7075 T6 Aluminum Sheet

7075 T6 Aluminum Sheet

Alloy 7075 t6 aluminum sheets are the outstanding member of the 7xxx series and remains the baseline among the highest strength alloys available. Zinc is the primary alloying element giving it strength comparable to steel. Temper T651 possesses good fatigue strength, fair machinability,...

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Alloy 7075 t6 aluminum sheets are the outstanding member of the 7xxx series and remains the baseline among the highest strength alloys available. Zinc is the primary alloying element giving it strength comparable to steel. Temper T651 possesses good fatigue strength, fair machinability, resistance welding and corrosion resistance ratings. Alloy 7075 in temper T7x51 has superior stress corrosion resistance and replaces the 2xxx alloy in the most critical applications. It is widely used by the aircraft industry with the typical specifications of ASTM B209, AMS-QQ-A-250/4, as well as many end users requirements.

 

General 7075 characteristics: Very high strength material used for highly stressed structural parts. The T7351 temper offers improved stress-corrosion cracking resistance.

 

The mechanical properties of 7075 alloy depend greatly on the temper of the material

Un-heat-treated 7075 alloy plate(7075-0 temper) has maximum tensile strength no more than 280 MPa (40,000 psi), and maximum yield strength no more than 140 MPa (21,000 psi). The material has an elongation (stretch before ultimate failure) of 9–10%. It is very highly corrosion-resistant and has good strength

 

T6 temper 7075 alloy plate( 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%. The T6 temper is usually achieved by homogenizing the cast 7075 at 450 °C for several hours, quenching, and then aging at 120 °C for 24 hours. This yields the peak strength of the 7075 alloy. The strength is derived mainly from finely dispersed eta and eta' precipitates both within grains and along grain boundaries

 

T651 temper 7075 has an ultimate tensile strength of 570 MPa (83,000 psi) and yield strength of 500 MPa (73,000 psi). It has a failure elongation of 3–9%. These properties can change depending on the form of material used. Thicker plate may exhibit lower strengths and elongation than the numbers listed above

 

Chemical Composition:

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Technical Parameters:

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Applications:

7075 aluminum alloy mainly used in aircraft fittings, gears and shafts, fuse parts, meter shafts and gears, missile parts, regulating valve parts, worm gears, keys, aircraft, aerospace and defense applications; bike frames, all terrain vehicle (ATV) sprockets.

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Quality Control :

Our company has built the quality supervision department and aluminum lab to control the quality . We have complete test line to make sure our products's quality to meet per customers requirements!

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FAQ :

Q: Are you trading company or manufacturer ?

A:We are factory.

Q:Can you do ODM and OEM?

A: Yes,We do.

Q: Can you provide free samples to us ?

A: Yes, we can provide free samples , however, the samples cost should be paid by your company . And we will refund the samples cost after order confirmed .


Why choose us?

• With us your money in safe your business in safe

• Full Refund in case of bad quality or late delivery 

• Quality Assurance contract

• Over 100 models can totaly satisfy your request

• Free Samples Offer & Small order Welcomed

• After Sales Service 24*7

• 2 years warranty period


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