-
公开(公告)号：US10605121B2
公开(公告)日：2020-03-31
申请号：US16005118
申请日：2018-06-11
Applicant: Rolls-Royce North American Technologies, Inc. , Rolls-Royce High Temperature Composites, Inc.
Inventor： Daniel K. Vetters , Todd Engel , Robert J. Shinavski
IPC: F01D25/24
Abstract: An assembly for a gas turbine engine includes a carrier and a supported component comprising ceramic matrix composite materials. The assembly also includes a retention assembly for coupling the supported component to the carrier.
-
公开(公告)号：US10550709B2
公开(公告)日：2020-02-04
申请号：US15088884
申请日：2016-04-01
Applicant: Rolls-Royce North American Technologies, Inc. , Rolls-Royce Corporation , Rolls-Royce plc , Rolls-Royce High Temperature Composites Inc.
Inventor： Daniel K. Vetters , Aaron D. Sippel , David J. Thomas , Andrew J. Eifert , Paul A. Davis , Simon L. Jones , Steven M. Hillier , Peter Broadhead , Joseph Doyle , Michael Jacquinto , Wesley Thibault , Jun Shi , Roderick Townes
Abstract: A blade track assembly is disclosed. The blade track assembly comprises a plurality of ceramic matrix composite blade track segments arranged circumferentially adjacent to one another around a central axis. Each of the blade track segments includes an arcuate runner extending in a circumferential direction around a portion of the central axis and is coupled to circumferentially adjacent blade track segments.
-
公开(公告)号：US20190323371A1
公开(公告)日：2019-10-24
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.
-
公开(公告)号：US20190293533A1
公开(公告)日：2019-09-26
申请号：US16359855
申请日：2019-03-20
Inventor： Austin Warmuth
Abstract: A system includes a load actuator, a strain measurement device, and a computing device. The computing device is configured to receive an unconditioned displacement signal from the strain measurement device. The unconditioned displacement signal represents displacement of a specimen under load from the load actuator. The computing device is further configured to separate the unconditioned displacement signal into a measurement signal and a control signal. The computing device is further configured to filter the control signal to generate a filtered control signal and control the load actuator based on the filtered control signal. The computing device is further configured to determine a strain on the specimen based on the measurement signal.
-
公开(公告)号：US20190255732A1
公开(公告)日：2019-08-22
申请号：US16278265
申请日：2019-02-18
Inventor： Scott Nelson , Quinlan Shuck , Sean Landwehr , Sungbo Shim
IPC: B28B1/00 , B29C64/165 , B33Y10/00 , B33Y40/00 , C04B35/80 , C04B35/622 , C04B35/628 , C04B35/657
Abstract: A system and method for forming a porous ceramic preform is provided. The method may include forming a stacked powder structure including a binder layer and a powder layer on the binder layer. The binder layer may be formed by depositing a binder with a spray nozzle on a substrate. The powder layer may be formed by depositing a powder on the binder layer. The porous ceramic preform may be formed by heating the stacked powder structure to pyrolyze the binder. The porous ceramic preform is configured to be infiltrated by a molten material. The substrate may comprise a ceramic fiber preform. After melt infiltration of the porous ceramic preform and the ceramic fiber preform, a densified ceramic feature having a predetermined geometry may be formed on a ceramic matrix composite (CMC) component.
-
Patent Agency Ranking
公开(公告)号：US20190100466A1
公开(公告)日：2019-04-04
申请号：US16138251
申请日：2018-09-21
Inventor： Stephen Isaiah Harris
IPC: C04B35/80 , C04B35/628 , C04B35/626 , C04B35/573 , C04B35/624 , C23C2/04 , C04B35/64 , C04B35/65
Abstract: A method of forming a composite article may include impregnating an inorganic fiber porous preform with a first slurry composition. The slurry composition includes particles, a solvent, and a pre-gellant material. Gelling of the pre-gellant material in the slurry composition is initiated to substantially immobilize the particles and yield a gelled article. The method also includes impregnating the gelled article with a second solution that includes a high char-yielding component, and pyrolyzing the high char-yielding component to yield carbon and form a green composite article. The green composite article is then infiltrated with a molten metal or alloy infiltrant to form the composite article. The molten infiltrant reacts with carbon, and the final composite article may include less residual metal or alloy than a composite article formed without using the second solution.
-
公开(公告)号：US10227264B2
公开(公告)日：2019-03-12
申请号：US14798019
申请日：2015-07-13
Inventor： Stephen Isaiah Harris
IPC: C04B35/00 , C04B35/80 , C04B35/573 , C04B35/626 , C04B35/628 , C04B35/624 , C04B35/64 , C04B35/65 , C23C2/04
Abstract: A method of forming a composite article may include impregnating an inorganic fiber porous preform with a first slurry composition. The slurry composition includes particles, a solvent, and a pre-gellant material. Gelling of the pre-gellant material in the slurry composition is initiated to substantially immobilize the particles and yield a gelled article. The method also includes impregnating the gelled article with a second solution that includes a high char-yielding component, and pyrolyzing the high char-yielding component to yield carbon and form a green composite article. The green composite article is then infiltrated with a molten metal or alloy infiltrant to form the composite article. The molten infiltrant reacts with carbon, and the final composite article may include less residual metal or alloy than a composite article formed without using the second solution.
-
公开(公告)号：US20180371947A1
公开(公告)日：2018-12-27
申请号：US15992976
申请日：2018-05-30
Applicant: Rolls-Royce Corporation , Rolls-Royce High Temperature Composites, Inc. , Rolls-Royce North American Technologies Inc.
Inventor： Aaron D. Sippel , Ted J. Freeman , Joseph P. Lamusga , Daniel K. Vetters , Sean E. Landwehr , Bruce E. Varney
Abstract: An assembly for a gas turbine engine includes ceramic material containing (i.e. ceramic matrix composite) segments and joints that couple the segments together.
-
公开(公告)号：US20180346386A1
公开(公告)日：2018-12-06
申请号：US16058712
申请日：2018-08-08
Inventor： Anthony Martin Goetz , Robert J. Shinavski , Stephen Isaiah Harris , Sean E. Landwehr
IPC: C04B35/80 , C04B41/45 , C04B35/565 , C04B41/50 , C04B41/52 , C04B41/53 , C04B41/85 , C04B41/87 , C04B35/626 , C04B35/622 , C04B35/624 , C04B35/65 , C04B35/657 , C04B35/636 , C04B35/634 , C04B35/628 , C04B35/573
Abstract: A method of forming a composite article includes impregnating an inorganic fiber preform with a slurry composition. The slurry composition includes a particulate, a solvent, and a pre-gellant material. Gelling of the pre-gellant material in the slurry composition is initiated to immobilize the particulate and yield a gelled article, and substantially all solvent is removed from the gelled article to form a green composite article. The green composite article is then infiltrated with a molten infiltrant to form the composite article.
-
公开(公告)号：US20180306045A1
公开(公告)日：2018-10-25
申请号：US15950698
申请日：2018-04-11
Applicant: Rolls-Royce High Temperature Composites Inc. , Rolls-Royce North American Technologies Inc.
Inventor： Chris Barrett , Joseph P. Lamusga , Ted J. Freeman
IPC: F01D11/08
Abstract: A turbine shroud adapted for use in a gas turbine engine includes an attachment feature and a body. The attachment feature and the body are constructed of ceramic matrix composite materials. In an illustrative embodiment, the ceramic matrix composite materials form a blade track segment.
-
-
-
-
-
-
-
-
-
Search Results
232
records
(took 0.021 seconds)
