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公开(公告)号：US10718519B2
公开(公告)日：2020-07-21
申请号：US15893324
申请日：2018-02-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Steven D Porter , James Tilsley Auxier
Abstract: A heat shield panel for use in a gas turbine engine combustor is disclosed. The heat shield panel includes a hot side, a cold side and at least one attachment mechanism having a stud and a central axis extending through the stud and a plurality of standoff pins positioned circumferentially around the stud, the standoff pins having a radial extent, a circumferential extent that is greater than the radial extent, a radially outer surface having a radially convex shape and a radially inner surface having a radially concave shape.
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公开(公告)号：US20200217208A1
公开(公告)日：2020-07-09
申请号：US16239949
申请日：2019-01-04
Applicant: United Technologies Corporation
Inventor： James Tilsley Auxier , Jeffrey T. Morton , Matthew S. Gleiner , Parth Jariwala , Charles Thistle , Megan J. Kwolek
Abstract: A component for a gas turbine engine includes a body portion that extends between a leading edge and a trailing edge of the component. The trailing edge includes a flared region and a non-flared region. At least one discharge slot is disposed at least partially within the flared region of the component.
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公开(公告)号：US20190249873A1
公开(公告)日：2019-08-15
申请号：US15893324
申请日：2018-02-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Steven D. Porter , James Tilsley Auxier
CPC classification number: F23R3/002 , F05D2260/231 , F23R3/06 , F23R3/50 , F23R3/60 , F23R2900/00005 , F23R2900/00017 , F23R2900/03041 , F23R2900/03044 , F23R2900/03045
Abstract: A heat shield panel for use in a gas turbine engine combustor is disclosed. The heat shield panel includes a hot side, a cold side and at least one attachment mechanism having a stud and a central axis extending through the stud and a plurality of standoff pins positioned circumferentially around the stud, the standoff pins having a radial extent, a circumferential extent that is greater than the radial extent, a radially outer surface having a radially convex shape and a radially inner surface having a radially concave shape.
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公开(公告)号：US20190247914A1
公开(公告)日：2019-08-15
申请号：US15897312
申请日：2018-02-15
Applicant: United Technologies Corporation
Inventor： James Tilsley Auxier
CPC classification number: B22C9/10 , B22C3/00 , B22C9/103 , B22C9/12 , B22C9/22 , B22F5/007 , B22F7/08
Abstract: A refractory metal core laminate assembly, comprising: a first refractory metal core layer having exterior surfaces and a first side and a second side opposite the first side; a second refractory metal core layer having exterior surfaces and a first side and a second side opposite the first side, the second refractory metal core layer being arranged above the first refractory metal core layer with the second refractory metal core layer first side facing the first refractory metal core layer second side; a layer of a powder bed material between the first refractory metal core layer second side and the second refractory metal core layer first side; and a coating of the powder bed material coupled to the first refractory metal core layer exterior surfaces and the second refractory metal core layer exterior surfaces.
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35.发明申请公开(公告)号：US20190127882A1
公开(公告)日：2019-05-02
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
CPC classification number: C30B30/04 , B22D27/02 , B22D27/045 , C30B21/02 , F27B14/061 , F27B14/14 , F27D11/06 , F27D2099/0015 , H05B6/067 , H05B6/105
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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Patent Agency Ranking
36.发明申请公开(公告)号：US20190127878A1
公开(公告)日：2019-05-02
申请号：US15797888
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 layered susceptor comprising at least two layers of magnetic field attenuating material surrounding the chamber between the primary inductive coil and the mold to nullify the electromagnetic field in the hot zone of the furnace chamber.
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37.发明申请公开(公告)号：US20190127877A1
公开(公告)日：2019-05-02
申请号：US15797799
申请日：2017-10-30
Applicant: United Technologies Corporation
Inventor： Joseph V. Mantese , Thomas Anthony Rebbecchi , Ryan C. Breneman , Andrew Boyne , John Joseph Marcin , Dustin W. Davis , David Ulrich Furrer , James Tilsley Auxier
Abstract: A process for directional solidification of a cast part comprises energizing a primary inductive coil coupled to a chamber having a mold containing a material; energizing a primary inductive coil within the chamber to heat the mold via radiation from a susceptor, wherein the resultant electromagnetic field partially leaks through the susceptor coupled to the chamber between the primary inductive coil and the mold; determining a magnetic flux profile of the electromagnetic field; sensing a magnetic flux leakage past the susceptor within the chamber; generating a control field from a secondary compensation coil coupled to the chamber, wherein the control field controls the magnetic flux experienced by the cast part; and casting the material within the mold under the controlled degree of flux leakage.
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公开(公告)号：US10226812B2
公开(公告)日：2019-03-12
申请号：US14976333
申请日：2015-12-21
Applicant: United Technologies Corporation
Inventor： James Tilsley Auxier , Thomas N Slavens
IPC: B22C9/10 , B33Y10/00 , B33Y80/00 , B22C9/24 , B22F3/105 , B22F5/00 , B22F7/02 , B22D23/06 , B22D27/04 , C30B1/02 , B22F7/08 , B28B1/00 , B28B7/34
Abstract: A core for use in casting an internal cooling circuit within a gas turbine engine component includes an additively manufactured skeleton core portion manufactured of a refractory metal, a surround core portion that at least partially encapsulates the additively manufactured skeleton core portion, the surround core portion manufactured of a ceramic material, a surround core portion that at least partially encapsulates the additively manufactured skeleton core portion, the surround core portion manufactured of a ceramic material and a cooling hole shape that extends from the additively manufactured skeleton core portion through the surround core portion, the cooling hole shape operable to form a cooling hole.
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39.发明申请RADIOPAQUE PROTECTIVE FILL FOR MANUFACTURE, REPAIR, OR REMANUFACTURE OF COOLED COMPONENTS 审中-公开冷却组件的制造，维修或还原的放射性保护膜公开(公告)号：US20170038312A1
公开(公告)日：2017-02-09
申请号：US14817422
申请日：2015-08-04
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： James Tilsley Auxier , Lea Kennard Castle
CPC classification number: G01N23/00 , B22C1/02 , B22C9/10 , B22C9/103 , B22C9/105 , B22C9/24 , B22D29/001 , B22D29/005 , B22D46/00 , B23K26/18 , B23K26/389 , B23K35/3033 , B23K2101/001 , C22C19/00 , F01D5/005 , F05D2230/211 , F05D2300/50 , F05D2300/603 , G01M15/14
Abstract: A method of manufacturing a core for casting a component can include manufacturing a core for at least partially forming an internal passage architecture of a component with a material including radiopaque particles. A method can include removing a material including radio opaque particles from an internal passage architecture of a component; and inspecting the component via radiographic imaging at gamma/X-ray wavelengths to detect residual material. A core for use in casting an internal passage architecture of a component can include a material with radiopaque particles dispersed therein.
Abstract translation: 制造用于铸造部件的芯的方法可以包括制造用于至少部分地形成具有包括不透射线的颗粒的材料的部件的内部通道结构的芯。 一种方法可以包括从组件的内部通道结构去除包括不透射线的颗粒的材料; 并通过伽马/ X射线波长的射线成像检查部件以检测残留物质。 用于铸造部件的内部通道结构的芯可以包括具有分散在其中的不透射线颗粒的材料。
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公开(公告)号：US10760179B2
公开(公告)日：2020-09-01
申请号：US15797799
申请日：2017-10-30
Applicant: United Technologies Corporation
Inventor： Joseph V. Mantese , Thomas Anthony Rebbecchi , Ryan C. Breneman , Andrew Boyne , John Joseph Marcin , Dustin W. Davis , David Ulrich Furrer , James Tilsley Auxier
IPC: B22D27/02 , B22D27/04 , C30B11/00 , H05B6/08 , H05B6/44 , F27D21/00 , H05B6/36 , F27B14/14 , F27B14/06
Abstract: A process for directional solidification of a cast part comprises energizing a primary inductive coil coupled to a chamber having a mold containing a material; energizing a primary inductive coil within the chamber to heat the mold via radiation from a susceptor, wherein the resultant electromagnetic field partially leaks through the susceptor coupled to the chamber between the primary inductive coil and the mold; determining a magnetic flux profile of the electromagnetic field; sensing a magnetic flux leakage past the susceptor within the chamber; generating a control field from a secondary compensation coil coupled to the chamber, wherein the control field controls the magnetic flux experienced by the cast part; and casting the material within the mold under the controlled degree of flux leakage.
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