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公开(公告)号：US20170030214A1
公开(公告)日：2017-02-02
申请号：US15113566
申请日：2015-01-22
IPC分类号： F01D11/08
CPC分类号： F01D11/08 , F01D11/005 , F02C7/28 , F05D2220/32 , F05D2230/236 , F05D2240/11 , F05D2250/75 , F05D2300/6032
摘要： A turbine engine system comprising a turbine engine air seal having at least one contact portion. The turbine engine air seal having a MAXMET composite bonded to at least one contact portion.
摘要翻译： 一种涡轮发动机系统，包括具有至少一个接触部分的涡轮发动机空气密封。 涡轮发动机空气密封件具有与至少一个接触部分接合的MAXMET复合材料。
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公开(公告)号：US20170343003A1
公开(公告)日：2017-11-30
申请号：US15162699
申请日：2016-05-24
CPC分类号： F04D29/164 , F01D5/288 , F01D11/122 , F04D29/023 , F04D29/324 , F04D29/526 , F04D29/542 , F05D2300/609 , Y02T50/672
摘要： An abrasive coating comprising a plurality of first grit particles placed on a top surface of a substrate and spaced to provide channels for the removal of cut chips and rub debris and heat reduction. A plurality of second grit particles are placed between each of the first grit particles, and having a nominal size smaller than the first grit particles. A mixture of the second grit particles to the first grit particles comprises from about 75-98%. The second grit particles form a single layer or multiple layers and comprise height of 10 to 60% of that of the first grit particles. A matrix material is bonded to the top surface; the matrix material envelops the second grit particles and bonds to and partially surrounds the first grit particles. The first grit particles extend above the matrix material and the second grit particles relative to the top surface.
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公开(公告)号：US10794210B2
公开(公告)日：2020-10-06
申请号：US14732905
申请日：2015-06-08
摘要： A stiffness controlled abradable seal system for a gas turbine engine includes a cantilevered arm that supports one of a rotating seal surface and a static seal surface, a stiffness of the cantilevered arm controlled to achieve a desired operational temperature at a seal interface, and an optimally matched abradeable seal material with required thermo-physical and friction properties to enable desired wear mechanisms and maximized sealing and durability.
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4.发明授权公开(公告)号：US09957826B2
公开(公告)日：2018-05-01
申请号：US14731743
申请日：2015-06-05
CPC分类号： F01D11/001 , C04B35/5607 , C04B35/5611 , C04B35/5618 , C04B35/5622 , C04B35/58 , C04B35/58007 , C04B35/58014 , C04B35/58021 , C04B35/58028 , C04B2235/5212 , C10M109/00 , F01D11/122 , F05D2240/55 , F05D2300/226 , F05D2300/228 , F05D2300/509 , Y02T50/672
摘要： A stiffness controlled abradeable seal system for a gas turbine engine includes a cantilevered arm that supports one of a rotating seal surface and a static seal surface, a stiffness of the cantilevered arm controlled to achieve a desired operational temperature at a seal interface.
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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
发明人： Dmitri Novikov , David Ulrich Furrer , Sergei F Burlatsky , Hillary Anne Huttenhower , Vadim Atrazhev , Vadim Sultanov , Dmitry Dmitriev , John D Riehl , Charles R Watson
CPC分类号： C08G73/1085 , C08J3/18 , C08J3/24 , C08J3/28 , C08J2379/08 , C08K3/01 , C08K3/013 , C08K5/0016 , C08L79/08
摘要： A polymeric material process includes increasing a mobility within a polymer to enables specific alignment of polymer chains.
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6.发明申请公开(公告)号：US20160160673A1
公开(公告)日：2016-06-09
申请号：US14732905
申请日：2015-06-08
CPC分类号： F01D11/122 , F01D11/003 , F05D2240/307 , F05D2240/55 , F05D2300/226 , F05D2300/228 , F05D2300/50 , F05D2300/509 , Y02T50/672
摘要： A stiffness controlled abradable seal system for a gas turbine engine includes a cantilevered arm that supports one of a rotating seal surface and a static seal surface, a stiffness of the cantilevered arm controlled to achieve a desired operational temperature at a seal interface, and an optimally matched abradeable seal material with required thermo-physical and friction properties to enable desired wear mechanisms and maximized sealing and durability.
摘要翻译： 用于燃气涡轮发动机的刚性控制的可磨损密封系统包括支撑旋转密封表面和静态密封表面中的一个的悬臂，控制悬臂的刚度以在密封界面处实现期望的操作温度，并且最佳地 匹配的可磨损密封材料具有所需的热物理和摩擦性能，以实现所需的磨损机制，并实现最大的密封和耐用性。
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公开(公告)号：US20160024955A1
公开(公告)日：2016-01-28
申请号：US14775927
申请日：2013-12-16
发明人： Shahram Amini , Christopher W Strock , Sergei F Burlatsky , Dmitri Novikov , David Ulrich Fuller
IPC分类号： F01D11/12 , F01D9/04 , B23K1/00 , B23K1/19 , C23C24/04 , B23K20/22 , B23K26/34 , B23K26/00 , C23C4/12 , F01D5/28 , B23K20/02
CPC分类号： F01D11/122 , B23K1/0006 , B23K1/19 , B23K20/02 , B23K20/22 , B23K26/0006 , B23K26/34 , B23K2103/16 , C23C4/04 , C23C4/134 , 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
摘要： 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.
摘要翻译： 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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