Aluminium alloy will change strength

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SUMMARY

Aluminium alloys exhibit changes in strength when subjected to varying loads, particularly in the context of cyclic loading versus static loading. The discussion highlights that the alloy AlCu4Mg2 is suspected to be among the strongest, while 7001-T6, a zinc-copper-magnesium alloy, has a tensile strength of approximately 97 ksi and an endurance limit of 21.8 ksi for 500 million cycles. The effects of cyclic loading can lead to strain hardening, increasing strength but also brittleness, thereby reducing fatigue life. Understanding the S-N curve is essential for analyzing the performance of these materials under different loading conditions.

PREREQUISITES
  • Knowledge of aluminium alloy types, specifically AlCu4Mg2 and 7001-T6
  • Understanding of cyclic loading and static loading concepts
  • Familiarity with the S-N curve and its implications for material fatigue
  • Basic principles of work hardening and the Bauschinger Effect
NEXT STEPS
  • Research the properties and applications of AlCu4Mg2 alloy
  • Study the S-N curve for 7001-T6 and other aluminium alloys
  • Explore the effects of cyclic loading on material properties and fatigue life
  • Investigate the Bauschinger Effect and its relevance to aluminium alloys
USEFUL FOR

Materials engineers, structural engineers, and anyone involved in the design and analysis of components using aluminium alloys, particularly in applications subject to varying loads.

TSN79
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Is it the case that an Aluminium alloy will change strength (yield/ultimate) if subjectet to a varying load instead of a static one? I can't quite see why it should...can someone help me with this?
 
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You need to phrase your question a bit better. Are you talking about cyclic loads past the elastic limit? Are you referring to an S-N curve issue? Or are you possible talking about work hardening?
 
I suspect it is the former.

(TSN, you could look up "fatigue" and its origin in the "Bauschinger Effect". )
 
On the other hand, several Al-alloys are strengthened by work hardening...
 
Well, I have two questions to answer. First, which Al alloy is the strongest, and in what region would the yield/ultimate strengths for this alloy lie?
Second, Is this region the same if the alloy is subjectet to cyclic loads instead of static loads?

On the first question I suspect the combination AlCu4Mg2 is the strongest, but I'm not at all sure...
 
There are so many different alloys of aluminum out there, this is a bit of a tough question to answer.

Of the basic alloys that I am familiar with, 7001-T6 has the highest tensile strength of approximately 97 ksi. 7001-T6 is a zinc-copper-magnesium alloy that is age hardened.

In terms of cyclic loading, this is where you will want to look up an S-N curve for that material. The endurance limit for this alloy is 21.8 ksi which, as shown is for 500x10^6 cycles (infinite life). To answer your question, it will depend on how much load you are cyclically placing on the material. If you are continuously cycling past the yield point, you will strain hardent the material. In that case it will become stronger, but also much more brittle and, obviously, the fatigue life drops.
 

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