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    • 7. 发明公开
    • Repair and reclassification of superalloy components
    • Reparatur和Wiederherstellung von Bauteilen aus Superlegierungen
    • EP1685923A1
    • 2006-08-02
    • EP06250463.4
    • 2006-01-27
    • UNITED TECHNOLOGIES CORPORATION
    • Pietruska, NormanOlson, Walter E.Abriles, Beth K.Rutz, David A.
    • B23P6/00
    • B23P6/007C23C4/18C23C24/04F01D5/28F05D2230/80Y02T50/67
    • Novel materials and methods for repairing/reclassifying superalloy components are described herein. These materials are non-traditional blends of materials having a much higher base material content than traditional repair/reclassification materials. In embodiments used to repair/reclassify nickel-based components, these materials may comprise about 5-18.9 weight percent of a low melting point alloy and about 81.1-95 weight percent of a base material. In embodiments used to repair/reclassify cobalt-based components, these materials may comprise about 15-30 weight percent of a low melting point alloy and about 70-85 weight percent of a base material. These materials can be used to repair surface defects and/or build up worn or eroded areas of a component to meet precise dimensional and metallurgical requirements. These materials create robust repaired components having a dense, isothermally solidified structure having minimal borides and a high re-melt temperature.
    • 本文描述了用于修复/重新分类超级合金部件的新型材料和方法。 这些材料是具有比传统的修复/重新分类材料高得多的基础材料含量的非传统混合材料。 在用于修复/重新分类镍基组分的实施方案中,这些材料可以包含约5-18.9重量%的低熔点合金和约81.1-95重量%的基材。 在用于修复/重新分类钴基组分的实施方案中,这些材料可以包含约15-30重量%的低熔点合金和约70-85重量%的基材。 这些材料可用于修复表面缺陷和/或构建组件的磨损或侵蚀区域,以满足精确的尺寸和冶金要求。 这些材料产生具有致密的,等温凝固的具有最小硼化物和高再熔融温度的结构的强力修复组分。
    • 8. 发明公开
    • Abrasive material, especially for turbine blade tips
    • Schleifmaterial,insbesonderefürTurbineschaufelenden。
    • EP0273854A2
    • 1988-07-06
    • EP87630280.3
    • 1987-12-23
    • UNITED TECHNOLOGIES CORPORATION
    • Schaefer, Robert P.Rutz, David A.Lee, EdwardJohnson, Edward L.
    • C22C1/10C22C32/00
    • C22C32/00B22F1/0003B22F3/1035C22C1/1036F01D5/20
    • An abrasive material (22) comprised of a metal matrix (26) and evenly distributed ceramic particulates (24), is made by mixing powder metal with the ceramic powder and heating to a temperature sufficient to melt most, but not all of the powder. In this way the ceramic does not float to the top of the material, yet a dense material is ob­tained. A nickel superalloy matrix will have at least some remnants of the original powder metal structure, typically some equiaxed grains, along with a fine den­dritic structure, thereby imparting desirable high tem­perature strength when the abrasive material is applied to the tips of blades of gas turbine engines. Preferred matrices have a relatively wide liquidus-solidus tempe­rature range, contain a melting point depressant, and a reactive metal to promote adhesion to the ceramic.
    • 由金属基体(26)和均匀分布的陶瓷颗粒(24)组成的研磨材料(22)通过将粉末金属与陶瓷粉末混合并加热至足以熔化大部分但不是全部粉末的温度来制备。 以这种方式,陶瓷不会漂浮到材料的顶部,而是获得致密的材料。 镍超级合金基体将具有至少一些原始粉末金属结构的残余物,通常为一些等轴晶粒,以及细小的树枝状结构,从而当研磨材料施加到燃气涡轮发动机叶片的尖端时具有期望的高温强度 。 优选的基质具有相对宽的液相线 - 固相线温度范围,含有熔点抑制剂和活性金属以促进与陶瓷的粘附。