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公开(公告)号:US10954810B2
公开(公告)日:2021-03-23
申请号:US16221911
申请日:2018-12-17
Applicant: United Technologies Corporation
Inventor: Lawrence Binek , Matthew B. Kennedy , Evan Butcher , Jesse R. Boyer , Vijay Narayan Jagdale , Dmytro Mykolayovych Voytovych
Abstract: A unitary rub strip comprises a casing having an inner surface and an outer surface opposite the inner surface; a unitary rub strip is formed integral with the casing proximate the inner surface, wherein the unitary rub strip comprises a modified structure within the casing configured to abrade responsive to an interaction with a rotating element.
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公开(公告)号:US10144011B2
公开(公告)日:2018-12-04
申请号:US14972199
申请日:2015-12-17
Applicant: United Technologies Corporation
Inventor: Ying She , Aaron T. Nardi , Lawrence Binek
Abstract: A fluidized powder heat treatment classification assembly includes a gas source. A fluidized bed is connected to the gas source via a metered connection. The fluidized bed includes a first output connected to a powder classifier via at least a first valve. The powder classifier includes a catch container operable to decelerate a gas flow from the output and operable to catch particles entrained in the gas flow.
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公开(公告)号:US11541434B2
公开(公告)日:2023-01-03
申请号:US16243708
申请日:2019-01-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Lawrence Binek , David W. Morganson , Diana Giulietti
Abstract: An end effector for a vacuum system is disclosed. In various embodiments, the end effector includes a central duct having a first end configured for connection to a vacuum source and a second end defining a central duct inlet; a base member proximate the second end of the central duct; and a plurality of passages extending from an outer surface of the base member to an inner surface of the central duct, the plurality of passages characterized by a passage axis having an axial vector component.
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公开(公告)号:US11420263B2
公开(公告)日:2022-08-23
申请号:US16267816
申请日:2019-02-05
Applicant: United Technologies Corporation
Inventor: Lawrence Binek , Zachary Ryan Gibbons , Jesse R. Boyer
Abstract: A gas shield for an additive manufacturing system includes a bracket and a flexible curtain mounted to the bracket. A method of additively manufacturing includes removably mounting a gas shield to at least partially segregate a powder dispenser and a chamber.
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公开(公告)号:US11059048B2
公开(公告)日:2021-07-13
申请号:US16154145
申请日:2018-10-08
Applicant: United Technologies Corporation
Inventor: Ying She , Aaron T. Nardi , Lawrence Binek
Abstract: A fluidized powder heat treatment classification assembly includes a gas source. A fluidized bed is connected to the gas source via a metered connection. The fluidized bed includes a first output connected to a powder classifier via at least a first valve. The powder classifier includes a catch container operable to decelerate a gas flow from the output and operable to catch particles entrained in the gas flow.
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公开(公告)号:US20210003480A1
公开(公告)日:2021-01-07
申请号:US16503190
申请日:2019-07-03
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Lawrence Binek , David W. Morganson
Abstract: A method for inspecting a component made using an additive manufacturing process, the component having an internal conduit, is disclosed. In various embodiments, the method includes the steps of: attaching a fluid-blocking header to the component, the fluid-blocking header having an internal conformal surface configured to mate with an external conformal surface of the component; introducing a plugging media into the internal conduit; activating the fluid-blocking header to freeze the plugging media in a vicinity of the fluid-blocking header; pressurizing the internal conduit of the component; and analyzing a fluid flow characteristic at an outlet of the component to assess an occurrence of a blockage within the internal conduit.
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公开(公告)号:US20200332719A1
公开(公告)日:2020-10-22
申请号:US16388206
申请日:2019-04-18
Applicant: United Technologies Corporation
Inventor: Lawrence Binek , Matthew B. Kennedy , Jesse R. Boyer
IPC: F02C7/22
Abstract: An attritable engine includes an engine case, which includes an outer wall and a fuel rail integral with the outer wall. The fuel rail includes a fuel line integral with the outer wall, a fuel ring configured to receive fuel from the fuel line, and an injector throat configured to receive aerated fuel from the fuel ring. The engine case includes counter distortion webbing defining the injector throat and is integral with the fuel rail and the outer wall. The engine case includes a combustion chamber configured to receive fuel from the injector throat.
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公开(公告)号:US20200247056A1
公开(公告)日:2020-08-06
申请号:US16265159
申请日:2019-02-01
Applicant: United Technologies Corporation
Inventor: Lawrence Binek , Matthew J. Siopis
Abstract: An additive manufacturing method for an aircraft part having a polymer body and a metallic structural feature includes generating data defining the aircraft part with the metallic structural feature. A build process is determined for the polymer body of the aircraft part. The polymer body of the aircraft part is manufactured. A build path for a near net shape metallic structure is determined. The near net shape metallic structure is manufactured using an additive manufacturing process to direct metallic powder from a cold-spray nozzle on at least a section of the polymer body. The near net shape metallic structure is machined to provide the aircraft part having the polymer body and the metallic structural feature.
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公开(公告)号:US20200246871A1
公开(公告)日:2020-08-06
申请号:US16267816
申请日:2019-02-05
Applicant: United Technologies Corporation
Inventor: Lawrence Binek , Zachary Ryan Gibbons , Jesse R. Boyer
Abstract: A gas shield for an additive manufacturing system includes a bracket and a flexible curtain mounted to the bracket. A method of additively manufacturing includes removably mounting a gas shield to at least partially segregate a powder dispenser and a chamber.
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公开(公告)号:US20200182467A1
公开(公告)日:2020-06-11
申请号:US16212879
申请日:2018-12-07
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Lawrence Binek , Jesse R. Boyer , Dmytro Mykolayovych Voytovych
Abstract: A core engine article includes a combustor liner defining a combustion chamber therein and a turbine nozzle. The combustor liner includes a plurality of injector ports, and the plurality of injector ports have a shape that tapers to a corner on a forward side of the injector ports. The turbine nozzle includes a plurality of airfoils. The combustor liner and turbine nozzle are integral with one another. A method of making a core engine article is also disclosed.
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