The invention relates to a method for manufacturing a laminated or forged material, the thickness of which is 14 to 100 mm. The materials according to the invention are particularly suitable for manufacturing airplane underwing elements.
Aluminum—copper—lithium alloy product for a lower wing skin element with improved properties
2020-11-17
Patent
Electronic Resource
English
IPC: | C22C Legierungen , ALLOYS / B21B Walzen von Metall , ROLLING OF METAL / B21J FORGING , Schmieden / B64C AEROPLANES , Flugzeuge / C22F CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS OR NON-FERROUS ALLOYS , Verändern der physikalischen Struktur von Nichteisenmetallen oder Nichteisenlegierungen |
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