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1.发明授权公开(公告)号：US11097983B2
公开(公告)日：2021-08-24
申请号：US16521308
申请日：2019-07-24
Applicant: General Electric Company
Inventor： David Bruce Hall , James Joseph Murray , Jason Robert Parolini , Michael Alan Vallance , Juan Borja , Daniel George Norton , Jared Hogg Weaver , Daniel Gene Dunn
IPC: C04B35/80 , C04B35/117 , C04B35/628 , C04B35/657 , C04B35/64 , C04B35/14 , C04B35/18 , C04B35/44 , C04B35/56 , C04B35/563 , C04B35/573 , C04B35/58 , C04B35/584 , C04B35/83
Abstract: Methods for preparing ceramic matrix composites using melt infiltration and chemical vapor infiltration are provided as well as the resulting ceramic matrix composites. The methods and products include the incorporation of sacrificial fibers to provide improved infiltration of the fluid infiltrant. The sacrificial fibers are removed, such as decomposed during pyrolysis, resulting in the formation of regular and elongate channels throughout the ceramic matrix composite. Infiltration of the fluid infiltrant can then take place using the elongate channels resulting in improved density and an improved ceramic matrix composite product.
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公开(公告)号：US10391724B2
公开(公告)日：2019-08-27
申请号：US15433548
申请日：2017-02-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Jason Robert Parolini , John McConnell Delvaux , Canan Uslu Hardwicke , Glenn Curtis Taxacher , James Joseph Murray
Abstract: A method of forming a pre-form ceramic matrix composite mold for a ceramic matrix composite (CMC) component including providing pieces of CMC remnant scrap material and randomly arranging the pieces of CMC remnant scrap material relative to one another. The method further includes debulking the pieces of CMC remnant scrap material into a rigidized shape, the rigidized shape having gaps between adjacent pieces of CMC remnant scrap material of about 10 microns and about 10 mm and a gap spacing between about 50 microns and about 50 mm, and forming the rigidized shape into a mold.
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公开(公告)号：US09719420B2
公开(公告)日：2017-08-01
申请号：US14292969
申请日：2014-06-02
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Paul Stephen DiMascio , Victor John Morgan , Jason Robert Parolini , Glenn Curtis Taxacher , Frederic Woodrow Roberts, Jr. , Jacob John Kittleson , John McConnell Delvaux
IPC: F02C7/00 , B23K1/00 , B23P6/00 , B24B33/00 , C04B41/00 , C04B41/45 , C04B41/50 , C04B41/53 , C04B41/85 , C04B41/91 , C04B41/87 , C04B41/88 , C04B41/51 , C23C16/24
CPC classification number: F02C7/00 , B23K1/0018 , B23P6/002 , B23P6/007 , B24B33/00 , C04B41/009 , C04B41/4531 , C04B41/5025 , C04B41/5096 , C04B41/5144 , C04B41/53 , C04B41/85 , C04B41/87 , C04B41/88 , C04B41/91 , C23C16/24 , F05D2230/30 , F05D2230/90 , F05D2300/6033 , Y10T156/10 , Y10T428/24355 , C04B35/00 , C04B35/80 , C04B41/4529 , C04B41/4539 , C04B41/5133 , C04B41/0072
Abstract: A process of producing a ceramic matrix composite gas turbine component and a ceramic matrix composite gas turbine component are provided. The process includes modifying a surface of the ceramic matrix composite gas turbine component to produce a modified surface with a surface roughness of less than 6 micrometers. The modifying is selected from the group of techniques consisting of applying unreinforced matrix plies to the surface, vapor depositing silicon on the surface, honing the surface, applying braze paste to the surface, and combinations thereof. The component includes a modified surface including a surface roughness of less than 6 micrometers. The modified surface being selected from the group consisting of unreinforced matrix plies applied to a surface of the ceramic matrix composite gas turbine component, silicon vapor deposited on the surface, a honed surface, a braze paste applied to the surface, and combinations thereof.
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公开(公告)号：US09333578B2
公开(公告)日：2016-05-10
申请号：US14318934
申请日：2014-06-30
Applicant: General Electric Company
Inventor： Yan Cui , Srikanth Chandrudu Kottilingam , Jason Robert Parolini , Dechao Lin
CPC classification number: B23K1/0008 , B22F7/062 , B23K1/0018 , B23K1/19 , B23K35/0238 , B23K2101/001 , B23K2103/166 , B32B5/02 , B32B2262/106 , B32B2264/105 , B32B2313/04 , B32B2603/00 , B32B2605/00 , C22C47/06
Abstract: Methods of providing a fiber reinforced braze include providing a substrate, disposing at least a first fiber reinforcement layer on the substrate, wherein the at least first fiber reinforcement layer comprises a fiber material, disposing at least a first braze layer on the at least first fiber reinforcement layer, wherein a melt temperature of the braze layer is lower than a melt temperature of the fiber material, and heating the at least first fiber reinforcement layer and the at least first braze layer to bond the fiber reinforced braze to the substrate.
Abstract translation: 提供纤维增强钎焊的方法包括提供基底，在基底上设置至少第一纤维加强层，其中至少第一纤维增强层包括纤维材料，在至少第一纤维上设置至少第一钎焊层 加强层，其中所述钎焊层的熔融温度低于所述纤维材料的熔融温度，以及加热所述至少第一纤维增强层和所述至少第一钎焊层以将所述纤维增强的钎焊粘合到所述基材。
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5.发明授权公开(公告)号：US09234430B2
公开(公告)日：2016-01-12
申请号：US13741565
申请日：2013-01-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Ronald Ralph Cairo , Paul Stephen DiMascio , Jason Robert Parolini
CPC classification number: F01D5/284 , F01D5/28 , F01D5/282 , Y10T428/1317
Abstract: A ceramic matrix composite article and a process of fabricating a ceramic matrix composite are disclosed. The ceramic matrix composite article includes a matrix distribution pattern formed by a manifold and ceramic matrix composite plies laid up on the matrix distribution pattern, includes the manifold, or a combination thereof. The manifold includes one or more matrix distribution channels operably connected to a delivery interface, the delivery interface configured for providing matrix material to one or more of the ceramic matrix composite plies. The process includes providing the manifold, forming the matrix distribution pattern by transporting the matrix material through the manifold, and contacting the ceramic matrix composite plies with the matrix material.
Abstract translation: 公开了一种陶瓷基复合制品及其制造方法。 陶瓷基复合制品包括由歧管形成的矩阵分布图案和铺设在矩阵分布图案上的陶瓷基质复合层，包括歧管或其组合。 歧管包括可操作地连接到输送界面的一个或多个矩阵分配通道，配置用于向一个或多个陶瓷基质复合层提供基体材料的输送界面。 该方法包括提供歧管，通过将基质材料输送通过歧管形成基质分布图案，并使陶瓷基质复合层与基质材料接触。
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Patent Agency Ranking
公开(公告)号：US11724969B2
公开(公告)日：2023-08-15
申请号：US16220822
申请日：2018-12-14
Applicant: General Electric Company
Inventor： Matthew Troy Hafner , John McConnell Delvaux , Jason Robert Parolini , Rajendra Kumar Bordia , Quan Li
CPC classification number: C04B41/4584 , C04B41/4543 , C04B41/4545 , C04B41/5031 , C04B41/5035 , C04B41/5045 , F01D5/282 , F05D2240/11 , F05D2300/603 , F05D2300/6033 , F05D2300/611
Abstract: A ceramic matrix composite (CMC) component includes at least one seal surface, the at least one seal surface disposed adjacent an interfacing surface for providing a seal therebetween; and a coating disposed on the seal surface. The coating includes an aluminum oxide and/or a silicon dioxide.
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公开(公告)号：US11117839B2
公开(公告)日：2021-09-14
申请号：US16393360
申请日：2019-04-24
Applicant: General Electric Company
Inventor： Jason Robert Parolini , Canan Uslu Hardwicke , Srikanth Chandrudu Kottilingam , James Joseph Murray, III
IPC: C04B41/45
Abstract: Various embodiments include methods for densifying a melt infiltrated ceramic matrix composite (CMC) article, and a densified melt infiltrated CMC article formed thereby. Particular embodiments include a method including: providing a porous CMC preform within a first region of a casting apparatus; providing a molten densifier within a pressure head area of a second region of the casting apparatus, the first and second regions being operably connected and the molten densifier including at least one source of silicon; and applying a first pressure to the molten densifier within the pressure head, thereby infiltrating voids within the porous CMC preform with the molten densifier and forming a densified melt infiltrated CMC article.
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公开(公告)号：US10087519B1
公开(公告)日：2018-10-02
申请号：US15629532
申请日：2017-06-21
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Jason Robert Parolini , John McConnell Delvaux , Srikanth Chandrudu Kottilingam , James Joseph Murray , Canan Uslu Hardwicke , Matthew Troy Hafner
Abstract: A method of making a preform and preform formed by the method. The method includes providing a first pre-preg ply including at least a first fiber and a first resin. The method also includes providing a second pre-preg ply including at least a second fiber and a second resin over at least a portion of the first pre-preg ply. Heat or electromagnetic radiation is used to at least partially cure the first and second resins to form a cured preform. Heat is applied to pyrolyze at least a portion of the resin of the cured preform to form a pyrolyzed preform. A mechanical stimulus including at least one of controlled drying, local explosions, or ultrasonic energy is applied to the pyrolyzed preform. The mechanically treated pyrolyzed preform is subsequently densified by melt infiltration to form a densified preform.
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公开(公告)号：US20180272568A1
公开(公告)日：2018-09-27
申请号：US15465726
申请日：2017-03-22
Applicant: General Electric Company
Inventor： Jason Robert Parolini , Matthew Troy Hafner , James Joseph Murray , Srikanth Chandrudu Kottilingam , Canan Uslu Hardwicke , John McConnell Delvaux
IPC: B29C35/02 , B29C33/38 , C04B35/80 , C04B35/626 , C04B35/628 , C04B35/657
CPC classification number: B29C35/02 , B29C33/38 , B29L2031/7504 , B32B18/00 , C04B35/62645 , C04B35/62844 , C04B35/62876 , C04B35/657 , C04B35/803 , C04B35/806 , C04B2235/3217 , C04B2235/3826 , C04B2235/3873 , C04B2235/5224 , C04B2235/524 , C04B2235/5244 , C04B2235/5248 , C04B2235/6026 , C04B2235/6028 , C04B2235/616 , C04B2235/945 , C04B2237/38 , C04B2237/62 , C04B2237/64 , F01D5/282 , F01D5/284 , F05D2260/204 , F05D2300/6033
Abstract: The present disclosure is directed to a method for forming a passage in a composite component. The method includes forming a cavity in a fiber preform. The cavity forms a portion of the passage. The method also includes inserting a core into the cavity and placing one or more fiber plies onto the fiber preform to form a fiber preform assembly. The method further includes thermally processing the fiber preform assembly and densifying the fiber preform assembly to form the composite component. The method also includes removing the core from the composite component.
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10.发明授权Apparatus and method to reduce wear and friction between CMC-to-metal attachment and interface 有权降低CMC与金属附件和界面之间磨损和摩擦的装置和方法公开(公告)号：US09500083B2
公开(公告)日：2016-11-22
申请号：US13685230
申请日：2012-11-26
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Ronald Ralph Cairo , Jason Robert Parolini , John McConnell Delvaux
IPC: F01D5/14 , C04B35/117 , C04B35/185 , C04B35/565 , C04B35/80 , C04B35/83 , C04B37/02 , F01D5/30 , F23R3/00 , F23R3/60
CPC classification number: F01D5/14 , C04B35/117 , C04B35/185 , C04B35/565 , C04B35/803 , C04B35/806 , C04B35/83 , C04B37/026 , C04B2235/5224 , C04B2235/5228 , C04B2235/5244 , C04B2235/5248 , C04B2235/963 , C04B2237/123 , C04B2237/365 , C04B2237/38 , C04B2237/405 , C04B2237/592 , C04B2237/64 , C04B2237/66 , C04B2237/708 , C04B2237/76 , C04B2237/84 , F01D5/3084 , F01D5/3092 , F05D2300/6033 , F23R3/007 , F23R3/60 , F23R2900/00017 , Y10T29/49336
Abstract: An apparatus to reduce wear and friction between CMC-to-metal attachment and interface, including a metal layer configured for insertion between a surface interface between a CMC component and a metal component. The surface interface of the metal layer is compliant relative to asperities of the surface interface of the CMC component. A coefficient of friction between the surface interface of the CMC component and the metal component is about 1.0 or less at an operating temperature between about 300° C. to about 325° C. and a limiting temperature of the metal component.
Abstract translation: 一种降低CMC与金属附件和界面之间的磨损和摩擦的装置，包括配置成插入在CMC组件和金属部件之间的表面界面之间的金属层。 金属层的表面界面相对于CMC部件的表面界面的粗糙度是顺从的。 在约300℃至约325℃的操作温度和金属组分的极限温度之间，CMC组分的表面界面与金属组分之间的摩擦系数约为1.0或更小。
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