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31. 发明申请

US20090178736A1 ARTICLE HAVING COBALT-PHOSPHOROUS COATING AND METHOD FOR HEAT TREATING 有权
标题翻译：具有钴 - 磷光涂层的物品和热处理方法
公开(公告)号：US20090178736A1
公开(公告)日：2009-07-16
申请号：US12015089
申请日：2008-01-16
申请人： Blair A. Smith , Aaron T. Nardi
发明人： Blair A. Smith , Aaron T. Nardi
IPC分类号： B32B37/06 , B05D3/02 , B32B15/04 , B32B19/00 , B32B15/00 , C22F1/10
CPC分类号： C25D5/50 , C22F1/10 , C23C2/28 , C23C4/18 , C23C26/00 , C25D3/562 , C25D15/02 , F15B15/1457 , Y10T428/12861
摘要： A method of processing an article having a substrate and a cobalt-phosphorous coating disposed on the substrate includes heat treating the article. At least one physical characteristic of the cobalt-phosphorous coating is altered using the heat treating to thereby change a performance characteristic of the article. For example, the article may be an actuator component having a bore or a shaft that is movably disposed at least partially within the bore.
摘要翻译：一种处理具有基板和设置在基板上的钴 - 磷涂层的物品的方法包括对物品进行热处理。使用热处理改变钴 - 磷涂层的至少一种物理特性，从而改变制品的性能特征。例如，制品可以是具有孔或轴的致动器部件，其可移动地至少部分地设置在孔内。

32. 发明申请

US20120119132A1 ARTICLE HAVING GOOD WEAR RESISTANCE 有权
标题翻译：具有良好耐磨性的产品
公开(公告)号：US20120119132A1
公开(公告)日：2012-05-17
申请号：US13237102
申请日：2011-09-20
申请人： Glenn Gradischer , Kevin M. Rankin , Blair A. Smith , Angelina Y. Cheung
发明人： Glenn Gradischer , Kevin M. Rankin , Blair A. Smith , Angelina Y. Cheung
IPC分类号： F16K27/00 , C23C4/06 , C23C4/10
CPC分类号： C23C30/00 , C23C4/08 , C23C8/68 , C23C8/70 , Y10T137/0318 , Y10T137/7036
摘要： An article having good wear resistance includes a first component including a boride coating and a second component including a cobalt-chromium-molybdenum coating that is in sliding contact with the boride coating of the first component.
摘要翻译：具有良好耐磨性的制品包括包括硼化物涂层的第一组分和包含与第一组分的硼化物涂层滑动接触的钴 - 铬 - 钼涂层的第二组分。

33. 发明授权

US08833382B2 Article having good wear resistance 有权
标题翻译：物品具有良好的耐磨性
公开(公告)号：US08833382B2
公开(公告)日：2014-09-16
申请号：US13237102
申请日：2011-09-20
申请人： Glenn Gradischer , Kevin M. Rankin , Blair A. Smith , Angelina Y. Cheung
发明人： Glenn Gradischer , Kevin M. Rankin , Blair A. Smith , Angelina Y. Cheung
IPC分类号： F16K27/00 , C23C4/08 , C23C30/00 , C23C8/70 , C23C8/68
CPC分类号： C23C30/00 , C23C4/08 , C23C8/68 , C23C8/70 , Y10T137/0318 , Y10T137/7036
摘要： An article having good wear resistance includes a first component including a boride coating and a second component including a cobalt-chromium-molybdenum coating that is in sliding contact with the boride coating of the first component.
摘要翻译：具有良好耐磨性的制品包括包括硼化物涂层的第一组分和包含与第一组分的硼化物涂层滑动接触的钴 - 铬 - 钼涂层的第二组分。

34. 发明申请

US20130343898A1 PROPELLER BLADE WITH CARBON FOAM SPAR CORE 有权
标题翻译：螺旋桨叶与碳泡沫SPORE核心
公开(公告)号：US20130343898A1
公开(公告)日：2013-12-26
申请号：US13533218
申请日：2012-06-26
申请人： Michael E. Folsom , Blair A. Smith , David P. Nagle
发明人： Michael E. Folsom , Blair A. Smith , David P. Nagle
IPC分类号： F01D5/14 , B23P15/04
CPC分类号： B64C11/26 , B29D99/0025 , B64C11/205 , B64C11/22 , B64C11/24 , B64C27/473 , Y10T29/49337
摘要： According to one embodiment, a propeller blade includes a carbon foam core and a structural layer that surrounds at least a portion of the carbon foam core.
摘要翻译：根据一个实施例，螺旋桨叶片包括碳泡沫芯和围绕碳泡沫芯的至少一部分的结构层。

35. 依法登记的发明

USH1207H Chromic acid anodization of titanium 失效
公开(公告)号：USH1207H
公开(公告)日：1993-07-06
申请号：US652407
申请日：1991-02-07
申请人： Blair A. Smith
发明人： Blair A. Smith
IPC分类号： C25D11/26
CPC分类号： C25D11/26
摘要： The present invention discloses a method of forming an adhesion promoting oxide surface on titanium in which the titanium surface is first abraded and then anodized in hydrofluoric acid free chromic acid.

36. 发明授权

US09139287B2 Propeller blade with carbon foam spar core 有权
标题翻译：螺旋桨叶片采用碳质泡沫芯棒
公开(公告)号：US09139287B2
公开(公告)日：2015-09-22
申请号：US13533218
申请日：2012-06-26
申请人： Michael E. Folsom , Blair A. Smith , David P. Nagle
发明人： Michael E. Folsom , Blair A. Smith , David P. Nagle
IPC分类号： B64C11/26 , B64C11/22 , B64C11/24
CPC分类号： B64C11/26 , B29D99/0025 , B64C11/205 , B64C11/22 , B64C11/24 , B64C27/473 , Y10T29/49337
摘要： According to one embodiment, a propeller blade includes a carbon foam core and a structural layer that surrounds at least a portion of the carbon foam core.
摘要翻译：根据一个实施例，螺旋桨叶片包括碳泡沫芯和围绕碳泡沫芯的至少一部分的结构层。

37. 发明申请

US20130039765A1 AIRCRAFT PROPELLERS 有权
标题翻译：飞机螺旋桨
公开(公告)号：US20130039765A1
公开(公告)日：2013-02-14
申请号：US13208897
申请日：2011-08-12
申请人： Blair A. Smith , David J. Grulke
发明人： Blair A. Smith , David J. Grulke
IPC分类号： B64C11/00
CPC分类号： B64C11/008 , B64C11/04 , B64C11/24 , B64C11/30
摘要： An aircraft propeller taper bore insert apparatus includes an outer surface, the outer surface dimensioned and configured to fit within an aircraft propeller taper bore or an aircraft propeller balancing tube, and an inner surface, the inner surface defining an inner cavity configured to receive a balancing medium, the inner surface comprising a plurality of retention formations arranged thereon, and the plurality of retention formations being configured to support the balancing medium.
摘要翻译：飞行器螺旋桨锥孔插入装置包括外表面，外表面的尺寸和构造适于装配在飞行器螺旋桨锥形孔或飞行器螺旋桨平衡管内以及内表面中，内表面限定内腔，其构造成接收平衡介质，所述内表面包括布置在其上的多个保持结构，并且所述多个保持结构被配置为支撑所述平衡介质。

38. 发明授权

US5881972A Electroformed sheath and airfoiled component construction 失效
标题翻译：电铸护套和翼型部件结构
公开(公告)号：US5881972A
公开(公告)日：1999-03-16
申请号：US811628
申请日：1997-03-05
申请人： Blair A. Smith , John M. Graff
发明人： Blair A. Smith , John M. Graff
IPC分类号： B64C11/20 , C25D1/00 , C25D3/56 , B64C3/36
CPC分类号： C25D3/562 , B64C11/205 , C25D1/00 , F04D29/324 , F05D2240/303
摘要： A sheath for covering and protecting a component leading edge of an airfoiled component is disclosed. The sheath includes a sheath leading edge, and a first protective side and a second protective side, wherein the first and second protective sides are merged at the sheath leading edge. A cavity is formed between the first and second protective sides, wherein the cavity is adapted to have the airfoiled component positioned therein and engage an inside surface of each of the first and second protective sides. The sheath is formed from a material including cobalt, and preferably a nickel-cobalt composition. Preferred embodiments include cobalt in the nickel-cobalt composition present between 8-32 wt. % and 30-54 wt. %, based on the weight of the sheath. An airfoiled component construction is also disclosed. This construction includes a main structural component formed in the shape of an airfoil, wherein the main structural component has a leading edge, and a sheath covering and protecting the leading edge, wherein the sheath is formed from a material including cobalt such as a nickel-cobalt composition. Preferred embodiments include cobalt in the nickel-cobalt composition present between 8-32 wt. % and 30-54 wt. %, based on the weight of the sheath.
摘要翻译：公开了一种用于覆盖和保护翼型部件的部件前缘的护套。鞘包括护套前缘，第一保护侧和第二保护侧，其中第一和第二保护侧在护套前缘处合并。在第一和第二保护侧之间形成空腔，其中空腔适于将翼型部件定位在其中并与第一和第二保护侧中的每一个的内表面接合。护套由包括钴的材料形成，优选由镍 - 钴组合物形成。优选的实施方案包括存在于8-32重量％的镍 - 钴组合物中的钴。％和30-54wt。％，基于护套的重量。还公开了一种翼型部件结构。这种结构包括形成为翼型形状的主要结构部件，其中主要结构部件具有前缘，以及覆盖并保护前缘的护套，其中护套由包括钴的材料形成，例如镍 - 钴组成。优选的实施方案包括存在于8-32重量％的镍 - 钴组合物中的钴。％和30-54wt。％，基于护套的重量。

39. 发明授权

US08882464B2 Aircraft propellers 有权
标题翻译：飞机螺旋桨
公开(公告)号：US08882464B2
公开(公告)日：2014-11-11
申请号：US13208897
申请日：2011-08-12
申请人： Blair A. Smith , David J. Grulke
发明人： Blair A. Smith , David J. Grulke
IPC分类号： B64C11/20 , B64C11/00 , B64C11/04
CPC分类号： B64C11/008 , B64C11/04 , B64C11/24 , B64C11/30
摘要： An aircraft propeller taper bore insert apparatus includes a tapered outer surface, the outer surface dimensioned and configured to fit within and be of substantially a same size and shape as an aircraft propeller taper bore or an aircraft propeller balancing tube, and an inner surface, the inner surface defining an inner cavity configured to receive a balancing medium, the inner surface comprising a plurality of retention formations arranged thereon, and the plurality of retention formations being configured to support the balancing medium.
摘要翻译：飞机推进器锥孔插入装置包括锥形外表面，外表面的尺寸和构造适合于与飞行器螺旋桨锥形孔或飞行器螺旋桨平衡管和内表面相配合并且具有基本相同的尺寸和形状，内表面限定被配置为接收平衡介质的内腔，所述内表面包括布置在其上的多个保持结构，并且所述多个保持结构被配置为支撑所述平衡介质。

40. 发明申请

US20120024403A1 INORGANIC COKE RESISTANT COATINGS TO PREVENT AIRCRAFT FUEL SYSTEM FOULING 审中-公开
标题翻译：无机防焦油漆，以防飞机燃油系统
公开(公告)号：US20120024403A1
公开(公告)日：2012-02-02
申请号：US12847497
申请日：2010-07-30
申请人： Marc E. Gage , Blair A. Smith
发明人： Marc E. Gage , Blair A. Smith
IPC分类号： F03B11/02
CPC分类号： F02C7/222 , F05D2230/313 , F05D2230/314 , F05D2230/90 , F05D2300/20 , F05D2300/22 , F05D2300/226 , F05D2300/228 , F05D2300/611 , Y10T137/8593
摘要： A fuel system for delivering fuel to an engine includes a fuel tank, a hot section in fluid communication with the fuel tank for delivering fuel for combustion by the engine, and a ceramic coating applied to at least a portion of the hot section for reducing fuel coking. The ceramic coating is selected from carbides, nitrides, carbonitrides, silicides and mixtures thereof.
摘要翻译：用于将燃料输送到发动机的燃料系统包括燃料箱，与燃料箱流体连通的用于输送发动机燃烧燃料的热部分，以及施加到热部分的至少一部分以用于还原燃料的陶瓷涂层焦化陶瓷涂层选自碳化物，氮化物，碳氮化物，硅化物及其混合物。

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