Method of preparing turbine blades for spray coating and mounting for fixing such a turbine blade
    2.
    发明授权
    Method of preparing turbine blades for spray coating and mounting for fixing such a turbine blade 有权
    制备用于喷涂和安装涡轮叶片的涡轮叶片的方法

    公开(公告)号:US07717058B2

    公开(公告)日:2010-05-18

    申请号:US11518554

    申请日:2006-09-08

    IPC分类号: B05C21/00

    CPC分类号: C23C4/01 B05B12/20

    摘要: The invention relates to a method of preparing turbine blades for spray coating their blade region that is subjected to the medium flowing through during operation in a spray coating apparatus, in which the turbine blade is inserted with its blade root into a cavity of a mounting in such a way that it protrudes with the blade region that adjoins the blade root from an opening of the cavity to form a gap between the rim of the opening and the turbine blade, and in which the gap is bridged by a shielding fixed on the mounting, which is characterized in that a shielding layer of a plastic which is resistant during the spray coating is used for the shielding, the shielding layer being arranged in such a way that it reaches up to the boundary between the blade root and the blade region.

    摘要翻译: 本发明涉及一种制备涡轮机叶片的方法,用于在喷涂装置中在其操作期间经受介质流动的叶片区域喷涂其中,其中涡轮机叶片以其叶片根部插入安装的空腔中 这样一种方式使得其与从腔的开口邻接叶片根部的叶片区域突出,以在开口的边缘和涡轮叶片之间形成间隙,并且其中间隙由固定在安装件上的屏蔽物桥接 其特征在于,在喷涂期间耐用的塑料的屏蔽层用于屏蔽,屏蔽层以使其到达叶片根部和叶片区域之间的边界的方式布置。

    Method of preparing turbine blades for spray coating and mounting for fixing such a turbine blade
    3.
    发明申请
    Method of preparing turbine blades for spray coating and mounting for fixing such a turbine blade 有权
    制备用于喷涂和安装涡轮叶片的涡轮叶片的方法

    公开(公告)号:US20070110910A1

    公开(公告)日:2007-05-17

    申请号:US11518554

    申请日:2006-09-08

    IPC分类号: B05D7/00 B05C11/11 B05C13/02

    CPC分类号: C23C4/01 B05B12/20

    摘要: The invention relates to a method of preparing turbine blades for spray coating their blade region that is subjected to the medium flowing through during operation in a spray coating apparatus, in which the turbine blade is inserted with its blade root into a cavity of a mounting in such a way that it protrudes with the blade region that adjoins the blade root from an opening of the cavity to form a gap between the rim of the opening and the turbine blade, and in which the gap is bridged by a shielding fixed on the mounting, which is characterized in that a shielding layer of a plastic which is resistant during the spray coating is used for the shielding, the shielding layer being arranged in such a way that it reaches up to the boundary between the blade root and the blade region.

    摘要翻译: 本发明涉及一种制备涡轮机叶片的方法,用于在喷涂装置中在其操作期间经受介质流动的叶片区域喷涂其中,其中涡轮机叶片以其叶片根部插入安装的空腔中 这样一种方式使得其与从腔的开口邻接叶片根部的叶片区域突出,以在开口的边缘和涡轮叶片之间形成间隙,并且其中间隙由固定在安装件上的屏蔽物桥接 其特征在于,在喷涂期间耐用的塑料的屏蔽层用于屏蔽,屏蔽层以使其到达叶片根部和叶片区域之间的边界的方式布置。