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    INTEGRAL INSTRUMENTATION IN ADDITIVELY MANUFACTURED COMPONENTS OF GAS TURBINE ENGINES
    1.
    发明申请
    INTEGRAL INSTRUMENTATION IN ADDITIVELY MANUFACTURED COMPONENTS OF GAS TURBINE ENGINES 审中-公开
    气体涡轮发动机的大量制造成分的综合仪表

    公开(公告)号：WO2014105245A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/063372

    申请日：2013-10-04

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： HUDON, David J. ,  ROBERTS, Steven D. ,  SCHIRTZINGER, Gary A. ,  OTT, Joe

    IPC: F01D5/12 ,  F01D5/00 ,  F02C7/00 ,  G01K1/16

    CPC classification number: F01D21/003 ,  F01D17/02 ,  F01D17/08 ,  F05D2230/22 ,  F05D2230/30 ,  F05D2260/83 ,  Y10T29/49

    Abstract: An article includes a body portion made of a metal and configured for use in a gas turbine engine, a sensing feature monolithically formed with the body portion, and an interior passage connected to the sensing feature and passing through the body portion. An article with integrated sensing features may be made additive manufacturing, resulting in a structure having internal passageways connecting an aperture at one surface of the monolithic article to a second aperture at another surface of the monolithic article at the opposite end of the internal passageway.

    Abstract translation: 一种物品包括由金属制成并构造成用于燃气涡轮发动机的主体部分，与主体部分整体形成的感测特征，以及连接到感测特征并穿过主体部分的内部通道。 具有集成感测特征的物品可以被制成添加剂制造，从而形成一个结构，其内部通道将整体制品的一个表面处的孔连接到在内部通道的相对端处的整体制品的另一个表面处的第二孔。

    VANE ARM ASSEMBLY FOR A GAS TURBINE ENGINE AND CORRESPONDING GAS TURBINE ENGINE
    2.
    发明公开
    VANE ARM ASSEMBLY FOR A GAS TURBINE ENGINE AND CORRESPONDING GAS TURBINE ENGINE 审中-公开

    公开(公告)号：EP3683408A3

    公开(公告)日：2020-08-05

    申请号：EP19209583.4

    申请日：2019-11-15

    Applicant: United Technologies Corporation

    Inventor： PRATT, William S. ,  BINTZ, Matthew E. ,  ROBERTS, Steven D. ,  HART, Adam

    IPC: F01D17/16 ,  F04D29/56

    Abstract: A vane arm assembly (100) for a gas turbine engine (20) is provided including: a vane arm (102) having a first end (106), a second end (110) opposite the first end, and an aperture (116) proximate the second end, the aperture being defined by an aperture wall (142); a vane stem (108) extending through the aperture of the vane arm; a mechanical fastener (112) retaining a position of the vane arm in the longitudinal direction of the vane stem; and an impedance clip (114) partially enclosing a portion of the second end of the vane arm to provide redundant position retention of the vane arm in the longitudinal direction of the vane stem. A corresponding gas turbine engine (20) is also provided comprising a compressor section (24); a combustor section (26); a turbine section (28); and such a vane arm assembly (100) operatively coupled to an actuator ring and to at least one adjustable guide vane in the compressor section.

    INSERTS FOR SLOTTED INTEGRALLY BLADED ROTOR
    4.
    发明公开
    INSERTS FOR SLOTTED INTEGRALLY BLADED ROTOR 审中-公开

    公开(公告)号：EP3708778A1

    公开(公告)日：2020-09-16

    申请号：EP20151301.7

    申请日：2020-01-10

    Applicant: United Technologies Corporation

    Inventor： BEHLING, Weston ,  LEROUX, Jason ,  FULLER, Robert B. ,  ROBERTS, Steven D.

    IPC: F01D5/34 ,  F01D11/00 ,  B23P15/00 ,  F01D5/14 ,  F01D5/28

    Abstract: Integrally bladed rotors (IBRs) are described. The IBRs include a central hub (306;506;606), an outer rim (302;502;602) defining an outer circumference of the central hub, the outer rim defining a plurality of platforms, a plurality of circumferentially distributed blades (304;504;604), wherein a blade extends from each of the plurality of platforms, a rotor slot (308;508) arranged between two adjacent blades, wherein the rotor slot is defined by a cut within the outer rim, and a rotor slot insert (520;612) installed within the rotor slot, the rotor slot insert sized and shaped to fit within the rotor slot and prevent air leakage from a first side (608) of the central hub to a second side (610) of the central hub through the rotor slot during operation of the integrally bladed rotor.

    VANE ARM ASSEMBLY FOR A GAS TURBINE ENGINE AND CORRESPONDING GAS TURBINE ENGINE
    6.
    发明公开
    VANE ARM ASSEMBLY FOR A GAS TURBINE ENGINE AND CORRESPONDING GAS TURBINE ENGINE 审中-公开

    公开(公告)号：EP3683408A2

    公开(公告)日：2020-07-22

    申请号：EP19209583.4

    申请日：2019-11-15

    Applicant: United Technologies Corporation

    Inventor： PRATT, William S. ,  BINTZ, Matthew E. ,  ROBERTS, Steven D. ,  HART, Adam

    IPC: F01D17/16 ,  F04D29/56

    Abstract: A vane arm assembly (100) for a gas turbine engine (20) is provided including: a vane arm (102) having a first end (106), a second end (110) opposite the first end, and an aperture (116) proximate the second end, the aperture being defined by an aperture wall (142); a vane stem (108) extending through the aperture of the vane arm; a mechanical fastener (112) retaining a position of the vane arm in the longitudinal direction of the vane stem; and an impedance clip (114) partially enclosing a portion of the second end of the vane arm to provide redundant position retention of the vane arm in the longitudinal direction of the vane stem. A corresponding gas turbine engine (20) is also provided comprising a compressor section (24); a combustor section (26); a turbine section (28); and such a vane arm assembly (100) operatively coupled to an actuator ring and to at least one adjustable guide vane in the compressor section.

    VARIABLE VANE ACTUATION SYSTEM WITH NESTED DIRECT VANE ANGLE MEASUREMENT SHAFT
    7.
    发明公开
    VARIABLE VANE ACTUATION SYSTEM WITH NESTED DIRECT VANE ANGLE MEASUREMENT SHAFT 审中-公开

    公开(公告)号：EP3564491A1

    公开(公告)日：2019-11-06

    申请号：EP19160412.3

    申请日：2019-03-01

    Applicant: United Technologies Corporation

    Inventor： PRATT, William S. ,  AMARI, Martin Richard ,  ROBERTS, Steven D. ,  STANLEY, Ryan M.

    IPC: F01D17/16

    Abstract: A variable vane actuation system (62) of a gas turbine engine (20) is provided. The variable vane actuation system (62) including: a variable vane (72); a vane stem (68) operably associated with the variable vane (72), wherein the variable vane (72) is configured to rotate with the vane stem (68); a vane arm (64) having vane stem end (88) and a vane pin end (76) opposite the vane stem end (88), the vane arm (64) being operably connected to the vane stem (68) at the vane stem end (88); and a rotational variable differential transformer (100) operably connected to the vane stem (68), the rotational variable differential transformer (100) configured to detect an amount of rotation of the vane stem (68).

    SELF-RETAINING VANE ARM ASSEMBLY FOR GAS TURBINE ENGINE
    8.
    发明公开
    SELF-RETAINING VANE ARM ASSEMBLY FOR GAS TURBINE ENGINE 审中-公开

    公开(公告)号：EP3533973A1

    公开(公告)日：2019-09-04

    申请号：EP18215629.9

    申请日：2018-12-21

    Applicant: United Technologies Corporation

    Inventor： KJELBY, Diane C. ,  PRATT, William S. ,  HART, Adam ,  ROBERTS, Steven D.

    IPC: F01D17/16 ,  F04D29/56 ,  F02C9/20

    Abstract: A vane arm assembly (100) for a gas turbine engine (20). The vane arm assembly includes a vane arm (102) defining an aperture at an end thereof with an aperture wall. The vane arm assembly also includes a vane stem (108) extending through the aperture of the vane arm. The vane arm assembly further includes a mechanical fastener (112) retaining a position of the vane arm in the longitudinal direction of the vane stem. The vane arm assembly yet further includes an impedance ring (114) disposed within the aperture of the vane arm and within an impedance ring groove (140) defined by the vane stem to provide redundant position retention of the vane arm in the longitudinal direction of the vane stem.

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