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公开(公告)号:US10989408B2
公开(公告)日:2021-04-27
申请号:US16130837
申请日:2018-09-13
Applicant: United Technologies Corporation
Inventor: Lawrence Binek , Evan Butcher , Matthew B. Kennedy , Vijay Narayan Jagdale , Jesse R. Boyer , Dmytro Mykolayovych Voytovych
Abstract: A component for a gas turbine engine is disclosed. In various embodiments, the component includes a diffuser ring, a combustor and a spring element connecting the diffuser ring to the combustor.
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公开(公告)号:US10883369B2
公开(公告)日:2021-01-05
申请号:US15913722
申请日:2018-03-06
Applicant: United Technologies Corporation
Inventor: Wendell V. Twelves, Jr. , Kathleen E. Sinnamon , Lexia Kironn , Evan Butcher , Joe Ott , Matthew E. Lynch
Abstract: A ceramic component retention system includes a metallic component, a ceramic component, and at least one spring element arranged between the metallic component and the ceramic component. The metallic component has a first coefficient of thermal expansion, and the ceramic component has a second coefficient of thermal expansion. The at least one spring element is configured to mechanically couple the ceramic component to the metallic component.
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公开(公告)号:US10737363B2
公开(公告)日:2020-08-11
申请号:US16253501
申请日:2019-01-22
Applicant: United Technologies Corporation
Inventor: Joe Ott , Wendell V. Twelves, Jr. , Evan Butcher , Lexia Kironn
IPC: B24B5/06 , B22F3/24 , B24B1/04 , B24B5/40 , B29C64/35 , B33Y40/00 , B22F3/105 , B22F5/10 , B33Y10/00 , B33Y30/00
Abstract: A tool includes a flexible section; a head that extends form the flexible section; and an exciter within the head. A method of additively manufacturing a component including burrowing a tool into a conglomerated powder within an internal passage of an additively manufactured component, the tool vibrating in a manner to facilitate removal of the conglomerated powder.
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公开(公告)号:US20200230779A1
公开(公告)日:2020-07-23
申请号:US16842050
申请日:2020-04-07
Applicant: United Technologies Corporation
Inventor: Wendell V. Twelves , Joe Ott , Evan Butcher , John P. Rizzo, JR.
Abstract: A method for abrasive flow machining includes moving an abrasive media through a high-aspect passage of a workpiece. Local pressure of the abrasive media is increased at target abrasion surfaces of the high-aspect passage using a passage geometry that is configured to direct flow of the abrasive media into the target abrasion surfaces such that the target abrasion surfaces are preferentially polished by the abrasive media over other, non-targeted surfaces of the high-aspect passage at which the flow of the abrasive media is not directed into.
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公开(公告)号:US20200182155A1
公开(公告)日:2020-06-11
申请号:US16213047
申请日:2018-12-07
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Lawrence Binek , Evan Butcher , Jesse R. Boyer , Om P. Sharma , Bryan G. Dods , Vijay Narayan Jagdale
Abstract: A propulsion system according to an example of the present disclosure, includes a core engine and an outer casing surrounding the core engine. The outer casing includes an integral injector assembly. The injector assembly includes a wall that defines a cavity, the wall being integral with the outer casing. A method of operating a propulsion system and method of making a component of a propulsion system are also disclosed.
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公开(公告)号:US10598556B2
公开(公告)日:2020-03-24
申请号:US15112127
申请日:2014-08-08
Applicant: United Technologies Corporation
Inventor: Lyutsia Dautova , Wendell V. Twelves, Jr. , Joe Ott , Evan Butcher , Gary A. Schirtzinger , Rainer J. Herbert
IPC: B22F5/04 , B33Y40/00 , B33Y10/00 , B23K26/342 , G01L1/25 , G01N23/20 , B22F3/105 , F01D21/00 , B23K26/70 , B23K103/14
Abstract: A method of monitoring the residual stress in surface and near surface regions of a component includes identifying predetermined locations on the surface of a component that are expected to experience high stress during normal operating conditions of the component. Marker particles are introduced into the component during additive manufacture of the component at the predetermined locations. Then, the residual stress of the component is measured at a location corresponding with the marker material using x-ray techniques.
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公开(公告)号:US20190061238A1
公开(公告)日:2019-02-28
申请号:US16112213
申请日:2018-08-24
Applicant: United Technologies Corporation
Inventor: Gary A. Schirtzinger , Wendell V. Twelves, JR. , Evan Butcher , Lyutsia Dautova , Joe Ott
IPC: B29C64/165 , B33Y30/00 , B29C70/30 , B33Y10/00 , B29C64/141 , B29C64/112 , B29C70/68 , B29C70/38 , B29C64/118 , B29C64/106 , B29C64/147
Abstract: A machine for fabricating a fiber-reinforced component by additive manufacture is disclosed. The machine may have a surface, a matrix feed configured to deposit a plurality of matrix layers on the surface, and a fiber feed configured to deposit a fiber layer on at least one of the plurality of matrix layers. The deposition of the plurality of matrix layers and the fiber layer may be controlled by a computer.
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公开(公告)号:US20190030608A1
公开(公告)日:2019-01-31
申请号:US16148589
申请日:2018-10-01
Applicant: United Technologies Corporation
Inventor: Joe Ott , Wendell V. Twelves, JR. , Sergey Mironets , Lexia Kironn , Evan Butcher , Gary A. Schirtzinger
Abstract: A method of forming a metal component with two and three dimensional internal functionally graded alloy composition gradients includes forming the component by a powder based layer-by-layer additive manufacturing process. The areal composition distribution of each powder layer is determined by simultaneously depositing different powders and powder mixtures through a mixing valve attached to a single nozzle during powder deposition. The layers are then sintered with a directed energy source to form a forging preform. The preform is then forged to form a component.
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公开(公告)号:US20180178432A1
公开(公告)日:2018-06-28
申请号:US15901584
申请日:2018-02-21
Applicant: United Technologies Corporation
Inventor: Evan Butcher , Wendell Twelves , Gary Schirtzinger , Joe Ott , Lyutsia Dautova
IPC: B29C47/00 , B33Y30/00 , B33Y10/00 , B29C64/118 , B29C64/20 , B29C69/00 , B29C64/165 , B29C65/00 , D02G3/22 , B29C64/106 , B29C47/02 , B29C47/08 , B29C47/10 , B29K55/02 , B29K71/00 , B29K105/10 , B29L31/00
CPC classification number: B29C48/05 , B29C48/0022 , B29C48/154 , B29C48/266 , B29C48/2886 , B29C48/2888 , B29C64/106 , B29C64/118 , B29C64/165 , B29C64/20 , B29C66/69 , B29C69/001 , B29K2055/02 , B29K2071/00 , B29K2105/10 , B29L2031/707 , B33Y10/00 , B33Y30/00 , D02G3/22 , Y10T428/2929
Abstract: Components may be manufactured by co-extruding a polymer filament and a fiber filament from a nozzle. The polymer filament and the fiber filament may be heated within the nozzle, which may couple the polymer filament to the fiber filament. The co-extruded filament may result in long reinforcing fibers which provide strength to the components.
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公开(公告)号:US09823143B2
公开(公告)日:2017-11-21
申请号:US15026674
申请日:2014-09-24
Applicant: United Technologies Corporation
Inventor: Wendell V. Twelves, Jr. , Evan Butcher , Lexia Kironn , Gary A. Schirtzinger , Joe Ott
IPC: G01L1/22 , F16F1/02 , F16F7/12 , B22F3/105 , B22F7/06 , B33Y80/00 , B22F5/10 , B22F3/11 , B22F7/08 , B29C64/153 , B33Y10/00
CPC classification number: G01L1/22 , B22F3/1055 , B22F3/1118 , B22F5/10 , B22F7/06 , B22F7/08 , B22F2003/1056 , B29C64/153 , B29K2995/0089 , B33Y10/00 , B33Y80/00 , F16F1/025 , F16F7/12 , Y02P10/295
Abstract: A method includes designing a part. The part includes at least one internal structure. The internal structure is designed to provide strain mitigation, energy dissipation, or impact resistance for the part during an emergency condition. The part is built by a layer-by-layer additive manufacturing process. While building the part, the internal structure is connected to the part.
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