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公开(公告)号：US20200182472A1
公开(公告)日：2020-06-11
申请号：US16786475
申请日：2020-02-10
Applicant: Rolls-Royce High Temperature Composites Inc.
Inventor： Sujit Nanda
IPC: F23R3/48
Abstract: A fluid conduit may be provided comprising a ceramic matrix composite (CMC) cross-over tube and a flange. The CMC cross-over tube may comprise a first end configured to extend into a first combustor liner of a gas turbine engine, and a second end configured to extend into a second combustor liner of a gas turbine engine. The interior of the CMC cross-over tube may define a passageway. The flange may extend outwardly from an outer surface of the CMC cross-over tube. The flange may be configured to engage at least one of the first combustor liner and the second combustor liner.
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公开(公告)号：US10577978B2
公开(公告)日：2020-03-03
申请号：US15803336
申请日：2017-11-03
Applicant: Rolls-Royce Corporation , Rolls-Royce North American Technologies, Inc. , Rolls-Royce High Temperature Composites Inc.
Inventor： Ted J. Freeman , Aaron D. Sippel , Daniel K. Vetters , David J. Thomas , Alexandra R. Baucco , Joseph P. Lamusga
Abstract: An assembly adapted for use in a gas turbine engine has a carrier component and a supported component. The assembly including a mounting system for coupling the supported component to the carrier component and a seal adapted to resist the movement of gasses between the supported component to the carrier component. In an illustrative embodiment, the assembly is a turbine shroud segment for blocking gasses from passing over turbine blades included in the gas turbine engine.
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公开(公告)号：US10577961B2
公开(公告)日：2020-03-03
申请号：US15959906
申请日：2018-04-23
Applicant: Rolls-Royce High Temperature Composites Inc. , Rolls-Royce Corporation , Rolls-Royce North American Technologies Inc. , Rolls-Royce plc
Inventor： Stephen Harris , Aaron D. Sippel , Ted J. Freeman , Anthony Razzell
Abstract: A turbine wheel for use in a gas turbine engine having a plurality of blades attached to a rotor disk. The blades each fit within slots formed in the rotor disk to couple the blades to the rotor disk. Platform segments are arranged about each of the blades.
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公开(公告)号：US10577951B2
公开(公告)日：2020-03-03
申请号：US15365498
申请日：2016-11-30
Applicant: Rolls-Royce North American Technologies, Inc. , Rolls-Royce High Temperature Composites Inc.
Inventor： Daniel K. Vetters , Ted J. Freeman , Andrew J. Lazur , Robert J. Shinavski , Wayne S. Steffier
Abstract: A gas turbine engine includes a turbine having turbine blades and a shroud having a blade track for positioning radially outside of the blades. At least one of the blades and the blade track are secured in place using a dovetail connection between a dovetail receiver and a dovetail assembly formed to include a contoured root.
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公开(公告)号：US10519807B2
公开(公告)日：2019-12-31
申请号：US15491601
申请日：2017-04-19
Applicant: Rolls-Royce Corporation , Rolls-Royce High Temperature Composites, Inc. , Rolls-Royce North American Technologies, Inc.
Inventor： Brian J. Shoemaker , Joseph P. Lamusga , Ted J. Freeman
Abstract: Turbine assemblies for a turbine of a gas turbine engine are disclosed herein. The turbine assemblies include a carrier and a blade track. The blade track extends around blades of a turbine wheel assembly to block gasses passed along a gas path from moving over the blades without causing the blades to rotate during operation of the turbine assembly. The blade track includes a plurality of blade track segments arranged circumferentially adjacent to one another about a central axis to form a ring. A retention ring engages both the carrier and the blade track segments to facilitate coupling and sealing.
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Patent Agency Ranking
166.发明申请公开(公告)号：US20190367417A1
公开(公告)日：2019-12-05
申请号：US15995537
申请日：2018-06-01
Applicant: Rolls-Royce High Temperature Composites Inc.
Inventor： Stephen Harris
IPC: C04B35/80 , C04B35/565 , F01D5/28
Abstract: A method of controllably coating a fiber preform has been developed. The method includes infiltrating a fiber preform with a first solvent to form a solvent-filled preform. After the infiltration, a slurry is applied to one or more outer surfaces of the solvent-filled preform to form a slurry coating thereon. The slurry coating comprises particulate solids dispersed in a second solvent having a vapor pressure higher than that of the first solvent. The slurry coating and the solvent-filled preform are dried. During drying, the second solvent evaporates from the slurry coating before the first solvent evaporates from the solvent-filled preform. The slurry coating dries to form a porous surface coating comprising the particulate solids on the one or more outer surfaces of the solvent-filled preform. The drying of the solvent-filled preform continues after formation of the porous surface coating to remove the first solvent.
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公开(公告)号：US20190360097A1
公开(公告)日：2019-11-28
申请号：US15989697
申请日：2018-05-25
Applicant: Rolls-Royce High Temperature Composites Inc.
Inventor： Stephen Harris
Abstract: An apparatus for coating specimens includes a reaction chamber and a plurality of reaction modules in the reaction chamber for containing specimens to be coated, where each reaction module includes a module inlet and a module outlet. A plurality of conduits are configured to be in fluid communication with at least one gas source external to the reaction chamber, and each of the conduits terminates in one of the reaction modules for delivery of gaseous reagents to the specimens to be coated. The module outlets are in fluid communication with the reaction chamber for expulsion of gaseous reaction products from the reaction modules.
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公开(公告)号：US10406640B2
公开(公告)日：2019-09-10
申请号：US14974802
申请日：2015-12-18
Inventor： Stephen Isaiah Harris
IPC: B23K26/50 , B23P6/04 , H05B6/80 , B23K26/00 , B23K9/00 , B23K15/00 , C04B35/565 , C04B35/628 , C04B35/80 , B23K103/08 , B23K103/16 , B23K103/00
Abstract: A method for repairing a ceramic matrix composite (CMC) article including a ceramic material in a matrix including a metal alloy, wherein a localized region of the metal alloy has a defect. The method includes applying heat to the localized region for a time sufficient to increase the temperature of the metal alloy in the localized region above the melt temperature thereof and cause the metal alloy in the localized region to flow and seal the crack.
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公开(公告)号：US20190185384A1
公开(公告)日：2019-06-20
申请号：US15845612
申请日：2017-12-18
Inventor： Sungbo Shim , Michael Abbott
IPC: C04B35/80 , C04B35/657 , C04B35/628
CPC classification number: C04B35/806 , C04B35/573 , C04B35/6263 , C04B35/62849 , C04B35/62852 , C04B35/6286 , C04B35/62863 , C04B35/62868 , C04B35/62871 , C04B35/62892 , C04B35/62894 , C04B35/657 , C04B2235/424 , C04B2235/427 , C04B2235/428 , C04B2235/5244 , C04B2235/5248 , C04B2235/5436 , C04B2235/5445 , C04B2235/5472 , C04B2235/606 , C04B2235/612 , C04B2235/616
Abstract: A method including infiltrating a porous fiber preform with a slurry including a carrier fluid and a first plurality of solid particles wherein the first plurality of solid particles includes at least a first ceramic material, drying the slurry to form a greenbody preform, machining the greenbody preform to a target dimension, depositing a protective layer precursor including a second plurality of solid particles on the machined greenbody preform wherein the second plurality of solid particles includes at least a second ceramic material, and infiltrating the machined greenbody preform with a molten infiltrant to form a composite article including an integral protective layer.
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公开(公告)号：US10215056B2
公开(公告)日：2019-02-26
申请号：US15179295
申请日：2016-06-10
Inventor： Aaron D. Sippel , Ted J. Freeman , David J. Thomas , Robert J. Shinavski , Zacheriah A. Cole
Abstract: A turbine shroud for positioning radially outside of blades of a turbine rotor includes a carrier, a blade track, and a track attachment system. The blade track is moved radially outwardly into a cavity of the carrier, and the track attachment system is adjusted to block radially inward movement of the blade track out of the cavity.
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