.

Available Aluminum Alloy 3D Printing Spherical Powder Forgings Pipes Tubes Bars Plates Sheets Strips Wires Rods

Petrol Steel Co.,Ltd is a professional available aluminum alloy 3d printing spherical powder forgings pipes tubes bars plates sheets strips wires rods manufacturer supplying you with customized available aluminum alloy 3d printing spherical powder forgings pipes tubes bars plates sheets strips wires rods, welcome to wholesale products from our factory.Available Aluminum alloy 3D printing spherical powder Forgings pipes tubes bars plates sheets Strips wires RodsWe are leading manufacturer and stockiest of Aluminum alloy in China.Aluminum alloy 1000 / Aluminum Alloy 1050A Technical Data SheetAluminum alloy 1000 / Aluminum Alloy 1050A  Chemical Composition LimitsWeight%SiFeCuMnMgZnTiAlVOthers1050A EAA0.25 max0.40 max0.05 max0.05 max0.05 max0.07 max0.05 max99.5 min-0.031050 USA0.25 max0.40 max0.05 max0.05 max0.05 max0.05 max0.03 max99.5 min0.050.03Aluminum Alloy 1050 (1050A) is a popular grade of Aluminum. Alloy 1050 (1050A) is known for its excellent corrosion resistance, high ductility and highly reflective finish. Alloy 1050 (1050A) is typically used for chemical process plant equipment, food industry containers, pyrotechnic powder, architectural flashings, lamp reflectors, cable sheathing.Aluminum alloy 1000 / Aluminum Alloy 1050A Typical Mechanical PropertiesMaterialTemperTensile Strength (N/mm²)Yield Strength (N/mm²)Elongation in 50mm (%)1050 BarF60 (min)-23Aluminum Alloy 1050 A Tube is available the following size ranges.Outside Diameter - 0.25mm (0.010") up to 16.00mm (0.625")Wall - 0.05mm (0.002") up to 1.00mm (0.040")Straight Lengths - 1.00mm (0.040") up to 5000.00mm (197")Coils Lengths - 5 Meters to 15 MetersStandard Tolerance- OD &ID +/-0.03mm (0.0012")Wall +/- 10%Tight Tolerance - OD&ID +/- 0.015mm (0.0006")Wall +/-3%Some thin wall tubes up to 25.40 mm (1.000") can be supplied. Aluminum alloy 1000 / Aluminum Alloy 1050A SpecificationsUNS A91050BS - 1B and 5L36Australia - A1050French - A5Germany - 3.0255 - Al99.5Italy - UNI 9001/2Spain - L-3051Sweden - 4007Aluminum alloy 1000 / Aluminum Alloy 1080AAluminum alloy 1000 / Aluminum Alloy 1080A Technical Data SheetAluminum alloy 1000 / Aluminum Alloy 1080A Chemical Composition LimitsWeight%SiFeCuMnMgZnTiGaVOther eachAl1080 USA0.150.150.030.020.020.030.030.030.050.0299.801080 EAA0.150.150.030.020.020.060.020.03-0.0299.80Aluminum alloy 1000 / Aluminum Alloy 1080A SpecificationsBS 1AAl 99.8AWCO-99.8%Werkstoff Nr.3.0285BA 99.8%Duricilium-TA (99.8%)Star-99.8Aluminum alloy 1000 / Aluminum Alloy 1100Aluminum alloy 1000 / Aluminum Alloy 1100 Technical Data SheetAluminum alloy 1000 / Aluminum Alloy 1100 Chemical Composition LimitsWeight%AlCuSi + FeMnZnOthers1100Rem0.05 - 0.0200.95 max0.05 max0.10 max0.05 (each)      0.15 (total)Aluminum 1100 is a commercially pure aluminum. 1100 has excellent welding characteristics; it is also soft and ductile so is ideal for applications that require intricate forming as it work hardens slower than other alloys. 1100 is however non-heat treatable. As 1100 has excellent resistance to corrosion it is widely used in the chemical and food processing industries also for giftware and applications where eye appeal is important.Aluminum alloy 1000 / Aluminum Alloy 1100 Mechanical PropertiesMaterialTemperTensile Strength ksiYield Strength (ksi min)Elongation % in 2"0.064" SheetMin 90° Cold Bend Radius for .064 " Thick.53.HHH.1T11001100-H1822 (min)-41-2TAluminum alloy 1000 / Aluminum Alloy 1100 Specifications1100 - 0 SheetAMS 4001ASTM B 209QQ-A-250/11100 H-14 SheetAMS 4003ASTM B 209QQ-A-250/1Aluminum alloy 1000 / Aluminum Alloy 1200Aluminum alloy 1000 / Aluminum Alloy 1200 Technical Data SheetAluminum alloy 1000 / Aluminum Alloy 1200 Chemical Composition LimitsWeight%Si +FeCuMnAlZnTiOthers12001.0 max0.05 max0.05 max99.0 max0.10 max0.05 max0.05 (each)      0.15 (total)Aluminum 1200 is a very good atmospheric corrosion resistance and workability. Aluminum 1200 has a high thermal conductivity and reflectivity but lower than for 1050A, very good weldability which is slightly higher strength than 1050A.Aluminum alloy 1000 / Aluminum Alloy 1200 Mechanical PropertiesMaterial      Sheet, Strip, PlateTemperThickness (mm)Tensile Strength (N/mm²)Elongation in 50mm %    0.5mm0.8mm1.3mm2.6mm30mm1200F3.0 - 25.O0.2 - 6.070 - H120.2 - 6.H140.2 - 12.H160.2 - 6.H180.2 - 3.0140 (min)2344-Aluminum alloy 1000 / Aluminum Alloy 1200 SpecificationsSimilar Specifications:6L16, Alloy 1200 sheet and strip H14 or H246L17, Alloy 1200 sheet and strip O Temper5L34, Alloy 1200 Forging Stock and Forgings4L54, Alloy 1200 Tube Drawn Hydraulically testedL116, Alloy 1200 Tube DrawnBS 1CAl 99.0Alcoa-102BA 99.0%Duricilium-T (99.0%)Star-99.2Hiduminium-1C. The Aluminum alloy 1000 items which we can manufacture and supply are the followings.Aluminum alloy 1000 Rod3D printing spherical powder AluminumAluminum alloy 1000 RingsAluminum alloy 1000 ForgingsAluminum alloy 1000 pipeAluminum alloy 1000 tubeAluminum alloy 1000 barsAluminum alloy 1000 platesAluminum alloy 1000 sheetsAluminum alloy 1000 StripAluminum alloy 1000 wireAluminum alloy 1000 fitting UnionAluminum alloy 1000 Pipe ElbowsAluminum alloy 1000 PIPE TeeAluminum alloy 1000 ADAPTERSAluminum alloy 1000 pipe bendAluminum alloy 1000 reducersAluminum alloy 1000 fitting capsAluminum alloy 1000 pipe outletsAluminum alloy 1000 Stub EndsAluminum alloy 1000 CouplingsAluminum alloy 1000 pipe Nipples Aluminum alloy 1000 BUSHINGSAluminum alloy 1000 pipes socketsAluminum alloy 1000 Pipe GasketAluminum alloy 1000 pipe jointsAluminum alloy 1000 pipe CrossAluminum alloy 1000 Pipe WyesAluminum alloy 1000 seal ringAluminum alloy 1000 FlangeAluminum alloy 1000 boltsAluminum alloy 1000 nutsAluminum alloy 2000 / Aluminum Alloy 2011Aluminum alloy 2000 / Aluminum Alloy 2011 Technical Data SheetAluminum alloy 2000 / Aluminum 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)Aluminum 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 Aluminum machining. Alloy 2011 is used for screws, bolts, fittings, nuts, automatic lathe and screw machine products.Aluminum alloy 2000 / Aluminum Alloy 2011 Mechanical PropertiesMaterialTempsThickness (min)Tensile Strength (N/mm²) minYield Strength (N/mm²) minElongation on 50mm (%)2011 BarTD<10 BarTD BarTD BarTF<65 BarTF>652951958Aluminum alloy 2000 / Aluminum Alloy 2011 SpecificationsSimilar SpecificationsBS FC1Alcoa-800AWCO-308BA 308Durcilium-LHiduminium-39Decoltal-500QQ-A-225/3Aluminum alloy 2000 / Aluminum 2014A /2014 AluminumAluminum alloy 2000 / Aluminum 2014A /2014 Aluminum Technical Data Sheet Aluminum alloy 2000 / Aluminum 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 maxAluminum 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.Aluminum alloy 2000 / Aluminum 2014A /2014 Aluminum Mechanical PropertiesMaterialTemperThickness (mm)Tensile Strength min (N/mm²)Yield Strength min (N/mm²)Elongation in 50 mm     0.5 mm0.8 mm1.3 mm2.6 mm3.0 mm2014 SheetT4 Bare0.2-6. SheetT6 Bare0.2-6. SheetT4 Clad0.2-1. SheetT4 Clad1.6-6. SheetT6 Clad0.2-1. SheetT6 Clad1.6-6.MaterialTemperDiameter (mm)Tensile Strength min ((N/mm²)Yield Strength (min) (N/mm²)Elongation on 5.65 V (min)2014 BarT4<20 BarT BarT BarT BarT BarT BarTAluminum alloy 2000 / Aluminum 2014A /2014 Aluminum SpecificationsUNS A92014Werkstoff Nr. 3.1255Werkstoff Nr. 3.1254AMS 4028 Sheet and Plate - Alloy 2014 T0AMS 4029 Sheet and Plate - Alloy 2014 T651AMS 4121 Bars, Rods, Wire (rolled or cold finished) - Alloy 2014 T6AMS 4133 Forgings, Rolled Rings - Alloy 2014 T6AMS 4134 Die Forgings - Alloy 2014 T4AMS 4135 Superseded by 4133 Forgings, Rolled Rings - Alloy 2014 T6AMS 4153 Extrusions - Alloy 2014 T6BS 7L37 Rivet StockBS 3L63 TubeBS 2L77 Forging Stock T6 TemperBS 2L87 Bars and Sections T6 TemperBS 2L93 Plate Alloy 2014ABS L102 Bars and Sections T4 TemperBS L103 Forging Stock T4 TemperBS L105 Tube T4 Temper S07-1011, S07-1012BS L156 Sheet and Strip T4 TemperBS L157 Sheet and Strip T6 TemperBS L158 Sheet and Strip T4 Temper Close Tolerance.BS L159 Sheet and Strip T6 Temper Close Tolerance.BS L163 Clad Sheet and Strip T3 TemperBS L163 Clad Sheet and Strip T4 TemperBS L164 Clad Sheet and StripBS L165 Clad Sheet and Strip T6 TemperBS 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 T6511BS H15, HS15, HP15, HT15, HE15.AlCu4SiMgA-U4SGQQ-A-200/2QQ-A-225/4QQ-A-250/3DTD 5010, Alloy 2014ADTD 5030, DTD 5040 EN 2087EN 2088EN 2089 SHEETEN 2395 SHEETEN 2100 BAR T4511, EN 2634 BAR T4511EN 2324 BAR, EN 2639 BAR, EN 2384, EN2635 T6, T6511EN 2634 (with peripheral coarse grain control)EN 2639 (with peripheral coarse grain control)EN 2635 (with peripheral coarse grain control)AECMA 2387Aluminum alloy 2000 / Aluminum 2014A /2014 Aluminum Similar SpecificationBS H15Alcan GB-26SAWCO-305Birmetal-478BA 305 and BA 355Durcilium-KHiduminium-66Avional-660 and Avional-662BAEM 0039, BAEM 0128 and BAEM 0173MIL-A-12545 Aluminum alloy 2000 / Aluminum Alloy 2017AAluminum alloy 2000 / Aluminum Alloy 2017A Technical Data SheetAluminum alloy 2000 / Aluminum 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 maxAluminum 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.Aluminum alloy 2000 / Aluminum Alloy 2017A Mechanical PropertiesMaterialConditionTensile Strength (N/mm²) minYield StrengthElongation in 4D %  ksiMpaksiMpa 20172017-T4 BarAluminum alloy 2000 / Aluminum Alloy 2017A SpecificationsUNS A92017Werkstoff Nr. 3.1325ASTM B211 and ASTM B316FED QQ-A-225/5 Bar, Rod and WireFED QQ-A-430 Wire and RivetsAMS 4118 Bar, Rod and Wire 2017-T4 cold finishedAIR 9051AAluminum alloy 2000 / Aluminum Alloy 2024 (2024A)Aluminum alloy 2000 / Aluminum Alloy 2024 (2024A) Technical Data SheetAluminum alloy 2000 / Aluminum 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 maxRemAluminum 2024 (2024A) is one of the most popular high strength Aluminum 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.Aluminum alloy 2000 / Aluminum Alloy 2024 (2024A) SpecificationsAluminum alloy 2000 / Aluminum Alloy 2024 (2024A) SpecificationsExtrustions /Part NumbersBS 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 15-235-07MB Aluminum alloy 2000 / Aluminum Alloy 2031Aluminum alloy 2000 / Aluminum Alloy 2031 Technical Data SheetAluminum alloy 2000 / Aluminum 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 totalAluminum alloy 2000 / Aluminum Alloy 2031 Mechanical PropertiesMaterialTemperCondition of sampleSize of Bar (mm)Tensile Strength min (N/mm²)Yield Strength min (N/mm²)Elongation on 5.65v2031 ForgingsTBForged< ForgingsTBExtruded< ForgingsTFForged< ForgingsTFExtruded<2003852856Aluminum alloy 2000 / Aluminum Alloy 2031 SpecificationsBS H12Alcan GB-D15SBA 307Hiduminium-56Aluminum alloy 2000 / Aluminum Alloy 2219 (AMS 4162 / AMS 4094)Aluminum alloy 2000 / Aluminum Alloy 2219 Technical Data SheetAluminum alloy 2000 / Aluminum 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 total0.05-0.150.10-0.25Aluminum 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. Aluminum 2219 is typically used in a range of aerospace applications such as high temperature structural applications including space booster and fuel tanks.Aluminum alloy 2000 / Aluminum Alloy 2219 Mechanical PropertiesAluminum alloy 2000 / Aluminum Alloy 2219 - Bar / ExtrusionsMaterialTemperDirectionTensile Strength ksiYield Strength ksiElongation in 2" (%)2219 (AMS 4162)T8511L584262219 (AMS 4162)T8511LT56394Aluminum alloy 2000 / Aluminum 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"62467-8Aluminum alloy 2000 / Aluminum 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"58428Aluminum alloy 2000 / Aluminum Alloy 2219 SpecificationsAMS 4031 - 2219-0/F Sheet, PlateAMS 4066 - 2219-T8511 Drawn, Seamless TubingAMS 4068 - 2219-T3511 Drawn, Seamless TubingAMS 4094 - 2219 T81 Clad Sheet / T851 Clad PlateAMS 4095 - 2219 T31 Clad Sheet / T351 Clad PlateAMS 4096 - 2219-0 Clad Sheet / PlateAMS 4143 - 2219-T6 Forgings / Rolled or Forged RingsAMS 4144 - 2219-T852/T851 Hand ForgingsAMS 4162 - 2219-T8511 ExtrusionsAMS 4313 - 2219-T351/T352 Forgings/Rolled or forged ringsDMS1719 - 2219 T81 Alclad SheetQQ-A-250/30 - 2219 Bare Sheet, PlateQQ-A-367QQ-A-430MIL-A-22771MIL-A-46118ASTM B209ASTM B211ASTM B221 ASTM B241ASTM B316 Aluminum alloy 2000 / Aluminum Alloy 2618A (Aluminum 2618)Aluminum alloy 2000 / Aluminum Alloy 2618A Technical Data SheetAluminum alloy 2000 / Aluminum 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 maxMaterialSizeDiameter (mm)Tensile Strength min (N/mm²)Yield Strength min (N/mm²)Elongation in 50 mm %2618AExtruded Bar0.25"383510Alloy 6061 Bar - T651 / T6 condition and extruded T6511/T6 Aluminum alloy 6000 / Aluminum Alloy 6061 Specifications  BS L117 Alloy 6061 Tube Drawn T6   BS L118 Alloy 6061 Tube Drawn T6 Hydraulically Tested   H20  HE20 6061 Extrusions  HP20 6061 Plate  HS20 6061 Sheet  AMS 4009 6061-0 Foil   AMS 4021 6061-0 Alclad Sheet and Plate  AMS 4022 6061 Alclad Sheet and Plate Cancelled  AMS 4023 6061 Alclad Sheet and Plate Cancelled  AMS 4025 6061-0 Sheet and Plate  AMS 4026 6061-T4 Sheet T451 Plate  AMS 4027 6061-T6 Sheet and T651 Plate  AMS 4053 6061 Cancelled  AMS 4079 6061-0 Tube Drawn Seamless Close Tolerence   AMS 4080 6061-0 Tube Drawn Seamless  AMS 4081 6081-T4 Tube Drawn Seamless Hydraulic  AMS 4082 6061-T6 Tube Drawn Seamless  AMS 4083 6061-T6 Tube Drawn Seamless Hydraulic  AMS 4091 Superseded by AMS 4081  AMS 4092 Superseded by AMS 4082  AMS 4093 Superseded by AMS 4083  AMS 4113 6061-T6 Extruded shapes  AMS 4115 6061-0 Cold finished bars, rod, wire  AMS 4116 6061-T4 Cold finished bars, rod, wire  AMS 4117 6061-T6/T651 Cold finished bars, rod, wire  AMS 4127 6061-T6 Forgings Rolled or Forged   AMS 4128 6061-T451 Bars Rolled or Forged  AMS 4129 6061-T651 Superseded by 4117  AMS 4146 6061-T4 Forgings  AMS 4150 6061-T6 Extrusions and Rings  AMS 4160 6061-0 Extrusion   AMS 4161 6061-T4 Extrusion   AMS 4172 6061-T4511 Extrusion  AMS 4173 6061-T6511 Extrusion  QQ-A-200/8 6061-T6/T6511 Extruded bar, tube, section  QQ-A-200/16 6061-T6 extruded stuctural shapes   QQ-A-225/8 6061-T6 / T651 Cold finished bar, tube, section  QQ-A-250/11 6061 Sheet and Plate  WW-T-700/6 6061-T6 Seamless, drawn tube  MIL-T-7081 6061-T6 Hydraulic tube  QQ-A-367 6061 Forgings  WS 3.3211  WS 3.3214  EN 2392 6061-T6 Tube  EN 2694 6061-T6 Sheet, strip  EN 3341 6061-T4 Sheet, strip  EN 3342 6061-T4 Extruded bar  EN 3557   EN 4213 6061-T651 Plate  AWCO-22  Birmetal-016  BA22  Duricilium-Q  Hiduminium-43  LA 380  ABM 2-3023  ABM 2-3025  ABM 2-3026  ABS 5144  ABS 5151  BACM 123   BACM 171 6061-0 Tube  A-GSUC   L-3453  ASN-A-3277  NCT 15-238-01  AIR 9048.210 6061-0 Sheet  AIR 9048.220 6061-T4 Sheet  AIR 9048.230 6061-0 Sheet  AIR 9048.240 6061-T6 Sheet  AIR 9049 Aluminum alloy 7000 / Aluminum Alloy 7017Aluminum alloy 7000 / Aluminum Alloy 7017 Technical Data SheetAluminum alloy 7000 / Aluminum Alloy 7017 Chemical Composition LimitsWeight%AlSiFeCuMnCrMgZnTiZrOthersMn+Cr7017Bal0.35 max0.45 max0.20 max0.05-0.500.035 max2.0 - 3.04.0 - 5.20.15 max0.10-0.250.05 each      0.15 total0.15 minAluminum Alloy 7017 is a heat treatable alloy that age hardens naturally. Alloy 7017 is used in armoured vehiclesAluminum alloy 7000 / Aluminum Alloy 7020Aluminum alloy 7000 / Aluminum Alloy 7020 Chemical Composition LimitsWeight%AlSiFeCuMnCrMgZnZrZr + TiOther EachOthers Total7020Bal0.350.400.200.050 - 0.500.10 - 0.351.0-1.44.0 - 5.00.080 - 0.200.80 - 0.250.05 max0.15 maxAluminum Alloy 7020 is a heat treatable alloy that age hardens naturally and therefore will recover properties in a heat affected zone after welding. Alloy 7020 is used in armoured vehicles, military bridges, motor cycle and bicycle frames.Aluminum alloy 7000 / Aluminum Alloy 7020 Mechanical PropertiesMaterialTemperTensile Strength (MPa)Yield Strength (MPa)Elongation %Alloy 7020 PlateTProperties dependant on thicknessAluminum alloy 7000 / Aluminum Alloy 7020 Specifications  Similar Specifications:  BS H17  Alcan GB-D74S  BA 733  Hiduminium-45  EN AW - AlZn4,5Mg  WS 3.4335 Aluminum alloy 7000 / Aluminum Alloy 7050 (AMS 4050 / AMS 4342)Aluminum alloy 7000 / Aluminum Alloy 7050 Chemical Composition LimitsWeight%AlZrSiFeCuMnMgCrZnTiOther EachOthers Total7050 min87.30.08--2.0-1.9-5.7---7050 max90.30.150.120.152.60.102.60.046.70.060.050.15Aluminum alloy 7050 is an aerospace grade of Aluminum combining high strength, stress corrosion cracking resistance and toughness. It is particularly suited for heavy plate applications (3" to 6" thick) due to it's lower quench sensitivity and retention of strength in thicker sections. Aluminum 7050 therefore is the premium choice aerospace Aluminum for applications such as fuselage frames, bulkheads and wing skins.Aluminum 7050 plate is available in two tempers. T7651 (AMS 4201) combines the highest strength with good exfoliation corrosion resistance and average SCC resistance. T7451 (AMS 4050) provides better SCC resistance and excellent exfoliation resistance at slightly lower strength levels. Aircraft Materials can also supply 7050 in round bar with temper T74511 (AMS 4342).  Aluminum alloy 7000 / Aluminum Alloy 7050 Mechanical PropertiesMaterialTemperThicknessTensile Strength (ksi)Yield Strength (ksi)Elongation in 2" %Alloy 7050 Plate (longitudinal)T7451<2.0746410Alloy 7050 Plate (longitudinal)T74512.0 -3.073639Alloy 7050 Plate (longitudinal)T74513.0 - 4.072629Alloy 7050 Plate (longitudinal)T74514.0 - 5.071619Alloy 7050 Plate (longitudinal)T76510.25 - 1.076669Alloy 7050 Plate (longitudinal)T76511.0 - 1.577679Alloy 7050 Plate (longitudinal)T76511.5 - 2.076669Alloy 7050 Plate (longitudinal)T76512.0 - 3.076668MaterialTemperTensile Strength (ksi)Yield Strength (ksi)Elongation in 2" %Alloy 7050 Bar (AMS 4340)T7651179697Alloy 7050 Bar (AMS 4340)T7351170608Alloy 7050 Bar (AMS 4342)T7451173637Aluminum alloy 7000 / Aluminum Alloy 7050SpecificationsExtrustions /Part Numbers     AMS 4050: 7050-T7451 Plate      AMS 4107:7050-T74 Die Forging      AMS 4108:7050-T7452 Hand Forgings      AMS 4201: 7050-T7651 Plate      AMS 4333: 7050-T7452 Forgings      AMS 4340: 7050-T76511 Extrusions      AMS 4341: 7050-T73511 Extrusions      AMS 4342: 7050-T74511 Extrusions     BACT76511      BACT76511      BACT76511      BAC1518-940/7050T76511      BACT76511Aluminum alloy 7000 / Aluminum Alloy 7075Aluminum alloy 7000 / Aluminum Alloy 7075 Chemical Composition LimitsWeight%AlSiFeCuMnMgCrZnTiOther EachOthers Total7075 minRem--1.2-2.10.185.1---7075 maxRem0.400.502.00.302.90.286.10.200.050.15Aluminum Alloy 7075 offers the highest strength of the common screw machine alloys. The superior stress corrosion resistance of the T173 and T7351 tempers makes alloy 7075 a logical replacement for 2024, 2014 and 2017 in many of the most critical applications. The T6 and T651 tempers have fair machinability. Alloy 7075 is heavily utilized by the aircraft and ordnance industries because of its superior strength.Aluminum alloy 7000 / Aluminum Alloy 7075 Mechanical PropertiesMaterialTemperSize (")Tensile Strength (ksi)Yield Strength (ksi)Elongation in 2" %Alloy 7075 BarT651-77667Alloy 7075 BarT7351<4"685610Alloy 7075 BarT73511<0.2568587Alloy 7075 BarT735110.25 - 1.570618Alloy 7075 BarT735111.5 - 3.069598Alloy 7075 BarT6511<0.2578707Alloy 7075 BarT65110.25 - 0.581737Alloy 7075 BarT65110.5 - 3.081727MaterialTemperThickness (in)Tensile Strength (ksi)Yield Strength (ksi)Elongation %Alloy 7075 SheetT6 Bare0.125 - 0.2578698Alloy 7075 SheetT651 Bare0.25 - 0.5078679Alloy 7075 SheetT651 Bare0.5 - 1.078687Alloy 7075 SheetT6 Clad0.188 - 0.2575648Alloy 7075 SheetT651 Clad0.25 - 0.5075659Alloy 7075 SheetT651 Clad0.5 - 1.0078687Aluminum alloy 7000 / Aluminum Alloy 7075 Physical PropertiesCharacteristicEnglishMetricNominal Density (68° F / 20°C)0.101 lbs./ in ³2.80 Mg/m³Melting Range990° F - 1175° F532°C - 635 °CSpecific Heat (212 °F / 100°C0.23 BTU/lb - °F960 J/kg-°KSAluminum alloy 7000 / Aluminum Alloy 7075 pecificationsExtrustions /Part NumbersBS 2 L95 Alloy 7075-T651 Plate      BS 2 L88 Alloy 7075-T6 Clad Sheet and Strip      BS L160 Alloy 7075-T73511 Bars and Sections      BS L161 Alloy 7075 Forging Stock and Forgings      BS L162 Alloy 7075 Forging Stock and Forgings      BS L170 Alloy 7075-T6511 Bars and Sections      DTD 5110 7075 Clad Plate      DTD 5124 7075 Bars and Sections      AMS 4038 7075-T651 Superseded by AMS 4045      AMS 4039 7075-T651 Superseded by AMS 4049      AMS 4044 7075 -0 Sheet and Plate      AMS 4045 7075-T6 Sheet and T651 Plate      AMS 4046 7075-T6 Alclad one side Sheet, T651 Plate      AMS 4048 7075-T0 Alclad Sheet and Plate      AMS 4049 7075 -T6 Alclad Sheet and T651 Plate      AMS 4078 7075-T351 Plate      AMS 4122 7075-T6 Cold finished rod, bar, wire      AMS 4123 7075-T651 Cold finished bar, rod      AMS 4124 7075-T7351 Cold finished bar, rod, wire      AMS 4126 7075-T6 Forgings      AMS 4131 7075-T74 Forgings      AMS 4139 7075 Forgings (Non-Current)      AMS 4141 7075-T73 Die Forgings      AMS 4147 7075-T7352 Forgings      AMS 4154 7075-T6 Extrusions      AMS 4166 7075-T73 Extrusion      AMS 4167 7075-T73511 Extrusions      AMS 4168 7075-T6511 Extrusions Unstraightened      AMS 4169 7075-T6511 Extrusions Straightened      AMS 4174 7075-T73 Flash Welded Rings      AMS 4186 7075-TF Cold finished bar, rod, wire      AMS 4187 7075-0 Cold finished bar, rod, wire      QQ-A-250/13 7075-0 Alclad sheet and plate      QQ-A-250/13 7075-T6 Alclad sheet and plate      QQ-A-250/18 7075-0 Clad one side, sheet and plate      QQ-A-250/18 7075-T6 Clad one side, sheet and plate      QQ-A-250/24 7075-T7651 Plate      QQ-A-250/25 7075 Sheet, clad with7072-T76      QQ-A-250/26 7075 Sheet, clad with7011-T76      QQ-A-367 Alloy 7075-T6 Forgings      MIL-A-22771      AIR 9048.690 7075-T7351 Plate      AIR 9048.700 7075-T7351 Plate      AIR 9048.710 7075-T7351 Plate      AIR 9049AND10133-1401/7075T6511      AND10134-1006/7075T73511      AND10136-2001/7075T3511      AND10136-2401/7075T6511      ANDT73511      AND10136-2404/7075T6511      AND10136-2407/7075T6511      AND10136-3004/7075T73511      AND10138-0604/7075T6511      BACT6      BACT6      BACT6      BACT62      BACT6      BACT62      BACT6      BACT6      BACT62      BACT62      BACT6      BACT6511      BACT6511      BACT6511      BAC      BACT6511      BACT6511      BACT6511      BACT6511      BACT6511      BACT6511      BACT6      BACT73511      BAC1518-940/7075T6511      BACT73511      BACT65ONE OF THE KIND, MILLIONS OF CHOICESSUPERIOR QUALITYPROMPT DELIVERYFAVORABLE FEEDBACKALL AVAILABLE IN PESCOSELECT PESCO, YOU WILL BE RIGHTFor more info and price of Aluminum alloy, please send us inquiry and you will have quick reply soon.


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