GAMMA TITANIUM DUAL PROPERTY HEAT TREAT SYSTEM AND METHOD
    1.
    发明申请
    GAMMA TITANIUM DUAL PROPERTY HEAT TREAT SYSTEM AND METHOD 审中-公开
    GAMMA TITANIUM DUAL PROPERTY热处理系统和方法

    公开(公告)号:WO2014031234A1

    公开(公告)日:2014-02-27

    申请号:PCT/US2013/048395

    申请日:2013-06-28

    Abstract: A method for forming a part having a dual property microstructure includes the steps of: forming a blank having a narrow top portion and a wide base portion; heating the blank to an elevated temperature; and forming a dual property microstructure in the blank by cooling different portions of the blank at different cooling rates.

    Abstract translation: 一种形成具有双性质微结构的部件的方法包括以下步骤:形成具有窄顶部和宽基部的坯料; 将坯料加热至高温; 并通过以不同的冷却速率冷却坯料的不同部分,在坯料中形成双重性能微观结构。

    POWDER METALLURGY ALLOY EXTRUSION
    2.
    发明申请
    POWDER METALLURGY ALLOY EXTRUSION 审中-公开
    粉末冶金合金挤压

    公开(公告)号:WO2014152172A1

    公开(公告)日:2014-09-25

    申请号:PCT/US2014/027033

    申请日:2014-03-14

    Abstract: A method for forming an article (60) by introducing one or more powders (331) into a bag (310). Vacuum is applied to the bag. The bag is sealed. The one or more powders in the sealed bag are forged to form a first precursor (604) of the article. The precursor is extruded into a shaped die to form at least a second precursor (606) of the article.

    Abstract translation: 一种通过将一种或多种粉末(331)引入袋(310)中来形成物品(60)的方法。 将真空施加到袋子上。 袋子被密封。 密封袋中的一种或多种粉末被锻造以形成制品的第一前体(604)。 将前体挤出成型模具以形成制品的至少第二前体(606)。

    METHOD OF FORMING GAS TURBINE ENGINE COMPONENTS

    公开(公告)号:EP3680060A1

    公开(公告)日:2020-07-15

    申请号:EP20151545.9

    申请日:2020-01-13

    Abstract: A method of forming a gas turbine engine component (160) includes attaching a cover skin to an airfoil body, the airfoil body and the cover skin cooperating to define pressure and suction sides of an airfoil (161), and moving the airfoil (161) in a forming line (178) including a plurality of stations (180). The plurality of stations (180) include a set of heating stations (180B), a deforming station (180C) and a set of cool down stations (180D). The moving step includes positioning the airfoil (161) in the set of heating stations (180B) to progressively increase a temperature of the airfoil (161), then positioning the airfoil (161) in the deforming station (180C) including causing the airfoil (161) to deform between first and second dies (188, 189), and then positioning the airfoil (161) in the set of cool down stations (180D) to progressively decrease the temperature of the airfoil (161).

    GAMMA TITANIUM DUAL PROPERTY HEAT TREAT SYSTEM AND METHOD
    7.
    发明公开
    GAMMA TITANIUM DUAL PROPERTY HEAT TREAT SYSTEM AND METHOD 有权
    GAMMA钛双特性热处理系统和方法

    公开(公告)号:EP2888384A1

    公开(公告)日:2015-07-01

    申请号:EP13831687.2

    申请日:2013-06-28

    Abstract: A method for forming a part having a dual property microstructure includes the steps of: forming a blank having a narrow top portion and a wide base portion; heating the blank to an elevated temperature; and forming a dual property microstructure in the blank by cooling different portions of the blank at different cooling rates.

    Abstract translation: 一种用于形成具有双特性微结构的部件的方法包括以下步骤:形成具有窄顶部和宽底部的坯件; 将坯料加热至高温; 并通过以不同的冷却速率冷却坯料的不同部分而在坯件中形成双性能微结构。

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