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公开(公告)号：WO2015102690A3
公开(公告)日：2015-09-11
申请号：PCT/US2014057972
申请日：2014-09-29
Applicant: UNITED TECHNOLOGIES CORP
Inventor： AMINI SHAHRAM , SCHMIDT WAYDE R , KASHYAP TANIA BHATIA , HERMANN MARK A , SHEEDY PAUL , LIMARGA ANDI M , MCCAFFREY MICHAEL G
IPC: C04B35/64 , C04B35/645
CPC classification number: B28B1/24 , B28B1/52 , B28B11/243 , C04B35/524 , C04B35/532 , C04B35/806 , C04B38/0022 , C04B2235/48 , C04B2235/5252 , C04B2235/602 , C04B2235/616
Abstract: A disclosed method of forming a ceramic article includes forming a pre-ceramic polymer article within a mold tool, and performing a first pyrolizing step on the initial pre-ceramic polymer article to form a ceramic article. The method further includes performing at least one pre-heat treatment polymer infiltration and pyrolizing (PIP) cycle on the ceramic article and an initial heat treatment cycle of the ceramic article after the at least one pre-heat treatment PIP cycle. Subsequent PIP cycles and heat treatment cycles are performed in combination to form a ceramic article including a desired density.
Abstract translation: 公开的形成陶瓷制品的方法包括在模具内形成预陶瓷聚合物制品，并且在初始陶瓷前体聚合物制品上进行第一热解步骤以形成陶瓷制品。 该方法还包括在陶瓷制品上进行至少一个预热处理聚合物渗透和热解（PIP）循环以及在至少一个预热处理PIP循环之后的陶瓷制品的初始热处理循环。 随后的PIP循环和热处理循环联合进行以形成包括期望密度的陶瓷制品。
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公开(公告)号：WO2014149097A3
公开(公告)日：2014-11-13
申请号：PCT/US2013075292
申请日：2013-12-16
Applicant: UNITED TECHNOLOGIES CORP
Inventor： AMINI SHAHRAM , STROCK CHRISTOPHER W , BURLATSKY SERGEI F , NOVIKOV DMITRI , FURRER DAVID ULRICH
CPC classification number: F01D11/122 , B23K1/0006 , B23K1/19 , B23K20/02 , B23K20/22 , B23K26/0006 , B23K26/34 , B23K2203/16 , C23C4/04 , C23C24/04 , F01D5/288 , F01D9/041 , F01D11/12 , F01D11/20 , F05D2220/30 , F05D2230/236 , F05D2230/237 , F05D2230/312 , F05D2230/60 , F05D2230/90 , F05D2240/125 , F05D2240/307 , F05D2300/6032
Abstract: A turbine engine system includes a turbine engine component having an airfoil portion and a tip, which turbine engine component having a MAXMET composite bonded to the tip. The MAXMET composite has MAX phases in a metal matrix.
Abstract translation: 涡轮发动机系统包括具有翼型部分和尖端的涡轮发动机部件，该涡轮发动机部件具有结合到尖端的MAXMET复合材料。 MAXMET复合材料在金属基体中具有MAX相位。
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Patent Agency Ranking
公开(公告)号：EP2971560A4
公开(公告)日：2016-06-22
申请号：EP13878721
申请日：2013-12-16
Applicant: UNITED TECHNOLOGIES CORP
Inventor： AMINI SHAHRAM , STROCK CHRISTOPHER W , BURLATSKY SERGEI F , NOVIKOV DMITRI , FURRER DAVID ULRICH
IPC: F01D5/28 , B23K1/00 , B23K1/19 , B23K20/02 , B23K20/22 , B23K26/00 , B23K26/34 , B23K103/16 , C04B35/56 , C04B35/58 , C04B41/51 , C23C24/04 , F01D5/14 , F01D9/04 , F01D11/12 , F01D11/20 , F02C7/30
CPC classification number: F01D11/122 , B23K1/0006 , B23K1/19 , B23K20/02 , B23K20/22 , B23K26/0006 , B23K26/34 , B23K2203/16 , C23C4/04 , C23C24/04 , F01D5/288 , F01D9/041 , F01D11/12 , F01D11/20 , F05D2220/30 , F05D2230/236 , F05D2230/237 , F05D2230/312 , F05D2230/60 , F05D2230/90 , F05D2240/125 , F05D2240/307 , F05D2300/6032
Abstract: A turbine engine system includes a turbine engine component having an airfoil portion and a tip, which turbine engine component having a MAXMET composite bonded to the tip. The MAXMET composite has MAX phases in a metal matrix.
Abstract translation: 涡轮发动机系统包括具有翼型部分和尖端的涡轮发动机部件，该涡轮发动机部件具有结合到尖端的MAXMET复合材料。 MAXMET复合材料在金属基体中具有MAX相。
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4.发明公开GAS TURBINE ENGINE COMPONENT COATING WITH SELF-HEALING BARRIER LAYER 审中-公开GASTURBINENMOTORKOMPONENTENBESCHICHTUNG MIT SELBSTHEILENDER SPERRSCHICHT
公开(公告)号：EP3074619A4
公开(公告)日：2017-04-26
申请号：EP14865602
申请日：2014-11-05
Applicant: UNITED TECHNOLOGIES CORP
Inventor： STROCK CHRISTOPHER W , AMINI SHAHRAM
CPC classification number: C23C28/042 , C23C4/06 , C23C4/10 , F01D5/288 , F01D25/00 , F02C7/24 , F05D2300/182 , F05D2300/2261 , F05D2300/2283
Abstract: A component for high temperature applications includes a substrate and a layer of an aluminum-containing MAX phase material and another material applied to the substrate.
Abstract translation: 用于高温应用的部件包括衬底和含铝的MAX相材料层以及施加到衬底的另一种材料。
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公开(公告)号：EP2971536A4
公开(公告)日：2016-11-02
申请号：EP13878288
申请日：2013-12-16
Applicant: UNITED TECHNOLOGIES CORP
Inventor： AMINI SHAHRAM , STROCK CHRISTOPHER W , BURLATSKY SERGEI F , NOVIKOV DSMITRI
CPC classification number: F01D25/04 , F01D5/16 , F01D5/282 , F01D5/288 , F01D9/02 , F01D25/005 , F05D2300/6032 , Y02T50/672 , Y10T156/10
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.
Abstract translation: 提供了一种用于燃气轮机的防振风扇导叶。 风扇导叶包括由MAXMET复合材料制成的减震部件。 阻尼部件可以是覆盖风扇导叶体的一些或全部的盖。 或者，风扇引导叶片体或整个叶片体的部分可以由MAXMET复合材料制成。 本公开使用MAXMET复合材料在循环弹性变形期间展示的超高度，完全可逆的非线性弹性滞后行为，以便阻尼振动。
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6.发明公开CERAMIC ARTICLE AND METHOD THEREFOR USING PARTICLE INFILTRATION AND PRECERAMIC POLYMER INFILTRATION 审中-公开KERAMIKARTIKEL UND VERFAHRENDAFÜRMIT PARTIKELINFILTRATION UND INFILTRATIONPRÄKERAMISCHERPOLYMERE
公开(公告)号：EP3063104A4
公开(公告)日：2017-07-19
申请号：EP14858836
申请日：2014-10-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor： AMINI SHAHRAM , TANG XIA , SCHMIDT WAYDE R , KASHYAP TANIA BHATIA
IPC: C04B35/14 , C04B35/571 , C04B35/622 , C04B35/64 , C04B35/80
CPC classification number: C04B35/806 , C04B35/571 , C04B35/64 , C04B41/52 , C04B2235/32 , C04B2235/3804 , C04B2235/3817 , C04B2235/3826 , C04B2235/3852 , C04B2235/3891 , C04B2235/422 , C04B2235/483 , C04B2235/5208 , C04B2235/5244 , C04B2235/5248 , C04B2235/616
Abstract: A method of fabricating a ceramic article includes providing a porous body that includes a plurality of fiber bundles that has an intra-bundle porosity and an inter-bundle porosity, infiltrating the intra-bundle porosity and the inter-bundle porosity with a mixture of particles in a liquid carrier, the particles having an average size selected with respect to at least the intra-bundle porosity, removing the liquid carrier from the porous body to deposit the particles in the intra-bundle porosity and in the inter-bundle porosity, infiltrating a preceramic polymer into a remaining intra-bundle porosity and a remaining inter-bundle porosity, and thermally converting the preceramic polymer to a ceramic material.
Abstract translation: 一种制造陶瓷制品的方法包括提供多孔体，所述多孔体包括具有束内孔隙率和束间孔隙率的多个束束，所述束束内孔隙率和束间孔隙率用颗粒的混合物渗透 在液体载体中，所述颗粒具有相对于至少所述束内孔隙度选择的平均尺寸，从所述多孔体去除所述液体载体以将所述颗粒沉积在所述束内孔隙度和所述束间孔隙度中，渗透 预陶瓷聚合物分成剩余的束内孔隙和剩余的束间孔隙，并且将陶瓷前驱体聚合物热转化为陶瓷材料。
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7.发明公开PROCESSING METHOD FOR PIP DERIVED CMC ARTICLE 审中-公开VERARBEITUNGSVERFAHRENFÜREINEN AUS PIP GEWONNENEN CMC-ARTIKEL
公开(公告)号：EP3055273A4
公开(公告)日：2017-06-28
申请号：EP14876992
申请日：2014-09-29
Applicant: UNITED TECHNOLOGIES CORP
Inventor： AMINI SHAHRAM , SCHMIDT WAYDE R , KASHYAP TANIA BHATIA , HERMANN MARK A , SHEEDY PAUL , LIMARGA ANDI M , MCCAFFREY MICHAEL G
IPC: C04B35/64 , C04B35/645
CPC classification number: B28B1/24 , B28B1/52 , B28B11/243 , C04B35/524 , C04B35/532 , C04B35/806 , C04B38/0022 , C04B2235/48 , C04B2235/5252 , C04B2235/602 , C04B2235/616
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