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    ASSEMBLED BLADE PLATFORM
    1.
    发明申请
    ASSEMBLED BLADE PLATFORM 审中-公开
    组装的刀片平台

    公开(公告)号：WO2014031202A3

    公开(公告)日：2014-05-15

    申请号：PCT/US2013042846

    申请日：2013-05-28

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： MCCAFFREY MICHAEL G ,  HASKO GREGORY H ,  ABBOTT MICHAEL G

    IPC: F01D5/30 ,  F01D5/14 ,  F01D11/00

    CPC classification number: F01D5/147 ,  C04B37/001 ,  C04B2237/365 ,  C04B2237/38 ,  C04B2237/61 ,  C04B2237/84 ,  Y10T29/49336

    Abstract: A method of making a platform of a blade includes the steps of creating two platform sections by solidifying a material with a fabric in a mold and positioning a band of fabric around the two platform sections to retain an airfoil and define a blade. The method further includes the step of bonding the two platform sections together by solidifying the material to define a platform of a solid material. The platform is not bonded to the airfoil.

    Abstract translation: 一种制造刀片平台的方法包括以下步骤：通过在模具中用织物固化材料并且围绕两个平台部分定位织物带来形成两个平台部分以保持翼型并限定刀片。 该方法还包括通过固化材料以限定固体材料的平台来将两个平台部分结合在一起的步骤。 平台没有粘合到翼型上。

    GAS TURBINE ENGINE CERAMIC COMPONENT ASSEMBLY ATTACHMENT
    2.
    发明公开
    GAS TURBINE ENGINE CERAMIC COMPONENT ASSEMBLY ATTACHMENT 审中-公开
    恩宾恩·爱尔兰KERAMIKKOMPONENTENBAUGRUPPEFÜREINEN GASTURBINENMOTOR

    公开(公告)号：EP3022406A4

    公开(公告)日：2016-08-31

    申请号：EP14825748

    申请日：2014-06-17

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： COOK GRANT O III ,  ABBOTT MICHAEL G ,  MCCAFFREY MICHAEL G

    IPC: F01D25/28 ,  F01D5/02 ,  F01D5/28 ,  F01D9/04

    CPC classification number: F01D5/284 ,  F01D5/282 ,  F01D9/042 ,  F01D9/044 ,  F05D2230/23 ,  F05D2230/236 ,  F05D2300/6033 ,  Y02T50/672

    Abstract: A gas turbine engine component assembly includes first and second portions, wherein at least one of the first and second portions is a ceramic material. The first portion includes an aperture having a first angled surface. The second portion is disposed within the aperture and includes a second angled surface adjacent to the first angled surface. The first and second angled surfaces lock the first and second portions to one another under a pulling load. A bonding material operatively secures the first and second angled surfaces to one another.

    Abstract translation: 燃气涡轮发动机部件组件包括第一和第二部分，其中第一部分和第二部分中的至少一个是陶瓷材料。 第一部分包括具有第一倾斜表面的孔。 第二部分设置在孔内并且包括与第一倾斜表面相邻的第二倾斜表面。 第一和第二倾斜表面在牵引载荷下将第一和第二部分彼此锁定。 接合材料将第一和第二倾斜表面相互操作地固定。

    IMPROVED LAMINATE RESIN TRANSFER MOLDING OF FIBROUS PREFORMS USING PARTICLE FILLED RESIN SYSTEMS
    4.
    发明公开
    IMPROVED LAMINATE RESIN TRANSFER MOLDING OF FIBROUS PREFORMS USING PARTICLE FILLED RESIN SYSTEMS 审中-公开
    VERBESSERTES LAMINATHARZSPRITZPRESSEN VON FASERVORFORMEN MITHILFE VONPARTIKELGEFÜLLTENHARZSSTEMEN

    公开(公告)号：EP3162547A1

    公开(公告)日：2017-05-03

    申请号：EP16192942

    申请日：2016-10-07

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： ABBOTT MICHAEL G ,  READ KATHRYN S

    IPC: B29C70/48 ,  C04B35/80

    CPC classification number: B29C45/02 ,  B29C35/02 ,  B29C70/443 ,  B29C70/48 ,  B29C70/68 ,  B29K2083/00 ,  C04B35/571 ,  C04B35/806 ,  C04B2235/483 ,  C04B2235/616

    Abstract: A process for manufacturing a ceramic matrix composite component, said process comprising inserting at least one fibrous sheet (18) into a resin transfer molding system (10). The process includes wetting the at least one (dry or partially wetted) fibrous sheet (18) with a neat first pre-ceramic polymer resin (28). The process includes injecting a second pre-ceramic polymer resin including a filler material (34) into at least one fibrous sheet (18) and curing the pre-ceramic polymer resin (24).

    Abstract translation: 一种制造陶瓷基体复合部件的方法，所述方法包括将至少一个纤维片材（18）插入树脂传递模塑系统（10）中。 该方法包括用纯净的第一预陶瓷聚合物树脂（28）润湿至少一个（干燥或部分润湿的）纤维片材（18）。 该方法包括将包括填充材料（34）的第二预陶瓷聚合物树脂注入至少一个纤维片（18）中并固化预陶瓷聚合物树脂（24）。

    CMC AIRFOIL WITH MONOLITHIC CERAMIC CORE
    6.
    发明公开
    CMC AIRFOIL WITH MONOLITHIC CERAMIC CORE 审中-公开
    CMC-SCHAUFEL MIT MONOLITHISCHEM KERAMIKKERN

    公开(公告)号：EP3039245A4

    公开(公告)日：2017-05-03

    申请号：EP14840150

    申请日：2014-08-19

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： ABBOTT MICHAEL G ,  MCCAFFREY MICHAEL G ,  COOK GRANT O III

    IPC: F01D5/14 ,  F01D9/02

    CPC classification number: F01D5/284 ,  F01D5/14 ,  F01D5/187 ,  F01D5/282 ,  F05D2220/32 ,  F05D2230/23 ,  F05D2300/6033

    Abstract: An airfoil includes a core having a first surface, a skin having a second surface disposed over at least a portion of the first surface of the core, and at least one of a transient liquid phase (TLP) bond and a partial transient liquid phase (PTLP) bond. The bond(s) are disposed between the first surface and the second surface, joining the skin to the core.

    Abstract translation: 翼型件包括具有第一表面的芯体，具有布置在芯体的第一表面的至少一部分上方的第二表面的表皮，以及瞬态液相（TLP）结合和部分瞬态液相（ PTLP）债券。 粘合剂设置在第一表面和第二表面之间，将蒙皮与芯连接。

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