Tytuł artykułu
Autorzy
Identyfikatory
Warianty tytułu
Konferencja
Metody oceny struktury oraz własności materiałów i wyrobów/sympozjum ( XXII ; 6-8.XI.2007 ; Svratka, Czechy)
Języki publikacji
Abstrakty
The cast aluminium alloy A357 has been widely used in aircraft industry. Particularly, due to well known performance characteristics of aluminium alloys like strength/weight ratio (specific strength). This contribution deals with the effect of different heat treatment on mechanical characteristics of A357 cast aluminium alloy. As relevant parameters were chosen yield strength, ultimate strength, elongation and hardness. The material parameters were obtained using standard tensile test method and hardness measuring. Finally the obtained values of mechanical characteristics were compared with results which were publicized in literature.
Słowa kluczowe
Rocznik
Tom
Strony
19--19
Opis fizyczny
., Bibliogr. 5 poz., il., tab., wykr.
Twórcy
Bibliografia
- [1] MICHNA Š., LUKÁC I., OCENÁŠEK V., KORENÝ R., DRÁPALA J., SCHNEIDER H., MIŠKUFOVÁ A. a kol.: Encyklopedie hliníku. 1 vyd. Prešov: Adin, s. r. o., 2005, ISBN 80-89041-88-4.
- [2] CSN EN 10002-1 Kovové materiály - Zkoušení tahem - Cást 1: Zkušební metoda za okolní teploty, 2002.
- [3] CSN EN ISO 6507-1 Kovové materiály - Zkouška tvrdosti podle Vickerse - Cást 1: Zkušební metoda, 1999.
- [4] STARKE JR EA, STALEY JT.: Application of modern aluminum alloys to aircraft. Proc. Aerospace Sci 1996;32:131–172.
- [5] ALEXOPOULOS N.D., PANTELAKIS SP.G.: Quality evaluation of A357 cast aluminum alloy specimens subjected to different artificial aging treatment. Materials and Design, 25, 2004. 419–430
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPOG-0034-0004