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bang Aluminum Alloys: 1xxx-8xxx series

wuxi xsx baS Hap 'u' co., Ltd | Updated: Feb 20, 2017

铝棒.jpgnIt aluminum tun relatively. overcome, laH alloyed baS je latlh baS (alloying elements). alloyed HochHom aluminum marketplace SIch je latlh qaSlaH wa' element. depending on elements tuj treatment 'ej alloying, tev Sar bang, vo' QaQ Hoch, fabrication, resistance QaQ corrosion, ease ratio HoS--ngI' jen, QaQ weldability 'ej jen fracture toughness laH exhibit aluminum alloy series. ultimately wuv selection proper alloy series application nIS 'ej je Qap.

Series 1xxx Alloy aluminum

Series (1050, 1060, 1100, 1145, 1200, 1230, 1350 etc.) pagh alloy elements ngaS. proportion aluminum 99.3 – 99.9 vatlhvI' 'ej Dumerbe' meqchaj pong tiny impurities.1xxxare, ghogh pov corrosion resistance, jen thermal 'ej electrical conductivities, mechanicalproperties 'eS, je pov workability Sagh pujchoH SoQDaj. QI'yaH-hardenable alloys qel 'op tensile strengths 40 – 60 mpa Hap 'u' series. chaq Suq moderate ghur qaStaHvIS HoS pong strain hardening, Sut HabmoHwI' silicon 'ej impurities chaH Dapon 'e' yI.


Series 2xxx Alloy aluminum

aluminum tlhe' alloys (2011, 2014, 2017, 2018, 2124, 2219, 2319, 201.0 tI 203.0 tI 206.0 tI 224.0 tI 242.0 etc.) 'elbogh alloy element copper. alloys series jen HoS alloys. chav optimum bang such as "HoS" pong tuj treatment mIw. tensile HoS ghot tu'lu'. mej 400 mpa completion hardening.

qaStaHvIS taS heat-treat je, nagh 'ej rut nuv 'eS-carbon yoDSutlIj naQ exceed, bang mechanical. qaStaHvIS 'op instances employed precipitation tuj treatment (aging) qaStaHvIS mechanical bang ghur. jegh HoS, ghaH toy'wI'pu' loss neH elongation ghur treatment; 'e' 'angbogh Da tensile HoS 'oHbe' Hoch Dun.

wej ghaj aluminum alloys neH 2xxx series je QaQ corrosion resistance je alloys aluminum 'ach latlh 'ej bopummeH be je chaq subject to intergranular corrosion. aluminum grades 2xxx series neH QaQ QaQ HoS DeSDu' Hat poQ 'ay' Da'elDI' 150 ° [taH (300 ° f). except for ngoq 2219, weldability vuS aluminum tlhe' alloys 'ach machinability nIv ghaj series alloys 'op. alloy rav Qat 'ej commonly lo' neH aircraft construction ngoq 2024.


Series 3xxx Alloy aluminum

aluminum tlhe' alloys (3003, 3004, 3105, 383.0 tI 385.0; A360; 390.0) potlhmo' elementis manganese alloying, generally ghot tu'lu'. mej 20 vatlhvI' 'ach chaq QI'yaH-tuj treatable latlh HoS law' 1xxx series aluminum alloys. SeH laH effectively chel neH vuS Sut chu' manganese (Sovbe'bogh rur ghot tu'lu'. mej 1.5 vatlhvI') aluminum, lo' manganese je chaH Dapon 'e' yI element, qaStaHvIS neH puS alloys.


Series 4xxx Alloy aluminum

chaH Dapon 'e' yI alloy element neH 4xxx series alloys (4032, 4043, 4145, 4643 etc.) silicon, baS laH chel qaStaHvIS yap quantities (Da'elDI' 12 vatlhvI') substantial ghuS tet range luH. meq lo' aluminum-silicon alloys reH welding wire 'ej aluminum, muv, nuqDaq ghuS tet range puS DotlhDaj waw' baS poQlu' alloys brazing. aluminum alloys appreciable amounts silicon Sev moj Hurgh qIj 'ej wov charcoal applied 'ej yIDoH Ha' neH poQ architectural applications anodic oxide rIn.


Series 5xxx Alloy aluminum

chaH Dapon 'e' yI alloy element magnesium; HeghDI' ngat je chaH Dapon 'e' yI alloy element pagh je manganese wa'DIch ghot'e' DeghwI' moderate--jenwI'-HoS Qap-hardenable alloy. magnesium considerably vI'Iprup vaQ puS manganese je hardener – ghot tu'lu'. mej 0.8 vatlhvI' laH chel mg equal 1.25 vatlhvI' mn – 'ej 'oH neH considerably veb quantities. aluminum alloys neH series (5005, 5052, 5083, 5086, etc.) QaQ weld characteristics 'ej relatively QaQ resistance corrosion marine muD seawater 'ej ghaj

'ach limitations vaj lan bIr Qap 'ej, Qap Hat (150 ° f) amount permissible veb-magnesium aluminum alloys susceptibility stress-corrosion cracking webqu'meH nov.


Series 6xxx Alloy aluminum

aluminum alloys neH 6xxx series (6061, 6063) silicon magnesium approximately neH proportions poQ formation magnesium silicide (mg2si), vaj chaHvaD tuj chenmoH treatable je ngaS. naH jajmeymaj HoS Hoch QaQ formability, weldability, machinability, relatively QaQ corrosion resistance, medium HoS je je HochHom 2xxx 7xxx 'ej alloys, 6xxx series aluminum alloys. chaq qaStaHvIS t4: HoSnIS (taS tuj treated 'ach not precipitation tuj treated) Dumerbe' 'ej rach qaSpu'DI' Dumerbe' bang t6 naQ pong precipitation tuj treatment aluminum grades neH heat-treatable ghom.


Series 7xxx Alloy aluminum

zinc. ghaH qaStaHvIS 1 8 vatlhvI' amounts chaH Dapon 'e' yI alloy element neH 7xxx series aluminum alloys (7075, 7050, 7049, 710.0 tI 711.0 etc.), 'ej ghaH smaller Sut chu' magnesium ghot'e' qaStaHvIS heat-treatable alloys moderate vInoH jen HoS coupled. 600 mpa qaStaHvIS 'op cases chaq exceed tensile strengths ranging SabtaHbogh 450 – 500 mpa. alloys prone corrosion, stress especially HeghDI' welded.

motlh je chel latlh elements, such as copper chromium, 'ej pa' mach quantities. lo' 7xxx series alloys airframe tlham, mobile luch, latlh highly stress 'ay' je. reduce resistance corrosion pe'vIl vaj pumDI' qoghlIj stress exhibit 'ej pIj utilized neH loQ overage: HoSnIS Dunmo' combinations HoS, corrosion resistance, fracture toughness 'ej DuHIvDI' veb HoS 7xxx aluminum alloys.


Series 8xxx Alloy aluminum

8xxx series (8006 tI 8111 tI 8079 tI 850.0 tI 851.0 tI 852.0) qen, Hatlh yoS nuv yIlo' series 2xxx 7xxx elements alloying reserve. rewbe'mey'e' ngat tuj-sink jan, yuvtlhe' stock, aluminium oSrIq, 'ej ngaj. DanoHmeH HoS Hutlh tera'Daq veQ loss ghur qaStaHvIS electrical conductivity, 'ej vaj lI' neH qabwIj conductor alloys je 8017 Sut HabmoHwI' nickel. Hach aluminum-lithium alloy 8090, baS exceptionally jen HoS stiffness je, aerospace applications. correspond aluminum alloys neH 8000 series Unified mI' pat a98xxx etc.

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