公开(公告)号：US20240102392A1

公开(公告)日：2024-03-28

申请号：US18536428

申请日：2023-12-12

Applicant: General Electric Company

Inventor： Anquan Wang ,  Ryan Christopher Jones ,  Paul Christopher Schilling ,  Craig Alan Gonyou

IPC: F01D5/18

CPC classification number: F01D5/186

Abstract: An apparatus relating to a component for a turbine engine which generates a hot gas fluid flow, and provides a cooling fluid flow. The component having a wall separating the hot gas fluid flow from the cooling fluid flow and having a heated surface along which the hot gas fluid flow flows and a cooled surface facing the cooling fluid flow. At least one cooling hole including a connecting passage extending from a first inlet located at the cooled surface, to a first outlet located at the heated surface, the connecting passage defining a downstream flow direction from the first inlet to the first outlet, the connecting passage comprising a metering section fluidly coupled to the first inlet and defining a metered centerline and a diffusing section, downstream of the metering section, defining a diffused centerline, and fluidly coupling the metering section to the first outlet.

公开(公告)号：US10822958B2

公开(公告)日：2020-11-03

申请号：US16249285

申请日：2019-01-16

Applicant: General Electric Company

Inventor： Anquan Wang ,  Ryan Christopher Jones ,  Paul Christopher Schilling ,  Craig Alan Gonyou

IPC: F01D5/18

Abstract: An apparatus and method relating to a cooling hole of a component of a turbine engine. The component can include a wall separating the hot gas fluid flow from the cooling fluid flow and having a heated surface along which the hot gas fluid flow flows and a cooled surface facing the cooling fluid flow and at least one cooling hole comprising at least one inlet at the cooled surface, at least one outlet at the heated surface, with the outlet having a modified outlet shape.

公开(公告)号：US12173897B2

公开(公告)日：2024-12-24

申请号：US17651743

申请日：2022-02-18

Applicant: General Electric Company

Inventor： Ryan Christopher Jones ,  Paul Christopher Schilling ,  Andrew Scott Bilse ,  Daniel Endecott Osgood ,  Donald Lee Gardner

IPC: F23R3/00 ,  F23R3/60

Abstract: Embodiments of a combustor assembly for a turbine engine are generally provided. The combustor assembly includes a first separable portion defining a dome assembly, and a second separable portion defining a deflector assembly. The first separable portion and the second separable portion are coupled together at a fitted interface.

公开(公告)号：US11280492B2

公开(公告)日：2022-03-22

申请号：US16110162

申请日：2018-08-23

Applicant: General Electric Company

Inventor： Ryan Christopher Jones ,  Donald Lee Gardner ,  Paul Christopher Schilling ,  Andrew Scott Bilse ,  Daniel Endecott Osgood

IPC: F23R3/00 ,  F23R3/60

Abstract: Embodiments of a combustor assembly for a turbine engine are generally provided. The combustor assembly includes a first separable portion defining a dome assembly, and a second separable portion defining a deflector assembly. The first separable portion and the second separable portion are coupled together at a fitted interface.

公开(公告)号：US20200224539A1

公开(公告)日：2020-07-16

申请号：US16249285

申请日：2019-01-16

Applicant: General Electric Company

Inventor： Anquan Wang ,  Ryan Christopher Jones ,  Paul Christopher Schilling ,  Craig Alan Gonyou

IPC: F01D5/18

Abstract: An apparatus and method relating to a cooling hole of a component of a turbine engine. The component can include a wall separating the hot gas fluid flow from the cooling fluid flow and having a heated surface along which the hot gas fluid flow flows and a cooled surface facing the cooling fluid flow and at least one cooling hole comprising at least one inlet at the cooled surface, at least one outlet at the heated surface, with the outlet having a modified outlet shape.

公开(公告)号：US20220325889A1

公开(公告)日：2022-10-13

申请号：US17651743

申请日：2022-02-18

Applicant: General Electric Company

Inventor： Ryan Christopher Jones ,  Paul Christopher Schilling ,  Andrew Scott Bilse ,  Daniel Endecott Osgood ,  Donald Lee Gardner

IPC: F23R3/00 ,  F23R3/60

Abstract: Embodiments of a combustor assembly for a turbine engine are generally provided. The combustor assembly includes a first separable portion defining a dome assembly, and a second separable portion defining a deflector assembly. The first separable portion and the second separable portion are coupled together at a fitted interface.

公开(公告)号：US11440097B2

公开(公告)日：2022-09-13

申请号：US16273474

申请日：2019-02-12

Applicant: General Electric Company

Inventor： Ryan Christopher Jones ,  Jun Zheng Hu ,  John Alan Manteiga ,  Xuefeng Zhang ,  Earl Neal Dunham ,  Paul Christopher Schilling ,  Johnnattan Tennessee Ugarte ,  Justin Michael Stekli ,  Justin Adam Masters

IPC: B29C64/153 ,  B29C64/40 ,  B22F3/24 ,  B22F10/80 ,  B22F10/47 ,  B22F10/66 ,  B22F10/62 ,  B22F3/11 ,  B33Y10/00 ,  B33Y40/00 ,  B33Y50/02 ,  B22F10/20 ,  B29C64/393 ,  B22F10/30

Abstract: A method for additively manufacturing a component includes generating, via imaging software, a plurality of slices of a support structure of the component based on component geometry. The method also includes melting or fusing, via the additive manufacturing system, layers of material to a build platform of the component so as to form the support structure according to the plurality of slices. The support structure includes a lattice configuration having of a plurality of support members arranged together to form a plurality of cells. Further, the method includes melting or fusing, via the additive manufacturing system, a component body to the support structure. After the component body solidifies, the method includes removing all of the support structure from the component body to form the component.

公开(公告)号：US20220268443A1

公开(公告)日：2022-08-25

申请号：US17663079

申请日：2022-05-12

Applicant: General Electric Company

Inventor： Andrew Scott Bilse ,  Craig Alan Gonyou ,  Paul Christopher Schilling ,  Hojjat Nasr ,  Ryan Christopher Jones ,  Donald Lee Gardner

IPC: F23R3/00 ,  F23R3/10

Abstract: A combustor assembly for a heat engine is generally provided. The combustor assembly includes a liner wall defining a combustion chamber, and a deflector assembly. The deflector assembly includes a radially extended first wall disposed adjacent to the combustion chamber, and further an axially extended second wall disposed forward of the first wall and adjacent thereto. The second wall is coupled to the liner wall.

公开(公告)号：US20200024951A1

公开(公告)日：2020-01-23

申请号：US16037662

申请日：2018-07-17

Applicant: GENERAL ELECTRIC COMPANY

Inventor： William Charles Herman ,  Jacob Romeo Rendon ,  Duane Allan Busch ,  Ryan Christopher Jones ,  Paul Christopher Schilling ,  Zachary Daniel Webster ,  Tingfan Pang ,  Gregory Terrence Garay ,  Steven Robert Brassfield

IPC: F01D5/08

Abstract: An apparatus and method relating to a cooling hole of a component of a turbine engine. The cooling hole can extend from an inlet to an outlet to define a passage. The cooling hole can include a laid back section where a coating can be applied. The method can include forming the cooling hole in the component and applying the coating to the component to maintain a specific geometry.

公开(公告)号：US20210317745A1

公开(公告)日：2021-10-14

申请号：US17068235

申请日：2020-10-12

Applicant: General Electric Company

Inventor： Anquan Wang ,  Ryan Christopher Jones ,  Paul Christopher Schilling ,  Craig Alan Gonyou

IPC: F01D5/18

Abstract: An apparatus and method relating to a cooling hole of a component of a turbine engine. The component can include a wall separating the hot gas fluid flow from the cooling fluid flow and having a heated surface along which the hot gas fluid flow flows and a cooled surface facing the cooling fluid flow and at least one cooling hole comprising at least one inlet at the cooled surface, at least one outlet at the heated surface, with the outlet having a modified outlet shape.