中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

19 records (took 0.036 seconds)

    Shroud assembly for gas turbine engine
    11.
    发明授权
    Shroud assembly for gas turbine engine 有权

    公开(公告)号：US10301960B2

    公开(公告)日：2019-05-28

    申请号：US14797240

    申请日：2015-07-13

    Applicant: General Electric Company

    Inventor： David Scott Stapleton ,  Bryce Loring Heitman ,  Laura Isabelle Armanios

    IPC: F01D11/18 ,  F01D11/08 ,  F01D9/04 ,  F01D25/24 ,  F01D25/00 ,  F02C3/04

    Abstract: Shroud assemblies for gas turbine engines are provided. A shroud assembly includes a hanger having a forward hanger arm, a rear hanger arm, and a hanger body extending between the forward hanger arm and the rear hanger arm. The shroud assembly further includes a shroud having a forward surface, a rear surface, and an inner surface and outer surface extending between the forward surface and the rear surface, the outer surface radially spaced from the inner surface, the shroud connected to the hanger. The shroud assembly further includes a support member positioned axially forward of the forward hanger arm, the support member having a radially outer portion connected to the forward hanger arm and a radially inner portion axially spaced from the shroud such that a gap is defined between the radially inner portion and an axially adjacent surface of the shroud.

    SHROUDS AND METHODS FOR FORMING TURBINE COMPONENTS
    12.
    发明申请
    SHROUDS AND METHODS FOR FORMING TURBINE COMPONENTS 审中-公开

    公开(公告)号：US20170107840A1

    公开(公告)日：2017-04-20

    申请号：US14882909

    申请日：2015-10-14

    Applicant: General Electric Company

    Inventor： David Scott Stapleton ,  Robert Charles Groves, II

    IPC: F01D11/08 ,  F01D25/12 ,  F02C3/04 ,  F04D29/52 ,  F04D29/58 ,  F04D29/64 ,  F01D25/00 ,  F04D29/02

    Abstract: Shrouds and methods for forming turbine components are provided. A shroud includes a shroud body which includes a forward surface, a rear surface axially spaced from the forward surface, an inner surface extending between the forward surface and the rear surface, and an outer surface extending between the forward surface and the rear surface and radially spaced from the inner surface. The shroud further includes a forward flange extending from the outer surface of the shroud body, and a rear flange extending from the outer surface of the shroud body, the rear flange axially spaced from the forward flange. The shroud further includes a cooling passage defined in the shroud, the cooling passage extending generally circumferentially through the shroud.

    Shrouds and methods for forming turbine components
    14.
    发明授权
    Shrouds and methods for forming turbine components 有权

    公开(公告)号：US10689998B2

    公开(公告)日：2020-06-23

    申请号：US14882909

    申请日：2015-10-14

    Applicant: General Electric Company

    Inventor： David Scott Stapleton ,  Robert Charles Groves, II

    IPC: F01D11/24 ,  F01D25/24 ,  F01D11/08 ,  F01D25/00 ,  F01D25/12 ,  F02C3/04 ,  F04D29/02 ,  F04D29/52 ,  F04D29/58 ,  F04D29/64

    Abstract: Shrouds and methods for forming turbine components are provided. A shroud includes a shroud body which includes a forward surface, a rear surface axially spaced from the forward surface, an inner surface extending between the forward surface and the rear surface, and an outer surface extending between the forward surface and the rear surface and radially spaced from the inner surface. The shroud further includes a forward flange extending from the outer surface of the shroud body, and a rear flange extending from the outer surface of the shroud body, the rear flange axially spaced from the forward flange. The shroud further includes a cooling passage defined in the shroud, the cooling passage extending generally circumferentially through the shroud.

    Spline for a turbine engine
    15.
    发明授权
    Spline for a turbine engine 有权

    公开(公告)号：US10648362B2

    公开(公告)日：2020-05-12

    申请号：US15441586

    申请日：2017-02-24

    Applicant: General Electric Company

    Inventor： Robert Charles Groves, II ,  David Scott Stapleton

    IPC: F01D11/00 ,  F01D25/12 ,  F01D11/08

    Abstract: A shroud assembly for a turbine engine comprising a plurality of circumferentially arranged shroud segments having confronting end faces defining first and second radially spaced surfaces. The shroud assembly includes a forward edge spanning to an aft edge to define an axial direction and a set of confronting seal channels formed in each of the confronting end faces with a spline seal located within the confronting seal channels.

    SPLINE FOR A TURBINE ENGINE
    17.
    发明申请
    SPLINE FOR A TURBINE ENGINE 审中-公开

    公开(公告)号：US20180340437A1

    公开(公告)日：2018-11-29

    申请号：US15441463

    申请日：2017-02-24

    Applicant: General Electric Company

    Inventor： Robert Charles Groves, II ,  David Scott Stapleton

    IPC: F01D11/00

    Abstract: A shroud assembly for a turbine engine comprising a plurality of circumferentially arranged shroud segments having confronting end faces defining first and second radially spaced surfaces. The shroud assembly includes a forward edge spanning to an aft edge to define an axial direction and a set of confronting seal channels formed in each of the confronting end faces with a spline seal located within the confronting seal channels.

Patent Agency Ranking