Aluminium 2000

We are leading manufacturer and stockist of Aluminium 2000 in China.Aluminium 2000 / Aluminium Alloy 2011 Aluminium 2000 / Aluminium Alloy 2011 Technical Data SheetAluminium 2000 / Aluminium Alloy 2011 Chemical Composition LimitsWeight%AlSiFeCuZnBiPbOthers2011Bal0.40 max0.70 max5.0-6.00.30 max0.20-0.600.20-0.600.05 (each)      0.15 (total)Aluminium 2011 is a heat treatable high strength alloy with high fatigue strength and excellent free machining characteristics. Due to the high copper content of Alloy 2011 makes it the best choice for aluminium machining. Alloy 2011 is used for screws,Website:http://www.petrosteels.com, bolts, fittings, nuts, automatic lathe and screw machine products.Aluminium 2000 / Aluminium Alloy 2011 Mechanical PropertiesMaterialTempsThickness (min)Tensile Strength (N/mm²) minYield Strength (N/mm²) minElongation on 50mm (%)2011 BarTD<1031025562011 BarTD10-3531025582011 BarTD35-5029523082011 BarTF<6531022582011 BarTF>652951958Aluminium 2000 / Aluminium Alloy 2011 Specifications  Similar Specifications  BS FC1  Alcoa-800  AWCO-308  BA 308  Durcilium-L  Hiduminium-39  Decoltal-500  QQ-A-225/3Aluminium 2000 / Aluminium 2014A /2014 Aluminum Aluminium 2000 / Aluminium 2014A /2014 Aluminum Technical Data SheetAluminium 2000 / Aluminium 2014A /2014 Aluminum Chemical Composition LimitsWeight%AlSiFeCuMnCrMgNiZnTi+ZrTiOther EachOther Total2014a AECMARem0.50 - 0.900.50 max3.9 - 5.00.4-1.20.10 max0.2-0.80.1 max0.25 max0.20 max0.15 max0.05 max0.15 max2014 USARem0.50-1.200.7 max3.9 - 5.00.4 - 1.20.10 max0.2-0.8-0.25 max-0.15 max0.05 max0.15 maxAluminium Alloy 2014 (2014 A) is a copper based alloy with very high strength together with excellent machining characteristics. Alloy 2014 is commonly used in many aerospace structural applications due to its high strength. Other applications include military vehicles, bridges, weapons manufacture and structural applications.Aluminium 2000 / Aluminium 2014A /2014 Aluminum Mechanical PropertiesMaterialTemperThickness (mm)Tensile Strength min (N/mm²)Yield Strength min (N/mm²)Elongation in 50 mm0.5 mm0.8 mm1.3 mm2.6 mm3.0 mm2014 SheetT4 Bare0.2-6.040022513141414142014 SheetT6 Bare0.2-6.0440380667782014 SheetT4 Clad0.2-1.6385240131414--2014 SheetT4 Clad1.6-6.0395245---14142014 SheetT6 Clad0.2-1.6420345778--2014 SheetT6 Clad1.6-6.0420355---99MaterialTemperDiameter (mm)Tensile Strength min ((N/mm²)Yield Strength (min) (N/mm²)Elongation on 5.65 V (min)2014 BarT4<20370230112014 BarT420-75390250112014 BarT475-15039025092014 BarT4150-20037023082014 BarT651020-7548043572014 BarT651075-15046542072014 BarT6510150-2004353907Aluminium 2000 / Aluminium 2014A /2014 Aluminum Specifications UNS A92014  Werkstoff Nr. 3.1255  Werkstoff Nr. 3.1254  AMS 4028 Sheet and Plate - Alloy 2014 T0  AMS 4029 Sheet and Plate - Alloy 2014 T651  AMS 4121 Bars, Rods, Wire (rolled or cold finished) - Alloy 2014 T6  AMS 4133 Forgings, Rolled Rings - Alloy 2014 T6  AMS 4134 Die Forgings - Alloy 2014 T4  AMS 4135 Superseded by 4133 Forgings, Rolled Rings - Alloy 2014 T6  AMS 4153 Extrusions - Alloy 2014 T6  BS 7L37 Rivet Stock  BS 3L63 Tube  BS 2L77 Forging Stock T6 Temper  BS 2L87 Bars and Sections T6 Temper  BS 2L93 Plate Alloy 2014A  BS L102 Bars and Sections T4 Temper  BS L103 Forging Stock T4 Temper  BS L105 Tube T4 Temper S07-1011, S07-1012  BS L156 Sheet and Strip T4 Temper  BS L157 Sheet and Strip T6 Temper  BS L158 Sheet and Strip T4 Temper Close Tolerance.  BS L159 Sheet and Strip T6 Temper Close Tolerance.  BS L163 Clad Sheet and Strip T3 Temper  BS L163 Clad Sheet and Strip T4 Temper  BS L164 Clad Sheet and Strip  BS L165 Clad Sheet and Strip T6 Temper  BS L166 Clad Sheet and Strip T4 Temper Close Tolerance.  BS L167 Clad Sheet and Strip T6 Temper close Tolerance.  BS L168 Bars and Sections T6, T6510 and T6511  BS H15, HS15, HP15, HT15, HE15.  AlCu4SiMg  A-U4SG  QQ-A-200/2  QQ-A-225/4  QQ-A-250/3  DTD 5010, Alloy 2014A  DTD 5030, DTD 5040  EN 2087  EN 2088  EN 2089 SHEET  EN 2395 SHEET  EN 2100 BAR T4511, EN 2634 BAR T4511  EN 2324 BAR, EN 2639 BAR, EN 2384, EN2635 T6, T6511  EN 2634 (with peripheral coarse grain control)  EN 2639 (with peripheral coarse grain control)  EN 2635 (with peripheral coarse grain control)  AECMA 2387Aluminium 2000 / Aluminium 2014A /2014 Aluminum Similar Specification  BS H15  Alcan GB-26S  AWCO-305  Birmetal-478  BA 305 and BA 355  Durcilium-K  Hiduminium-66  Avional-660 and Avional-662  BAEM 0039, BAEM 0128 and BAEM 0173  MIL-A-12545 Aluminium 2000 / Aluminium Alloy 2017A Aluminium 2000 / Aluminium Alloy 2017A Technical Data SheetAluminium 2000 / Aluminium Alloy 2017A Chemical Composition LimitsWeight%AlSiFeCuMnMgCrZnTiOthers EachOther Total2017 USARem0.20-0.80.7 max3.5-4.50.40-1.00.40-0.80.10 max0.25 max0.15 max0.05 max0.15 maxWeight%AlSiFeCuMnMgCrZnZr + TiOthers EachOther Total2017A EAARem0.20-0.80.7 max3.5-4.50.40-1.00.40-1.00.10 max0.25 max0.25 max0.05 max0.15 maxAluminium Alloy 2017 (2017 A) has high strength with excellent fatigue strength. Alloy 2017 also has very good machining characteristics. It is suitable for welding only by resistance welding. Alloy 2017 (2017 A) is used for various applications from high strength structural components, aircraft, machine construction, military equipment, rivets.Aluminium 2000 / Aluminium Alloy 2017A Mechanical PropertiesMaterialConditionTensile Strength (N/mm²) minYield StrengthElongation in 4D %ksiMpaksiMpa20172017-T4 Bar553793222112Aluminium 2000 / Aluminium Alloy 2017A Specifications  UNS A92017  Werkstoff Nr. 3.1325  ASTM B211 and ASTM B316  FED QQ-A-225/5 Bar, Rod and Wire  FED QQ-A-430 Wire and Rivets  AMS 4118 Bar, Rod and Wire 2017-T4 cold finished  AIR 9051AAluminium 2000 / Aluminium Alloy 2024 (2024A) Aluminium 2000 / Aluminium Alloy 2024 (2024A) Technical Data SheetAluminium 2000 / Aluminium Alloy 2024 (2024A) Chemical Composition LimitsWeight%SiFeCuMnMgCrZnTiOther EachOther TotalAl2024 USA0.50 max0.50 max3.8-4.90.3-0.91.2-1.80.10 max0.25 max0.15 max0.05 max0.15 maxRem2024A France0.15 max0.20 max3.7-4.50.15-0.81.2-1.50.10 max0.25 max0.15 max0.05 max0.15 maxRemAluminium 2024 (2024A) is one of the most popular high strength Aluminium alloys when it is the heat treated condition. Due to 2024 (2024A) high strength and excellent fatigue resistance it is commonly used on structures and components in the aircraft and transportation industries. Aluminium 2000 / Aluminium Alloy 2024 (2024A) SpecificationsAluminium 2000 / Aluminium Alloy 2024 (2024A) SpecificationsExtrustions /Part Numbers     BS L97 Plate T351      BS L98 Plate T4      BS L109 Clad Sheet T4      BS L110 Clad Sheet T42      DTD 5100      WS 3.1354, BARE      WS 3.1364, ALCLAD      WS 3.1355      AMS 4033 Plate T351      AMS 4034 Plate Clad T351      AMS 4035 Sheet T0      AMS 4036 Sheet T3 Clad One Side, Plate T351      AMS 4037 Sheet T3, Plate T351      AMS 4040 Sheet T0 Clad      AMS 4041 Sheet T3 and T351 Clad Plate      AMS 4088 Tube T3 Drawn      AMS 4112 Wire rod / Bar Cold Finished T6      AMS 4119 Wire rod / Bar Cold Finished T351      AMS 4120 Wire rod / Bar Cold Finished T4      AMS 4152 Extruded Wire / Rod / Bar / Shapes T3      AMS 4165 Extruded Wire / Rod / Bar / Shapes T3511      FED QQ-A200/3      FED QQ-A225/6      FED QQ-A 250/4 SHEET      FED QQ-A 250/5 CLAD SHEET      MIL-T-50777 Seamless Tube      MIL-A-81596 Foil      QQ-A-200/3 2024 Extruded Rod, Bar, Shapes, tube and Wire      QQ-A-225/6 2024 Rolled, Drawn, Cold Finished Wire Rod and Bar      QQ-A-250/4 2024 Sheet and Plate O , T351, T851      QQ-A-250/5 2024 Alclad Sheet and Plate O, T3.      WW-T-700/3 2024 Drawn Seamless Tube      British Aerospace S071009      AIRBUS - ABM1-1005      BAEM 0145 and BAEM 0172      AIR 9048.630      AIR 9048.100      AIR 9048.110      AIR 9048.120      AIR 9048.130 Clad Sheet      AIR 9048.140 Clad Sheet      AIR 9049      AIR 9051A      AECMA 2710      EN 4101 T4 FORMING QUALITY      EN 2090 CLAD SHEET      EN 2091 CLAD SHEET      EN 2419 T351      EN2321 BAR      EN2318 BAR      EN 2638 (with peripheral coarse grain control)      EN 2633 (with peripheral coarse grain control)      EN 2703 CLAD SHEET      EN 3447 (with peripheral coarse grain control)      EN 3474      EN 3550 BAR      EN 3997      EN 3998      EN 3999      EN 4001 CLAD SHEET      EN 4101      EN 6000      ASN-A-3001 T351      ASN-A 3010 SHEET      ASN-A 3012      ASN-A 3058 Bar      ASN-A 3351      ASN-A 3048      CCT LA279      NCT 10-235-03MD      NCT 15-235-06MB      NCT 15-235-07MBAluminium 2000 / Aluminium Alloy 2031 Aluminium 2000 / Aluminium Alloy 2031 Technical Data SheetAluminium 2000 / Aluminium Alloy 2031 Chemical Composition LimitsWeight%SiFeCuMnMgNiZnTiOthers20310.50 / 1.30.60 / 1.21.8 / 2.80.50 max0.6 / 1.20.6 / 1.40.20 max0.20 max0.05 each      0.15 totalAluminium 2000 / Aluminium Alloy 2031 Mechanical PropertiesMaterialTemperCondition of sampleSize of Bar (mm)Tensile Strength min (N/mm²)Yield Strength min (N/mm²)Elongation on 5.65v2031 ForgingsTBForged<150310160132031 ForgingsTBExtruded<200310145132031 ForgingsTFForged<15038530062031 ForgingsTFExtruded<2003852856Aluminium 2000 / Aluminium Alloy 2031 Specifications  BS H12  Alcan GB-D15S  BA 307  Hiduminium-56Aluminium 2000 / Aluminium Alloy 2219 (AMS 4162 / AMS 4094) Aluminium 2000 / Aluminium Alloy 2219 Technical Data SheetAluminium 2000 / Aluminium Alloy 2219 Chemical Composition LimitsWeight%AlSiFeCuMnMgZnTiOthersVZn2219Bal0.20 max0.30 max5.80-6.800.20-0.400.02 max0.10 max0.02-0.100.050 each      0.15 total0.05-0.150.10-0.25Aluminium Alloy 2219 is a high strength alloy which combines good machinability and good mechanical properties. 2219 is useful over a temperature range of -452°F to 600°F, is readily weldable and has good fracture toughness. In the T8 condition it is resistant to stress corrosion cracking. Aluminium 2219 is typically used in a range of aerospace applications such as high temperature structural applications including space booster and fuel tanks.Aluminium 2000 / Aluminium Alloy 2219 Mechanical Properties Aluminium 2000 / Aluminium Alloy 2219 - Bar / ExtrusionsMaterialTemperDirectionTensile Strength ksiYield Strength ksiElongation in 2" (%)2219 (AMS 4162)T8511L584262219 (AMS 4162)T8511LT56394Aluminium 2000 / Aluminium Alloy 2219 - Sheet / Plater (Bare)MaterialTemperThicknessTensile Strength ksiYield Strength ksiElongation in 2" (%)2219 (QQ-A-250/30)00.020"-2.0032 max16 max122219 (QQ-A-250/30)T3510.250" - 2.00"4628102219 (QQ-A-250/30)T8510.250" - 2.00"62467-8Aluminium 2000 / Aluminium Alloy 2219- Sheet / Plater (Clad) Temper T81 / T851MaterialTemperThicknessTensile Strength ksiYield Strength ksiElongation in 2" (%)2219 (AMS 4094)T81/ T8510.020"-0.039"493762219 (AMS 4094)T81/ T8510.039"-0.099"554172219 (AMS 4094)T81/ T8510.099"-0.249"584372219 (AMS 4094)T81/ T8510.245"-0.499"58428Aluminium 2000 / Aluminium Alloy 2219 Specifications  AMS 4031 - 2219-0/F Sheet, Plate  AMS 4066 - 2219-T8511 Drawn, Seamless Tubing  AMS 4068 - 2219-T3511 Drawn, Seamless Tubing  AMS 4094 - 2219 T81 Clad Sheet / T851 Clad Plate  AMS 4095 - 2219 T31 Clad Sheet / T351 Clad Plate  AMS 4096 - 2219-0 Clad Sheet / Plate  AMS 4143 - 2219-T6 Forgings / Rolled or Forged Rings  AMS 4144 - 2219-T852/T851 Hand Forgings  AMS 4162 - 2219-T8511 Extrusions  AMS 4313 - 2219-T351/T352 Forgings/Rolled or forged rings  DMS1719 - 2219 T81 Alclad Sheet  QQ-A-250/30 - 2219 Bare Sheet, Plate  QQ-A-367  QQ-A-430  MIL-A-22771  MIL-A-46118  ASTM B209  ASTM B211  ASTM B221  ASTM B241  ASTM B316Aluminium 2000 / Aluminium Alloy 2618A (Aluminum 2618) Aluminium 2000 / Aluminium Alloy 2618A Technical Data SheetAluminium 2000 / Aluminium Alloy 2618A Chemical Composition LimitsWeight%AlSiFeCuMnMgNiZnTiZr + TiOther EachOthers Total2618 USARem0.10-0.250.9-1.31.9-2.7-1.3-1.80.9-1.20.10 max0.04-0.10-0.05 max0.15 max2618A EAARem0.15-0.250.9-1.41.8-2.70.25 max1.2-1.80.8-1.40.15 max0.20 max0.25 max0.05 max0.15 maxAluminium Alloy 2618A (Aluminum 2618) is a high strength aluminium alloy which contains both copper and magnesium. Alloy 2618 (2618A) has good machinability and is fair resistance to atmospheric attack. Aluminium Alloy 2618A (Aluminum 2618) is typically used in aerospace and defence components. It is commonly used for pistons and rotating aircraft parts due to it's ability to work in higher temperature applications. 2618 is also used in high performance autosport applications.Aluminium 2000 / Aluminium Alloy 2618A Mechanical PropertiesMaterialSizeDiameter (mm)Tensile Strength min (N/mm²)Yield Strength min (N/mm²)Elongation in 50 mm %2618AExtruded Bar<1040032052618Extruded Bar10-1004203407Aluminium 2000 / Aluminium Alloy 2618A Specifications  DTD 717A T6 Forging Stock and Forgings  DTD 731B T6 Forging Stock and Forgings  DTD 745A T6 Forging Stock and Forgings  DTD 5070B Clad Sheet and Strip (DTD5070)  DTD 5014 A Bars and Sections (DTD5014)  DTD 5084A T6 Forging Stock and Forgings  MSRR 8018  MSRR 8016 Plate  BS Pre-1980 H16  CM001-1 T6  CM001-3 H28  Hiduminium 58  GB-D19S  SO7-1103 (S07-1103)  A-U2GN  UNI 9002/6  L-3171  AIRBUS - ABM1-1006  BAEM 1101 and BAEM 1103  MM 0531  AIR 9048.640 T351, T851  AIR 9051A  AIR 9048.150  AIR 9048.170 CLAD SHEET  AIR 9048.640  Werkstoff Nr. 3.1924 T651  AECMA  EN 2123 T351, T851  EN 3553 T6511 BAR  ASN-A-3355  ASN-A-3357  CCT LA 767 The Aluminium 2000 items which we can manufacture and supply are the followings.  Aluminium 2000 Rod  Aluminium 2000 Rings  Aluminium 2000 Forgings  Aluminium 2000 pipe  Aluminium 2000 tube  Aluminium 2000 bars  Aluminium 2000 plates  Aluminium 2000 sheets  Aluminium 2000 Strip  Aluminium 2000 wire  Aluminium 2000 fitting Union  Aluminium 2000 Pipe Elbows  Aluminium 2000 PIPE Tee  Aluminium 2000 ADAPTERS  Aluminium 2000 pipe bend  Aluminium 2000 reducers  Aluminium 2000 fitting caps  Aluminium 2000 pipe outlets  Aluminium 2000 Stub Ends  Aluminium 2000 Couplings  Aluminium 2000 pipe Nipples  Aluminium 2000 BUSHINGS  Aluminium 2000 pipes sockets  Aluminium 2000 Pipe Gasket  Aluminium 2000 pipe joints  Aluminium 2000 pipe Cross  Aluminium 2000 Pipe Wyes  Aluminium 2000 seal ring  Aluminium 2000 Flange  Aluminium 2000 bolts  Aluminium 2000 nutsONE OF THE KIND, MILLIONS OF CHOICES SUPERIOR QUALITY PROMPT DELIVERY FAVORABLE FEEDBACK ALL AVAILABLE IN PESCO SELECT PESCO, YOU WILL BE RIGHT For more info and price of Aluminium 2000, please send us inquiry and you will have quick reply soon.


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