Ceramic casting cores with controlled surface texture
    1.
    发明授权
    Ceramic casting cores with controlled surface texture 失效
    具有受控表面纹理的陶瓷铸芯

    公开(公告)号:US06588484B1

    公开(公告)日:2003-07-08

    申请号:US09597311

    申请日:2000-06-20

    IPC分类号: B22C910

    CPC分类号: B22C9/10

    摘要: A method of making a ceramic core is provided wherein the ceramic core is grit blasted using abrasive grit media particulates directed at the core through a preformed apertured mask or pattern to impart a controlled pattern of surface concavities to the core surface by impingement of the abrasive grit media thereon. Another method of making a ceramic casting core is provided wherein the ceramic core is formed in a molding die having a fugitive textured mask or a permanent textured insert positioned on the die surface to impart a controlled surface texture or roughness to the core surfaces.

    摘要翻译: 提供了一种制造陶瓷芯的方法,其中陶瓷芯使用通过预成型的孔径掩模或图案指向芯的磨料砂粒介质颗粒进行喷砂处理,以通过冲击磨料砂砾将表面凹陷的受控图案赋予芯表面 介质上。 提供制造陶瓷铸造芯的另一种方法,其中陶瓷芯形成在具有短暂纹理化掩模或位于模具表面上的永久性纹理插入件的模制模中,以赋予芯表面受控的表面纹理或粗糙度。

    Composite core for casting
    3.
    发明授权
    Composite core for casting 失效
    复合芯铸造

    公开(公告)号:US06453981B1

    公开(公告)日:2002-09-24

    申请号:US09440611

    申请日:1999-11-15

    IPC分类号: B22C910

    CPC分类号: B22C9/101 B22C9/103

    摘要: A cast product is a housing for a power steering comprising a pair of large holes for both a contact valve and a cylinder, and a small hole connected to the large holes. In order to mold such a cast product, a composite core has large core portions for the large holes and small core portions for the small hole. The large core portions include resin films used to coat the outer periphery of metal bases exposed in a cavity. The small core portions include a resin body formed of a resin connected to the resin films on the outer periphery of the metal bases.

    摘要翻译: 铸造产品是用于动力转向器的壳体,其包括用于接触阀和气缸的一对大孔和连接到大孔的小孔。 为了模制这种铸造产品,复合芯具有用于大孔的大芯部和用于小孔的小芯部。 大的芯部包括用于涂覆露出在空腔中的金属基底的外周的树脂膜。 小芯部包括由与金属基体的外周上的树脂膜连接的树脂形成的树脂体。

    Multipiece core assembly
    4.
    发明授权
    Multipiece core assembly 有权
    多芯组装

    公开(公告)号:US06186217B1

    公开(公告)日:2001-02-13

    申请号:US09203441

    申请日:1998-12-01

    IPC分类号: B22C910

    CPC分类号: B22C7/026 B22C9/103

    摘要: A plurality of individual thin wall, arcuate (e.g. airfoil shaped) core elements are formed in respective master dies to have integral interlocking locating features, the individual core elements are prefired in respective ceramic setter supports to have integral locating features, the prefired core elements are assembled together using the locator features of adjacent core elements, and the assembled core elements are adhered together using ceramic adhesive introduced at internal joints defined between mating interlocked locating features. The multi-wall ceramic core assembly so produced comprises the plurality of spaced apart thin wall, arcuate core elements and joined together by at the internal joints defined between the adhered interlocked locating features.

    摘要翻译: 多个单独的薄壁,弓形(例如翼型)芯元件形成在相应的主模具中以具有一体的互锁定位特征,各个芯元件预先在相应的陶瓷安装器支架中具有整体的定位特征,预烧芯元件 使用相邻芯元件的定位器特征组装在一起,并且组装的芯元件使用引入在配合的互锁定位特征之间限定的内部接头处的陶瓷粘合剂粘合在一起。 如此生产的多壁陶瓷芯组件包括多个间隔开的薄壁,弧形芯元件,并通过在粘附的互锁定位特征之间限定的内部接头处连接在一起。

    Aircraft door and mold for casting the door

    公开(公告)号:US06619372B2

    公开(公告)日:2003-09-16

    申请号:US09874914

    申请日:2001-06-05

    IPC分类号: B22C910

    摘要: An aircraft door has an inner framework integrally connected to an outer skin by simultaneously casting the framework and the skin in a mold that holds a single core for each frame element in the form of a rib in a freight door or a beam in a passenger door. The ribs extend circumferentially relative to a longitudinal central axis of the aircraft. The beams extend in parallel to the central aircraft axis. The single core is selected from at least one core type and four core types at the most. The frame elements in the form of ribs or beams have open arches for a considerable weight reduction.

    Ceramic core and method of making

    公开(公告)号:US06578623B2

    公开(公告)日:2003-06-17

    申请号:US09968654

    申请日:2001-10-01

    IPC分类号: B22C910

    CPC分类号: B22C9/10 B22C3/00

    摘要: Method of making a ceramic core for casting an industrial gas turbine engine airfoil having a large airfoil pitch by forming a precursor core (chill) of smaller dimensions than the final desired ceramic core, firing the chill, applying a thin ceramic skin to the fired chill to form a coated core of final dimensions, and then firing the coated core. Firing of the thin ceramic skin reduces airfoil pitch shrinkage resulting from the latter firing operation to reduce overall core dimensional tolerance variations.

    Casting core and method of casting a gas turbine engine component
    9.
    发明授权
    Casting core and method of casting a gas turbine engine component 有权
    铸造核心和铸造燃气涡轮发动机部件的方法

    公开(公告)号:US06557621B1

    公开(公告)日:2003-05-06

    申请号:US09480331

    申请日:2000-01-10

    IPC分类号: B22C910

    CPC分类号: B22C9/103

    摘要: An integral ceramic casting core includes a base portion with a plurality of rods extending therefrom and a plurality of apertures formed therein. The base portion defines a passageway for the passage of a cooling media within a cast component. The plurality of rods forming cooling media inlet passages to the passageway and the plurality of apertures are adapted to receive molten metal therein and form heat transfer pedestals within the passageway.

    摘要翻译: 整体陶瓷铸造芯包括具有从其延伸的多个杆的基部和在其中形成的多个孔。 基座部分限定用于铸造部件内的冷却介质通过的通道。 形成到通道和多个孔的冷却介质入口通道的多个杆适于在其中容纳熔融金属,并在通道内形成热传递基座。

    Composite core for casting metallic objects
    10.
    发明授权
    Composite core for casting metallic objects 有权
    用于铸造金属物体的复合芯

    公开(公告)号:US06478073B1

    公开(公告)日:2002-11-12

    申请号:US09833772

    申请日:2001-04-12

    IPC分类号: B22C910

    摘要: A composite core structure is used for metal casting in order to form cavities of preselected sizes and shapes within the casting. The composite core has an insoluble support member that can be metallic and a soluble portion disposed around at least a part of the support member. When the composite core is used in a casting process, such as a die casting process, the soluble portion is dissolved after the casting process is complete, and the insoluble portion is then removed from the cavity that was formed through the use of the composite core.

    摘要翻译: 复合芯结构用于金属铸造,以便在铸件内形成预选尺寸和形状的腔。 复合芯具有不溶性支撑构件,其可以是金属的,并且可溶部分设置在支撑构件的至少一部分周围。 当复合芯用于铸造工艺(例如压铸工艺)中时,在铸造工艺完成后,可溶部分被溶解,然后将不溶部分从通过使用复合芯形成的空腔中移除 。