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公开(公告)号：US10823419B2
公开(公告)日：2020-11-03
申请号：US15909106
申请日：2018-03-01
Applicant: General Electric Company
Inventor： Ryan Christopher Jones , Scott Matthew Bush , Paul Christopher Schilling , Andrew Scott Bilse
Abstract: The present subject matter provides a combustion system which comprising: a cowl; a deflector configurated to include a ring body, a plurality of swirlers integrated on the ring body and a plurality of arms integrally extending outward from the ring body; an annular inner liner attached with the cowl; and an annular outer liner attached with the cowl. The deflector is positioned between the inner liner and the outer liner; the deflector, the inner liner and the outer line define a combustion chamber thereamong. The deflector is attached to the cowl via the plurality of arms, but the arms are rigid enough to work together to fix the deflector with the cowl while allowing for thermal expansion flexibility therebetween at the same time.
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公开(公告)号：US20200063961A1
公开(公告)日：2020-02-27
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
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.
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公开(公告)号：US20200063583A1
公开(公告)日：2020-02-27
申请号：US16107227
申请日：2018-08-21
Applicant: General Electric Company
Inventor： Andrew Scott Bilse , Donald Lee Gardner , Craig Alan Gonyou , Paul Christopher Schilling , Hojjat Nasr , Ryan Christopher Jones
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.
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Patent Agency Ranking
公开(公告)号：US20250129939A1
公开(公告)日：2025-04-24
申请号：US18990952
申请日：2024-12-20
Applicant: General Electric Company
Inventor： Ryan Christopher Jones , Paul Christopher Schilling , Andrew Scott Bilse , Daniel Endecott Osgood , Donald Lee Gardner
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.
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公开(公告)号：US11873734B2
公开(公告)日：2024-01-16
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
CPC classification number: F01D5/186
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.
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公开(公告)号：US11339966B2
公开(公告)日：2022-05-24
申请号：US16107227
申请日：2018-08-21
Applicant: General Electric Company
Inventor： Andrew Scott Bilse , Donald Lee Gardner , Craig Alan Gonyou , Paul Christopher Schilling , Hojjat Nasr , Ryan Christopher Jones
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.
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公开(公告)号：US10816213B2
公开(公告)日：2020-10-27
申请号：US15909107
申请日：2018-03-01
Applicant: General Electric Company
Inventor： Ryan Christopher Jones , Scott Matthew Bush , Paul Christopher Schilling , Andrew Scott Bilse
Abstract: A combustor includes an outer liner, an inner liner, an annular cowl joining upstream ends of the outer and inner liners, and an annular deflector configured to shield the cowl from hot combustion gases in a combustion chamber defined between the outer liner, the inner liner and the deflector. The cowl has at least one opening for introduction of fuel and compressed air. The deflector includes at least one swirler. The cowl defines at least one axial cowl hole, and the deflector defines at least one corresponding axial deflector hole, wherein the corresponding deflector hole and cowl hole are configured to receive a fastener for fastening together the cowl and the deflector.
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公开(公告)号：US20200254519A1
公开(公告)日：2020-08-13
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: B22F3/105 , B22F3/24 , B29C64/153 , B29C64/393 , B29C64/40
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.
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