1.00.350.100.500.500.150.25余量A413.0S12A A1413011.0-13.0 1.3 1.00.350.100.500.500.150.25余量C433.0S5C A34430 4.5-6.0 2.00.60.350.100.500.500.150.25余量518.0G8A A051800.35 1.80.250.357.5-8.50.150.150.250.25余量欧盟标准EN1706：1998欧盟压铸铝合金化学成分和力学性能表合金牌号化学成分代号Si Fe Cu Mn Mg Ni Zn Pb Sn Ti 抗拉强度Mpa最小屈服强度Mpa最小伸长率%最小布氏硬度HB最小ENAC-434009.0-11.00.45-0.90.080.550.20-0.500.150.150.150.050.152******** ENAC-4430010.5-13.50.45-0.90.080.550.150.152******** ENAC-444008.0-11.00.550.080.500.100.050.150.050.050.152******** ENAC-460008.0-11.00.6-1.1 2.0-4.00.550.15-0.550.55 1.20.350.250.2240140<180 ENAC-4610010.0-12.00.45-1.01.5-2.50.550.300.45 1.70.250.250.2240140<180 ENAC-462007.5-9.50.8 2.0-3.50.15-0.650.15-0.550.35 1.20.250.150.2240140180 ENAC-465008.0-11.00.6-1.2 2.0-4.00.550.15-0.550.55 3.00.350.250.20240140<180 ENAC-4710010.5-13.50.6-1.10.7-1.20.550.350.300.550.200.100.152******** ENAC-512002.50.45-0.90.100.558.0-10.50.100.250.100.100.152********中华人民共和国国家标准—铝合金 GB/T 15115-94压铸铝合金的化学成分和力学性能序号合金牌号化学成分%力学功能(不低于)合金代号硅铜锰镁铁镍钛锌铅锡铝抗拉强度6ЪN/mm2伸长度δ/%(Lo=50)布氏硬度HB5/250/301YZAISil2YL10210.0-13.0≤0.6≤0.6≤0.05≤1.2≤0.3余2202602YZAISi10Mg YL1048.0-10.5≤0.30.2-0.50.17-0.30≤1.0≤0.3≤0.05≤0.01余2202703YZAISil2Cu2YL10811.0-13.01.0-2.00.3-0.90.4-1.0≤1.0≤0.05≤1.0≤0.05≤0.01余2401904YZAISi9 Cu4YL1127.5-9.5 3.0-4.0≤0.5≤0.3≤1.2≤0.5≤1.2≤0.1≤0.1余2401855YZAISillCu3YL1139.6-12.0 1.5-3.5≤0.5≤0.3≤1.2≤0.5≤1.0≤0.1≤0.1余2301806YZAISil7Cu5Mg YL11716.0-18.04.0-5.0≤0.50.45-0.65≤1.2≤0.1≤0.1≤1.2余220＜17YZAIMg5Sil YL3020.8-1.3≤0.10.1-0.44.5-5.5≤1.2≤0.2≤0.2余220270中华人民共和国国家标准压铸锌合金的化学成分和力学性能化学成分，%序号合金牌号主要成分杂质含量（不大于）合金代号铝铜镁锌铁铅锡镉铜1ZZnA14Y YX040 3.5-4.30.02-0.06其余0.10.0050.0030.0040.25 2ZZnA14CU1Y YX041 3.5-4.30.75-1.250.03-0.08其余0.10.0050.0030.0043ZZnA14CU3Y YX043 3.5-4.3 2.5-3.00.02-0.06其余0.10.0050.0030.004力学性能抗拉强度6Ъ(N/mmˉ2)伸长度δ/%Lo=50布氏硬度性HB5/250/30250180270290320295日本工业标准JIS H5302:2000日本压铸铝合金化学成分表JIS牌号ISO牌号Cu Si Mg Zn Fe Mn Ni Sn Pb Ti Al ADC1 1.0以下11.0-13.00.3以下0.5以下 1.3以下0.3以下0.5以下0.1以下余量ADC1C A1-Sil2CuFe1.2以下11.0-13.50.3以下0.5以下 1.3以下0.5以下0.30 以下0.1以下0.20 以下0.2以下余量ADC2A1-Si12Fe0.10 以下 11.0-13.50.10以下0.1以下 1.3以下0.5以下0.1以下0.05以下0.1以下0.2以下余量ADC30.6以下9.0-10.00.4-0.60.5以下 1.3以下0.3以下0.5以下0.1以下余量ADC50.2以下0.3以下 4.0-8.50.1以下 1.8以下0.3以下0.1以下0.1以下余量ADC60.1以下 1.0以下 2.5-4.00.4以下0.8以下0.4-0.60.1以下0.1以下余量ADC7A1-Si5Fe0.10 以下 4.5-6.00.1以下0.1以下 1.3以下0.5以下0.1以下0.1以下0.1以下0.20以下余量ADC8A1-Si6Cu4Fe3.0-5.0 5.0-7.00.3以下 2.0以下 1.3以下0.2-0.60.3以下0.1以下0.2以下0.2以下余量ADC10 2.0-4.07.5-9.50.3以下 1.0以下 1.3以下0.5以下0.5以下0.2以下余量ADC10Z 2.0-4.07.5-9.50.3以下 3.0以下 1.3以下0.5以下0.5以下0.2以下余量ADC11A1-Si8Cu3Fe2.5-4.07.5-9.50.3以下 1.2以下 1.3以下0.6以下0.5以下0.2以下0.3以下0.2以下余量ADC12 1.5-3.59.6-12.00.3以下 1.0以下 1.3以下0.5以下0.5以下0.2以下余量ADC12Z 1.5-3.59.6-12.00.3以下 3.0以下 1.3以下0.5以下0.5以下0.2以下余量日本压铸铝合金机械性能表抗拉试验硬度试验牌号抗拉强度MPa耐力MPa延伸率%HB HRB平均值σASTM平均值σASTM平均值σASTM平均值σASTM平均值σADC12504629017222130 1.70.63.571.2 3.57236.2 5.5ADC32794832017935170 2.7 1.03.571.4 1.87636.7 2.2ADC5(213)65310(145)26190 5.0(66.4) 2.474(30.1) 3.7ADC6266612801722364 3.210.064.7 2.36727.3 3.9ADC102413432015718160 1.50.53.573.6 2.48339.4 3.0ADC122284131015414150 1.40.83.574.1 1.58640.0 1.8ADC1419328320188312500.50.1<176.8 1.710843.1 2.1。
铝合金 成分
铝合金成分
铝合金是一种由铝和其他金属或非金属元素组成的合金材料。
其成分
可以根据不同的需求和用途而有所不同，但通常包括以下几个元素：
1. 铝（Al）：铝是铝合金的主要成分，通常占到合金总重量的60%以上。
它具有轻、强、耐腐蚀等优良性能，是制造航空器、汽车、建筑
等领域中广泛使用的材料。
2. 铜（Cu）：铜是一种常用的添加元素，可以提高铝合金的强度和硬度。
通常含量在2-7%之间。
3. 锰（Mn）：锰也是一种常用的添加元素，可以提高铝合金的强度和韧性。
通常含量在0.3-1.5%之间。
4. 硅（Si）：硅可以提高铝合金的强度和耐磨性。
通常含量在0.2-1.5%之间。
5. 锌（Zn）：锌可以提高铝合金的耐腐蚀性能。
通常含量在0.2-1%
之间。
6. 镁（Mg）：镁可以提高铝合金的强度和硬度，并且具有良好的耐腐
蚀性能。
通常含量在0.5-6%之间。
7. 铁（Fe）：铁是铝合金中的杂质元素，含量较低，但会影响其机械性能和耐腐蚀性能。
除了以上几种元素外，还有一些其他的添加元素，如锆、钛、镍、铬等，它们的作用各不相同，可以根据具体需求进行添加。
总之，铝合金的成分是多种多样的，不同的成分组合可以得到不同性能的材料。
在实际应用中需要根据具体需求进行选择和设计。
铝合金各国牌号对照及化学成分表
Al-Si8Cu3Fe
Al-Si9 Al-Si12(Fe) Al-Si10Mg(Fe) Al-Si8Cu3 Al-Si9Cu3(Fe) Al-Si9Cu3(Fe)(Zn) Al-Si11Cu2(Fe) Al-Si11Cu3(Fe) Al-Si12Cu1(Fe) Al-Si17Cu4Mg
JIS H 5302 - 2006
JIS H 5302 - 2006
JIS H 5302 - 2006
ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007 ISO 3522 - 2007
挤出用铝合金 标准
EN 573-3 EN 573-4 EN 573-3 EN 573-3 EN 573-3
Al Si8Cu3 Al Si9Cu1Mg Al Si9Cu3(Fe) Al Si9Cu3(Fe)(Zn) Al Si11Cu2(Fe) Al Si11Cu3(Fe) Al Si12(Cu) Al Si12Cu1(Fe) Al Si12CuMgNi Al Si17Cu4Mg
压铸用铝合金 标准
GB/T15114 GB/T15114 GB/T15115 GB/T15114 GB/T15114 GB/T15114 GB/T15114 GB/T15114
铝合金常用材料对照表
5A03
原LF3
1A30
原L4－1
2014
－
5A05
原LF5
1100
代LF5－1
2014A
－
5B05
原LF10
1200
代L5
2214
－
5A06
原LF6
1235
－
2017
－
5B06
原LF14
2A01
原LY1
2017A
－
5A12
原LF12
2A02
原LY2
2117
－
5A13
原LF13
2A04
原LY4
2218
－
5A03
原LF3
1A30
原L4－1
2014
－
5A05
原LF5
1100
代LF5－1
2014A
－
5B05
原LF10
1200
代L5
2214
－
5A06
原LF6
1235
－
2017
－
5B06
原LF14
2A01
原LY1
2017A
－
5A12
原LF12
2A02
原LY2
2117
－
5A13
原LF13
2A04
原LY4
2218
－
6060
－
7003
原LC12
5754
－
6061
原LD30
7005
－
5056
原LF5－1
6063
原LD31
7020
－
5356
－
6063A
铝合金化学成分
ADC12 压铸 9.6-12.0 ≤0.30 1.5-3.5 ≤1.3 ≤3.0 ≤0.50 ≤0.3 余量 JISH5302
ADC12Z 压铸 9.6-12.0 ≤0.30 1.5-3.5 ≤1.3 ≤3.0 ≤0.50 ≤0.3 余量 JISH5302
AC4B 重力 7.0-10.0 ≤0.50 ≤0.20 余量 JISH5202
AC4H 重力 6.5-7.5 0.2-0.4 ≤0.20 ≤0.20 ≤0.10 ≤0.10 ≤0.10 余量 JISH5202
ADC1 压铸 11.0-13.0 ≤0.3 ≤1.0 ≤1.3 ≤0.5 ≤0.30 ≤0.1 余量 JISH5302
390 压铸 16.0-18.0 0.45-0.65 4.0-5.0 ≤1.3 ≤0.1 ≤0.10 余量 ASTMB85
413 压铸 11.0-13.0 ≤0.1 ≤1.0 ≤2.0 ≤0.50 ≤0.15 余量 ASTMB85
日本 AC2B 重力 5.0-7.0 ≤0.50 2.0-4.0 ≤1.0 ≤1.0 ≤0.35 ≤0.20 余量 JISH5202
YL104 压铸 8.0-10.5 0.17-0.30 ≤0.3 ≤1.0 ≤0.3 0.2-0.5 ≤0.05 ≤0.01 余量 GB/T15115
YL112 压铸 7.5-9.5 ≤0.3 3.0-4.0 ≤1.2 ≤1.2 ≤0.5 ≤0.1 ≤0.1 余量 GB/T15115
YL113 压铸 9.6-12.0 ≤0.3 1.5-3.5 ≤1.2 ≤1.0 ≤0.5 ≤0.1 ≤0.1 余量 GB/T15115
铝合金锭——成分性能对比
• 锡 Sn ：≤0.01(杂质)
• 铅 Pb：≤0.05(杂质)
• 注：杂质总和: (砂型铸造)≤1.1; (金属型铸造)≤1.4
zl105力学性能
• 抗拉强度 σb (MPa)：≥225
伸长率 δ5 (%)：≥0.5
• 硬度 （HB)：≥70(5/250/30)HBS
• 抗拉强度 σb (MPa)：≥145 • 屈服强度σb（MPa)：≥180 • 伸长率 δ5 (%)：≥4 • 硬度 (HB )：≥50(5/250/30) • 铸造方法：
砂型铸造加变质处理; 熔模铸造加变质处理; 金属型铸造加变质处理（F态.SB.RB.KB)。
3 zl104铝合金
• 材料名称: ZAlSi9Mg
ADC12力学性能
• 抗拉强度 σb (MPa)：≥230 • 伸长率 δ5 (%)：≥1 • 硬度 (HB )：80
Fe含量对ADC12铝合金组织及性能的影响
• 过高的铁含量容易使铸件出现硬质点，机加工有困难，断面有片状金 属复合物，浇口易出现缺肉现象，铸件韧性下降等！
• 过低，容易出现粘模等现象.
• 铜 Cu ：≤0.1(杂质)交付形态
• 锌 Zn：≤0.25(杂质)钛+稀土 Ti+Zr：≤0.15(杂质)
• 锡 Sn ：≤0.01(杂质)
• 铅 Pb：≤0.01(杂质)
• 注：杂质总和:(砂型铸造)≤1.1;( 金属型铸造)≤1.4
zl104力学性能
• 抗拉强度 σb (MPa)：≥195 • 伸长率 δ5 (%)：≥1.5 • 硬度 （HB)：≥65(5/250/30) • 热处理规范：
• 标准：GB/T 15115-2009
铝合金牌号成分对照表
铝合金牌号成分对照表AL1/系纯铝1系纯铝，含铝量大于99%以上。
这个系列的最低含铝量，比如1050，其含铝量为99.5%。
生产过程比较单一，价格相对比较便宜，是目前常规工业中最常用的一个系列。
AL-Cu2/系铝铜合金2系列铝合金代表2024、2A12(即LY12)。
2系列铝板的特点是硬度较高，具有很高的强度和良好的切削加工性能，但耐腐蚀性较差。
其中以铜元素含量最高，大概在3-5%左右。
2系列铝材属于航空铝材，价格较高。
AL-Mn3/系铝锰合金3系列铝合金代表3003、3A21为主。
3系列是由锰元素为主要成分。
含量在1.0-1.5之间，是一款防锈功能较好的系列，用于加工需要有良好的成形性能、高的抗蚀性可焊性好的零件部件。
AL-Mg5/系铝镁合金5系列铝合金代表5052、5083、5A06。
5系列铝属于较常用的合金铝板系列，主要元素为镁，含镁量在3-5%之间。
又可以称为铝镁合金。
主要特点为密度低，抗拉强度高，延伸率高，疲劳强度好，但不可做热处理强化。
在相同面积下铝镁合金的重量低于其他系列，在常规工业中应用也较为广泛。
AL-Mg-Si6/系铝镁硅合金6系列铝合金代表6061、6063、6082，主要含有镁和硅两种元素。
6系属热处理可强化合金，具有良好的可成型性、可焊接性、可机加工性，同时具有中等强度，在退火后仍能维持较好的操作性，适用于对抗腐蚀性、氧化性要求高的应用。
可使用性好，容易涂层，加工性好。
AL-Zn7/系铝锌合金7系铝合金代表7075主要含有锌元素。
也属于航空系列，是铝镁锌铜合金，是可热处理合金，属于超硬铝合金，有良好的耐磨性.也有良好的焊接性，但耐腐蚀性较差。
该系当中以7075-T651铝合金尤为上品，被誉为铝合金中最优良的产品，强度高、远胜任何软钢。
此合金并具有良好机械性及阳极反应。
以上内容就是7种铝合金牌号化学成分表了，希望可以帮到大家！。
铝合金常用材料对照表
5356
－
6063A
－
7022
－
5456
－
6070
原LD2－2
7050
－
5082
－
6181
－
7075
－
5182
－
6082
－
7475
－
5083
原LF4
7A01
原LB1
8A06
原L6
5183
－
7A03
原LC3
8011
曾用LT98
5086
－
7A04
原LC4
8090
－
6A02
原LD2
7A05
曾用705
－
－
代 号
名 称
说 明 与 应 用
F
自由加工状态
适用于在成型过程中，对于加工硬化和热处理条件无特殊要求的
产品，该状态产品的力学性能不作规定
O
退火状态
适用于经完全退火获得最低强度的加工产品
H
加工硬化状态
适用于通过加工硬化提高强度的产品，产品在加工硬化后可经过
（也可不经过）使强度有所降低的附加热处理
H代号后面必须根有两位或三位阿拉伯数字
2124
2024
2024
AlCuMg2
D16AVTV
2B16
2319
锻铝
2A80
2N01
AK4
2A90
2218
2018
AK2
2A14
2014
2014
2014
AlCuSiMn
AK8
超硬铝
7A09
7175
7075
7075
AlZnMgCu1.5
铝合金成分对照表(完整)
0.15 余量 0.15 余量 0.15 余量
0.20
AlMn0.5Mg0.5 3.0505 0.6
0.7
0.3 0.30-0.8 0.20-0.8 0.2
0.4 —
—
0.05
AlMn1Mg0.5 3.0525 0.6
0.7
0.3 1.0-1.5 0.20-0.6 0.1
0.25 0.1
—
0.05
AlMn1Mg1 3.0526 0.3
0.7 0.25 1.0-1.5 0.8-1.3
0.4
0.1 0.40-1.0 4.0-4.9 0.05-0.25 0.25 0.15
—
0.05
AlMg5Mn 3.3549 0.2
0.35 0.15 0.20- 4.0-5.0
0.1
0.25 0.1
—
0.05
0.50
AlMn1
3.0515 0.5
0.7
0.1 0.9-1.5 0.3
0.1
0.2 0.1
—
0.05
AlMg5
3.3555 0.4
0.5
0.1 0.10-0.6 4.5-5.6 0.2
0.2 0.2
(Mn+Cr)0.10-0.6
0.05
AlMg2Mn0.3 3.3525 0.4
0.5 0.15 0.10- 1.7-2.4 0.15 0.15 0.15
—
0.05
0.50
AlMg2Mn0.8 3.3527 0.4 0.55 0.1 0.50-1.1 1.6-2.5 0.3
0.4 —
—
0.05
AlMn1Mg0.5 3.0525 0.6
铝合金材料成分对照表
铝合金锭化学成分对照表标准2009-11-2715:16:06阅读51评论0字号：大中小订阅JISH5202-1986AC1A 4.0-5.0 1.20 Max0.15 Max0.30 Max0.50 Max0.30 Max0.05 Max0.25 MaxAC1B 4.0-5.00.20 Max 0.15-0.350.10 Max0.35 Max0.10 Max0.05 Max0.05-0.30AC2A 3.0-4.5 4.0-6.00.25 Max0.55 Max0.80 Max0.55 Max0.30 Max0.20 Max AC2B 2.0-4.0 5.0-7.00.50 Max 1.00 Max 1.00 Max0.50 Max0.35 Max0.20 MaxAC3A0.25 Max 10.0-13.00.15 Max0.30 Max0.80 Max0.35 Max0.10 Max0.20 MaxAC4A0.25 Max8.0-10.00.30-0.60.25 Max0.55 Max0.30-0.60.10 Max0.20 Max AC4B 2.0-4.07.0-10.00.50 Max 1.00 Max 1.00 Max0.50 Max0.35 Max0.20 MaxAC4C0.25 Max 6.5-7.50.25-0.450.35 Max0.55 Max0.35 Max0.10 Max0.20 MaxAC4CH0.20 Max 6.5-7.50.20-0.400.10 Max0.20 Max0.10 Max0.05 Max0.20 MaxAC4D 1.0-1.5 4.5-5.50.40-0.600.30 Max0.60 Max0.50 Max0.20 Max0.20 MaxAC5A 3.5-4.50.60 Max 1.2-1.80.15 Max0.80 Max0.35 Max1.7-2.30.20 Max AC7A0.10 Max0.20 Max 3.5-5.50.15 Max0.30 Max0.60 Max0.05 Max0.20 Max AC7B0.10 Max0.20 Max9.5-11.00.10 Max0.30 Max0.10 Max0.05 Max0.20 MaxAC8A0.8-1.311.0-13.00.7-1.30.15 Max0.80 Max0.15 Max0.80-1.500.20 MaxAC8B 2.0-4.08.5-10.50.50-1.50.50 Max 1.00 Max0.50 Max 0.10-1.000.20 MaxAC8C 2.0-4.08.5-10.50.50-1.50.50 Max 1.00 Max0.50 Max0.50 Max0.20 MaxAC9A0.50-1.522-240.50-1.50.20 Max0.80 Max0.50 Max 0.50-1.500.20 MaxAC9B0.50-1.518-200.50-1.50.20 Max0.80 Max0.50 Max 0.50-1.500.20 Max铝合金锭化学成份(%)铜硅镁锌铁锰镍钛JISH2212-1990ADC 1 1.0 Max 11.0-13.00.30 Max0.5 Max0.9 Max0.3 Max0.5 MaxADC 30.6 Max9.0-10.00.4-0.60.5 Max0.9 Max0.3 Max0.5 Max ADC 50.2 Max0.3 Max 4.1-8.50.1 Max 1.1 Max0.3 Max0.1 Max ADC 60.1 Max 1.0 Max 2.6-4.00.4 Max0.8 Max0.4-0.60.1 Max ADC 10 2.0-4.07.5-9.50.3 Max 1.0 Max0.9 Max0.5 Max0.5 Max ADC 10Z 2.0-4.07.5-9.50.3 Max 3.0 Max0.9 Max0.5 Max0.5 Max ADC 12 1.5-3.59.6-12.00.3 Max 1.0 Max0.9 Max0.5 Max0.5 Max ADC 12Z 1.5-3.59.6-12.00.30 Max 3.0 Max0.9 Max0.5 Max0.5 MaxADC 14 4.0-5.016.0-18.00.5-0.65 1.5 Max0.9 Max0.5 Max0.3 MaxDIN226 2.0-3.58.0-11.00.1-0.5 1.20 Max 1.0 Max0.1-0.40.30 Max0.1 Max U.S.A铜硅镁锌铁锰镍钛A356.10.25 Max 6.5-7.50.25-0.450.35 Max0.50 Max0.35 Max0.25 MaxA3600.60 Max 9.00-10.000.40-0.600.50 Max 1.30 Max0.35 Max0.50 MaxA360.10.60 Max9.0-10.00.45-0.600.40 Max 1.00 Max0.35 Max0.50 MaxA380.03.00-4.007.50-9.500.30 Max 3.00 Max 1.30 Max0.50 Max0.50 MaxA380.13.00-4.007.50-9.500.10 Max 2.90 Max 1.00 Max0.50 Max0.50 MaxA3832.00-3.009.50-11.500.10 Max 3.00 Max 1.30 Max0.50 Max0.30 MaxA383.12.00-3.009.50-11.500.10 Max 2.90 Max 1.00 Max0.50 Max0.30 MaxA413.1 1.00 Max 11.0-13.00.10 Max0.40 Max 1.00 Max0.35 Max0.50 MaxA413.20.10 Max 11.0-13.00.05 Max0.05 Max0.60 Max0.05 Max0.05 MaxU.K铜硅镁锌铁锰镍钛LM20.70-2.509.00-11.500.30 Max 2.00 Max 1.00 Max0.50 Max0.50 Max0.20 MaxLM42.00-4.004.00-6.000.15 Max0.50 Max0.80 Max0.20-0.600.30 Max0.20 MaxLM50.10 Max0.30 Max 3.00-6.000.10 Max0.60 Max0.30-0.700.10 Max0.20 MaxLM60.10 Max 10.00-13.000.10 Max0.10 Max0.60 Max0.50 Max0.10 Max0.20 MaxLM90.10 Max 10.00-13.000.20-0.600.10 Max0.60 Max0.30-0.700.10 Max0.20 Max铜硅镁锌铁锰镍钛LM100.10 Max0.25 Max 9.50-11.000.10 Max0.35 Max0.10 Max0.10 Max0.20 MaxLM129.00-11.00 2.50 Max0.20-0.400.80 Max 1.00 Max0.60 Max0.50 Max0.20 MaxLM130.70-1.5010.00-12.000.80-1.500.50 Max 1.00 Max0.50 Max1.50 Max0.20 MaxLM161.00-1.504.50-5.500.40-0.600.10 Max0.60 Max0.50 Max0.25 Max0.20 MaxLM180.10 Max 4.50-6.000.10 Max0.10 Max0.60 Max0.50 Max0.10 Max0.20 MaxLM200.40 Max 10.00-13.000.20 Max0.20 Max 1.00 Max0.50 Max0.10 Max0.20 MaxLM213.00-5.005.00-7.000.10-0.30 2.00 Max 1.00 Max0.20-0.600.30 Max0.20 MaxLM222.80-3.804.00-6.000.05 Max0.15 Max0.60 Max0.20-0.600.15 Max0.20 MaxLM243.00-4.007.50-9.500.30 Max 3.00 Max 1.30 Max0.50 Max0.50 Max0.20 MaxLM250.10 Max 6.50-7.500.20-0.450.10 Max0.50 Max0.30 Max0.10 Max0.20 MaxLM262.00-4.008.50-10.500.50-1.50 1.00 Max 1.20 Max0.50 Max1.00 Max0.20 MaxLM271.50-2.506.00-8.000.30 Max 1.00 Max0.80 Max0.20-0.600.30 Max0.20 MaxLM281.30-1.8017.00-20.000.80-1.500.20 Max0.70 Max0.60 Max0.80-1.500.20 MaxLM290.80-1.3022.00-25.000.80-1.300.20 Max0.70 Max0.60 Max0.80-1.300.20 MaxLM304.00-5.0016.00-18.000.40-0.700.20 Max 1.10 Max0.30 Max0.10 Max0.20 MaxU.K铜硅镁锌铁锰镍钛ZYCMAK2 2.5-3.00.02-0.05BAL0.1ZYCMAK30.25 Max 0.02-0.05BAL0.1ZYCMAK50.75-1.250.03-0.08BAL0.1ZYCMAK70.25 Max 0.005-0.02BAL0.075ZYCMAK80.8-1.30.8-1.3BAL0.075ZDC-10.75-1.250.03-0.06BAL0.02 MaxZDC-20.001Max0.03-0.06BAL0.01 MaxZDC-32.75-3.250.03-0.06BAL0.02 MaxZYC-A0.5 Max 0.02-0.06BAL0.1 Max锌合金锭化学成份（%）ZYC-B0.5 Max 0.02-0.06BAL0.1 MaxZYC-C0.5 Max 0.02-0.06BAL0.1 Max铅锡铬铝0.05 Max0.05 Max0.05 Max BAL 0.05 Max0.05 Max0.05 Max BAL 0.15 Max0.05 Max0.15 Max BAL 0.20 Max0.10 Max0.20 Max BAL 0.10 Max0.10 Max0.15 Max BAL 0.10 Max0.05 Max0.15 Max BAL 0.20 Max0.10 Max0.20 Max BAL 0.10 Max0.05 Max0.10 Max BAL 0.05 Max0.05 Max0.05 Max BAL 0.10 Max0.05 Max0.15 Max BAL 0.05 Max0.05 Max0.15 Max BAL 0.05 Max0.05 Max0.15 Max BAL 0.05 Max0.05 Max0.15 Max BAL 0.05 Max0.05 Max0.10 Max BAL 0.10 Max0.10 Max0.10 Max BAL 0.10 Max0.10 Max0.10 Max BAL 0.10 Max0.10 Max0.10 Max BAL 0.10 Max0.10 Max0.10 Max BAL铅锡铬铝0.1 Max BAL0.1 Max BAL0.1 Max BAL0.1 Max BAL0.3 Max BAL0.3 Max BAL0.2 Max BAL0.3 Max BAL0.3 Max BAL 0.20 Max0.10 Max BAL 铅锡铬铝BAL0.15 Max BAL0.15 Max BAL0.35 Max BAL0.35 Max BAL0.15 Max BAL0.15 Max BAL0.15 Max BAL0.05 Max BAL 铅锡铬铝0.30 Max0.20 Max BAL 0.10 Max0.10 Max BAL 0.05 Max0.05 Max BAL 0.10 Max0.05 Max BAL 0.10 Max0.05 Max BAL0.05 Max0.05 Max BAL0.10 Max0.10 Max BAL0.10 Max0.10 Max BAL0.10 Max0.05 Max BAL0.10 Max0.05 Max BAL0.10 Max0.10 Max BAL0.20 Max0.10 Max BAL0.10 Max0.05 Max BAL0.30 Max0.20 Max BAL0.10 Max0.05 Max BAL0.20 Max0.10 Max BAL0.20 Max0.10 Max BAL0.10 Max0.10 Max BAL0.10 Max0.10 Max BAL0.10 Max0.10 Max铅锡铬铝镉0.0050.003 3.5-4.30.0040.0050.003 3.5-4.30.0040.0050.003 3.5-4.30.0040.0030.001 3.5-4.30.0020.0060.0038.0-8.80.0060.0030.001Max 3.9-4.30.001Max0.0030.001Max 3.9-4.30.001Max0.0030.001Max 3.9-4.30.001Max0.015 Max 0.003Max 3.5-4.30.004Max0.015 Max 0.003Max 3.5-4.30.004Max0.015 Max 0.003Max 3.5-4.30.004Max。