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| Session 2: High Strength Aluminum Alloy Airframe Applications | ||||
| Location: Room 605 (Washington State Convention Center) | ||||
| (Please check final room assignments on-site). | ||||
| Session Description: | ||||
| Session Chair: | Mr. Michael Niedzinski Alcan Aerospace, Chicago, IL | |||
| 1:30 PM | LAT062.2 | 2198 – Advanced Aluminium-Lithium Alloy for A350 Fuselage Skin Sheet | ||
| 2:00 PM | LAT062.3 | Development of 7140 T7651 Thick Plate for Structural Airframe Components | ||
| 2:30 PM | Break | |||
| 3:00 PM | LAT062.4 | Generation of Design Data for a New Al-Li Plate Product (2050-T8) | ||
| 3:30 PM | LAT062.5 | Damage Tolerance Capability of 2139 Plate (an Al-Cu-Mg-Ag Based Alloy) | ||
| 4:00 PM | LAT062.6 | Microstructure and Properties of Spraycast and Forged Al-Li-Mg-Zr-(Sc) Alloys for Airframe Applications | ||
| 4:30 PM | LAT062.7 | New Developments in Extruded Integrally Stiffened Panels | ||