The present disclosure describes methods for forming metal components, including aircraft landing gear components, from high strength and suitably high ductility titanium alloys, including an improved Ti-5553 alloy.


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    Title :

    HEAT TREATMENT OF TITANIUM ALLOY


    Contributors:

    Publication date :

    2016-09-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    C22F CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS OR NON-FERROUS ALLOYS , Verändern der physikalischen Struktur von Nichteisenmetallen oder Nichteisenlegierungen / B64C AEROPLANES , Flugzeuge / C22C Legierungen , ALLOYS



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