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    ADDITIVE MANUFACTURING PROCESS DISTORTION MANAGEMENT
    21.
    发明公开
    ADDITIVE MANUFACTURING PROCESS DISTORTION MANAGEMENT 审中-公开
    VERZERRUNGSVERWALTUNGFÜRVERFAHREN ZUR ADDITIVEN FERTIGUNG

    公开(公告)号：EP3089862A1

    公开(公告)日：2016-11-09

    申请号：EP15733072.1

    申请日：2015-01-02

    Applicant: United Technologies Corporation

    Inventor： MIRONETS, Sergey ,  KIRONN, Lexia ,  OTT, Joe ,  PORRETTI, Louis

    IPC: B29C67/00

    CPC classification number: B29C67/0088 ,  B22F3/1055 ,  B22F2003/1056 ,  B22F2003/1057 ,  B29C64/153 ,  B29C64/20 ,  B29C64/386 ,  B33Y10/00 ,  B33Y30/00 ,  B33Y50/02

    Abstract: A method is provided for additive manufacturing. This method includes monitoring a current to a recoater blade. The monitored current is compared to a predetermined current. An operation is initiated in response to the monitored current exceeding the predetermined current. Another method for additive manufacturing includes comparing a movement of a recoater blade to an expected movement. A single exposure sequence is initiated in response to movement of the recoater blade being different than an expected movement. An additive manufacturing system is also provided which includes a recoated blade and a control. The control is operable to identify resistance to movement of the recoater blade.

    Abstract translation: 提供了一种用于添加剂制造的方法。 该方法包括监测到重涂刀片的电流。 将监视的电流与预定电流进行比较。 响应于超过预定电流的监视电流启动操作。 添加剂制造的另一种方法包括将再涂布刀片的运动与预期的运动进行比较。 响应于重涂器刀片的运动而不同于预期的运动而启动单个曝光序列。 还提供了包括重涂刀片和控制装置的添加剂制造系统。 该控制可操作以识别对重涂器叶片的运动的阻力。

    TUBE ASSEMBLY
    22.
    发明公开
    TUBE ASSEMBLY 有权
    ROHRANORDNUNG

    公开(公告)号：EP2963347A1

    公开(公告)日：2016-01-06

    申请号：EP15175177.3

    申请日：2015-07-03

    Applicant: United Technologies Corporation

    Inventor： OTT, Joe ,  RUP, Jr., John J. ,  FUNK, Stanley J. ,  MOURA, Dennis M. ,  KIRONN, Lexia ,  COFFEY, Roger O.

    IPC: F23R3/28

    CPC classification number: F28F1/00 ,  F16L9/18 ,  F16L59/14 ,  F23D2211/00 ,  F23D2900/00016 ,  F23R3/283

    Abstract: A tube assembly that may be for a fuel nozzle (20) of a fuel system of a gas turbine engine may have a first tube (56) defining a first flowpath (59) along a centerline (52), a second tube (58) generally spaced radially outward from the first tube (56) with a first void (60) located between and defined by the first and second tubes (56, 58), and a support structure (68) located in the first void (60) and extending between the first and second tubes (56, 58). The support structure (68) is constructed and arranged to minimize or eliminate thermal conduction between the tubes (56, 58). The entire assembly may be additive manufactured as one unitary piece. One example of a method of operation may include designed-for breakage of the structural support (68) due to thermal stresses thereby further minimizing thermal conduction between tubes (56, 58).

    Abstract translation: 可用于燃气涡轮发动机的燃料系统的燃料喷嘴（20）的管组件可以具有沿着中心线（52）限定第一流路（59）的第一管（56），第二管（58） 通常与第一管（56）径向向外隔开，第一空腔（60）位于第一和第二管（56,58）之间并由第一和第二管（56,58）限定;以及位于第一空腔（60）中的支撑结构（68） 在第一和第二管（56,58）之间延伸。 支撑结构（68）被构造和布置成最小化或消除管（56,58）之间的热传导。 整个组件可以是作为一个整体件制造的添加剂。 操作方法的一个实例可以包括设计用于由于热应力破坏结构支撑件（68），从而进一步最小化管（56,58）之间的热传导。

    LINE REPLACEABLE FUEL NOZZLE APPARATUS, SYSTEM AND METHOD
    24.
    发明公开
    LINE REPLACEABLE FUEL NOZZLE APPARATUS, SYSTEM AND METHOD 审中-公开

    公开(公告)号：EP3511627A1

    公开(公告)日：2019-07-17

    申请号：EP19153954.3

    申请日：2015-12-18

    Applicant: United Technologies Corporation

    Inventor： DAI, Zhongtao ,  KOPP-VAUGHAN, Kristin ,  HYLAND, Dave ,  HANSON, Russell B ,  KIRONN, Lexia

    IPC: F23R3/28 ,  F23R3/34 ,  F23R3/14

    Abstract: In various embodiments, a fuel injector (120; 220; 320; 530; 630) may comprise a fuel nozzle (230; 330; 430) and a pilot stage (252; 350). The fuel nozzle (230; 330; 430) may define a main fuel channel (231; 534), a secondary fuel channel (233; 536), a simplex fuel channel (235; 538) and a heat shield area (232). The main fuel channel (231; 534) may be disposed about at least a portion of the simplex fuel channel (235; 538). The secondary fuel channel (233; 536) may be disposed about at least a portion of the simplex fuel channel (235; 538). The heat shield area (232) may be configured to separate and protect the fuel channels from a heat load to prevent fuel coking. The pilot stage (252; 350) may be operatively coupled to the fuel nozzle (230; 330; 430) and may be configured to receive fuel from the secondary fuel channel (233; 536) or the simplex fuel channel (235; 538). The main stage (242) may be operatively coupled to the fuel nozzle (230; 330; 430). The main stage (242) may be configured to receive fuel from the main fuel channel (231; 534).

    TUBE ASSEMBLY
    30.
    发明授权
    TUBE ASSEMBLY 有权
    管组件

    公开(公告)号：EP2963347B1

    公开(公告)日：2017-11-15

    申请号：EP15175177.3

    申请日：2015-07-03

    Applicant: United Technologies Corporation

    Inventor： OTT, Joe ,  RUP, Jr., John J. ,  FUNK, Stanley J. ,  MOURA, Dennis M. ,  KIRONN, Lexia ,  COFFEY, Roger O.

    IPC: F23R3/28

    CPC classification number: F28F1/00 ,  F16L9/18 ,  F16L59/14 ,  F23D2211/00 ,  F23D2900/00016 ,  F23R3/283

    Abstract: A tube assembly that may be for a fuel nozzle (20) of a fuel system of a gas turbine engine may have a first tube (56) defining a first flowpath (59) along a centerline (52), a second tube (58) generally spaced radially outward from the first tube (56) with a first void (60) located between and defined by the first and second tubes (56, 58), and a support structure (68) located in the first void (60) and extending between the first and second tubes (56, 58). The support structure (68) is constructed and arranged to minimize or eliminate thermal conduction between the tubes (56, 58). The entire assembly may be additive manufactured as one unitary piece. One example of a method of operation may include designed-for breakage of the structural support (68) due to thermal stresses thereby further minimizing thermal conduction between tubes (56, 58).

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