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Solute enhanced strain hardening of aluminum alloys to achieve improved combinations of strength and toughness
Solute enhanced strain hardening of aluminum alloys to achieve improved combinations of strength and toughness
Details
Title
Solute enhanced strain hardening of aluminum alloys to achieve improved combinations of strength and toughness
Author(s)
Hovanec, Christopher James
Advisor(s)
Kalidindi, Surya
;
Doherty, R. D. (Roger Davidge), 1939-
Keywords
Materials science
;
Metallurgy
;
Aluminum alloys
Date
2011-04
Publisher
Drexel University
Thesis
Ph.D., Materials Science and Engineering -- Drexel University, 2011
Abstract
The feasibility of achieving improved combinations of strength and toughness in aluminum alloy 2524 through solute enhanced strain hardening (SESH) has been explored in this study and shown to be viable. The effectiveness of SESH is directly dependent on the strain hardening rate (SHR) of the material being processed. Aluminum alloy 2524 naturally ages to the T4-temper after solution heat treating and quenching. The SHR of strain free and post cold rolled material as a function of natural aging time has been measured by means of simple compression. It has been determined that the SHR of AA2524 is more effective with solute in solution rather than clustered into GP zones. It has also been shown that the typical rapid formation of GP zones at room temperature (natural aging) is inhibited by moderate cold rolling strains (ɛCR ≥ 0.2) through dislocation aided vacancy annihilation.The practical limitations of quenching rate have been determined using hardness and eddy current electrical conductivity measurements. It has been shown that too slow of a quench rate results in solute being lost to both the formation of GP zones and embrittling precipitates during the quench, while too rapid of a quench rate results in mid-plane cracking of the work piece during the SESH processing. The mid-plane cracking was overcome by using an uphill quenching procedure to relieve residual stresses within the work piece. Aluminum alloy 2524 strengthened through SESH to a yield strength 11% greater than that in the T6-Temper exhibits: equivalent toughness, 5% greater UTS, 1% greater elongation, 7% greater R.A., and absorbs 15% more energy during tensile testing. At yield strengths comparable to published data for 2x24 alloys, the SESH 2524 exhibited up to a 60% increase in fracture toughness. The fractured surfaces of the SESH material exhibited transgranular dimpled rupture as opposed to the grain boundary ductile fracture (GBPF) observed in the artificially aged material.
URI
http://hdl.handle.net/1860/3520
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