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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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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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