LEADING EDGE PROTECTION AND METHOD OF MAKING
    1.
    发明申请
    LEADING EDGE PROTECTION AND METHOD OF MAKING 审中-公开
    领先的边缘保护和制作方法

    公开(公告)号:WO2013172894A3

    公开(公告)日:2014-02-06

    申请号:PCT/US2013026663

    申请日:2013-02-19

    Abstract: A method of forming a leading edge protection component includes depositing particles using a cold spray process on a mandrel to form a leading edge protection component; and removing the leading edge protection structure from the mandrel. The leading edge protection can be formed in one or more pieces and involve using one or more mandrels.

    Abstract translation: 形成前缘保护部件的方法包括使用冷喷涂工艺在芯棒上沉积颗粒以形成前缘保护部件; 并从心轴移除前缘保护结构。 前缘保护可以形成在一个或多个部件中并涉及使用一个或多个心轴。

    LEADING EDGE PROTECTION AND METHOD OF MAKING
    2.
    发明申请
    LEADING EDGE PROTECTION AND METHOD OF MAKING 审中-公开
    主要的边缘保护和制造方法

    公开(公告)号:WO2013172894A4

    公开(公告)日:2014-03-27

    申请号:PCT/US2013026663

    申请日:2013-02-19

    Abstract: A method of forming a leading edge protection component includes depositing particles using a cold spray process on a mandrel to form a leading edge protection component; and removing the leading edge protection structure from the mandrel. The leading edge protection can be formed in one or more pieces and involve using one or more mandrels.

    Abstract translation: 形成前缘保护部件的方法包括使用冷喷涂工艺在心轴上沉积颗粒以形成前缘保护部件; 并从心轴上移除前缘保护结构。 前缘保护可以形成为一个或多个部件并且涉及使用一个或多个心轴。

    COLD SPRAY NOZZLE ASSEMBLY
    6.
    发明专利

    公开(公告)号:SG11201509306XA

    公开(公告)日:2015-12-30

    申请号:SG11201509306X

    申请日:2014-01-15

    Abstract: A cold spray nozzle assembly is disclosed that includes a nozzle body formed from a first material and an adapter body formed from a second material wherein each body has a passage the communicates with one another along an axis. The nozzle body is formed from a polymeric material and the adapter body formed from a metallic material.

    EROSION RESISTANT AND HYDROPHOBIC ARTICLE

    公开(公告)号:SG11201405223RA

    公开(公告)日:2014-10-30

    申请号:SG11201405223R

    申请日:2013-02-23

    Abstract: A gas turbine engine includes an airfoil having a core that has a first hardness and a surface on the core. The surface includes a plurality of geometric features that have a second, greater hardness. The geometric features define a surface porosity by area percent and a corresponding surface solidity by area percent. The surface includes a ratio of the surface solidity divided by the surface porosity that is 1.8 or greater. The geometric features and the ratio establish the surface to be hydrophobic, and the second, greater hardness and the ratio establish an erosion rate of the surface that is equal to or less than an erosion rate of the core under identical erosion conditions.

    LEADING EDGE PROTECTION AND METHOD OF MAKING

    公开(公告)号:SG11201403853PA

    公开(公告)日:2014-10-30

    申请号:SG11201403853P

    申请日:2013-02-19

    Abstract: A method of forming a leading edge protection component includes depositing particles using a cold spray process on a mandrel to form a leading edge protection component; and removing the leading edge protection structure from the mandrel. The leading edge protection can be formed in one or more pieces and involve using one or more mandrels.

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