首页> 外国专利> CONSTRUCTION ELEMENT HAVING A BOND STRUCTURE FOR A TURBO ENGINE, METHOD FOR THE PRODUCTION OF A CONSTRUCTION ELEMENT HAVING A BOND STRUCTURE FOR A TURBO ENGINE, AND TURBO ENGINE HAVING A CONSTRUCTION ELEMENT HAVING A BOND STRUCTURE

CONSTRUCTION ELEMENT HAVING A BOND STRUCTURE FOR A TURBO ENGINE, METHOD FOR THE PRODUCTION OF A CONSTRUCTION ELEMENT HAVING A BOND STRUCTURE FOR A TURBO ENGINE, AND TURBO ENGINE HAVING A CONSTRUCTION ELEMENT HAVING A BOND STRUCTURE

机译:具有涡轮发动机粘结结构的构造元件,具有涡轮发动机粘结结构的构造元件的制造方法和具有粘结结构的构造元件的涡轮发动机的制造方法

摘要

A construction element, particularly adapted and configured for use in a turbo engine, in particular an aircraft engine, wherein a bond coat having a bond structure and thereabove a ceramic coat are disposed on a base. The lateral faces of the bond structure in the cross section are configured so as to be free of undercuts, wherein peak structures and/or trough structures are present, and the peak of the cross section of a peak structure has a mean peak angle (α) of less than or equal to 90°, most particularly less than 45°, and/or the trough structure has a valley angle in the range 90°≤β170°.
机译:一种特别适于和构造用于涡轮发动机,特别是飞机发动机的结构元件,其中具有粘结结构的粘结涂层和其上的陶瓷涂层布置在基座上。结合结构在横截面上的侧面被构造成没有底切,其中存在峰结构和/或槽结构,并且峰结构的横截面的峰具有平均峰角(α)。 )小于或等于90°,​​最优选小于45°,和/或槽结构的谷角在90°≤β<170°的范围内。

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