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    TURBINE ENGINE COMPONENT WITH DUAL PURPOSE RIB
    1.
    发明申请
    TURBINE ENGINE COMPONENT WITH DUAL PURPOSE RIB 审中-公开
    涡轮发动机组件与双用途RIB

    公开(公告)号：WO2014105658A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/076761

    申请日：2013-12-19

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： CHUONG, Conway ,  BUDNICK, Matthew

    IPC: F02C7/20 ,  F01D25/28

    CPC classification number: F02C7/28 ,  F01D9/02 ,  F01D11/005 ,  F01D25/162 ,  F01D25/28 ,  F05D2240/55

    Abstract: An assembly for a gas turbine engine includes a component, a fairing, and a seal. The fairing is disposed adjacent to the component and defines a primary gas flow path. The fairing has a rib that is located outside of the primary flow path and extends from an outer surface of the fairing. The seal is disposed between the rib and the component.

    Abstract translation: 用于燃气涡轮发动机的组件包括部件，整流罩和密封件。 整流罩靠近部件设置并限定主要气体流动路径。 整流罩具有位于主流路外部并从整流罩的外表面延伸的肋。 密封件设置在肋和部件之间。

    MECHANICAL LINKAGE FOR SEGMENTED HEAT SHIELD
    2.
    发明申请
    MECHANICAL LINKAGE FOR SEGMENTED HEAT SHIELD 审中-公开
    机械连接装置

    公开(公告)号：WO2014105512A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/075632

    申请日：2013-12-17

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： BUDNICK, Matthew ,  CHUONG, Conway ,  SCOTT, Jonathan A.

    IPC: F02C7/20 ,  F02C7/24 ,  F01D25/28

    CPC classification number: F01D9/041 ,  F01D25/145 ,  F01D25/162 ,  F01D25/24 ,  F01D25/246 ,  F01D25/28 ,  F01D25/30 ,  F05D2220/32 ,  F05D2240/15 ,  F05D2260/231 ,  F05D2260/30 ,  F05D2260/31

    Abstract: A turbine exhaust case comprises a frame, a fairing, a heat shield and a mechanical linkage. The frame comprises an outer ring, an inner ring, and a plurality of struts joining the outer ring and the inner ring. The fairing comprising a ring-strut-ring structure disposed within the frame. The heat shield is disposed between the frame and the fairing. The mechanical linkage couples the heat shield to the fairing. In one embodiment, the heat shield comprises a multi-piece heat shield that inhibits heat transfer between the frame and the fairing. In various embodiments, the mechanical linkage comprises a slip joint or a fixed joint for coupling the heat shield to the fairing.

    Abstract translation: 涡轮机排气箱包括框架，整流罩，隔热罩和机械连杆。 框架包括外圈，内圈和连接外环和内圈的多个支柱。 整流罩包括设置在框架内的环形支撑结构。 隔热罩设置在框架和整流罩之间。 机械连接将隔热罩连接到整流罩。 在一个实施例中，隔热罩包括防止框架和整流罩之间的热传递的多件式隔热罩。 在各种实施例中，机械联动装置包括用于将隔热罩连接到整流罩的滑动接头或固定接头。

    PASSAGES TO FACILITATE A SECONDARY FLOW BETWEEN COMPONENTS
    3.
    发明申请
    PASSAGES TO FACILITATE A SECONDARY FLOW BETWEEN COMPONENTS 审中-公开
    促进组件之间的二次流动的通道

    公开(公告)号：WO2014105492A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/075449

    申请日：2013-12-16

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： CHUONG, Conway ,  BUDNICK, Matthew

    IPC: F01D25/12 ,  F02C7/12

    CPC classification number: F02C7/20 ,  F01D11/14 ,  F01D25/12 ,  F01D25/162 ,  F01D25/243 ,  F01D25/265 ,  F01D25/28 ,  Y02T50/675

    Abstract: An annular mount for a gas turbine engine includes a first flange and a second flange. The first flange has an arcuate shape, and the second flange extends from the first flange. The second flange has an interface surface along at least one side and has a plurality of mounting apertures extending therethrough. The channels extend along a length of the interface surface from a first edge to a second edge.

    Abstract translation: 用于燃气涡轮发动机的环形安装件包括第一凸缘和第二凸缘。 第一凸缘具有弓形形状，第二凸缘从第一凸缘延伸。 第二凸缘具有沿着至少一个侧面的界面，并具有贯穿其中的多个安装孔。 通道沿着接口表面的长度从第一边缘延伸到第二边缘。

    PLATE FOR DIRECTING FLOW AND FILM COOLING OF COMPONENTS
    4.
    发明申请
    PLATE FOR DIRECTING FLOW AND FILM COOLING OF COMPONENTS 审中-公开
    用于指导部件的流动和膜冷却的板

    公开(公告)号：WO2014133648A2

    公开(公告)日：2014-09-04

    申请号：PCT/US2013/075422

    申请日：2013-12-16

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： CHUONG, Conway ,  BUDNICK, Matthew

    CPC classification number: F01D25/246 ,  F01D25/162 ,  F05D2260/201 ,  Y02T50/675

    Abstract: An assembly includes a gas turbine engine component and a plate. The plate is spaced from a surface of the component and generally conforms to the shape of the surface. The plate and component form a passageway that allows for passage of a secondary gas flow between the component and the plate.

    Abstract translation: 组件包括燃气涡轮发动机部件和板。 该板与部件的表面间隔开并且大致与表面的形状一致。 板和部件形成允许在部件和板之间通过辅助气流的通道。

    HEAT SHIELD BASED AIR DAM FOR A TURBINE EXHAUST CASE
    5.
    发明申请
    HEAT SHIELD BASED AIR DAM FOR A TURBINE EXHAUST CASE 审中-公开
    用于涡轮机排气的热屏蔽空气

    公开(公告)号：WO2014105573A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/076169

    申请日：2013-12-18

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： YEAGER, William ,  CHUONG, Conway ,  BUDNICK, Matthew

    IPC: F01D25/30 ,  F01D25/24 ,  F02C7/20

    CPC classification number: F01D25/14 ,  F01D9/041 ,  F01D9/065 ,  F01D25/162 ,  F01D25/30 ,  F02C7/18 ,  F05D2240/15 ,  Y02T50/675

    Abstract: A turbine exhaust case employed in an industrial gas turbine engine includes a frame, a fairing and a heat shield. The frame includes an outer ring, an inner ring, and struts connected between the outer ring and the inner ring. The fairing includes a fairing outer ring, a fairing inner ring, and fairing struts connected between the fairing outer ring and the fairing inner ring. The heat shield is located between the frame outer ring and the fairing outer ring and provides a thermal barrier between the fairing outer ring and the frame outer ring, wherein the heat shield includes an aft portion having a flange that interfaces with the frame outer ring to form an air dam that directs cooling airflow forward along the frame outer ring within an outer diameter cavity formed between the frame outer ring and the heat shield.

    Abstract translation: 在工业燃气涡轮发动机中使用的涡轮机排气箱包括框架，整流罩和隔热罩。 框架包括外环和内圈以及连接在外圈和内圈之间的支柱。 整流罩包括整流罩外圈，整流罩内圈和连接在整流罩外圈和整流罩内圈之间的整流罩支柱。 隔热罩位于框架外圈和整流罩外圈之间，并且在整流罩外圈和框架外圈之间提供隔热罩，其中隔热罩包括具有凸缘的后部，该凸缘与框架外圈 在形成在框架外圈和隔热罩之间的外径腔内形成一个空气坝，该空气坝沿着框架外环向前引导冷却气流。

    CORRUGATED MID-TURBINE FRAME THERMAL RADIATION SHIELD
    6.
    发明申请
    CORRUGATED MID-TURBINE FRAME THERMAL RADIATION SHIELD 审中-公开

    公开(公告)号：WO2014058483A3

    公开(公告)日：2014-04-17

    申请号：PCT/US2013/046780

    申请日：2013-06-20

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： ZIMMERMANN, Alisha ,  LIEBEL, Christina, S, ,  CHUONG, Conway

    IPC: F01D25/24 ,  F01D25/00 ,  F02C7/00

    Abstract: A corrugated shield comprises a mounting base and a corrugated ring section. The mounting base is disposed at an aft end of the ring section for securing the shield ring section within a generally annular cavity. The generally annular cavity is defined at least in part by a hot fluid flow path boundary wall, and a radially adjacent and spaced apart cold fluid flow path boundary wall. The corrugated ring section is configured to substantially block a line of sight between the hot fluid flow path boundary wall and the cold fluid flow path boundary wall.

    GAS TURBINE SEAL ASSEMBLY AND SEAL SUPPORT
    7.
    发明申请
    GAS TURBINE SEAL ASSEMBLY AND SEAL SUPPORT 审中-公开
    气体涡轮密封组件和密封支撑

    公开(公告)号：WO2014105800A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/077437

    申请日：2013-12-23

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： CHUONG, Conway ,  BUDNICK, Matthew

    IPC: F01D11/02 ,  F01D25/24 ,  F02C7/28

    CPC classification number: F01D11/003 ,  F01D11/005 ,  F01D25/162 ,  F01D25/246 ,  F01D25/30 ,  F02C7/28 ,  F05D2220/32

    Abstract: A gas turbine engine assembly includes a second module interconnected with a first module along a joint such that a surface of a second radial wall faces a surface of a first radial wall, with a cavity defined in part by the first and second radial walls. A seal assembly includes a finger seal, and a seal support ring having a backing ring portion and a flow discourager arm. The backing ring is secured to one of the first radial wall and the second radial wall, and the flow discourager arm extends axially through the cavity into a recess formed in the other of the first and second radial walls. The finger seal includes a free end contacting an inner side of the flow discourager arm.

    Abstract translation: 燃气涡轮发动机组件包括沿着接头与第一模块相互连接的第二模块，使得第二径向壁的表面面对第一径向壁的表面，其中空腔部分地由第一和第二径向壁限定。 密封组件包括指状密封件和具有背衬环部分和流动阻挡件臂的密封件支撑环。 背衬环固定到第一径向壁和第二径向壁中的一个，并且流动障碍物臂轴向延伸穿过空腔进入形成在第一和第二径向壁中的另一个中的凹部中。 手指密封件包括接触流动打气机臂的内侧的自由端。

    SLIDER SEAL
    10.
    发明申请
    SLIDER SEAL 审中-公开
    滑块密封

    公开(公告)号：WO2014105598A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/076368

    申请日：2013-12-19

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： CHUONG, Conway ,  BUDNICK, Matthew ,  WEIDNER, Darrell

    IPC: F02C7/28 ,  F01D25/00

    CPC classification number: F01D25/24 ,  F05D2260/80 ,  Y02T50/672

    Abstract: An assembly for a gas turbine engine includes a component, a seal element, and a seal cap. The component defines a pocket adapted to accept the seal element and the pocket allows for sliding movement of the component relative to the seal element. The seal cap overlying the pocket and the seal element.

    Abstract translation: 用于燃气涡轮发动机的组件包括部件，密封元件和密封盖。 该部件限定适于接受密封元件的口袋，并且该口袋允许该部件相对于该密封件的滑动运动。 密封帽覆盖在口袋和密封元件上。

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