PROCESS FOR MANUFACTURING A BIMETALLIC PART USING A DILATION-CAUSING THERMAL TREATMENT

    公开(公告)号:US20210238706A1

    公开(公告)日:2021-08-05

    申请号:US16973111

    申请日:2019-06-27

    Abstract: A process for manufacturing a bimetallic part by means of a first component formed by a first aluminum alloy and a second component formed by a second aluminum alloy, said process involving: assembling the first component and the second component to obtain an assembled part; applying a thermal treatment to the assembled part at a temperature of 100 to 250° C., the thermal treatment causing the assembled part to deform, in particular as a result of a metallurgical deformation by a precipitation of hardening phases of the first component and/or the second component; cooling the part to ambient temperature, upon which the part remains deformed. The process involves, prior to the assembling step, an estimation of the degree of deformation that the assembled part will undergo under the effect of the thermal treatment.

    IMPROVED STRUCTURAL ELEMENTS OBTAINED BY LINEAR FRICTION WELDING
    2.
    发明申请
    IMPROVED STRUCTURAL ELEMENTS OBTAINED BY LINEAR FRICTION WELDING 审中-公开
    通过线性摩擦焊接获得的改进的结构元件

    公开(公告)号:US20170050264A1

    公开(公告)日:2017-02-23

    申请号:US14392149

    申请日:2014-06-24

    CPC classification number: B23K20/2336 B23K20/1205 B23K2101/006 B23K2103/10

    Abstract: The invention concerns a method for forming by welding along a flat surface an article. The method according to the invention is particularly useful to improve strength and elongation of welded joints obtained by linear friction welding. Structural articles of aircrafts obtained with the method of the invention are advantageous, in particular aircraft structural members.

    Abstract translation: 本发明涉及一种通过沿平坦表面焊接制品的方法。 根据本发明的方法特别可用于提高通过线性摩擦焊接获得的焊接接头的强度和伸长率。 通过本发明的方法获得的飞行器的结构物品是有利的,特别是飞行器结构构件。

Patent Agency Ranking