When.com Web Search

Search results

  1. Results From The WOW.Com Content Network
  2. 7075 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7075_aluminium_alloy

    T6 temper 7075 has an ultimate tensile strength of 510–540 MPa (74,000–78,000 psi) and yield strength of at least 430–480 MPa (63,000–69,000 psi). It has a failure elongation of 5–11%. [9] The T6 temper is usually achieved by homogenizing the cast 7075 at 450 °C for several hours, quenching, and then ageing at 120 °C for 24 hours.

  3. 7068 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7068_aluminium_alloy

    7068-T6511 has typical ultimate tensile strength of 710 MPa (103 ksi) versus a similar product produced from 7075-T6511 that would have a typical ultimate tensile strength of 640 MPa (93 ksi). Typical yield strength for alloy 7068-T6511 is 683 MPa (99.1 ksi) versus 590 MPa (86 ksi) for a similar product produced from 7075 -T6511. [ 2 ]

  4. Aluminium–zinc alloys - Wikipedia

    en.wikipedia.org/wiki/Aluminium–zinc_alloys

    Aluminium brass is a technically rather uncommon term for high-strength and partly seawater-resistant copper-zinc cast and wrought alloys with 55–66% copper, up to 7% aluminium, up to 4.5% iron, and 5% manganese. Aluminium bronze is technically correct as bronze, a zinc-free copper-tin casting alloy with aluminium content.

  5. Aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/Aluminium_alloy

    A brief historical overview of alloys and manufacturing technologies is given in Ref. [4] Aluminium alloys are used extensively in aircraft due to their high strength-to-weight ratio. Pure aluminium is much too soft for such uses, and it does not have the high tensile strength that is needed for building airplanes and helicopters.

  6. 7065 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7065_aluminium_alloy

    The combination of high strength and fracture toughness properties and corrosion resistance makes 7065 suitable as a replacement for 7010, 7050, 7075, 7475 and other alloys for critical intermediate thickness applications. [3] Spar, rib, and integrally machined structural parts for new, derivative, or retrofit aircraft. [3]

  7. 7050 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7050_aluminium_alloy

    It has high toughness, high strength. It has high stress corrosion cracking resistance. [1] It has electric conductivity of value having 40 percent of copper. [2] 7050 aluminium is known as a commercial aerospace alloy. [3]

  8. 7022 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7022_aluminium_alloy

    Like most other highly alloyed alloys, 7022 is a high strength alloy, with yield strength of 370 MPa. Designed to be resistant to stress corrosion cracking, it has decent corrosion and oxidation resistance comparable to 7075 aluminium alloy [1] but worse than 7039 aluminium alloy. Good machinability, thermal conductivity and dimensional ...

  9. 7072 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/7072_aluminium_alloy

    Shear strength 62 MPa Elastic modulus 70-80 GPa Poisson's ratio 0.33 Thermal conductivity 227 W/mK Ultimate Tensile Strength 75 MPa [2] Designations. 7072 can be ...