According to one implementation, a magnesium-lithium alloy in which at least lithium is added to magnesium is manufactured by giving a strain to a magnesium-lithium alloy workpiece, after a solution treatment, and progressing an aging of the magnesium-lithium alloy workpiece without a heat treatment. The strain is given by a cold working. The aging is progressed after giving the strain. Further, according to one implementation, an aircraft part includes the above-mentioned magnesium-lithium alloy as a material. Further, according to one implementation, a method of manufacturing an aircraft part includes processing the above-mentioned magnesium-lithium alloy.


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    Titel :

    Magnesium-lithium alloy, method of manufacturing magnesium-lithium alloy, aircraft part, and method of manufacturing aircraft part


    Beteiligte:
    MIURA AYAKO (Autor:in)

    Erscheinungsdatum :

    25.08.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    C22C Legierungen , ALLOYS / C22F CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS OR NON-FERROUS ALLOYS , Verändern der physikalischen Struktur von Nichteisenmetallen oder Nichteisenlegierungen / B62D MOTOR VEHICLES , Motorfahrzeuge



    METHOD OF MANUFACTURING A MAGNESIUM-LITHIUM ALLOY

    MIURA AYAKO | Europäisches Patentamt | 2020

    Freier Zugriff



    Production of MAGNESIUM-Alloy Aircraft Parts

    GRANT, L. B. | SAE Technical Papers | 1940


    Production of magnesium-alloy aircraft parts

    Grant, L.B. | Engineering Index Backfile | 1940