中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

29 records (took 0.02 seconds)

    ASYMMETRIC APPLICATION OF COOLING FEATURES FOR A CAST PLATE HEAT EXCHANGER
    22.
    发明申请
    ASYMMETRIC APPLICATION OF COOLING FEATURES FOR A CAST PLATE HEAT EXCHANGER 审中-公开

    公开(公告)号：US20190293367A1

    公开(公告)日：2019-09-26

    申请号：US16276801

    申请日：2019-02-15

    Applicant: United Technologies Corporation

    Inventor： William P. Stillman ,  Michael A. Disori ,  Matthew A. Devore ,  Dave J. Hyland ,  Adam J. Diener

    IPC: F28F3/08 ,  F28F3/02

    Abstract: A cast plate heat exchanger includes a first surface including a first surface inlet end and a first group of augmentation features defining a first average density of augmentation features across the first surface. A second surface is in heat transfer communication with the first surface. The second surface includes a second surfaces inlet end and a second group of augmentation features defining a second average density of augmentation features across the second surface. A total augmentation feature density ratio is defined from the first average density of augmentation features to the second average density of augmentation features. A first region is shared by both the first surface and the second surface and covers at least a portion of the first surface inlet end. The first region includes a first region augmentation feature density ratio that is less than the total augmentation feature density ratio.

    Secondary seal device(s) with alignment tab(s)
    23.
    发明授权
    Secondary seal device(s) with alignment tab(s) 有权

    公开(公告)号：US10221714B2

    公开(公告)日：2019-03-05

    申请号：US15004556

    申请日：2016-01-22

    Applicant: United Technologies Corporation

    Inventor： Christopher J. Peters ,  Dave J. Hyland

    IPC: F01D11/04 ,  F01D5/02 ,  F01D9/02 ,  F16J15/44 ,  F01D11/02

    Abstract: An assembly is provided for rotational equipment with an axial centerline. This assembly includes a primary seal device, a ring structure and a secondary seal device. The primary seal device is configured as a hydrostatic non-contact seal device. The primary seal device includes a plurality of seal shoes and a seal base. The seal shoes are arranged circumferentially about the axial centerline in an annular array. The seal base circumscribes the annular array of the seal shoes. The ring structure is axially engaged with the seal base. The secondary seal device is mounted with the ring structure. The secondary seal device includes a seal ring body and an alignment tab. The seal ring body is configured to substantially seal an annular gap between the ring structure and the seal base. The alignment tab projects out from the seal ring body and into an aperture in the ring structure. The alignment tab is adapted to substantially rotationally locate and/or fix the secondary seal device to the ring structure.

    High Compressor Exit Guide Vane Assembly to Pre-Diffuser Junction
    25.
    发明申请
    High Compressor Exit Guide Vane Assembly to Pre-Diffuser Junction 审中-公开
    高压缩机出口指南叶片装配到预扩散器结

    公开(公告)号：US20160169245A1

    公开(公告)日：2016-06-16

    申请号：US14935628

    申请日：2015-11-09

    Applicant: United Technologies Corporation

    Inventor： Jonathan Jeffery Eastwood ,  Dave J. Hyland ,  Timothy Dale ,  Matthew R. Willett

    IPC: F04D29/54 ,  F04D19/02

    CPC classification number: F04D29/542 ,  F01D9/023 ,  F01D9/041 ,  F01D11/005 ,  F04D29/083 ,  F05D2220/3219 ,  F05D2230/642 ,  F05D2260/36

    Abstract: A pre-diffuser and exit guide vane (EGV) system for a gas turbine engine includes an annular EGV assembly containing a number of guide vanes and having an annular opening bounded by a radially inner annular sealing surface at a first radius and a radially outer annular sealing surface at a second radius. First and second seals substantially matching the first and second radii respectively join the EGV assembly to an annular pre-diffuser having an annular opening bounded by radially inner and outer annular sealing surfaces at substantially the first and second radii. The seals seal the inner sealing surface of the EGV assembly to the inner sealing surface of the pre-diffuser and the second seal seals the outer sealing surface of the EGV assembly to the outer sealing surface of the pre-diffuser, such that the EGV assembly annular opening is in fluid communication with the annular opening of the pre-diffuser.

    Abstract translation: 用于燃气涡轮发动机的预扩散器和出口导叶（EGV）系统包括环形EGV组件，其包含多个导向叶片，并且具有环形开口，该环形开口由第一半径处的径向内部环形密封表面限定，并且径向外部环形 密封表面在第二个半径。 基本上匹配第一和第二半径的第一和第二密封分别将EGV组件连接到环形预扩散器，该环形预扩散器具有基本上第一和第二半径处的径向内部和外部环形密封表面限定的环形开口。 密封件将EGV组件的内部密封表面密封到预扩散器的内部密封表面，并且第二密封件将EGV组件的外部密封表面密封到预扩散器的外部密封表面，使得EGV组件 环形开口与预扩散器的环形开口流体连通。

    Pre-Diffuser Strut for Gas Turbine Engine
    26.
    发明申请
    Pre-Diffuser Strut for Gas Turbine Engine 审中-公开
    燃气轮机发动机前扩散器支柱

    公开(公告)号：US20160169049A1

    公开(公告)日：2016-06-16

    申请号：US14934435

    申请日：2015-11-06

    Applicant: United Technologies Corporation

    Inventor： Jonathan Jefferey Eastwood ,  Dave J. Hyland ,  Timothy Dale

    IPC: F01D25/28 ,  F01D25/24

    CPC classification number: F01D25/28 ,  F01D9/04 ,  F01D9/041 ,  F01D9/065 ,  F01D25/24 ,  F04D29/54 ,  F04D29/542 ,  F05D2220/32 ,  F05D2230/21 ,  F23R3/06 ,  F23R3/50 ,  Y02T50/671 ,  Y02T50/675

    Abstract: A pre-diffuser of an inner diffuser case of a gas turbine engine may comprise an annular outer wall and an annular inner wall radially inside of the annular outer wall to define a passage for primary airflow therebetween. The pre-diffuser may further comprise at least one strut extending radially between the annular inner wall and the annular outer wall and at least one aperture formed in the strut that extends radially through the strut, the annular inner wall, and the annular outer wall. The pre-diffuser may further comprise at least one hollow cavity formed in the strut, and the hollow cavity may be separate from the aperture.

    Abstract translation: 燃气涡轮发动机的内部扩散器壳体的预扩散器可以包括环形外壁和环形外壁径向内侧的环形内壁，以限定用于其间的主要气流的通道。 预扩散器还可以包括至少一个在环形内壁和环形外壁之间径向延伸的支柱，以及形成在支柱中的至少一个孔，其径向延伸穿过支柱，环形内壁和环形外壁。 预扩散器还可以包括形成在支柱中的至少一个中空腔，并且中空腔可以与孔分离。

    OUTER DIFFUSER CASE FOR A GAS TURBINE ENGINE
    27.
    发明申请
    OUTER DIFFUSER CASE FOR A GAS TURBINE ENGINE 审中-公开
    用于气体涡轮发动机的外部扩散器箱

    公开(公告)号：US20160160687A1

    公开(公告)日：2016-06-09

    申请号：US14958287

    申请日：2015-12-03

    Applicant: United Technologies Corporation

    Inventor： Jonathan J. Eastwood ,  Dave J. Hyland ,  Timothy Dale

    IPC: F01D25/24 ,  F01D9/02 ,  F04D29/52 ,  F01D25/26 ,  F01D5/02 ,  F04D29/32

    CPC classification number: F01D25/243 ,  F01D5/02 ,  F01D9/02 ,  F01D25/24 ,  F01D25/26 ,  F01D25/30 ,  F01D25/34 ,  Y02T50/671

    Abstract: An outer diffuser case of a diffuser case assembly for use in a gas turbine engine may have a housing orientated about an engine axis, a forward flange projecting radially outward from the housing, a mid-flange spaced axially aft of the forward flange and projecting radially inward from the housing, and an aft flange projecting radially outward from the housing. The mid flange is spaced axially between the forward and aft flanges and is configured to detachably engage an inner diffuser case of the case assembly. The forward flange is configured to detachably engage a high pressure compressor and the aft flange is configured to detachably engage a high pressure turbine of the engine.

    Abstract translation: 用于燃气涡轮发动机的扩散器壳体组件的外部扩散器壳体可以具有围绕发动机轴线定向的壳体，从壳体径向向外突出的前凸缘，前凸缘的中间凸缘间隔开的轴向后部并且径向突出 从壳体向内，以及从壳体径向向外突出的后凸缘。 中间凸缘在前凸缘和后凸缘之间轴向隔开并且构造成可拆卸地接合壳体组件的内部扩散器壳体。 前凸缘构造成可拆卸地接合高压压缩机，并且后凸缘构造成可拆卸地接合发动机的高压涡轮机。

Patent Agency Ranking