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    BLOCKAGE-RESISTANT VANE IMPINGEMENT TUBES AND TURBINE NOZZLES CONTAINING THE SAME
    1.
    发明公开
    BLOCKAGE-RESISTANT VANE IMPINGEMENT TUBES AND TURBINE NOZZLES CONTAINING THE SAME 审中-公开

    公开(公告)号：EP3382150A1

    公开(公告)日：2018-10-03

    申请号：EP18163199.5

    申请日：2018-03-21

    申请人： Honeywell International Inc.

    发明人： KINGTON, Harry Lester ,  CRITES, Daniel C. ,  HOWE, Jeff

    IPC分类号： F01D5/18 ,  F01D9/04

    CPC分类号： F01D9/041 ,  F01D5/189 ,  F01D9/065 ,  F05D2240/127 ,  F05D2250/71 ,  F05D2260/201 ,  F05D2260/2212 ,  F05D2260/22141 ,  Y02T50/676

    摘要： Vane impingement tubes (34,90) having blockage deterrent features are provided, as turbine nozzles (12) containing blockage-resistant vane impingement tubes. In an embodiment, the turbine nozzle includes inner and outer annular endwalls (24, 26), and turbine nozzle vanes (28) between the annular endwalls. Vane impingement tubes are inserted into the turbine nozzle vanes. The vane impingement tubes each includes a tube body (56, 93), an impingement outlet (40, 40', 92) formed in the tube body and configured to discharge airflow for impingement against the turbine nozzle vanes, a first flow-turning feature (74, 100) located in the tube body, and an inlet (68, 102) formed in the tube body and configured receive cooling airflow in a substantially radial direction. The first flow-turning feature turns the airflow received through the inlet in a substantially axial direction, which is perpendicular to the radial direction, prior to discharge through the impingement outlet.

    OIL FLOW ENHANCER BEARING ASSEMBLY
    3.
    发明授权
    OIL FLOW ENHANCER BEARING ASSEMBLY 有权
    油流增强器轴承总成

    公开(公告)号：EP3032046B1

    公开(公告)日：2018-04-11

    申请号：EP15197418.5

    申请日：2015-12-02

    申请人： Rolls-Royce Corporation

    发明人： Burnside, Phillip N. ,  Turk, Angela

    IPC分类号： F01D25/18 ,  F02C7/06 ,  F16C33/66

    CPC分类号： F02C7/06 ,  F01D25/18 ,  F05D2240/70 ,  F05D2250/71 ,  F16C19/06 ,  F16C33/6659 ,  F16C33/6685 ,  F16C2360/23

    摘要： A bearing assembly (110) may comprise a housing (113), a slinger disk (128), and a bearing (115). The housing (113) may be configured to receive a shaft (112) and having at least one scavenge passage (114) between an outer housing portion (118) and an inner housing portion (116). The slinger disk (128) may have a plurality of flow guides (212) configured to direct a lubricant flow (134) toward the at least one scavenge passage (114). The scavenge passage (114) may be configured to provide a lubricant flow (134) through the bearing (115). Lubricant flow (134) may be provided in a forward direction, through the bearing (115) and opposite a windage direction.

    INLET PARTICLE SEPARATORS SYSTEM WITH HIGH CURVATURE HUB
    8.
    发明公开
    INLET PARTICLE SEPARATORS SYSTEM WITH HIGH CURVATURE HUB 审中-公开
    具有高曲率轮毂的入口颗粒分离器系统

    公开(公告)号：EP3189880A1

    公开(公告)日：2017-07-12

    申请号：EP16195638.8

    申请日：2016-10-25

    申请人： Honeywell International Inc.

    发明人： PEARSON, John Taylor ,  SHEORAN, Yogendra Yogi ,  BOULDIN, Bruce Dan ,  JUDD, Zedic Daniel ,  GUERRA, Eduardo ,  CHOU, David

    IPC分类号： B01D45/04 ,  B01D45/12 ,  B64D33/02 ,  F02C7/052

    CPC分类号： F04D29/701 ,  B01D45/08 ,  B01D45/12 ,  B01D45/16 ,  B64D33/02 ,  B64D2033/0246 ,  F02C7/05 ,  F02C7/052 ,  F04D29/522 ,  F04D29/542 ,  F04D29/545 ,  F05D2250/71 ,  Y02T50/671

    摘要： An inlet particle separator system for a vehicle engine includes a hub section, a shroud section, and a splitter. The hub section has a hub outer surface that diverges, relative to the axis of symmetry, to a hub apex. The shroud section has a shroud inner surface that surrounds, and is spaced apart from, at least a portion of the hub section to define a main flow passageway between the hub outer surface and the shroud inner surface. The splitter is disposed downstream of the air inlet and extends into the main flow passageway to divide the main flow passageway into a scavenge flow path and an engine flow path. The hub section and the shroud section are configured such that the cross sectional flow area of the main flow passageway decreases downstream of the air inlet to define a throat section that is disposed upstream of the hub apex.

    摘要翻译： 用于车辆发动机的入口颗粒分离器系统包括毂部分，护罩部分和分流器。 轮毂部分具有轮毂外表面，该轮毂外表面相对于对称轴线向轮毂顶点发散。 护罩部分具有护罩内表面，该护罩内表面围绕轮毂部分的至少一部分并与轮毂部分的至少一部分间隔开，以在轮毂外表面和护罩内表面之间限定主流动通路。 分流器布置在空气入口的下游并且延伸到主流动通路中以将主流动通路分成清扫流动路径和发动机流动路径。 轮毂部分和护罩部分构造成使得主流动通道的横截面流动面积在进气口的下游减小以限定设置在轮毂顶点上游的喉部。

    TURBINE DISCS AND METHODS OF FABRICATING THE SAME
    9.
    发明公开
    TURBINE DISCS AND METHODS OF FABRICATING THE SAME 审中-公开
    TURBINENSCHEIBEN UND VERFAHREN ZUR HERSTELLUNG DAVON

    公开(公告)号：EP3176367A1

    公开(公告)日：2017-06-07

    申请号：EP16200008

    申请日：2016-11-22

    申请人： GEN ELECTRIC

    发明人： NEELI SUDHAKAR ,  ELDRID SACHEVEREL QUENTIN ,  YOUNG ROBERT CORMACK ,  PULANECKI MARIUSZ

    IPC分类号： F01D5/08

    CPC分类号： F01D5/187 ,  F01D5/066 ,  F01D5/08 ,  F01D5/087 ,  F05D2220/32 ,  F05D2230/00 ,  F05D2250/71 ,  F05D2260/202

    摘要： A turbine disc 202 having a radius and a circumference is provided. The turbine disc includes a central aperture 402 and a plurality of cooling channels 316, 414 circumferentially spaced about the central aperture such that the cooling channels are in flow communication with the central aperture. Each of the cooling channels has a radially inner end 424, a radially outer end 426, and a lengthwise axis 422 that is curved between the radially inner end and the radially outer end.

    摘要翻译： 提供具有半径和圆周的涡轮盘202。 涡轮盘包括中心孔402和围绕中心孔圆周地间隔开的多个冷却通道316,414，使得冷却通道与中心孔流动连通。 每个冷却通道具有径向内端424，径向外端426和在径向内端和径向外端之间弯曲的纵向轴线422。