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公开(公告)号：US20230114116A1
公开(公告)日：2023-04-13
申请号：US17499085
申请日：2021-10-12
Applicant: General Electric Company
Inventor： Gerardo Antonio Salazar Lois , Daniel J. Kirtley , Nicholas John Bloom , Shai Birmaher , Ryan Christopher Jones
Abstract: A combustor for a gas turbine includes a ceramic matrix composite (CMC) dome with a swirler mounting wall formed integral with the CMC dome, and a swirler assembly including a plurality of clevis dome attachment members for connecting the swirler assembly to the CMC dome. Bushings are arranged within a plurality of dome-side swirler assembly mounting openings of the swirler mounting wall, and the CMC dome is arranged within respective ones of the plurality of clevis dome attachment members of the swirler assembly. A swirler-dome connecting member is disposed through each of the clevis dome attachment members so as to mount the swirler assembly to the CMC dome.
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32.发明申请公开(公告)号：US20220332050A1
公开(公告)日：2022-10-20
申请号：US17234277
申请日：2021-04-19
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Justin Stekli , Bathrinarayanan Mukundan , Ryan Christopher Jones , Paul C. Schilling
IPC: B29C64/386 , B33Y50/00 , G06F30/10 , G05B19/4099
Abstract: A printing device receives modeling data that defines a three-dimensional solid model of a component body having a plurality of faces and a plurality of edges. Each of the faces meets another face of the component body at a respective edge of the component body. The printing device interrogates one or more faces of the component body to identify one or more looped geometries, and defines a lattice exclusion area having a boundary formed based at least in part on one or more faces of the component body that correspond to the looped geometries. The printing device generates a printer output of the component body and a lattice support structure for the component body. The printer output of the lattice support structure is outside of the lattice exclusion area.
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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：US11187412B2
公开(公告)日：2021-11-30
申请号：US16108674
申请日：2018-08-22
Applicant: General Electric Company
Inventor： Andrew Scott Bilse , Craig Alan Gonyou , Ryan Christopher Jones
Abstract: A heat engine including a wall assembly is generally provided. The wall assembly includes a plurality of radial walls coupled together via a connecting member. The radial wall defines a flow opening therethrough. A flow cavity is defined between the plurality of radial walls and the connecting member.
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公开(公告)号：US11021968B2
公开(公告)日：2021-06-01
申请号：US16195048
申请日：2018-11-19
Applicant: General Electric Company
Inventor： Daniel Endecott Osgood , Tingfan Pang , Gregory Terrence Garay , Zachary Daniel Webster , Ryan Christopher Jones
Abstract: A cast component having reduced cross flow linking cavities and method of casting may include a body. The body may define a plurality of internal flow channels. The plurality of internal flow channels may include a first internal flow channel and a second internal flow channel. The cast component may also include a plurality of linking cavities obstructing unintended fluid communication between the first internal flow channel and the second internal flow channel through the plurality of linking cavities.
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Patent Agency Ranking
公开(公告)号：US10927692B2
公开(公告)日：2021-02-23
申请号：US16055987
申请日：2018-08-06
Applicant: General Electric Company
Inventor： Ryan Christopher Jones , Daniel Endecott Osgood , Zachary Daniel Webster , Gregory T. Garay , Tingfan Pang
Abstract: A turbomachinery sealing apparatus including a first turbomachinery component having a first end face, and a seal extending away from the first end face, the seal being connected to a wall of the component by a tab extending between the wall and the seal.
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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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公开(公告)号：US20200157947A1
公开(公告)日：2020-05-21
申请号：US16195048
申请日：2018-11-19
Applicant: General Electric Company
Inventor： Daniel Endecott Osgood , Tingfan Pang , Gregory Terrence Garay , Zachary Daniel Webster , Ryan Christopher Jones
Abstract: A cast component having reduced cross flow linking cavities and method of casting may include a body. The body may define a plurality of internal flow channels. The plurality of internal flow channels may include a first internal flow channel and a second internal flow channel. The cast component may also include a plurality of linking cavities obstructing unintended fluid communication between the first internal flow channel and the second internal flow channel through the plurality of linking cavities.
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公开(公告)号：US20200063963A1
公开(公告)日：2020-02-27
申请号：US16108674
申请日：2018-08-22
Applicant: General Electric Company
Inventor： Andrew Scott Bilse , Craig Alan Gonyou , Ryan Christopher Jones
Abstract: A heat engine including a wall assembly is generally provided. The wall assembly includes a plurality of radial walls coupled together via a connecting member. The radial wall defines a flow opening therethrough. A flow cavity is defined between the plurality of radial walls and the connecting member.
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