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公开(公告)号：US20190084892A1
公开(公告)日：2019-03-21
申请号：US15710954
申请日：2017-09-21
Applicant: General Electric Company
Inventor： Suresh Subramanian , Mark Eugene Noe , James Dale Steibel , Jason David Shapiro , Brandon ALlanson Reynolds , Kurtis C. Montgomery , Jared Hogg Weaver , Daniel Gene Dunn
IPC: C04B37/00 , C04B35/80 , C04B35/657 , C04B35/628
Abstract: A ceramic matrix composite article includes a chemical vapor infiltration ceramic matrix composite base portion including ceramic fiber reinforcement material in a ceramic matrix material having between 0% and 5% free silicon. The ceramic matrix composite article further includes a melt infiltration ceramic matrix composite covering portion including a ceramic fiber reinforcement material in a ceramic matrix material having a greater percentage of free silicon than the chemical vapor infiltration ceramic matrix composite base portion.
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公开(公告)号：US20160114351A1
公开(公告)日：2016-04-28
申请号：US14522016
申请日：2014-10-23
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Jared Hogg Weaver , Daniel Gene Dunn
CPC classification number: C22C1/10 , C04B41/009 , C04B41/52 , C04B41/89 , C22C1/1036 , F01D5/005 , F05D2230/80 , F05D2300/6033 , C04B35/565 , C04B35/806 , C04B14/386 , C04B41/4539 , C04B41/455 , C04B41/4572 , C04B41/4582 , C04B41/5059 , C04B41/4523 , C04B41/5096
Abstract: A method for repair of composite materials includes applying a formulation to a ceramic matrix composite substrate. The formulation comprises a liquid carrier, a ceramic filler dispersed within the carrier, and a polymeric binder disposed in the carrier. The method further includes removing the carrier from the formulation to form a green composition; pyrolyzing the green composition to form a porous composition; disposing a liquid metal or metalloid within the pores of the porous composition to form an intermediate composite composition; and converting the liquid metal or metalloid to solid state to form a solid composite composition.
Abstract translation: 复合材料的修复方法包括将制剂施用于陶瓷基质复合基材。 该制剂包含液体载体，分散在载体内的陶瓷填料，以及设置在载体中的聚合物粘合剂。 该方法还包括从制剂中除去载体以形成绿色组合物; 热解绿色组合物以形成多孔组合物; 在多孔组合物的孔内设置液态金属或准金属以形成中间复合组合物; 并将液态金属或准金属转化为固态以形成固体复合组合物。
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公开(公告)号：US20240279125A1
公开(公告)日：2024-08-22
申请号：US18170107
申请日：2023-02-16
Applicant: General Electric Company
Inventor： Jerome Geoffrey Magnant , Jared Hogg Weaver
IPC: C04B37/00
CPC classification number: C04B37/003 , C04B37/001 , C04B2237/58
Abstract: A unitary ceramic component is provided that includes a first ceramic component; a second ceramic component; and a series-hybrid joint coupling the first ceramic component to the second ceramic component. The series-hybrid joint includes a first bonding interface coupling the first ceramic component and the second ceramic component and a second bonding interface coupling the first ceramic component and the second ceramic component. The first bonding interface exhibits properties that are different from the second bonding interface.
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14.发明授权公开(公告)号：US12017962B2
公开(公告)日：2024-06-25
申请号：US16807864
申请日：2020-03-03
Applicant: General Electric Company
Inventor： Daniel Gene Dunn , Gregory Scot Corman , Jared Hogg Weaver
IPC: F01D5/28 , B32B18/00 , C04B35/573 , C04B35/63 , C04B35/80 , C04B37/00 , C23C16/32 , F01D5/00 , F01D9/04 , F01D25/16 , F02K1/82 , F02K9/97 , F23R3/00
CPC classification number: C04B37/005 , B32B18/00 , C04B35/573 , C04B35/6316 , C04B35/80 , C04B37/001 , C23C16/325 , F01D5/005 , F01D5/282 , F01D5/284 , F01D5/288 , F01D9/041 , F01D25/162 , F02K1/82 , F02K9/97 , F23R3/007 , C04B2235/428 , C04B2235/5244 , C04B2235/616 , C04B2237/083 , C04B2237/365 , C04B2237/38 , F05D2220/32 , F05D2230/80 , F05D2240/11 , F05D2300/2261 , F05D2300/6033
Abstract: Provided is a method including obtaining ceramic matrix composite (CMC) with a first matrix portion including a silicon carbide and silicon phase dispersed therewithin, disposing a coating thereupon to form a sealed part, and forming thereupon another segment comprising a CMC, which may be another matrix portion including a silicon carbide and a silicon phase dispersed within therewithin. Also provided is a gas turbine component with a CMC segment including a matrix portion including a silicon carbide and a silicon phase dispersed therewithin, a sealing layer including silicon carbide enclosing the first segment, and a second segment on the sealing layer, wherein the second segment includes a melt-infiltrated CMC having a matrix portion including a silicon carbide and a silicon phase dispersed therewithin.
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公开(公告)号：US20230416163A1
公开(公告)日：2023-12-28
申请号：US17851751
申请日：2022-06-28
Applicant: General Electric Company
Inventor： Jerome Geoffrey Magnant , Jared Hogg Weaver , Daniel Gene Dunn
CPC classification number: C04B37/003 , B23K1/19 , C04B2237/086 , C04B2237/16 , C04B2237/60 , C04B2237/61 , B23K2103/52
Abstract: Methods for forming a unitary ceramic component are provided. The method may include: positioning a braze reactant layer in a contact area between a first densified ceramic component and a second densified ceramic component; positioning a pack material around at least a portion of the first densified ceramic component or the second densified ceramic component; positioning at least one infiltrate source in fluid communication with the braze reactant layer; and thereafter, heating the at least one infiltrate source, the pack material, the first densified ceramic component, and the second densified ceramic component to a braze temperature that is at or above a melting point of at least one phase of the infiltrate composition such that at least one phase of infiltrate composition melts and flows into the braze reactant layer and reacts with a ceramic precursor compound therein to form a ceramic material.
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Patent Agency Ranking
16.发明公开公开(公告)号：US20230416162A1
公开(公告)日：2023-12-28
申请号：US17851269
申请日：2022-06-28
Applicant: General Electric Company
Inventor： Juan P. Borja , Daniel Gene Dunn , Jared Hogg Weaver , Anant Achyut Setlur
CPC classification number: C04B37/003 , F01D9/02 , F01D5/282 , F01D25/005 , B32B18/00 , F05D2220/32 , F05D2230/20 , F05D2240/12 , F05D2240/30 , F05D2300/6033 , C04B2237/16 , C04B2237/38 , C04B2237/61 , C04B2237/84
Abstract: A method for modifying a composite component may include positioning a barrier segment between an infiltrated segment of the composite component and a green segment to form an assembly; and initiating an infiltration process. The barrier segment may have a barrier segment permeability that is lower than a permeability of the infiltrated segment, a permeability of the green segment, or both. A composite component may include an infiltrated segment infiltrated with a molten material during a prior infiltration process; a green segment that is uninfiltrated; and a barrier segment having a microstructure different from the infiltrated segment, the green segment, or both. The microstructure of the barrier segment may be configured to slow a flow of material between the infiltrated segment and the green segment during a subsequent infiltration process.
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公开(公告)号：US20210238101A1
公开(公告)日：2021-08-05
申请号：US17234176
申请日：2021-04-19
Applicant: General Electric Company
Inventor： Jared Hogg Weaver , Gregory Scot Corman , Krishan Lal Luthra
IPC: C04B37/00 , C04B35/628 , C04B35/80 , C04B35/71 , C23C16/04
Abstract: According to a method set forth herein a plurality of preform plies having first and second preform plies can be associated together to define a preform. The preform can be subject to chemical vapor infiltration (CVI) processing to define a ceramic matrix composite (CMC) structure.
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公开(公告)号：US20190084891A1
公开(公告)日：2019-03-21
申请号：US15710965
申请日：2017-09-21
Applicant: General Electric Company
Inventor： James Dale Steibel , Suresh Subramanian , Suresh Viswanathan , Jared Hogg Weaver
IPC: C04B35/80 , C04B35/626 , B32B18/00 , B32B7/02
CPC classification number: C04B35/806 , B32B7/02 , B32B18/00 , B32B2264/108 , C04B35/573 , C04B35/6267 , C04B2235/3826 , C04B2235/422 , C04B2235/5244 , C04B2235/5264 , C04B2235/614 , C04B2235/616 , C04B2235/728 , C04B2235/80 , C04B2237/38 , F01D5/282 , F01D5/284 , F02K1/822 , F05D2300/222 , F05D2300/2261 , F05D2300/6033
Abstract: A method for forming a ceramic matrix composite article includes laying up a first group of plies; laying up a second group of plies, the first and second groups of plies being adjacent to each other; compacting the first group of plies and the second group of plies in the same processing step; and performing a first infiltration process on the first group of plies. The method also includes performing a second infiltration process on the second group of plies, the first infiltration process being one of a melt infiltration process or a chemical vapor infiltration process, and the second infiltration process being the other of the melt infiltration process or the chemical vapor infiltration process.
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公开(公告)号：US20180207837A1
公开(公告)日：2018-07-26
申请号：US15411012
申请日：2017-01-20
Applicant: General Electric Company
Inventor： Jared Hogg Weaver , Nathan Carl Sizemore
CPC classification number: B29C70/36 , B32B18/00 , C04B35/117 , C04B35/14 , C04B35/563 , C04B35/565 , C04B35/62863 , C04B35/62868 , C04B35/62871 , C04B35/62873 , C04B35/62897 , C04B35/638 , C04B35/803 , C04B35/806 , C04B2235/5224 , C04B2235/5228 , C04B2235/5232 , C04B2235/524 , C04B2235/5244 , C04B2235/5248 , C04B2235/5252 , C04B2235/5436 , C04B2237/341 , C04B2237/343 , C04B2237/36 , C04B2237/365 , C04B2237/38
Abstract: Methods for preparing ceramic products using liquid infusion technology and products formed from the same are provided. The methods and products include the incorporation of a particulate material and binder between ceramic fibers such that the fibers may be properly spaced during formation of the ceramic product. Ceramic matrix composite products can thereby be provided using near net shaping methods.
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公开(公告)号：US20250027414A1
公开(公告)日：2025-01-23
申请号：US18906542
申请日：2024-10-04
Applicant: General Electric Company
Inventor： Herbert Chidsey Roberts , Glenn Curtis Taxacher , Timothy P. Coons , Jared Hogg Weaver , Daniel Gene Dunn , Jerome Geoffrey Magnant
Abstract: Composite components and methods for adding a composite material to a composite component are provided. For example, a method comprises positioning a composite material segment against the composite component to form a component layup; applying an insulating material around at least a portion of the component layup to form an insulated layup; and densifying the insulated layup, where the composite component was previously densified before positioning the composite material segment against the composite component. In some embodiments, the composite material is ceramic matrix composite (CMC) and the composite material segment is a plurality of CMC plies. The composite component may be a CMC gas turbine engine component that comprises an original CMC component and a new CMC material segment joined to the original CMC component through the transfer of silicon between the original CMC component and the new CMC material segment during melt infiltration.
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