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公开(公告)号：US20200024749A1
公开(公告)日：2020-01-23
申请号：US16397092
申请日：2019-04-29
Applicant: United Technologies Corporation
Inventor： Christopher W. Strock , Shahram Amini
IPC: C23C28/04 , C23C4/06 , F01D25/00 , F02C7/24 , F01D5/28 , C04B41/87 , C04B41/00 , C04B41/50 , C23C4/10
Abstract: A method of providing a self-healing coating includes providing substrate, applying a layer of an aluminum-containing MAX phase material and another material to the substrate. The method includes exposing the layer to a temperature greater than 2000° F. to form alpha aluminum.
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112.发明授权公开(公告)号：US10533439B2
公开(公告)日：2020-01-14
申请号：US14934458
申请日：2015-11-06
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Changsheng Guo , Christopher W. Strock
IPC: F01D9/04 , F01D11/00 , F16J15/3204 , C23C16/02 , F16J15/328 , C23C16/34 , C23C16/27 , C23C16/56 , C23C28/04 , B23H1/10 , C25D11/04
Abstract: A component for a gas turbine engine is described. The component may comprise a body portion formed from a metallic material. The component may further comprise an abrasive surface forming at least one surface of the body portion, and the abrasive surface may be configured to abrade an abradable material. The abrasive surface may be formed from electrical discharge machining of the metallic material.
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公开(公告)号：US10513942B2
公开(公告)日：2019-12-24
申请号：US15037127
申请日：2014-11-04
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Christopher W. Strock , Enzo DiBenedetto
Abstract: A seal comprises a housing. A coating has at least two layers with a bond layer to be positioned between a housing and a second hard layer. The second hard layer is formed to be harder than the bond layer. The bond layer has a bond strength greater than or equal to 200 psi and less than or equal to 2000 psi. A gas turbine engine, and a method of forming a coating layer are also disclosed.
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公开(公告)号：US20190383164A1
公开(公告)日：2019-12-19
申请号：US16237065
申请日：2018-12-31
Applicant: United Technologies Corporation
Inventor： Shahram Amini , Christopher W. Strock , Sergei F. Burlatsky , Dmitri Novikov
Abstract: A vibration resistant fan guide vane for a gas turbine engine is provided. The fan guide vane comprises a vibration damping component made of a MAXMET composite. The damping component may be a cover that covers some or all of the fan guide vane body. Alternatively, portions of the fan guide vane body or the entire vane body may be made from MAXMET composites. The disclosure makes use of the ultrahigh, fully reversible, non-linear elastic hysteresis behavior that MAXMET composites exhibit during cyclic elastic deformation in order to damp vibration.
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公开(公告)号：US10480330B2
公开(公告)日：2019-11-19
申请号：US16407332
申请日：2019-05-09
Applicant: United Technologies Corporation
Inventor： Christopher W. Strock , Changsheng Guo
Abstract: A rub material (124) comprises a polymeric matrix (128) and polymeric micro-balloons (130) in the matrix.
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Patent Agency Ranking
公开(公告)号：US20190323365A1
公开(公告)日：2019-10-24
申请号：US16456569
申请日：2019-06-28
Applicant: United Technologies Corporation
Inventor： Christopher W. Strock , Paul M. Lutjen
IPC: F01D5/28 , F01D9/04 , F01D11/12 , F01D25/08 , B32B9/04 , B32B3/12 , C23C4/12 , F01D11/08 , B32B9/00 , B32B7/12 , B32B37/12
Abstract: A thermal barrier system includes a protective coating on a substrate, and a ceramic feature layer attached to the protective coating via an adhesive spray coat.
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公开(公告)号：US10406555B2
公开(公告)日：2019-09-10
申请号：US15889756
申请日：2018-02-06
Applicant: United Technologies Corporation
Inventor： Christopher W. Strock , Charles R. Beaudoin , Robert D. Richard , Steven G. Lemay
Abstract: A mask for masking a component at an annular boundary comprises a wall (90, 92) having an inner first rim portion having a first inner diameter (D1) and an outward rebate (140) adjacent the first rim portion.
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公开(公告)号：US20190195075A1
公开(公告)日：2019-06-27
申请号：US16287036
申请日：2019-02-27
Applicant: United Technologies Corporation
Inventor： Christopher W. Strock , Russell A. Beers
CPC classification number: F01D5/20 , F01D5/284 , F01D5/288 , F01D11/122 , F02C3/10 , F02K3/06 , F04D29/324 , F05D2230/31 , F05D2230/90 , F05D2240/307 , F05D2300/121 , F05D2300/173 , F05D2300/2112 , Y02T50/672
Abstract: A friction interface in a gas turbine engine includes an abradable component, such as a seal, and an abrasive component, such as a blade tip, in rubbing contact with each other. The abradable component is composed of a polymer matrix composite and the abrasive component is composed of a metal matrix with hard particles dispersed through the metal matrix. The metal matrix is an aluminum alloy and the hard particles are selected from oxides, nitrides, carbides, oxycarbides, oxynitrides, diamond and combinations thereof.
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公开(公告)号：US20190186281A1
公开(公告)日：2019-06-20
申请号：US15848729
申请日：2017-12-20
Applicant: United Technologies Corporation
Inventor： Pantcho Stoyanov , Christopher W. Strock , Kevin Seymour
CPC classification number: F01D11/122 , F01D25/005 , F05D2220/32 , F05D2230/237 , F05D2230/312 , F05D2230/40 , F05D2230/42 , F05D2230/60 , F05D2240/55 , F05D2300/173 , F05D2300/177 , F05D2300/48 , F05D2300/509 , F05D2300/603
Abstract: An air seal in a gas turbine engine includes a substrate. A bond coating layer is adhered to the substrate. An abradable layer is adhered to the bond coating layer. The abradable layer comprises a metal matrix discontinuously filled with a lubricious oxide solid lubricant filler.
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公开(公告)号：US20190143404A1
公开(公告)日：2019-05-16
申请号：US16245748
申请日：2019-01-11
Applicant: United Technologies Corporation
Inventor： Christopher W. Strock
Abstract: A method for manufacturing a powder comprises vaporizing a solvent; passing a metallic powder and a polymer powder through the solvent vapor to mix the metallic powder with the polymer powder; and removing the solvent.
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