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    • 9. 发明申请
    • Process For Producing A Lost Model, And Core Introduced Therein
    • 产生失落模型的过程,以及其中引入的核心
    • US20080202718A1
    • 2008-08-28
    • US11791189
    • 2005-11-04
    • Uwe PaulUrsula Pickert
    • Uwe PaulUrsula Pickert
    • B22C9/04B22C7/02B22C9/10
    • B22C9/10B22C7/02B22C9/04B33Y70/00B33Y80/00
    • The invention relates to a method for the production of a pattern for precision casting representation of turbine component comprising at least one cavity, whereby the prepared pattern comprises at least one core and an outer contour pattern, at least partly enclosing the core and at least partly defining the outer contour of the turbine component. The core is made from a hardening core material, which hardens during the course of the method and the outer contour pattern is made from a combustible or fusible material. The outer contour model is first produced with at least one cavity corresponding to the at least one cavity of the turbine component and subsequently, in order to form the at least one care, the hardening core material is introduced into the at least one cavity and hardened.
    • 本发明涉及一种用于制造包括至少一个空腔的涡轮机部件的精密铸造表示的图案的方法,由此所制备的图案包括至少一个芯部和外部轮廓图案,至少部分地包围所述芯部并且至少部分地包围 限定涡轮机部件的外轮廓。 芯由硬化芯材制成,其在该方法过程中变硬,并且外轮廓图案由可燃或可熔材料制成。 外轮廓模型首先被制造成具有对应于涡轮机部件的至少一个空腔的至少一个空腔,并且随后为了形成至少一个护理,硬化芯材料被引入到至少一个腔体中并被硬化 。
    • 10. 发明授权
    • Heat treatment method for monocrystalline or directionally solidified structural components
    • 单晶或定向凝固结构组分的热处理方法
    • US07892370B2
    • 2011-02-22
    • US11587897
    • 2005-04-28
    • Michael OttUwe Paul
    • Michael OttUwe Paul
    • C21D1/00C30B33/00
    • C22F1/10C21D9/00C30B11/003C30B29/52C30B33/00
    • The invention relates to a heat treatment method for monocrystalline or directionally solidified structural components. Said method comprises a heat treatment which results in dissolving at least one crystalline phase of the material of the structural component, referred to in the following as component material. The inventive method is characterized by carrying out the heat treatment by heating the structural component to a dissolution temperature required for dissolving the crystalline phase only in at least one first component area in which the stresses within the component material do not exceed a predetermined value. In at least one second component area in which the stresses within the component material exceed the predetermined value the material is only heated to a temperature below the dissolution temperature.
    • 本发明涉及单晶或定向凝固结构组分的热处理方法。 所述方法包括热处理,其导致以下结构组分的材料的至少一个结晶相溶解作为组分材料。 本发明的方法的特征在于,通过将结构组分加热到仅将结晶相溶解在组分材料中的应力不超过预定值的至少一个第一组分区域中所需的溶解温度来进行热处理。 在其中部件材料内的应力超过预定值的至少一个第二部件区域中,材料仅被加热到低于溶解温度的温度。