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公开(公告)号:US11639304B2
公开(公告)日:2023-05-02
申请号:US16784384
申请日:2020-02-07
Applicant: United Technologies Corporation
Inventor: John J. Gangloff, Jr. , Paul Sheedy , Rajiv Ranjan
Abstract: A method of fabricating a glass matrix composite includes providing a fiber preform in a cavity of a die tooling, the fiber preform circumscribing an interior region; providing a parison of glass matrix material in the interior region, the glass matrix material having a first viscosity; introducing pressurized inert gas into the parison to outwardly inflate the parison against the fiber preform; and while under pressure from the pressurized inert gas, decreasing the first viscosity of the glass matrix material to a second viscosity. The pressure and the second viscosity cause the glass matrix material to flow and infiltrate into the fiber preform to thereby form a consolidated workpiece. The consolidated workpiece is then cooled to form a glass matrix composite.
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公开(公告)号:US11602791B2
公开(公告)日:2023-03-14
申请号:US16131700
申请日:2018-09-14
Applicant: United Technologies Corporation
Inventor: John A. Sharon , Paul Sheedy , Ranadip Acharya , Vijay Narayan Jagdale
Abstract: A process for additive manufacturing of a metal alloy material is provided that includes: a) providing a feedstock powder comprising base powder particles with nanoparticles attached to surfaces of the base powder particles; b) providing an additive manufacturing system with a laser power source relatively movable at a scan speed; c) wherein the additive manufacturing system has a process window for the feedstock powder; and d) exposing the feedstock powder to a predetermined power input from the laser power source at a predetermined scan speed to produce the metal alloy material. The concentration by volume of nanoparticles within the feedstock powder is such that independent first and second microstructures may be produced within the metal alloy material.
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公开(公告)号:US11459650B2
公开(公告)日:2022-10-04
申请号:US15789393
申请日:2017-10-20
Applicant: United Technologies Corporation
Inventor: Xia Tang , David C. Jarmon , James T. Beals , R. Wesley Jackson , Paul Sheedy
IPC: C23C4/10 , C23C24/08 , C23C28/04 , C23C4/11 , C04B41/00 , C23C4/12 , C04B41/52 , C04B41/89 , F01D5/28 , C23C4/129 , C23C4/134 , F01D25/00
Abstract: A coated article including an article having a surface; an oxidation resistant bond coat layer deposited on the surface, the oxidation resistant bond coat layer comprising a healing silica matrix and at least one oxygen scavenger forming a metal silicide network dispersed within the healing silica matrix; and a top coat layer disposed upon the oxidation resistant bond coat layer, whereby the oxidation resistant bond coat layer is operable to seal a crack in the top coat layer.
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公开(公告)号:US11414355B2
公开(公告)日:2022-08-16
申请号:US16361040
申请日:2019-03-21
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Paul Sheedy , John A. Sharon , Wayde R. Schmidt , Neal Magdefrau
IPC: B32B18/00 , C04B35/80 , C04B37/00 , C04B35/645 , B33Y70/00 , B33Y80/00 , B22F5/00 , B22F7/00 , C04B35/571 , C04B35/628 , C04B35/83
Abstract: A turbine engine component may comprise a Ceramic Matrix Composite (CMC) structure including a plurality of nominally dense plies, wherein each of the plurality of the nominally dense plies are bonded by at least one of a Field Assisted Sintering Technique (FAST), a Spark Plasma Sintering (SPS), or a localized heating at a bonding interface. The turbine engine component may include an airfoil extending between a first platform and a second platform, wherein the airfoil, the first platform, and the second platform define the CMC structure.
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公开(公告)号:US20210039999A1
公开(公告)日:2021-02-11
申请号:US16536725
申请日:2019-08-09
Applicant: United Technologies Corporation
Inventor: Paul Sheedy , Neal Magdefrau , Wayde R. Schmidt
IPC: C04B35/80 , C04B35/628 , C04B41/89
Abstract: Disclosed is a method of making high temperature fiber including chemically bonding high temperature material to a fiber template at a first temperature to form a precursor fiber and processing the precursor fiber at a second temperature to form the high temperature fiber. The first temperature does not equal the second temperature. Also disclosed are high temperature fibers made by the method.
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公开(公告)号:US20200215640A1
公开(公告)日:2020-07-09
申请号:US16240308
申请日:2019-01-04
Applicant: United Technologies Corporation
Inventor: Paul Sheedy , John A. Sharon , Wayde R. Schmidt
Abstract: An embodiment of a method includes fabricating a first single crystal boule having a uniform composition and grain orientation. The first uniform single crystal boule is divided into a first plurality of layered shapes. The shapes of the first plurality are stacked with at least a second plurality of layered shapes along a first axis. The second plurality of layered shapes have at least one physical aspect differing from at least one corresponding physical aspect of the first plurality of layered shapes. The first plurality of layered shapes and at least the second plurality of layered shapes are joined via a field assisted sintering technique (FAST) to form a bulk component.
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公开(公告)号:US20200147897A1
公开(公告)日:2020-05-14
申请号:US16185201
申请日:2018-11-09
Applicant: United Technologies Corporation
Inventor: Wayde R. Schmidt , Paul Sheedy , John A. Sharon , Dustin D. Caldwell , Slade R. Culp
Abstract: An additive manufactured multi-portion article includes a first portion of an article manufactured by a first additive manufacturing process; and a second portion of the article manufactured by a second additive manufacturing process different than the first additive manufacturing process, the second portion attached to the first portion.
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公开(公告)号:US20200056488A1
公开(公告)日:2020-02-20
申请号:US15998730
申请日:2018-08-16
Applicant: United Technologies Corporation
Inventor: Richard Wesley Jackson , James T. Beals , Tania Bhatia Kashyap , Wayde R. Schmidt , Paul Sheedy , Xia Tang
IPC: F01D5/28 , C04B35/14 , C04B35/622 , C04B35/63
Abstract: An environmental barrier coating, comprising a substrate containing silicon; an environmental barrier layer applied to the substrate; the environmental barrier layer comprising an oxide matrix; an oxidant getter phase interspersed throughout the oxide matrix; and a self-healing phase interspersed throughout the oxide matrix.
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公开(公告)号:US20200010375A1
公开(公告)日:2020-01-09
申请号:US16550839
申请日:2019-08-26
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Xia Tang , Paul Sheedy , Tania Bhatia Kashyap , Wayde R. Schmidt , Daniel G. Goberman
IPC: C04B41/87 , B32B9/00 , C04B35/14 , C04B35/195 , C04B35/56
Abstract: An article includes a ceramic-based substrate and a barrier layer on the ceramic-based substrate. The barrier layer includes a matrix of barium-magnesium alumino-silicate or SiO2, a dispersion of silicon oxycarbide particles in the matrix, and a dispersion of particles, of the other of barium-magnesium alumino-silicate or SiO2, in the matrix.
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公开(公告)号:US20190329532A1
公开(公告)日:2019-10-31
申请号:US16259290
申请日:2019-01-28
Applicant: United Technologies Corporation
Inventor: Paul Sheedy , Wayde R. Schmidt , Erica L. Prevost , Alex J. Sember
IPC: B32B18/00 , C04B35/563 , C04B35/581 , C04B35/571 , C09J5/00 , C04B35/10 , C04B35/74 , C04B35/583 , C04B35/589
Abstract: A method of preparing a composite preform includes applying a tacky preceramic-polymer-based adhesive on a first fiber array arranging a second fiber array on the first fiber array, the adhesive holding the first and second fiber arrays together. A composite component is also disclosed.
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