Challenges of the metallic fuselage

ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006

Volumn 4, Issue , 2006, Pages 2110-2121

  Pacchione, M ^a   Telgkamp, J ^a  

^a Air bus   (Germany)

Author keywords

Al Li; Bonding; Metallic fuselage; SHM; Welding

Indexed keywords

ACCIDENT PREVENTION; AEROSPACE INDUSTRY; ALUMINUM ALLOYS; BINARY ALLOYS; COSTS; EFFICIENCY; FUSELAGES; LITHIUM ALLOYS; METALS; PRODUCT DESIGN;

AIRFRAME STRUCTURES; AL-LI; BONDING; LEVEL OF SAFETIES; MAXIMUM LEVELS; METALLIC FUSELAGE; METALLICS; MINIMUM COST; SHM; WELDING;

COMPETITION;

EID: 84878519648     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. A380 Briefing. Airbus, June 2005.
2. A350 Briefing. Airbus, 2005.
3. Schmidt H-J, Schmidt-Brandeker B, Damage tolerant design and analysis of current and future aircraft structure. AIAA 2003.
4. McConnell G, A350 Technologies. Technical press briefing, 2005.
5. Schmidt H-J, Damage Tolerance Technology for current and future aircraft structure. Plantema Lecture, ICAF 2005