专利检索 cpc:"C04B41/5059" 第 1 页

1.

发明公开
CERAMIC SUBSTATE WITH REACTION-BONDED SILICON CARBIDE HAVING DIAMOND PARTICLES 审中-公开

公开(公告)号：US20240360049A1

公开(公告)日：2024-10-31

申请号：US18761840

申请日：2024-07-02

申请人： II-VI Delaware, Inc.

发明人： Samuel M SALAMONE , Glenn EVANS, JR.

IPC分类号： C04B41/87 , B24B53/017 , B28B11/24 , C04B41/00 , C04B41/45 , C04B41/50

CPC分类号： C04B41/87 , B24B53/017 , B28B11/243 , C04B41/009 , C04B41/4511 , C04B41/4539 , C04B41/455 , C04B41/5059

摘要： A composite material can include: a substrate of a first reaction-bonded silicon carbide (first RB—SiC) material; and a reaction-bonded diamond-retaining silicon carbide (RB-DSiC) layer bonded to a surface of the substrate. In some aspects, the RB-DSiC layer includes diamond particles bonded with a second reaction-bonded silicon carbide (second RB—SiC) material. The diamond particles may be homogeneously distributed through the second RB—SiC or only at the surface thereof. The diamond particles can be in an ordered pattern or un-ordered pattern. For example, a CMP conditioning disc can include the composite material of one of the embodiments.

2.

发明公开
Powder Compositions Including Chopped Coated Silicon Carbide Fibers and Method of Producing or Repairing a Fiber-Reinforced Ceramic Matrix Composite 审中-公开

公开(公告)号：US20240182368A1

公开(公告)日：2024-06-06

申请号：US18075758

申请日：2022-12-06

申请人： Rolls-Royce North American Technologies Inc. , Rolls-Royce High Temperature Composites Inc.

发明人： Robert Hays , Chris Monteleone , Sujit Nanda

IPC分类号： C04B35/80 , C04B35/628 , C04B35/64 , C04B35/657 , C04B41/00 , C04B41/45 , C04B41/50 , C04B41/87

CPC分类号： C04B35/80 , C04B35/62863 , C04B35/62892 , C04B35/64 , C04B35/657 , C04B41/009 , C04B41/4539 , C04B41/4572 , C04B41/4596 , C04B41/5059 , C04B41/87 , C04B2235/3826 , C04B2235/428 , C04B2235/5244 , C04B2235/5252 , C04B2235/526 , C04B2235/616

摘要： A method of producing or repairing a fiber-reinforced ceramic matrix composite comprises delivering a powder composition comprising SiC particles and chopped coated SiC fibers into or onto a powder receptacle configured for composite fabrication or repair. After delivering the powder composition into or onto the powder receptacle, the SiC particles are densified to form a SiC matrix reinforced with the chopped coated SiC fibers, thereby producing or repairing a fiber-reinforced ceramic matrix composite.

3.

发明公开
MULTILAYER INTERFACE COATING WITH THERMALLY-GROWN OXIDE FOR IMPROVED DURABILITY 审中-公开

公开(公告)号：US20240018060A1

公开(公告)日：2024-01-18

申请号：US17866024

申请日：2022-07-15

申请人： Raytheon Technologies Corporation

发明人： Evan B. Callaway

IPC分类号： C04B41/50 , C04B41/52 , C04B35/80 , C04B41/89 , C04B41/87

CPC分类号： C04B41/5064 , C04B41/524 , C04B41/5059 , C04B35/80 , C04B41/89 , C04B41/87 , C04B2235/5252 , C04B2235/386 , C04B2235/9684 , C04B2235/3826

摘要： A coated fiber structure for use in a ceramic matrix composite comprises a fiber and a coating system applied to and circumscribing the fiber. The coating system comprises a first boron nitride layer, a silicon carbide layer extending coaxially with and in direct contact with the first boron nitride layer, a first thermally-grown oxide layer formed on the silicon carbide layer, and a second boron nitride layer extending coaxially with and in direct contact with the first thermally-grown oxide layer.

4.

发明公开
ADAPTIVE SURFACE TEXTURING FOR CERAMIC MATRIX COMPOSITES 审中-公开

公开(公告)号：US20230250033A1

公开(公告)日：2023-08-10

申请号：US17665069

申请日：2022-02-04

申请人： Raytheon Technologies Corporation

发明人： Zhigang Wang , Xia Tang , James T. Beals , Gajawalli V. Srinivasan , John D. Riehl , Brian T. Hazel , David A. Litton

IPC分类号： C04B41/50 , C04B41/45 , F01D5/28

CPC分类号： C04B41/5059 , C04B41/4531 , F01D5/282 , F01D5/284 , C04B2235/74

摘要： An adaptive surface texturing method is provided for use with a part formed of ceramic matrix composites (CMCs) to be coated with an environmental barrier coating (EBC). The method includes coating a CMC surface of the part with an initial coating, determining a contour and an undulation pattern of the CMC surface and designing a texturing pattern to follow the contour and the undulation pattern and to be formed in the initial coating based on a thickness of the initial coating and an average particle size of a slurry of the EBC.

5.

发明授权
Method for producing a surface layer on a ceramic matrix composite 有权

公开(公告)号：US11667580B2

公开(公告)日：2023-06-06

申请号：US17012977

申请日：2020-09-04

申请人： Rolls-Royce High Temperature Composites Inc.

发明人： Pathikumar Sellappan , Sungbo Shim , Kevin Mark Lukhard

IPC分类号： C04B35/80 , F01D25/08 , C04B35/628 , C04B35/657 , C04B41/00 , C04B41/50 , C04B41/87 , B28B11/04

CPC分类号： C04B35/80 , B28B11/041 , C04B35/62863 , C04B35/62873 , C04B35/657 , C04B41/009 , C04B41/5059 , C04B41/87 , F01D25/08 , C04B2235/3826 , C04B2235/48 , C04B2235/5252 , C04B2235/616 , F05D2220/32 , F05D2230/20 , F05D2230/90

摘要： A method is provided in which a resin coating is applied to a surface of a preform. The resin coating includes a carbonaceous resin and a particulate. The preform is added to a tooling. The preform, which is positioned in the tooling, is cured. The tooling is removed. The resin coating on the surface of the preform is pyrolyzed to form a resin carbon-char layer on the surface of the preform. The preform and the resin carbon-char layer are infiltrated with silicon to form a ceramic matrix composite (CMC) component including a layer of silicon carbide. During the infiltration, the silicon reacts with carbon in the resin carbon-char layer to form the layer of silicon carbide on the preform.

6.

发明授权
Ceramic composites with an intermediate layer having a carbon sink material for high temperature applications 有权

公开(公告)号：US11655194B2

公开(公告)日：2023-05-23

申请号：US16655626

申请日：2019-10-17

申请人： General Electric Company

发明人： Krishan Lal Luthra , Glen Harold Kirby , Julin Wan , Larry Steven Rosenzweig

IPC分类号： C04B41/00 , C04B35/80 , C04B41/50 , C04B41/52

CPC分类号： C04B41/009 , C04B35/80 , C04B41/5057 , C04B41/5059 , C04B41/5071 , C04B41/522 , C04B2235/3826 , C04B2235/5244

摘要： Coated components, along with methods of their formation, are provided. The coated component includes a ceramic substrate having a surface; an intermediate layer on the surface of the ceramic substrate; and an environmental barrier coating on the intermediate layer. The intermediate layer includes a carbon-sink material that inhibits accumulation of free carbon from a carbon-containing species within the intermediate layer, the ceramic substrate, or both.

7.

发明公开
C/C COMPOSITE AND METHOD FOR PRODUCING SAME, AND HEAT-TREATMENT JIG AND METHOD FOR PRODUCING SAME 审中-公开

公开(公告)号：US20230150888A1

公开(公告)日：2023-05-18

申请号：US17917384

申请日：2021-04-09

申请人： TOYO TANSO CO., LTD.

发明人： Syuhei TOMITA , Hiroshi MACHINO , Yoko NISHI

IPC分类号： C04B35/83 , C04B35/524 , C04B41/00 , C04B41/45 , C04B41/50 , C04B41/85

CPC分类号： C04B35/83 , C04B35/524 , C04B41/0072 , C04B41/457 , C04B41/5096 , C04B41/5015 , C04B41/5059 , C04B41/85 , C04B2235/428 , C04B2235/465 , C04B2235/5248 , C04B2235/5268

摘要： Provided is a C/C composite having a long life in an environment including a heating process and a cooling process and having less adverse effects on surrounding facilities and the quality of treatment objects. A C/C composite in which, in measurement for open pores by mercury porosimetry, an open porosity for open pores with a radius of not less than 0.4 μm and less than 10 μm in the C/C composite is 2.0% or less.

8.

发明申请
PLUGGED HONEYCOMB STRUCTURE 审中-公开

公开(公告)号：US20180272328A1

公开(公告)日：2018-09-27

申请号：US15907618

申请日：2018-02-28

申请人： NGK INSULATORS, LTD.

发明人： Kazuya YUKI

IPC分类号： B01J35/04 , B01D46/24 , B01D46/00 , B01D53/94 , C04B38/00

CPC分类号： B01J35/04 , B01D46/0061 , B01D46/2448 , B01D46/2466 , B01D53/9418 , B01D53/944 , B01D53/9454 , B01D2046/2481 , B01D2046/2496 , B01D2255/9155 , B01D2279/30 , B01J37/0215 , C04B38/0012 , C04B41/009 , C04B41/5089 , C04B41/85 , C04B35/00 , C04B38/0006 , C04B35/565 , C04B14/38 , C04B41/5037 , C04B41/5059

摘要： A plugged honeycomb structure, including: a plurality of honeycomb segments, a bonding layer and a circumferential wall disposed to surround circumference of a honeycomb segment bonded body where the plurality of honeycomb segments are bonded, wherein in the bonding layer, the bonding layer at a part that bonds the honeycomb segments disposed in contact with the circumferential wall is a circumferential bonding layer, and the bonding layer at a part that bonds the honeycomb segment including a center of gravity in a cross section orthogonal to the extending direction of cells of the honeycomb segment bonded body or at a position closest to the center of gravity and another honeycomb segment adjacent to the honeycomb segment is a center bonding layer, and a bonding strength A1 of the circumferential bonding layer is larger than a bonding strength A2 of the center bonding layer.