The Effect of Ageing Treatment of Aluminum Alloys for Fuselage Structure-Light Aircraft
As the material used for fuselage structure must
possess low density, high strength to weight ratio, the selection of
appropriate materials for fuselage structure is one of the most
important tasks. Aluminum metal itself is soft and low in strength. It
can be made stronger by giving proper combination of suitable alloy
addition, mechanical treatment and thermal treatment. The usual
thermal treatment given to aluminum alloys is called age-hardening
or precipitation hardening. In this paper, the studies are carried out on
7075 aluminum alloy which is how to improve strength level for
fuselage structure. The marked effect of the strength on the ternary
alloy is clearly demonstrated at several ageing times and
temperatures. It is concluded that aluminum-zinc-magnesium alloy
can get the highest strength level in natural ageing.
[1] Flinn Trojan, January 1968, Journal of Institute of Metals, Vol 7, 40-50.
[2] Dennis, W.H. 1961. Metallurgy of the Non-Ferrous Metals.
[3] Donald R. 1994, Askeland, The Science and Engineering of Materials,
Third Edition.
[4] A. K. Watkins and V. Kondic, November 1963, Foundry Journal, 53-63.
[5] I. J. Polemear, 1957-58, Journal of Institute of Metals, Vol-86, 113-121.
[1] Flinn Trojan, January 1968, Journal of Institute of Metals, Vol 7, 40-50.
[2] Dennis, W.H. 1961. Metallurgy of the Non-Ferrous Metals.
[3] Donald R. 1994, Askeland, The Science and Engineering of Materials,
Third Edition.
[4] A. K. Watkins and V. Kondic, November 1963, Foundry Journal, 53-63.
[5] I. J. Polemear, 1957-58, Journal of Institute of Metals, Vol-86, 113-121.
@article{"International Journal of Chemical, Materials and Biomolecular Sciences:62048", author = "Shwe Wut Hmon Aye and Kay Thi Lwin and Waing Waing Kay Khine Oo", title = "The Effect of Ageing Treatment of Aluminum Alloys for Fuselage Structure-Light Aircraft", abstract = "As the material used for fuselage structure must
possess low density, high strength to weight ratio, the selection of
appropriate materials for fuselage structure is one of the most
important tasks. Aluminum metal itself is soft and low in strength. It
can be made stronger by giving proper combination of suitable alloy
addition, mechanical treatment and thermal treatment. The usual
thermal treatment given to aluminum alloys is called age-hardening
or precipitation hardening. In this paper, the studies are carried out on
7075 aluminum alloy which is how to improve strength level for
fuselage structure. The marked effect of the strength on the ternary
alloy is clearly demonstrated at several ageing times and
temperatures. It is concluded that aluminum-zinc-magnesium alloy
can get the highest strength level in natural ageing.", keywords = "Aluminum alloy, ageing, heat treatment, strength.", volume = "2", number = "10", pages = "241-4", }