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Project 2:
Overaging of Al 7075
Group 2 - MSE 527L
Objective
Experimentally perform precipitation of Aluminium alloy 7075
Determine the effect of artificial ageing on hardness of Al-7075
Determine hardness of the alloy before and after the ageing process
Observe for optimum time duration of ageing of the alloy at a particular
temperature to obtain maximum strength
Compare the differences in mechanical properties, such as ductility, tensile
strength, yield strength, modulus of elasticity, and strain hardening exponent at
different aging times.
Aluminium 7075
● Ultimate Tensile strength : 74,000 psi - 78,000 psi
● Yield strength : 63,000 psi - 69,000 psi
● Material density : 2.810 g/cubic cm
● Specific gravity : 2.81
● Melting point : 900° F
● Modulus of Elasticity Tension : 10.4
● Modulus of Elasticity Torsion : 3.8
Rockwell Hardness Test
● Measures permanent depth of indentation produced by
load on the indenter
Depending upon hardness of material indenter to be used
The test axis should be within 2-degrees of perpendicular
for correct loading
We perform this test on Al-7075 samples before and after
ageing to observe the change
Background
Precipitation Hardening/Age Hardening
Formation of extremely small dispersed 2nd phase particles
GP Zones
Effects on strength and hardness
Overaging
When precipitation hardening has gone too far
Background
Tensile Test
All samples were subjected to tensile test to obtain
mechanical properties after the aging
From stress and strain curve obtained following
properties
Yield strength (YS)
Ultimate tensile Strength (UTS)
Ductility
Young’s Modulus (E) (YM)
Procedure
7075 Aluminum samples were labeled and the initial rockwell Hardness was
measured (Ten samples including two reference samples)
Samples were subjected to over aging at the 320 ºF (160 ºC) for 0,12,24,36,48
hours (Two samples at each time variant were taken for data accuracy)
Rockwell Hardness and conductivity was measured after the overaging process
Samples were then subjected to tensile test to compare the mechanical properties
differences due to aging process.
Hardness
Conductivity
Stress/Strain Curves
Tensile Strength
Yield Strength
Ductility
Modulus of Elasticity
Strain Hardening Exponent
Microstructure
Sample 1 100X Longitudinal Sample 1 100X Transverse
Microstructure
Sample 3 100X Longitudinal Sample 3 100X Transverse
Microstructure
Sample 5 100X Longitudinal Sample 5 100X Transverse
Microstructure
Sample 9 100X Longitudinal Sample 9 100X Transverse
Microstructure
Sample 1 500X Longitudinal Sample 9 500X Longitudinal
Microstructure
Sample 1 500X Transverse Sample 9 500X Transverse
APPLICATIONS:
● High strength to Density ratio: Transport, Aviation, Marine, Automotive
● The strength and lightweight characteristics enhances the
applications in other fields.
● Other applications: Rock climbing equipment
Bicycle components
Inline skating frames
Hang glider airframes
● The hobby grade models typically use 7075 or the 6061 for the
chassis plates.
APPLICATIONS:
● Interesting Application: Manufacturing of upper and lower receivers as
well as the extension tubes for the high quality M16 Rifles in American
military.
● Desert Tactical arms, SIG sauer and French armament company use
it for their precision rifles.
● Common applications: camping knife and fork sets.
● Wide use in mold manufacture: High strength
low density
Thermal properties
Ability to highly polished
References
1. "Heat Treatments: Introduction." Heat Treatments: Introduction. N.p., n.d. Web. 17 Apr. 2013.
<http://www.efunda.com/processes/heat_treat/introduction/heat_treatments.cfm>.
2. "Age Hardening." Bluewater Thermal Solutions. N.p., n.d. Web. 17 Apr. 2013. <http://bluewaterthermal.com/age-hardening/>.
3. T. V. Rajan, C. P. Sharma, Ashok K. Sharma. “Heat Treatment: Principles and Techniques” 15ed. New Delhi: Prentice-Hall, 2006. 336-8.
http://books.google.com/books?id=A2QG3UssqKUC&pg=PA336&lpg=PA336&dq=gp+II+zone&source=bl&ots=Gmso2xnIks&sig=dsRTDlPIE0
tyo2qF4YhpUGNLIsU&hl=en&sa=X&ei=tzJ_UaSRFOLtiwKqooDgAQ&ved=0CDoQ6AEwAQ#v=onepage&q=gp%20II%20zone&f=false
4. Effect of Ageing on Microstructure and Mechanical Properties of Bulk, Cryolled and Room temperature rolled Al 7075 Alloy by Sushantha Kumar
Panigrahi, R Jayaganthan; 2011.
5. "Rockwell Hardness Test Method | Newage Testing Instruments." Rockwell Hardness Test Method | Newage Testing Instruments. N.p., n.d. Web.
29 Nov. 2015.
6. "Rockwell Hardness Testing." Rockwell Hardness Testing. N.p., n.d. Web. 29 Nov. 2015.
7. "WWW.BUEHLER.COM." An ITW Company. N.p., n.d. Web. 29 Nov. 2015.
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Project 2- Overaging of Al 7075

  • 1. Project 2: Overaging of Al 7075 Group 2 - MSE 527L
  • 2. Objective Experimentally perform precipitation of Aluminium alloy 7075 Determine the effect of artificial ageing on hardness of Al-7075 Determine hardness of the alloy before and after the ageing process Observe for optimum time duration of ageing of the alloy at a particular temperature to obtain maximum strength Compare the differences in mechanical properties, such as ductility, tensile strength, yield strength, modulus of elasticity, and strain hardening exponent at different aging times.
  • 3. Aluminium 7075 ● Ultimate Tensile strength : 74,000 psi - 78,000 psi ● Yield strength : 63,000 psi - 69,000 psi ● Material density : 2.810 g/cubic cm ● Specific gravity : 2.81 ● Melting point : 900° F ● Modulus of Elasticity Tension : 10.4 ● Modulus of Elasticity Torsion : 3.8
  • 4. Rockwell Hardness Test ● Measures permanent depth of indentation produced by load on the indenter Depending upon hardness of material indenter to be used The test axis should be within 2-degrees of perpendicular for correct loading We perform this test on Al-7075 samples before and after ageing to observe the change
  • 5. Background Precipitation Hardening/Age Hardening Formation of extremely small dispersed 2nd phase particles GP Zones Effects on strength and hardness Overaging When precipitation hardening has gone too far
  • 7. Tensile Test All samples were subjected to tensile test to obtain mechanical properties after the aging From stress and strain curve obtained following properties Yield strength (YS) Ultimate tensile Strength (UTS) Ductility Young’s Modulus (E) (YM)
  • 8. Procedure 7075 Aluminum samples were labeled and the initial rockwell Hardness was measured (Ten samples including two reference samples) Samples were subjected to over aging at the 320 ºF (160 ºC) for 0,12,24,36,48 hours (Two samples at each time variant were taken for data accuracy) Rockwell Hardness and conductivity was measured after the overaging process Samples were then subjected to tensile test to compare the mechanical properties differences due to aging process.
  • 17. Microstructure Sample 1 100X Longitudinal Sample 1 100X Transverse
  • 18. Microstructure Sample 3 100X Longitudinal Sample 3 100X Transverse
  • 19. Microstructure Sample 5 100X Longitudinal Sample 5 100X Transverse
  • 20. Microstructure Sample 9 100X Longitudinal Sample 9 100X Transverse
  • 21. Microstructure Sample 1 500X Longitudinal Sample 9 500X Longitudinal
  • 22. Microstructure Sample 1 500X Transverse Sample 9 500X Transverse
  • 23. APPLICATIONS: ● High strength to Density ratio: Transport, Aviation, Marine, Automotive ● The strength and lightweight characteristics enhances the applications in other fields. ● Other applications: Rock climbing equipment Bicycle components Inline skating frames Hang glider airframes ● The hobby grade models typically use 7075 or the 6061 for the chassis plates.
  • 24. APPLICATIONS: ● Interesting Application: Manufacturing of upper and lower receivers as well as the extension tubes for the high quality M16 Rifles in American military. ● Desert Tactical arms, SIG sauer and French armament company use it for their precision rifles. ● Common applications: camping knife and fork sets. ● Wide use in mold manufacture: High strength low density Thermal properties Ability to highly polished
  • 25. References 1. "Heat Treatments: Introduction." Heat Treatments: Introduction. N.p., n.d. Web. 17 Apr. 2013. <http://www.efunda.com/processes/heat_treat/introduction/heat_treatments.cfm>. 2. "Age Hardening." Bluewater Thermal Solutions. N.p., n.d. Web. 17 Apr. 2013. <http://bluewaterthermal.com/age-hardening/>. 3. T. V. Rajan, C. P. Sharma, Ashok K. Sharma. “Heat Treatment: Principles and Techniques” 15ed. New Delhi: Prentice-Hall, 2006. 336-8. http://books.google.com/books?id=A2QG3UssqKUC&pg=PA336&lpg=PA336&dq=gp+II+zone&source=bl&ots=Gmso2xnIks&sig=dsRTDlPIE0 tyo2qF4YhpUGNLIsU&hl=en&sa=X&ei=tzJ_UaSRFOLtiwKqooDgAQ&ved=0CDoQ6AEwAQ#v=onepage&q=gp%20II%20zone&f=false 4. Effect of Ageing on Microstructure and Mechanical Properties of Bulk, Cryolled and Room temperature rolled Al 7075 Alloy by Sushantha Kumar Panigrahi, R Jayaganthan; 2011. 5. "Rockwell Hardness Test Method | Newage Testing Instruments." Rockwell Hardness Test Method | Newage Testing Instruments. N.p., n.d. Web. 29 Nov. 2015. 6. "Rockwell Hardness Testing." Rockwell Hardness Testing. N.p., n.d. Web. 29 Nov. 2015. 7. "WWW.BUEHLER.COM." An ITW Company. N.p., n.d. Web. 29 Nov. 2015.