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Aluminiumlithiumlegierung
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keywords:(Aluminiumlithiumlegierung)
Suppliers strive to extend service life, cut weight
Al-Li alloys and ultrahigh-strength steels for U.S. Navy aircraft
Aluminium-lithium aloy development. For parts made form thick plate
Large scale manufacturing of rapidly solidified aluminium alloys
Current status of aluminium-lithium based alloys
Weight reduction development programme features mechanically alloyed material
Short fatigue cracks in aluminium-lithium alloys
Superplastic forming of aluminium and titanium alloys application on civil aircraft
Advanced materials for aerospace structures
Status and prospects for aluminium-lithium alloy in aircraft structures
Flight simulation fatigue crack growth testing of aluminium alloys. Specific issues and guidelines
Lightweight materials for aircraft applications
Corrosion behaviour of aluminium-lithium alloy 8090-T81 in sea water
Advanced cast aluminium alloys for cast and deformed welded structures for aviation technology
Effect of cerium and impurities on fatigue and fracture properties of 8090 alloy sheets
FESTIP: Technology development in materials
Prospects for using aluminium-lithium alloys for stamped-welded aviations structures
Superplastic forming technology of aircraft structures for Al-Li alloy and high-strength Al alloy
Al-Li alloy 1441 for fuselage applications
Can aluminium-lithium alloys be used in welded constructions for cryogenic engineering?
Aluminum alloy advances for ground vehicles
Delamination behavior in Al-Li alloy C458
Aging Optimization of Aluminum-Lithium alloy C458 for application to cryotank structures
Identification of heat treatments for better formability in an aluminum-lithium alloy sheet
Materials progress: Al-Li alloy cuts weight in military airframe structures
Future space tank concepts. Manufacturing and assessment strategies
Progress at Alcan Aerospace on the friction stir welding of Al-Li 2050
Latest generation of Al-Li alloys developed by Alcan Aerospace
Advanced aluminium-lithium 1420 alloy for welded structures for aerospace technology
Characterization of an Aluminum–Lithium-Alloy-Based Composite Propellant at Elevated Pressures