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The T4 condition allows 6013 aluminum to be formed and demonstrates better stretch forming characteristics. The part can then be aged to the T6 condition without costly heat
contact2013425 · Aluminium / aluminum is a silverish white metal that is known for its versatility. Aluminium / aluminum can be combined with one of these elements – silicon,
contact2020530 · A96013) Aluminum. 6013 aluminum is a 6000-series aluminum alloy: there is significant alloying with both magnesium and silicon, and the alloy is formulated for
contactHigh-Strength 6013 Aluminum Sheets. Yield Strength: 50, 000 psi. Hardness: Brinell 120 (Medium) Temper: T651. Fabrication: Hot Rolled. As the strongest multipurpose
contact2020530 · 6013-T6 Aluminum. 6013-T6 aluminum is 6013 aluminum in the T6 temper. To achieve this temper, the metal is solution heat-treated and artificially aged
contactAluminum 6013-T651. General 6013 characteristics and uses: High strength and good corrosion resistance. Easily joined by all welding and brazing methods. Excellent
contact200951 · In this study T6 heat treatment is applied to Aluminium 6013 sheet and this sheet joined by using FSW technique. Tensile specimens were machined from the welded plate in the dimension of A0 = 12.5 ...
contact1 · The ultimate strength for 6063 aluminum alloy is 241 MPa (35,000 psi). Shear strength measures the maximum amount of shearing stress a material can undergo
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contact2022125 · Because of its high strength and good fracture toughness, 6013 aluminum alloy is widely used in auto and aircraft parts, such as the outer hood, outer decklid, and outer fuselage skin. An aluminum alloy must have good plastic forming ability in forming auto and aircraft parts and must have high deformation resistance in service. These
contact2013425 · Aluminium / aluminum is a silverish white metal that is known for its versatility. Aluminium / aluminum can be combined with one of these elements – silicon, magnesium, manganese, copper, and zinc, to form aluminium / aluminum alloys. Aluminium / aluminum 6013 alloy is a wrought alloy type with high strength, improved formability,
contactAluminum 6013 is a wrought alloy that offers high strength, and excellent compressive properties. The formability and corrosion resistance of Aluminum 6013 are also outstanding. The stress cracking resistance and weldability of Aluminum 6014 are highly rated and it is age-hardenable. It is often sold in the T4 condition and can be aged to the ...
contactThe T4 condition allows 6013 aluminum to be formed and demonstrates better stretch forming characteristics. The part can then be aged to the T6 condition without costly heat treating or annealing operations. The yield strength is 12% higher than Alclad 2024 and resistant to exfoliation and stress corrosion cracking. 6013 ALUMINUM APPLICATIONS.
contact201644 · aluminum alloy temper designations, the typical mechanical properties of representative wrought and cast aluminum alloys are presented in Tables 1 and 2, respectively. Table 1 Typical mechanical properties of wrought aluminum alloys(a) Tension Elongation, % Alloy and temper Strength, ksi Ultimate Yield In2in. 1⁄ 16 in. thick
contact202313 · Aircraft Aluminum European and American alternatives. Aluminium Alloys. Go to - 1000 - 2000 - 3000 - 4000 - 5000 - 6000 - 7000 - Other Aluminium Alloy 1000. Alloy Designation: UK ... 6013 : AMS 4216 6013-T6 Sheet AMS 4347 6013-T4 Sheet : 6056A: BS B6 Alloy 6056A : 6060 : WS 3.3535 WS3.3206: AlMgSi0.5 A-GS: 6062 :
contact200951 · In this study T6 heat treatment is applied to Aluminium 6013 sheet and this sheet joined by using FSW technique. Tensile specimens were machined from the welded plate in the dimension of A0 = 12.5 ...
contactAluminum content reported is calculated as remainder. Composition information provided by the Aluminum Association and is not for design. Key Words: Aluminium 2024-T351; AA2024-T351, Aluminium 2024-T4; UNS A92024; ISO AlCu4Mg1; NF A-U4G1 (France); DIN AlCuMg2; AA2024-T4, ASME SB211; CSA CG42 (Canada)
contact2020530 · 6013-T6 Aluminum. 6013-T6 aluminum is 6013 aluminum in the T6 temper. To achieve this temper, the metal is solution heat-treated and artificially aged until it meets standard mechanical property requirements. The graph bars on the material properties cards below compare 6013-T6 aluminum to: 6000-series alloys (top), all
contact202313 · Aircraft Aluminum European and American alternatives. Aluminium Alloys. Go to - 1000 - 2000 - 3000 - 4000 - 5000 - 6000 - 7000 - Other Aluminium Alloy 1000. Alloy Designation: UK ... 6013 : AMS 4216 6013-T6 Sheet AMS 4347 6013-T4 Sheet : 6056A: BS B6 Alloy 6056A : 6060 : WS 3.3535 WS3.3206: AlMgSi0.5 A-GS: 6062 :
contact201644 · aluminum alloy temper designations, the typical mechanical properties of representative wrought and cast aluminum alloys are presented in Tables 1 and 2, respectively. Table 1 Typical mechanical properties of wrought aluminum alloys(a) Tension Elongation, % Alloy and temper Strength, ksi Ultimate Yield In2in. 1⁄ 16 in. thick
contact2 · Aluminium is has a hardness of approximately 2.8. Aluminium – Crystal Structure. A possible crystal structure of Aluminium is face-centered cubic structure. In metals, and in many other solids, the atoms are arranged in regular arrays called crystals. A crystal lattice is a repeating pattern of mathematical points that extends throughout space.
contact2022310 · 6013 aluminium is a relatively new product developed specifically for aerospace applications. We stock and supply 6013 in sheet form. Our product is a aluminium-magnesium-silicon-copper alloy which benefits from low density, improved corrosion resistance and good compressive strength. 6013 aluminium sheet finds use in
contact2019618 · Für Aluminium wird der Präfix-Buchstabe A verwendet. JIS (Japan) JIS steht für Japanese Industrial Standards und wird vom Japanese Industrial Standards Committee (JISC) in Tokyo entwickelt. Die Bezeichnung von Aluminiumlegierungen erfolgt sehr ähnlich wie die des ANSI/AA-Systems. Sie beginnt mit dem Präfix JIS, gefolgt von
contact2019627 · Mn Cu 6013 [J]. , 2019, 6(2): 111-115. DOI: 10.12677/meng.2019.62016 Effect of Mn and Cu on Microstructure and Mechanical Properties of 6013 Aluminum Alloy Yimeng Wang, Chengwu Liu, Fan Feng ,
contactFrance / AFNOR NF, Aluminium :: Total Materia. The largest metals properties database available. Besides being is the most comprehensive metal properties database and knowledge source worldwide, with more than 10,000,000 property records for over 350,000 alloys, Total Materia gives you the highest quality and reliability of the only certified ...
contact201461 · PDF | Aluminum alloys are widely used in aircraft structures especially in the fuselage and wing fairings. For the joining of these structures, the... | Find, read and cite all the research you ...
contact2020530 · 6013-T6 Aluminum. 6013-T6 aluminum is 6013 aluminum in the T6 temper. To achieve this temper, the metal is solution heat-treated and artificially aged until it meets standard mechanical property requirements. The graph bars on the material properties cards below compare 6013-T6 aluminum to: 6000-series alloys (top), all
contact2022315 · 1. Introduction. The 6013 aluminum alloy is one of the few Al–Mg–Si–Cu alloys used in the aerospace industry [1, 2]; however, it has also been extensively used in machine manufacturing and mobile communication [[3], [4], [5]].The tensile strength of the 6013 aluminum alloy in the T6 state is 15% higher than that of 6061-T6, and the
contact6013 Aluminum Alloy Sheet Description Alloy 6013 is a new medium strength aerospace alloy that provides improved corrosion resistance and formability for use in aerospace applications including primary aircraft structures. Alloy 6013 is an aluminum-magnesium-s ilicon-copper alloy that has yield strengths 12% higher than alclad 2024-T3 and is ...
contact200071 · @misc{etde_, title = {Fatigue properties of the aluminium alloys 6013 and Al-Mg-Sc} author = {Wirtz, T, Luetjering, G, Gysler, A, Lenczowski, B, and Rauh, R} abstractNote = {The fatigue properties of the Al-alloys 6013 T6 and Al-Mg-Sc were compared under constant amplitude loading conditions. The fatigue strength as well as
contact200951 · In this study T6 heat treatment is applied to Aluminium 6013 sheet and this sheet joined by using FSW technique. Tensile specimens were machined from the welded plate in the dimension of A0 = 12.5 ...
contact0.214 BTU/lb-°F. Thermal Conductivity. 154 W/m-K. 1070 BTU-in/hr-ft²-°F. AA; Typical at 77°F. Melting Point. 582 - 652 °C. 1080 - 1205 °F. AA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater; Eutectic melting can be completely eliminated by homogenization.
contact199051 · The recently developed aluminum alloy 6013-T6 has been selected for the fuselage skin and other applications on the U.S. Navy's P-7A airplane, in place of the traditional 2024-T3 clad sheet. Alloy 6013-T6 is naturally corrosion resistant, like the well-established alloy 6061, and hence is used unclad. Its fatigue strength, fatigue crack
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