Researches Regarding Improvement of the Fatigue Limit by Heat Treatments of the Al-Alloys for Aeronautics Industry
Keywords:
thermomechanical treatment, aluminium alloy
Abstract
The laboratory experiments were made on the two aluminium alloyed qualities used for aeronautical industry. The structure and mechanical characteristics were analyzed and the gotten results were compared using those two types of the thermal treatments. Also, the conventional thermal treatment was used, consisting of the solution quenching and artificial heat ageing, mode in more working condition. A significantly improvement of the mechanical characteristics was ascertained to the thermical treated test-specimen.
References
[1]. Popescu N., - Tratamente termice neconventionale ET – Bucuresti 1990.
[2]. Dulamita T., Florian E, - Tratamente termice si termochimice EDP – Bucuresti 1982.
[3]. Cazimirovici E.,-Laminarea aliajelor speciale Ed. BREN 1998.
[2]. Dulamita T., Florian E, - Tratamente termice si termochimice EDP – Bucuresti 1982.
[3]. Cazimirovici E.,-Laminarea aliajelor speciale Ed. BREN 1998.
Published
2005-11-15
How to Cite
1.
DONIGA A, VASILESCU E, ISTRATE M, VASILESCU I, MACUTA S. Researches Regarding Improvement of the Fatigue Limit by Heat Treatments of the Al-Alloys for Aeronautics Industry. The Annals of “Dunarea de Jos” University of Galati. Fascicle IX, Metallurgy and Materials Science [Internet]. 15Nov.2005 [cited 28Apr.2024];28(2):74-7. Available from: https://www.gup.ugal.ro/ugaljournals/index.php/mms/article/view/3256
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