Researches Regarding Improvement of the Fatigue Limit by Heat Treatments of the Al-Alloys for Aeronautics Industry

  • Ana DONIGA "Dunarea de Jos" University of Galati, Romania
  • Elisabeta VASILESCU "Dunarea de Jos" University of Galati, Romania
  • Miltiade ISTRATE "Dunarea de Jos" University of Galati, Romania
  • Ioan VASILESCU "Dunarea de Jos" University of Galati, Romania
  • Silviu MACUTA "Dunarea de Jos" University of Galati, Romania

Résumé

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.

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Références

[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.
Publiée
2005-11-15
Rubrique
Articles

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