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公开(公告)号：CN104024616A
公开(公告)日：2014-09-03
申请号：CN201280065072.3
申请日：2012-10-31
Applicant: 费德罗-莫格尔公司
Inventor： 沃伦·博伊德·林顿
CPC classification number: F02F3/14 , B05D5/00 , C25D7/00 , F02B23/0603 , F02B2023/0612 , F02F3/12 , F05C2201/0403 , F05C2201/0418 , F05C2201/0421 , F05C2201/0424 , F05C2201/0427 , Y02T10/125
Abstract: 本发明提供一种用于柴油内燃机的活塞，该活塞包括一冠部，该冠部至少部分由钢形成并具有一燃烧表面，该燃烧表面带有一形成于其中的燃烧碗。该燃烧碗具有一燃烧碗边缘区域，并且一包括贵金属和难熔金属中的至少一种的涂层基本上仅涂覆于该燃烧碗边缘区域。在发动机运行过程中，当活塞处于上死点位置时，该涂层优选涂覆于燃烧碗边缘区域的与柴油燃料喷雾区域匹配的区域。
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公开(公告)号：CN1235658A
公开(公告)日：1999-11-17
申请号：CN97199375.0
申请日：1997-10-01
Applicant: 威斯顿布里奇国际有限公司
CPC classification number: F16K99/0001 , F04B43/043 , F04B53/1067 , F05C2201/0403 , F05C2201/0418 , F05C2201/046 , F15C5/00 , F16K99/0009 , F16K99/0015 , F16K99/0034 , F16K99/0057 , F16K2099/0074 , F16K2099/008 , F16K2099/0086 , F16K2099/0094 , Y10T137/0491 , Y10T137/7895
Abstract: 本发明涉及一种微加工流体装置(10),包括一个带有流动管(14)的基体(12)和一个可延展薄层(18),如泵送膜或形成止回阀的膜。薄层(18)是一个轧制金属片,最好由钛制成,并在流动管的覆盖区(20)通过阳极焊接与基体(12)连接。本发明用于制造止回阀。
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公开(公告)号：CN1134596C
公开(公告)日：2004-01-14
申请号：CN97199375.0
申请日：1997-10-01
Applicant: 威斯顿布里奇国际有限公司
CPC classification number: F16K99/0001 , F04B43/043 , F04B53/1067 , F05C2201/0403 , F05C2201/0418 , F05C2201/046 , F15C5/00 , F16K99/0009 , F16K99/0015 , F16K99/0034 , F16K99/0057 , F16K2099/0074 , F16K2099/008 , F16K2099/0086 , F16K2099/0094 , Y10T137/0491 , Y10T137/7895
Abstract: 本发明涉及一种微加工流体装置(10)，包括一个带有流动管(14)的基体(12)和一个可延展薄层(18)，如泵送膜或形成止回阀的膜。薄层(18)是一个轧制金属片，最好由钛制成，并在流动管的覆盖区(20)通过阳极焊接与基体(12)连接。本发明用于制造止回阀。
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4.发明申请Method of applying a metallic heat rejection coating onto a gas turbine engine component 失效将金属排斥涂层施加到燃气涡轮发动机部件上的方法公开(公告)号：US20030198750A1
公开(公告)日：2003-10-23
申请号：US10131518
申请日：2002-04-23
Inventor： Andrew Jay Skoog , Jane Ann Murphy , John Frederick Ackerman , Paul Vincent Arszman , Bryan Thomas Bojanowski , Timothy Ray Lattire
IPC: B05D003/02 , B05D001/36 , B05D001/02
CPC classification number: C23C4/18 , C23C4/02 , C23C24/04 , C23C24/08 , C23C28/042 , C23C30/00 , F05C2201/0418 , Y02T50/67
Abstract: A heat-rejection coating is applied to a metallic component of a gas turbine engine, preferably made of a nickel-base superalloy. A component surface is preferably pre-treated, as by polishing the component surface, thereafter pre-oxidizing the component surface, and thereafter applying a ceramic barrier coating onto the component surface. A reflective-coating mixture is air sprayed onto the pre-treated component surface. The reflective-coating mixture includes a metallic pigment, such as platinum, gold, palladium, and alloys thereof, and a reflective-coating-mixture carrier. The component with the reflective-coating mixture sprayed thereon is fired.
Abstract translation: 排气涂层被施加到优选由镍基超级合金制成的燃气涡轮发动机的金属部件上。 组分表面优选通过抛光组分表面进行预处理，然后预先氧化组分表面，然后在组件表面上施加陶瓷阻挡涂层。 反射涂层混合物被空气喷涂到预处理的组件表面上。 反射涂层混合物包括金属颜料，例如铂，金，钯及其合金，以及反射涂层混合物载体。 将其上喷射有反射涂层混合物的组分烧制。
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公开(公告)号：US08863720B2
公开(公告)日：2014-10-21
申请号：US13664778
申请日：2012-10-31
Applicant: Federal-Mogul Corporation
Inventor： Warran Boyd Lineton
CPC classification number: F02F3/14 , B05D5/00 , C25D7/00 , F02B23/0603 , F02B2023/0612 , F02F3/12 , F05C2201/0403 , F05C2201/0418 , F05C2201/0421 , F05C2201/0424 , F05C2201/0427 , Y02T10/125
Abstract: A piston for a diesel internal combustion engine including a crown portion at least partially formed of steel and having a combustion surface with a combustion bowl formed therein is provided. The combustion bowl presents a combustion bowl rim area, and a coating including at least one of a noble metal and a refractory metal is applied to substantially only the combustion bowl rim area. The coating is preferably applied in the areas of the combustion bowl rim area that are in line with the sprays of diesel fuel when the piston is in a top dead center position during operation of the engine.
Abstract translation: 一种柴油机内燃机的活塞，其特征在于，具备至少部分由钢制成的具有形成有燃烧碗的燃烧面的冠部的冠部。 燃烧碗具有燃烧碗边缘区域，并且包括贵金属和难熔金属中的至少一种的涂层仅基本上施加于燃烧碗边缘区域。 当在发动机操作期间活塞处于上止点位置时，该涂层优选地应用于燃烧碗边缘区域与柴油燃料喷雾一致的区域中。
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Patent Agency Ranking
6.发明授权Method of applying a metallic heat rejection coating onto a gas turbine engine component 失效将金属排斥涂层施加到燃气涡轮发动机部件上的方法公开(公告)号：US06720034B2
公开(公告)日：2004-04-13
申请号：US10131518
申请日：2002-04-23
Applicant: Andrew Jay Skoog , Jane Ann Murphy , John Frederick Ackerman , Paul Vincent Arszman , Bryan Thomas Bojanowski , Timothy Ray Lattire
Inventor： Andrew Jay Skoog , Jane Ann Murphy , John Frederick Ackerman , Paul Vincent Arszman , Bryan Thomas Bojanowski , Timothy Ray Lattire
IPC: B05D136
CPC classification number: C23C4/18 , C23C4/02 , C23C24/04 , C23C24/08 , C23C28/042 , C23C30/00 , F05C2201/0418 , Y02T50/67
Abstract: A heat-rejection coating is applied to a metallic component of a gas turbine engine, preferably made of a nickel-base superalloy. A component surface is preferably pre-treated, as by polishing the component surface, thereafter pre-oxidizing the component surface, and thereafter applying a ceramic barrier coating onto the component surface. A reflective-coating mixture is air sprayed onto the pre-treated component surface. The reflective-coating mixture includes a metallic pigment, such as platinum, gold, palladium, and alloys thereof, and a reflective-coating-mixture carrier. The component with the reflective-coating mixture sprayed thereon is fired.
Abstract translation: 排气涂层被施加到优选由镍基超级合金制成的燃气涡轮发动机的金属部件上。 组分表面优选通过抛光组分表面进行预处理，然后预先氧化组分表面，然后在组件表面上施加陶瓷阻挡涂层。 反射涂层混合物被空气喷涂到预处理的组件表面上。 反射涂层混合物包括金属颜料，例如铂，金，钯及其合金，以及反射涂层混合物载体。 将其上喷射有反射涂层混合物的组分烧制。
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公开(公告)号：US20130118438A1
公开(公告)日：2013-05-16
申请号：US13664778
申请日：2012-10-31
Applicant: Federal-Mogul Corporation
Inventor： Warran Boyd Lineton
CPC classification number: F02F3/14 , B05D5/00 , C25D7/00 , F02B23/0603 , F02B2023/0612 , F02F3/12 , F05C2201/0403 , F05C2201/0418 , F05C2201/0421 , F05C2201/0424 , F05C2201/0427 , Y02T10/125
Abstract: A piston for a diesel internal combustion engine including a crown portion at least partially formed of steel and having a combustion surface with a combustion bowl formed therein is provided. The combustion bowl presents a combustion bowl rim area, and a coating including at least one of a noble metal and a refractory metal is applied to substantially only the combustion bowl rim area. The coating is preferably applied in the areas of the combustion bowl rim area that are in line with the sprays of diesel fuel when the piston is in a top dead center position during operation of the engine.
Abstract translation: 一种柴油机内燃机的活塞，其特征在于，具备至少部分由钢制成的具有形成有燃烧碗的燃烧面的冠部的冠部。 燃烧碗具有燃烧碗边缘区域，并且包括贵金属和难熔金属中的至少一种的涂层仅基本上施加于燃烧碗边缘区域。 当在发动机操作期间活塞处于上止点位置时，该涂层优选地应用于燃烧碗边缘区域与柴油燃料喷雾一致的区域中。
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公开(公告)号：US06237619B1
公开(公告)日：2001-05-29
申请号：US09269816
申请日：1999-04-01
Applicant: Didier Maillefer , Philippe Renaud
Inventor： Didier Maillefer , Philippe Renaud
IPC: C23F100
CPC classification number: F16K99/0001 , F04B43/043 , F04B53/1067 , F05C2201/0403 , F05C2201/0418 , F05C2201/046 , F15C5/00 , F16K99/0009 , F16K99/0015 , F16K99/0034 , F16K99/0057 , F16K2099/0074 , F16K2099/008 , F16K2099/0086 , F16K2099/0094 , Y10T137/0491 , Y10T137/7895
Abstract: The invention relates to a micro-machined fluid-flow device (10) comprising a substrate (12) possessing a flow duct (14), a deformable thin layer (18) such a pump membrane or a valve-forming membrane. According to the invention, the thin layer (18) is a rolled metal sheet, preferably made of titanium, and connected to the substrate (12) in the zone (20) overlapping the flow duct, by an anodic bonding. The invention is applicable to making a valve.
Abstract translation: 本发明涉及一种微加工流体流动装置（10），其包括具有流动管道（14）的基底（12），诸如泵膜或阀形成膜的可变形薄层（18）。 根据本发明，薄层（18）是优选由钛制成的轧制金属板，并通过阳极接合连接到与流动管道重叠的区域（20）中的基板（12）。 本发明适用于制造阀门。
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公开(公告)号：US07879459B2
公开(公告)日：2011-02-01
申请号：US11768978
申请日：2007-06-27
Applicant: Melvin Freling , Kevin W. Schlichting
Inventor： Melvin Freling , Kevin W. Schlichting
CPC classification number: C23C4/02 , B22F2998/00 , C22C19/03 , C22C19/058 , C22C30/00 , C23C28/021 , C23C28/023 , C23C28/028 , C23C30/00 , F05B2230/311 , F05C2201/0418 , Y02T50/67 , Y10T428/12493 , Y10T428/12611 , Y10T428/1275 , Y10T428/12854 , Y10T428/12931 , B22F3/115
Abstract: A protective coating system includes a coating having a composition that includes about 5-40 wt % of chromium, of about 5-35 wt % of aluminum, about 0.1-9 wt % of at least one of silicon, hafnium, or magnesium, about 0.05-2 wt % of a Group IIIB Periodic Table element, a non-zero amount less than 13 wt % of at least one noble metal selected from platinum, palladium, and gold, and a balance including nickel, cobalt or iron.
Abstract translation: 保护性涂层系统包括具有组合物的涂层，该组合物包括约5-40wt％的铬，约5-35wt％的铝，约0.1-9wt％的硅，铪或镁中的至少一种，约为 0.05-2重量％的IIIB族周期表元素，非零量小于13重量％的至少一种选自铂，钯和金的贵金属，余量包括镍，钴或铁。
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公开(公告)号：US20090004503A1
公开(公告)日：2009-01-01
申请号：US11768978
申请日：2007-06-27
Applicant: Melvin Freling , Kevin W. Schlichting
Inventor： Melvin Freling , Kevin W. Schlichting
CPC classification number: C23C4/02 , B22F2998/00 , C22C19/03 , C22C19/058 , C22C30/00 , C23C28/021 , C23C28/023 , C23C28/028 , C23C30/00 , F05B2230/311 , F05C2201/0418 , Y02T50/67 , Y10T428/12493 , Y10T428/12611 , Y10T428/1275 , Y10T428/12854 , Y10T428/12931 , B22F3/115
Abstract: A protective coating system includes a coating having a composition that includes about 5-40 wt % of chromium, of about 5-35 wt % of aluminum, about 0.1-9 wt % of at least one of silicon, hafnium, or magnesium, about 0.05-2 wt % of a Group IIIB Periodic Table element, a non-zero amount less than 13 wt % of at least one noble metal selected from platinum, palladium, and gold, and a balance including nickel, cobalt or iron.
Abstract translation: 保护性涂层系统包括具有组合物的涂层，该组合物包括约5-40wt％的铬，约5-35wt％的铝，约0.1-9wt％的硅，铪或镁中的至少一种，约为 0.05-2重量％的IIIB族周期表元素，非零量小于13重量％的至少一种选自铂，钯和金的贵金属，余量包括镍，钴或铁。
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