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    AIRFOIL HAVING INTERNAL LATTICE NETWORK
    1.
    发明申请
    AIRFOIL HAVING INTERNAL LATTICE NETWORK 审中-公开
    具有内部网格网络的AIRFOIL

    公开(公告)号：WO2014011290A3

    公开(公告)日：2014-04-03

    申请号：PCT/US2013036511

    申请日：2013-04-14

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： FISK BENJAMIN T ,  PROPHETER-HINCKLEY TRACY A ,  TRACY ANITA L ,  LOUREIRO SERGIO M ,  KLUCHA AGNES

    IPC: F01D5/14 ,  F02C7/00

    CPC classification number: F04D29/388 ,  F01D5/16 ,  F02C3/04 ,  F02K3/06 ,  F04D29/325 ,  F05D2220/32 ,  F05D2240/24 ,  F05D2240/30

    Abstract: An airfoil includes an airfoil body that defines a longitudinal axis. The airfoil body includes a leading edge and a trailing edge and a first side wall and a second side wall that is spaced apart from the first side wall. The first side wall and the second side wall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. A lattice network connects the first side and the second side. The lattice network includes at least one enlarged node spaced apart from the first side wall and the second side wall and ribs that extend from the at least one enlarged node. Each of the ribs connects to one of the first side wall and the second side wall.

    Abstract translation: 翼型包括限定纵向轴线的翼型体。 翼型体包括前缘和后缘以及第一侧壁和与第一侧壁间隔开的第二侧壁。 第一侧壁和第二侧壁连接前缘和后缘并且至少部分地限定翼型体中的空腔。 格子网络连接第一面和第二面。 格子网络包括与第一侧壁和第二侧壁间隔开的至少一个放大节点以及从至少一个放大节点延伸的肋。 每个肋连接到第一侧壁和第二侧壁中的一个。

    AIRFOIL HAVING MINIMUM DISTANCE RIBS
    3.
    发明申请
    AIRFOIL HAVING MINIMUM DISTANCE RIBS 审中-公开
    AIRFOIL具有最小距离的RIBS

    公开(公告)号：WO2014011289A3

    公开(公告)日：2014-03-27

    申请号：PCT/US2013036510

    申请日：2013-04-14

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： FISK BENJAMIN T ,  PROPHETER-HINCKLEY TRACY A ,  DOLANSKY GREGORY M ,  TRACY ANITA L ,  TAFFET STEVEN

    IPC: F01D5/14 ,  F02C7/00

    CPC classification number: F01D5/147 ,  B23P15/02 ,  F01D5/187 ,  F05D2260/22141 ,  Y10T29/49336

    Abstract: An airfoil includes an airfoil body that defines a longitudinal axis. The airfoil body includes a leading edge and a trailing edge and a first side wall and a second side wall that is spaced apart from the first side wall to define a camber line there between. The first side wall and the second side wall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. Multiple ribs extend longitudinally in the cavity and are laterally spaced apart from each other relative to the longitudinal axis. In at least one plane that is perpendicular to the longitudinal axis, each of the ribs connects the first side wall and the second side wall along respective minimum distance directions that are perpendicular to the camber line. At least two of the respective minimum distance directions are non-parallel.

    Abstract translation: 翼型包括限定纵向轴线的翼型体。 翼型体包括前缘和后缘以及第一侧壁和第二侧壁，第二侧壁与第一侧壁间隔开以在其间限定弧线。 第一侧壁和第二侧壁连接前缘和后缘并且至少部分地限定翼型体中的空腔。 多个肋在腔内纵向延伸并且相对于纵向轴线彼此侧向间隔开。 在垂直于纵向轴线的至少一个平面中，每个肋沿着垂直于弧线的相应最小距离方向连接第一侧壁和第二侧壁。 各个最小距离方向中的至少两个是不平行的。

    MULTI-DIMENSIONAL COMPONENT BUILD SYSTEM AND PROCESS
    6.
    发明专利
    MULTI-DIMENSIONAL COMPONENT BUILD SYSTEM AND PROCESS 未知

    公开(公告)号：SG11201402665QA

    公开(公告)日：2014-09-26

    申请号：SG11201402665Q

    申请日：2013-01-17

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： MIRONETS SERGEY ,  KLUCHA AGNES ,  TWELVES JR WENDELL V ,  FISK BENJAMIN T

    IPC: F01D25/12

    Abstract: A multi-dimensional component building system (18) comprising a first chamber (10) adjacent to and in fluid communication with at least one second chamber (12) through at least one door, wherein the first chamber (10) is fluidly sealed from the at least one second chamber (12) if the at least one door is in a closed position, the at least one second chamber (12) configured to provide a base to a first platform in the first chamber (10) if at least one door is open and fluid parameters of the first chamber (10) and the at least one second chamber (12) are substantially equal, wherein the first chamber (10) includes the first platform moveable by a first piston adjacent a second platform moveable by a second piston, wherein the first platform is configured to receive at least one base, wherein a dispenser in communication with build-up material disposed on the second platform is configured to move a portion of the build-up material from the second platform onto the at least one base on the first platform, the first chamber (10) including a beam source to form a component on the at least one base from the build-up material by melting or sintering.

    AIRFOIL INCLUDING DAMPER MEMBER
    7.
    发明专利
    AIRFOIL INCLUDING DAMPER MEMBER 未知

    公开(公告)号：SG11201406220RA

    公开(公告)日：2014-11-27

    申请号：SG11201406220R

    申请日：2013-04-20

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： DOLANSKY GREGORY M ,  PROPHETER-HINCKLEY TRACY A ,  FISK BENJAMIN T

    IPC: F01D5/12 ,  F01D5/18 ,  F01D9/00 ,  F02K3/00 ,  F03C7/00

    Abstract: An airfoil includes an airfoil body that defines a longitudinal axis. The airfoil body includes a leading edge and a trailing edge and a first sidewall and a second sidewall that is faced apart from the first sidewall. The first sidewall and the second sidewall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. A damper member is enclosed in the cavity. The damper member includes a first end and a second end. The first end is connected in a first joint to the first sidewall at a first longitudinal location and the second end is connected in a second joint to the second sidewall at a second, different longitudinal location.

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