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    • 4. 发明申请
    • Ceramic core with composite insert for casting airfoils
    • 陶瓷芯与铸造翼型的复合插件
    • US20150053365A1
    • 2015-02-26
    • US14121824
    • 2014-10-21
    • Howmet Corporation
    • Boyd A. MuellerDarren K. RogersTimothy J. Molamphy
    • B22C9/10B22D25/02B22C9/24
    • B22C9/103B22C7/02B22C7/026B22C7/06B22C9/04B22C9/10B22C9/24B22D25/02B28B1/24B28B7/342B28B7/346B29C33/3807B29C33/40B29C45/0013B29C45/14467B29C2045/1477F01D5/147F05B2230/21F05D2260/36Y02T50/672
    • A multi-wall ceramic core for casting an airfoil with one or more internal cooling passages is made by preforming at least one fugitive core insert to have a joint-forming surface with a male and/or female joint feature and then forming at least one fugitive core insert in-situ adjacent and integrally connected and fused to the at least one preformed core insert at the joint-forming surface to form an interlocked, fused joint to form a composite core insert that includes features to form internal passage surfaces in the core when the composite core insert is removed. Another aspect involves preforming first and second fugitive core inserts to have respective joint-forming surfaces with respective snap-fittable joint features and assembling the first and second fugitive core inserts to form a composite core insert by snap fitting the snap-fittable joint features together to form an interlocked joint. The composite core insert is placed in a core molding die cavity, and a fluid ceramic material is introduced into the die cavity to form the ceramic core body incorporating the fugitive composite core insert therein.
    • 用于铸造具有一个或多个内部冷却通道的翼型件的多壁陶瓷芯通过预先形成至少一个短暂的芯插入件来形成具有阳和/或阴接头特征的接合形成表面,然后形成至少一个逃逸 芯插入件原位相邻并且一体地连接并且在所述接合形成表面处与所述至少一个预成形芯插入件熔合以形成互锁的熔接接头,以形成复合芯插入件,所述复合芯插入件包括在所述芯中形成内部通道表面的特征, 去除复合芯插件。 另一方面涉及预先形成第一和第二短片芯插入件以具有各自的接头形成表面和相应的卡扣可配合接头特征,并且组装第一和第二短片芯插入件以通过将卡扣配合结合部件卡扣配合而形成复合芯插入件 形成互锁接头。 将复合芯插入件放置在芯成型模腔中,并且将流体陶瓷材料引入模腔中以形成其中包含短效复合芯插入件的陶瓷芯体。
    • 9. 发明申请
    • Casting procedure, particularly for engine cylinder head
    • 铸造程序,特别适用于发动机气缸盖
    • US20060108084A1
    • 2006-05-25
    • US10530196
    • 2002-12-09
    • Bruno Bassi
    • Bruno Bassi
    • B22C9/04B22C7/06
    • B22C9/10B22C7/02B22C7/06B22C9/04B22C9/103
    • The present invention relates to a casting procedure for obtaining parts provided with inside cavities or holes, wherein said holes and/or cavities are obtained by laying into a mould or chill, intended to receive the molten metal, one or more cores made of sand or other material, and wherein a main core is used, realised into a special core box, along one or more secondary cores intended to be associated to said main core, comprising the following steps: coating at least one secondary core, only in the zones and by the pattern thickness with a layer of material intended to dissolve in contact with the molten metal; inserting the pre-coated secondary cores into the main core box yet to be moulded; moulding the main core box; and inserting the monolithic group obtained at the previous step, consisting of the main core, of the secondary cores and of the coating material that keeps them firmly connected, into the mould or chill intended to receive the molten metal. The cores to be coated can also be formed by hollow inserts (23) made of a heat resistant material, filled with sand polymerised resin, wherein the cavity represents the core pattern.
    • 本发明涉及一种用于获得设置有内部空腔或孔的部件的铸造步骤,其中所述孔和/或空腔通过铺设在用于容纳熔融金属的模具或冷却物中而获得,一个或多个芯由砂或 并且其中使用主芯体,沿着一个或多个旨在与所述主芯相关联的次级芯体实现为特殊芯盒,包括以下步骤:仅在所述区域中涂覆至少一个次级芯,以及 通过具有用于溶解与熔融金属接触的材料层的图案厚度; 将预涂的次级芯插入待成型的主芯盒中; 成型主芯盒; 并且将由上述步骤获得的整体组,将二次芯的主芯和保持它们牢固连接的涂层材料插入到用于接收熔融金属的模具或冷却物中。 待涂覆的芯也可以由填充有砂聚合树脂的耐热材料制成的中空插入件(23)形成,其中空腔表示芯图案。