Mechanical properties and corrosion behavior of extrusions for aircraft applications made by discontinously silicon-carbide-reinforced aluminum matrix composites

Materials Science Forum

Volumn 217-222, Issue PART 3, 1996, Pages 1593-1598

  Pinto, L ^a   Zschech, E ^b  

^a AEROSPATIALE   (France)

^b AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

Corrosion; Extrusion; Fatigue; Microstructure; MMC; Powder metallurgy; Young's modulus

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; ALUMINUM ALLOYS; CORROSION; ELASTIC MODULI; FATIGUE OF MATERIALS; METAL EXTRUSION; METALLOGRAPHIC MICROSTRUCTURE; POWDER METALLURGY; REINFORCEMENT; SILICON CARBIDE; STRENGTH OF MATERIALS;

CIVIL AIRCRAFT STRUCTURES; EXTRUDED PROFILES; WEIGHT SAVING;

METALLIC MATRIX COMPOSITES;

EID: 0029725552     PISSN: 02555476     EISSN: 16629752     Source Type: Book Series    
DOI: 10.4028/www.scientific.net/msf.217-222.1593     Document Type: Article

References (2)

1. J. Eliasson, R. Sandström: The role of the value of weight savings in the use of aluminum matrix composites. Proc. ICAA-4, Vol. 2, pp. 535-542 (1994)
2. G. Braun, Quasistatisches und zyklisches Verformungsverhalten von SiC-partikelverstärktem AlCu4.5Si0.8Mg0.5. Dissertation, Universität Karlsruhe (1994)