APERTURE PATTERN FOR GAS TURBINE ENGINE COMPONENT WITH INTEGRAL ALIGNMENT FEATURE

    公开(公告)号:US20230374914A1

    公开(公告)日:2023-11-23

    申请号:US17746541

    申请日:2022-05-17

    IPC分类号: F01D25/24 F01D25/28

    摘要: A structure for a gas turbine engine includes a first engine component, a second engine component and fasteners. The component apertures include first fastener apertures and intergroup apertures. The first fastener apertures are arranged into a plurality of groups. The first group is formed by N1-number of the first fastener apertures. The second group is formed by N2-number of the first fastener apertures where the N2-number is different than the N1-number. Each of the intergroup apertures is disposed circumferentially between and adjacent a respective circumferentially neighboring pair of the groups. The second engine component includes a surface and second fastener apertures. The surface axially engages the first engine component and covers the intergroup apertures. The fasteners attach the first engine component and the second engine component together. Each of the fasteners is mated with one of the first fastener apertures and one of the second fastener apertures.

    TURBOMACHINE MODULE PROVIDED WITH A PROPELLER AND OFFSET STATOR VANES

    公开(公告)号:US20230366325A1

    公开(公告)日:2023-11-16

    申请号:US18246554

    申请日:2021-09-29

    IPC分类号: F01D17/16 F01D25/24 F01D9/04

    摘要: A turbomachine module having a longitudinal axis, having a shroudless propeller which is rotated about the longitudinal axis by a drive shaft, which is connected at least to a compressor rotor, and at least one distributor comprising a plurality of stator vanes which extend along a radial axis which is perpendicular to the longitudinal axis Z from a fixed casing, the distributor being arranged downstream of the propeller. The fixed casing can be an inter-compressor casing which is arranged downstream of a low-pressure compressor, along the longitudinal axis, the inter-compressor casing having a ring which has a longitudinal axis and which is provided with sleeves intended to support the stator vanes, the inter-compressor casing and the ring being monobloc.

    Rotor with inlets to channels
    53.
    发明授权

    公开(公告)号:US11802482B2

    公开(公告)日:2023-10-31

    申请号:US17587847

    申请日:2022-01-28

    发明人: Viktor Kilchyk

    IPC分类号: F04D27/02 F01D5/02 F01D25/24

    CPC分类号: F01D5/02 F01D25/24

    摘要: A rotor includes a blade, a hub connected to a radially inner edge of the blade, an outlet, and a channel. The blade includes a first side between a leading edge and a trailing edge and a first channel inlet in the first side of the blade. The outlet is in a radially inner surface of the hub. The channel is between the first channel inlet and the outlet.

    TURBOCHARGER WITH VARIABLE GEOMETRIC FLUID GUIDE MECHANISM

    公开(公告)号:US20230287798A1

    公开(公告)日:2023-09-14

    申请号:US18321783

    申请日:2023-05-23

    申请人: IHI Corporation

    发明人: Takao ASAKAWA

    IPC分类号: F01D17/16 F01D25/24 F02B37/24

    摘要: A turbocharger includes a turbine housing accommodating a turbine wheel, a bearing housing rotatably supporting a rotating shaft to which the turbine wheel is fixed, a variable geometry mechanism accommodated in the turbine housing, surrounding the turbine wheel, and configured to guide a fluid to the turbine wheel, and a spring member held by the variable geometry mechanism and the bearing housing in an axial direction along the rotating shaft. The variable geometry mechanism has an inner circumferential portion surrounding a through hole in which the turbine wheel or the rotating shaft is disposed, and an outer circumferential portion located between the spring member and the turbine housing. The outer circumferential portion is distanced further away from a rotational axis of the rotating shaft than the inner circumferential portion. The outer circumferential portion includes a first end face contacting the spring member, and a second end face contacting the turbine housing.