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    PHYSICAL PROPERTY IMPROVEMENT OF IRON CASTINGS USING CARBON NANOMATERIALS
    1.
    发明申请
    PHYSICAL PROPERTY IMPROVEMENT OF IRON CASTINGS USING CARBON NANOMATERIALS 审中-公开
    使用碳纳米管的铁铸件的物理性能改进

    公开(公告)号：US20160083812A1

    公开(公告)日：2016-03-24

    申请号：US14787022

    申请日：2014-05-08

    Applicant: Kevin PICKRELL ,  DRESSER-RAND COMPANY

    Inventor： Kevin Pickrell

    IPC: C21C1/10 ,  C22C33/08 ,  C22C37/04 ,  B22D1/00 ,  C21C1/08

    CPC classification number: C21C1/105 ,  B22D1/00 ,  B22D19/14 ,  B82Y30/00 ,  C21C1/08 ,  C22C26/00 ,  C22C33/04 ,  C22C33/08 ,  C22C37/04 ,  C22C47/08 ,  C22C2026/001 ,  C22C2026/002

    Abstract: A method is provided for fabricating iron castings for metallic components. The method for fabricating the iron castings may include forming a molten solution by melting carbon and iron and combining carbon nanomaterials with the molten solution. A first portion of the carbon nanomaterials combined with the molten solution may be dispersed therein. The method may also include cooling the molten solution to solidify at least a portion of the carbon thereof to fabricate the iron castings. The first portion of the carbon nanomaterials may be dispersed in the iron castings.

    Abstract translation: 提供了一种用于制造用于金属部件的铁铸件的方法。 制造铁铸件的方法可以包括通过熔化碳和铁并将碳纳米材料与熔融溶液组合而形成熔融溶液。 与熔融溶液组合的碳纳米材料的第一部分可以分散在其中。 该方法还可以包括冷却熔融溶液以固化其至少一部分碳以制造铁铸件。 碳纳米材料的第一部分可以分散在铁铸件中。

    ONE-PIECE MANUFACTURING PROCESS
    2.
    发明申请
    ONE-PIECE MANUFACTURING PROCESS 审中-公开
    一体制造工艺

    公开(公告)号：US20140230247A1

    公开(公告)日：2014-08-21

    申请号：US14260582

    申请日：2014-04-24

    Applicant: Kevin Pickrell ,  Mark J. Kuzdzal

    Inventor： Kevin Pickrell ,  Mark J. Kuzdzal

    IPC: B23P15/02

    CPC classification number: B23P15/02 ,  B22C7/02 ,  B22C7/023 ,  B22C9/04 ,  B22D19/00 ,  B22F3/1055 ,  B22F5/04 ,  B23P15/006 ,  F01D5/147 ,  F05D2230/10 ,  F05D2230/211 ,  F05D2230/53 ,  Y02P10/292 ,  Y02P10/295 ,  Y10T29/4932

    Abstract: A method of making a turbomachine part, wherein the method can include machining a blank into a base having blades extending therefrom, the blades defining a channel therebetween. The method can also include forming a bridge constructed from refractory material in the channel between the blades, and forming a cover on the tops of the blades and over the channel, such that the base, the blades, and the cover form a single substantially homogenous turbomachine part once the bridge is removed.

    Abstract translation: 一种制造涡轮机零件的方法，其中所述方法可包括将坯件加工成具有从其延伸的刀片的底座中，所述刀片在其间限定通道。 该方法还可以包括在叶片之间的通道中形成由耐火材料构成的桥，并且在叶片的顶部和通道上形成盖，使得基部，叶片和盖形成单个基本均匀的 涡轮机零件一旦桥被拆除。

    ONE-PIECE MANUFACTURING PROCESS
    4.
    发明申请
    ONE-PIECE MANUFACTURING PROCESS 有权
    一体制造工艺

    公开(公告)号：US20120234512A1

    公开(公告)日：2012-09-20

    申请号：US13442068

    申请日：2012-04-09

    Applicant: Kevin Pickrell ,  Mark J. Kuzdzal

    Inventor： Kevin Pickrell ,  Mark J. Kuzdzal

    IPC: B22C9/10

    CPC classification number: B23P15/02 ,  B22C7/02 ,  B22C7/023 ,  B22C9/04 ,  B22D19/00 ,  B22F3/1055 ,  B22F5/04 ,  B23P15/006 ,  F01D5/147 ,  F05D2230/10 ,  F05D2230/211 ,  F05D2230/53 ,  Y02P10/292 ,  Y02P10/295 ,  Y10T29/4932

    Abstract: A method of making a turbomachine part, wherein the method can include machining a blank into a base having blades extending therefrom, the blades defining a channel therebetween. The method can also include forming a bridge constructed from refractory material in the channel between the blades, and forming a cover on the tops of the blades and over the channel, such that the base, the blades, and the cover form a single substantially homogenous turbomachine part once the bridge is removed.

    Abstract translation: 一种制造涡轮机零件的方法，其中所述方法可包括将坯件加工成具有从其延伸的刀片的底座中，所述刀片在其间限定通道。 该方法还可以包括在叶片之间的通道中形成由耐火材料构成的桥，并且在叶片的顶部和通道上形成盖，使得基部，叶片和盖形成单个基本均匀的 涡轮机零件一旦桥被拆除。

    One-piece manufacturing process
    5.
    发明授权
    One-piece manufacturing process 有权
    一体式制造工艺

    公开(公告)号：US08752609B2

    公开(公告)日：2014-06-17

    申请号：US13442068

    申请日：2012-04-09

    Applicant: Kevin Pickrell ,  Mark J. Kuzdzal

    Inventor： Kevin Pickrell ,  Mark J. Kuzdzal

    IPC: B22D19/00

    CPC classification number: B23P15/02 ,  B22C7/02 ,  B22C7/023 ,  B22C9/04 ,  B22D19/00 ,  B22F3/1055 ,  B22F5/04 ,  B23P15/006 ,  F01D5/147 ,  F05D2230/10 ,  F05D2230/211 ,  F05D2230/53 ,  Y02P10/292 ,  Y02P10/295 ,  Y10T29/4932

    Abstract: A method of making a turbomachine part, wherein the method can include machining a blank into a base having blades extending therefrom, the blades defining a channel therebetween. The method can also include forming a bridge constructed from refractory material in the channel between the blades, and forming a cover on the tops of the blades and over the channel, such that the base, the blades, and the cover form a single substantially homogenous turbomachine part once the bridge is removed.

    Abstract translation: 一种制造涡轮机零件的方法，其中所述方法可包括将坯件加工成具有从其延伸的刀片的底座中，所述刀片在其间限定通道。 该方法还可以包括在叶片之间的通道中形成由耐火材料构成的桥，并且在叶片的顶部和通道上形成盖，使得基部，叶片和盖形成单个基本均匀的 涡轮机零件一旦桥被拆除。

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