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公开(公告)号:US10400786B2
公开(公告)日:2019-09-03
申请号:US15344638
申请日:2016-11-07
Applicant: United Technologies Corporation
Inventor: Agnieszka M. Wusatowska-Sarnek , Sergei F. Burlatsky , David Ulrich Furrer , J. Michael McQuade
Abstract: A rotor for a turbomachine is provided which includes a hub; and a plurality of blades extending radially from the hub, the plurality of blades comprising a first subset of blades having first tips and an abrasive coating on the first tips, and a second subset of blades having second tips with no abrasive coating on the second tips, wherein a radius (R2) of the first subset of blades, including thickness of the abrasive coating, is greater than a radius (R1) of the second subset of blades, and wherein a base radius (R) of the first subset of blades, not including thickness of the abrasive coating, is less than the radius (R1) of the second subset of blades.
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42.
公开(公告)号:US10337121B2
公开(公告)日:2019-07-02
申请号:US15797855
申请日:2017-10-30
Applicant: United Technologies Corporation
Inventor: Joseph V. Mantese , Ryan C. Breneman , Thomas Anthony Rebbecchi , Andrew Boyne , John Joseph Marcin , Dustin W. Davis , David Ulrich Furrer , James Tilsley Auxier
Abstract: An induction furnace assembly comprising a chamber having a mold; a primary inductive coil coupled to the chamber; a susceptor surrounding the chamber between the primary inductive coil and the mold; and a shield material contained in a reservoir coupled to or proximate the mold between the susceptor and the mold; the shield material configured to attenuate a portion of an electromagnetic flux generated by the primary induction coil that is not attenuated by the susceptor.
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公开(公告)号:US10254730B2
公开(公告)日:2019-04-09
申请号:US15441620
申请日:2017-02-24
Applicant: United Technologies Corporation
Inventor: Sergei F. Burlatsky , Dmitri Novikov , William J. Brindley , David Ulrich Furrer
IPC: B33Y10/00 , B33Y30/00 , B33Y50/02 , G05B19/042 , G06F17/50 , B29C64/153 , B29C64/393 , B22F3/105
Abstract: A method of evaluating and validating additive manufacturing operations includes generating a multidimensional space defined by a plurality of bounds, each of the bounds being defined on a distinct parameter of an additive manufacturing process and each of the parameters being directly related to the occurrence of a horizontal lack of fusion flaw, each of the parameters being a dimension in a multi-dimensional coordinate system, determining a coordinate position of at least one additive manufacturing operation within the multi-dimensional coordinate system, and categorizing the operation as free of horizontal lack of fusion flaws when the coordinate position is within the multi-dimensional space.
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公开(公告)号:US10252510B2
公开(公告)日:2019-04-09
申请号:US15441649
申请日:2017-02-24
Applicant: United Technologies Corporation
Inventor: Sergei F. Burlatsky , Dmitri Novikov , William J. Brindley , David Ulrich Furrer
IPC: B33Y10/00 , B33Y30/00 , B33Y50/02 , B22F3/105 , G06F17/50 , B29C64/153 , B29C64/393 , B29K105/00
Abstract: A method of evaluating and validating additive manufacturing operations includes generating a multidimensional space defined by a plurality of bounds, each of the bounds being defined on a distinct parameter of an additive manufacturing process and each of the bounds being directly related to the occurrence of a downskin roughness flaw, each of the parameters being a dimension in a multi-dimensional coordinate system, determining a coordinate position of at least one additive manufacturing operation within the multi-dimensional coordinate system, and categorizing the operation as free of downskin roughness flaws when the coordinate position is within the multi-dimensional space.
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公开(公告)号:US10081082B2
公开(公告)日:2018-09-25
申请号:US14768633
申请日:2013-12-16
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: James O. Hansen , David Ulrich Furrer
CPC classification number: B23P15/04 , B21D53/78 , B21H7/00 , B21K3/04 , F01D5/288 , F04D29/324 , F05D2220/32 , F05D2230/20 , F05D2240/303
Abstract: A method for manufacturing a protective sheath for a fan blade leading edge is described. The method may comprise generating a preform plate from a stock plate wherein the preform plate has a flattened surface and an inclined surface having a spike flanked by a first side and a second side. The method may further comprise bending the first side and the second side away from the spike to generate a sheath intermediate followed by generating the protective sheath from the sheath intermediate by shaping an outer surface and an inner surface of the sheath intermediate to match the contour of the fan blade leading edge.
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公开(公告)号:US20180231014A1
公开(公告)日:2018-08-16
申请号:US15430783
申请日:2017-02-13
Applicant: United Technologies Corporation
Inventor: Pantcho P. Stoyanov , Agnieszka M. Wusatowska-Sarnek , Thomas D. Kasprow , David Ulrich Furrer , Sergei F. Burlatsky
CPC classification number: F04D29/164 , C23C4/12 , C23C24/04 , C23C28/022 , C23C28/027 , C23C28/324 , C23C28/3455 , C23C28/42 , F01D5/288 , F01D11/122 , F04D29/526 , F05D2230/31
Abstract: A multilayer abradable coating includes at least one first abradable layer; and at least one second abradable layer, wherein the first abradable layer and the second abradable layer have different properties related to erosion resistance.
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公开(公告)号:US20180171431A1
公开(公告)日:2018-06-21
申请号:US15890623
申请日:2018-02-07
Applicant: United Technologies Corporation
Inventor: Chris Vargas , Eric A. Hansen , Raymond C. Benn , Daniel A. Bales , Ivan M. Schmidt , David W. Anderson , David Ulrich Furrer , William F. Matzke
CPC classification number: C21D11/005 , C21D11/00 , C22F1/10
Abstract: A method of estimating an unknown solvus for a phase of a given alloy includes providing empirical data of a plurality of alloys from an alloy class, the empirical data at least including chemical compositions, heating rates, cooling rates and alloy solvus temperatures of the plurality of alloys, providing an alloy chemical composition, a selected heating rate and a selected cooling rate of another alloy from the alloy class that has an unknown solvus temperature, estimating the unknown solvus temperature based upon the empirical data to provide an estimated solvus temperature of the alloy, and establishing a solution heat treatment temperature corresponding to the estimated solvus temperature at which to treat a component that includes the alloy.
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公开(公告)号:US09884939B2
公开(公告)日:2018-02-06
申请号:US14921177
申请日:2015-10-23
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Dmitri Novikov , David Ulrich Furrer , Sergei F Burlatsky , Hillary Anne Huttenhower , Vadim Atrazhev , Vadim Sultanov , Dmitry Dmitriev , John D Riehl , Charles R Watson
CPC classification number: C08G73/1085 , C08J3/18 , C08J3/24 , C08J3/28 , C08J2379/08 , C08K3/01 , C08K3/013 , C08K5/0016 , C08L79/08
Abstract: A polymeric material process includes increasing a mobility within a polymer to enables specific alignment of polymer chains.
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公开(公告)号:US20170291370A1
公开(公告)日:2017-10-12
申请号:US15441683
申请日:2017-02-24
Applicant: United Technologies Corporation
Inventor: Sergei F. Burlatsky , Dmitri Novikov , William J. Brindley , David Ulrich Furrer
CPC classification number: B33Y50/00 , B22F3/1055 , B29C64/153 , B29C64/20 , B29C64/386 , B29C67/00 , B33Y30/00 , G06F17/5086 , G06F2217/12 , Y02P90/265
Abstract: A method of evaluating and validating additive manufacturing operations includes generating a multidimensional space defined by a plurality of bounds, each of the bounds being defined on a distinct parameter of an additive manufacturing process and each of the bounds being directly related to the occurrence of a vertical lack of fusion flaw, each of the parameters being a dimension in a multi-dimensional coordinate system, determining a coordinate position of at least one additive manufacturing operation within the multi-dimensional coordinate system, and categorizing the operation as free of vertical lack of fusion flaws when the coordinate position is within the multi-dimensional space.
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公开(公告)号:US20170291368A1
公开(公告)日:2017-10-12
申请号:US15441639
申请日:2017-02-24
Applicant: United Technologies Corporation
Inventor: Sergei F. Burlatsky , Dmitri Novikov , William J. Brindley , David Ulrich Furrer
CPC classification number: B33Y50/00 , B22F3/1055 , B22F2003/1057 , B22F2999/00 , B29C64/124 , B29C64/153 , B29C64/20 , B29C64/386 , B33Y10/00 , B33Y30/00 , B33Y50/02 , G06F17/5086 , G06F2217/12 , Y02P10/295 , Y02P90/265 , B22F2003/1056 , B22F2203/03
Abstract: A method of evaluating and validating additive manufacturing operations includes generating a multidimensional space defined by a plurality of bounds, each of the bounds being defined on a distinct parameter of an additive manufacturing process and each of the bounds being directly related to the occurrence of a balling flaw, each of the parameters being a dimension in a multi-dimensional coordinate system, determining a coordinate position of at least one additive manufacturing operation within the multi-dimensional coordinate system, and categorizing the operation as free of balling flaws when the coordinate position is within the multi-dimensional space.
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