Aircraft engine, gas turbine intake therefore, and method of guiding exhaust gasses

    公开(公告)号:US11891947B2

    公开(公告)日:2024-02-06

    申请号:US17808385

    申请日:2022-06-23

    摘要: A gas turbine intake has a swirl housing having a tangential inlet fluidly connecting an exhaust conduit, an annular outlet defined around a central axis and fluidly connecting a turbine gas path, a swirl path extending circumferentially around the central axis from the tangential inlet, and vanes located in the swirl housing, the vanes circumferentially interspaced from one another relative the central axis, each vane having a twisted and flat body having a length extending from a leading end to a trailing end, the leading end being oriented mainly circumferentially and axially at the swirl path, the trailing end being oriented mainly axially and radially at the annular outlet, the twisted and flat body twisting between leading and trailing ends around the central axis, around a radial axis perpendicular to the central axis, and around a tangential axis perpendicular to both the central axis and the radial axis.

    Housing for Flow-Conducting Components
    2.
    发明公开

    公开(公告)号:US20230265861A1

    公开(公告)日:2023-08-24

    申请号:US18017815

    申请日:2021-07-26

    申请人: KSB SE & Co. KGaA

    发明人: Tammuz NOBEL

    IPC分类号: F04D29/42 B33Y80/00

    摘要: A method for forming a housing for a flow-conducting component includes forming at least two functional regions of the housing having different material properties using at least one of radiation-induced melting and solidification of a build material and a process gas jet. Each functional region of the housing may be generated from a different construction material, and at least one functional layer may be formed with a reduced weight structure such as a honeycomb structure.

    IMPROVED SEAL SYSTEM FOR CENTRIFUGAL PUMPS HAVING AXIALLY SPLIT CASINGS
    8.
    发明申请
    IMPROVED SEAL SYSTEM FOR CENTRIFUGAL PUMPS HAVING AXIALLY SPLIT CASINGS 审中-公开
    改进的密封系统用于具有轴向分离箱的离心泵

    公开(公告)号:US20150300365A1

    公开(公告)日:2015-10-22

    申请号:US14647650

    申请日:2012-11-29

    IPC分类号: F04D29/42

    摘要: Disclosed invention is an improved sealing system for axially split, centrifugal pumps. The improved sealing system eliminates the need for a gasket between casing halves. In the improved sealing system, a fluid tight seal is provided by an elastomeric cord positioned within a groove carried by the flange of at least one half of the axially split pump casing.

    摘要翻译: 公开了一种用于轴向分离离心泵的改进的密封系统。 改进的密封系统消除了在半壳之间的垫圈的需要。 在改进的密封系统中,通过位于由轴向分离的泵壳的至少一半的凸缘承载的凹槽内的弹性体帘线提供流体密封。

    Turbocharger support housing having alignment features
    9.
    发明授权
    Turbocharger support housing having alignment features 有权
    具有对准特征的涡轮增压器支撑壳体

    公开(公告)号:US09127690B2

    公开(公告)日:2015-09-08

    申请号:US13535991

    申请日:2012-06-28

    摘要: A support housing for a turbocharger is provided. The support housing may include an end wall with a first side and a second side, and a protrusion extending from the first side of the end wall in a first direction and configured to receive the turbocharger. The support housing may also include a plurality of side walls extending from the second side of the end wall in a second direction opposite the first direction. The plurality of side walls together with the end wall may form a generally hollow enclosure. The support housing may also include a first mounting flange disposed at distal edges of the plurality of side walls and configured to engage an engine, and a first center opening disposed in the end wall and passing from the first side to the second side.

    摘要翻译: 提供了一种用于涡轮增压器的支撑壳体。 支撑壳体可以包括具有第一侧和第二侧的端壁,以及从第一方向的端壁的第一侧延伸并且构造成接收涡轮增压器的突起。 支撑壳体还可以包括从端壁的第二侧沿与第一方向相反的第二方向延伸的多个侧壁。 多个侧壁与端壁一起可以形成大致中空的外壳。 支撑壳体还可以包括设置在多个侧壁的远侧边缘处并构造成接合发动机的第一安装凸缘和设置在端壁中并从第一侧到第二侧的第一中心开口。

    TURBOCHARGER SUPPORT HOUSING HAVING IMPROVED DRAINAGE
    10.
    发明申请
    TURBOCHARGER SUPPORT HOUSING HAVING IMPROVED DRAINAGE 有权
    TURBOCHARGER支持改善排水的房屋

    公开(公告)号:US20130343929A1

    公开(公告)日:2013-12-26

    申请号:US13529325

    申请日:2012-06-21

    IPC分类号: F04D25/04 F04D25/08 F04D17/10

    摘要: A support housing is disclosed for use with a turbocharger. The support housing may have an end wall, a semi-cylindrical protrusion extending from the end wall in a first direction, and a plurality of side walls extending from the end wall in a second direction. The plurality of side walls together with the end wall may form a generally hollow enclosure. The support housing may also include a mounting flange disposed at distal edges of the plurality of side walls, and a center opening disposed in the end wall. The support housing may further include a collection cavity formed at a gravitationally lowest corner of the end wall below the center opening and substantially isolated from the enclosure formed by the plurality of side walls and the end wall, and a gutter passage formed in the end wall and extending from the center opening to the collection cavity.

    摘要翻译: 公开了一种与涡轮增压器一起使用的支撑壳体。 支撑壳体可以具有端壁,在第一方向上从端壁延伸的半圆柱形突出部以及在第二方向上从端壁延伸的多个侧壁。 多个侧壁与端壁一起可以形成大致中空的外壳。 支撑壳体还可以包括设置在多个侧壁的远侧边缘处的安装凸缘和设置在端壁中的中心开口。 支撑壳体还可以包括形成在中心开口下方的端壁的重力最低角处并且与由多个侧壁和端壁形成的外壳基本隔开的收集腔,以及形成在端壁中的沟槽通道 并从中心开口延伸到收集腔。