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公开(公告)号：US10526912B2
公开(公告)日：2020-01-07
申请号：US15134429
申请日：2016-04-21
Applicant: United Technologies Corporation
Inventor： Stanley J. Funk , Edward F. Pietraszkiewicz
Abstract: A method of designing a turbine blade includes the steps of forming at least two notches on a tip of a turbine blade, each of the at least two notches having a known dimension. The turbine blade has a pressure side and a suction side. The method further includes the step of operating a gas turbine engine including the turbine blade to expand a length of the turbine blade such that the tip of the turbine engages a casing. The method further includes the steps of viewing the tip of the turbine blade after the step of operating of the gas turbine engine, determining an appearance of the notches on the tip and determining a manufacturing length of the turbine blade based on the step of determining the appearance the notches.
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公开(公告)号：US20160003158A1
公开(公告)日：2016-01-07
申请号：US14790951
申请日：2015-07-02
Applicant: United Technologies Corporation
Inventor： Joe Ott , Stanley J. Funk , Roger O. Coffey , Shawn Stempinski , John J. Rup, JR. , Lyutsia Dautova , Dennis M. Moura
CPC classification number: F02C7/222 , F05D2220/32 , F23N1/00 , F23N2035/16 , F23R3/14 , F23R3/28 , F23R3/36 , F23R2900/00001
Abstract: A fluid dispensing apparatus that may be additive manufactured as one unitary piece and may be a fuel injector for a gas turbine engine includes a radial displacement bellows having an outer surface that faces and may be exposed to a surrounding environment and an interior surface that faces and may define at least in-part a flowpath extending along a centerline. The radial displacement bellows is constructed and arranged to move between an expanded state when a pressure differential between the environment and the flowpath is low to a restricted state when the pressure differential is high.
Abstract translation: 可以作为一个整体件制成的并且可以是用于燃气涡轮发动机的燃料喷射器的流体分配装置包括径向位移波纹管，其具有面向并可能暴露于周围环境的外表面和面向和 可以至少部分地限定沿着中心线延伸的流路。 当压差高时，径向位移波纹管被构造和布置成当环境和流路之间的压差低到受限状态时在膨胀状态之间移动。
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公开(公告)号：US20180087696A1
公开(公告)日：2018-03-29
申请号：US15825947
申请日：2017-11-29
Applicant: United Technologies Corporation
Inventor： Joe Ott , Dennis M. Moura , Stanley J. Funk , Shawn Stempinski , Roger O. Coffey , John J. Rup, JR. , Gary A. Schirtzinger , Lexia Kironn
CPC classification number: F16L11/22 , B23P15/00 , B33Y10/00 , B33Y80/00 , F02C7/222 , F05D2230/31 , F05D2260/36 , F16L39/005 , Y10T29/4932 , Y10T29/49325 , Y10T29/4933 , Y10T29/4935 , Y10T29/49391 , Y10T29/49393 , Y10T29/49442 , Y10T29/49444 , Y10T29/49636 , Y10T29/49904 , Y10T29/4998
Abstract: A method is provided involving an additive manufacturing system. This method includes a step of forming a first fluid conduit using the additive manufacturing system. The method also includes a step of providing a fluid coupling. The fluid coupling includes the first fluid conduit and a second fluid conduit. The first fluid conduit is connected to and fluidly coupled with the second fluid conduit. The first fluid conduit has a first configuration. The second fluid conduit has a second configuration that is different than the first configuration.
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公开(公告)号：US20160348913A1
公开(公告)日：2016-12-01
申请号：US15112985
申请日：2015-01-14
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Joe Ott , Gary A. Schirtzinger , Lexia Kironn , Dennis M. Moura , Stanley J. Funk , Roger O. Coffey
CPC classification number: F23R3/28 , F02C7/222 , F05D2220/32 , F05D2230/53 , F05D2240/35 , F05D2250/61 , F05D2260/231 , F05D2300/10 , F23D2213/00 , F23D2900/00018 , F23R2900/00005 , F23R2900/00018
Abstract: One embodiment includes a fuel injector. The fuel injector assembly comprises a conduit for conveying fuel from a fuel inlet to a nozzle. The conduit is located in a support, with the conduit, the nozzle, and the support being a single unitary piece. A thermally compliant feature is located at the nozzle which allows the fuel injector to adjust for differential thermal expansion.
Abstract translation: 一个实施例包括燃料喷射器。 燃料喷射器组件包括用于将燃料从燃料入口输送到喷嘴的导管。 导管位于支撑件中，导管，喷嘴和支撑件是单个整体件。 在喷嘴处设有热适应特征，其允许燃料喷射器调节差动热膨胀。
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公开(公告)号：US20160230590A1
公开(公告)日：2016-08-11
申请号：US15134429
申请日：2016-04-21
Applicant: United Technologies Corporation
Inventor： Stanley J. Funk , Edward F. Pietraszkiewicz
CPC classification number: F01D21/003 , F01D5/141 , F01D5/20 , F01D25/24 , F05D2220/32 , F05D2230/50 , F05D2240/307 , F05D2260/83 , Y10T29/49336
Abstract: A method of designing a turbine blade includes the steps of forming at least two notches on a tip of a turbine blade, each of the at least two notches having a known dimension. The turbine blade has a pressure side and a suction side. The method further includes the step of operating a gas turbine engine including the turbine blade to expand a length of the turbine blade such that the tip of the turbine engages a casing. The method further includes the steps of viewing the tip of the turbine blade after the step of operating of the gas turbine engine, determining an appearance of the notches on the tip and determining a manufacturing length of the turbine blade based on the step of determining the appearance the notches.
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Patent Agency Ranking
公开(公告)号：US10683952B2
公开(公告)日：2020-06-16
申请号：US15825947
申请日：2017-11-29
Applicant: United Technologies Corporation
Inventor： Joe Ott , Dennis M. Moura , Stanley J. Funk , Shawn Stempinski , Roger O. Coffey , John J. Rup, Jr. , Gary A. Schirtzinger , Lexia Kironn
Abstract: A method is provided involving an additive manufacturing system. This method includes a step of forming a first fluid conduit using the additive manufacturing system. The method also includes a step of providing a fluid coupling. The fluid coupling includes the first fluid conduit and a second fluid conduit. The first fluid conduit is connected to and fluidly coupled with the second fluid conduit. The first fluid conduit has a first configuration. The second fluid conduit has a second configuration that is different than the first configuration.
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公开(公告)号：US10508759B2
公开(公告)日：2019-12-17
申请号：US15661791
申请日：2017-07-27
Applicant: United Technologies Corporation
Inventor： Joe Ott , John J. Rup, Jr. , Shawn Stempinski , Stanley J. Funk , Dennis M. Moura , Lexia Kironn , Roger O. Coffey
IPC: F16L9/18 , B33Y10/00 , B23P15/00 , F23R3/28 , B33Y80/00 , B22F3/105 , F16L59/14 , F02C7/22 , B22F5/10
Abstract: A flowpath assembly has a first conduit defining a flowpath radially inward, and a second conduit spaced radially outward from the first conduit. A void defined between the first and second conduits contains an insulating material that may have a greater porosity than the first and second conduits. The assembly may be additive manufactured generally as one unitary piece with the raw material of the conduits being melted and solidified on a slice-by-slice basis and the insulating material being selectively bypassed by an energy gun of an additive manufacturing system.
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公开(公告)号：US10208673B2
公开(公告)日：2019-02-19
申请号：US14790951
申请日：2015-07-02
Applicant: United Technologies Corporation
Inventor： Joe Ott , Stanley J. Funk , Roger O. Coffey , Shawn Stempinski , John J. Rup, Jr. , Lyutsia Dautova , Dennis M. Moura
Abstract: A fluid dispensing apparatus that may be additive manufactured as one unitary piece and may be a fuel injector for a gas turbine engine includes a radial displacement bellows having an outer surface that faces and may be exposed to a surrounding environment and an interior surface that faces and may define at least in-part a flowpath extending along a centerline. The radial displacement bellows is constructed and arranged to move between an expanded state when a pressure differential between the environment and the flowpath is low to a restricted state when the pressure differential is high.
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公开(公告)号：US20170321824A1
公开(公告)日：2017-11-09
申请号：US15661791
申请日：2017-07-27
Applicant: United Technologies Corporation
Inventor： Joe Ott , John J. Rup, JR. , Shawn Stempinski , Stanley J. Funk , Dennis M. Moura , Lexia Kironn , Roger O. Coffey
CPC classification number: F16L9/18 , B22F3/1055 , B22F5/10 , B33Y10/00 , B33Y80/00 , F02C7/222 , F16L59/14 , F23R3/283 , F23R2900/00018
Abstract: A flowpath assembly has a first conduit defining a flowpath radially inward, and a second conduit spaced radially outward from the first conduit. A void defined between the first and second conduits contains an insulating material that may have a greater porosity than the first and second conduits. The assembly may be additive manufactured generally as one unitary piece with the raw material of the conduits being melted and solidified on a slice-by-slice basis and the insulating material being selectively bypassed by an energy gun of an additive manufacturing system.
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10.发明申请ADDITIVELY MANUFACTURED SWIRLER MOUNT INTERFACE FOR GAS TURBINE ENGINE COMBUSTOR 审中-公开燃气涡轮发动机配套设备的额外配置的SWIRLER MOUNT接口公开(公告)号：US20170059163A1
公开(公告)日：2017-03-02
申请号：US14796042
申请日：2015-07-10
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Joe Ott , Stanley J. Funk , Lyutsia Dautova , John J. Rup, JR. , Dennis M. Moura , Shawn Stempinski , Roger O. Coffey
IPC: F23R3/28
CPC classification number: F23R3/286 , B22F3/1055 , B22F5/009 , B22F7/062 , B22F2007/068 , B23P6/007 , B23P2700/13 , F23R3/12 , F23R3/28 , F23R3/283 , F23R2900/00018 , F23R2900/00019 , Y02P10/295
Abstract: A component for a gas turbine engine, the component according to one disclosed non-limiting embodiment of the present disclosure includes an additively manufactured wear surface.
Abstract translation: 用于燃气涡轮发动机的部件，根据本公开的一个公开的非限制性实施例的部件包括相加制造的磨损表面。
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