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1. 发明授权

US08697195B2 Method for forming a protective coating with enhanced adhesion between layers 有权
标题翻译：用于形成具有增强的层之间的粘合力的保护涂层的方法
公开(公告)号：US08697195B2
公开(公告)日：2014-04-15
申请号：US11307266
申请日：2006-01-30
申请人： David Bucci , Daniel A. Nowak , Paul S. Dimascio
发明人： David Bucci , Daniel A. Nowak , Paul S. Dimascio
IPC分类号： B05D3/04 , C23C14/02 , H05H1/00 , H05H1/32
CPC分类号： C23C10/60 , C23C10/06 , C23C10/48 , C23C26/00 , Y10T428/12472
摘要： A method for forming a protective coating on a substrate comprising, applying a bond coating to the substrate, the bond coating having a first surface roughness, ionizing an inert gas which flows into the surface of the bond coating so as to impart a second surface roughness to the bond coating greater than the first surface roughness, wherein the inert gas is ionized and caused to flow into the surface of the bond coating by a reverse polarity current supplied to an electrode which removes at least one electron from the inert gas, and applying a top coating to the bond coating. Additionally, a method for preparing a surface to receive and adhere to a coating comprising roughening the surface to create a micro-roughening network on the surface. In addition, a method of improving strain tolerance and cyclic spallation life of a protective coating.
摘要翻译：一种在基材上形成保护涂层的方法，包括：向所述基材施加粘合涂层，所述粘合涂层具有第一表面粗糙度，电离惰性气体，所述惰性气体流入所述粘结涂层的表面，以赋予第二表面粗糙度到大于第一表面粗糙度的粘结涂层，其中惰性气体被电离并通过提供给从惰性气体中除去至少一个电子的电极的反极性电流流入粘合涂层的表面，并施加粘合涂层的顶部涂层。另外，一种制备表面以接收和粘附到涂层上的方法，包括使表面变粗糙以在表面上产生微粗糙化网络。另外，提高保护涂层的耐应变性和循环剥落寿命的方法。

2. 发明申请

US20100068062A1 Turbine bucket with dovetail seal and related method 审中-公开
标题翻译：涡轮桶采用燕尾密封及相关方法
公开(公告)号：US20100068062A1
公开(公告)日：2010-03-18
申请号：US12232224
申请日：2008-09-12
申请人： Paul S. DiMascio , Graham D. Sherlock , Mark L. Hunt
发明人： Paul S. DiMascio , Graham D. Sherlock , Mark L. Hunt
IPC分类号： F01D5/30 , F16J15/10
CPC分类号： F01D5/3007 , F01D5/3061 , F01D5/3092 , F01D5/326 , F05D2230/23
摘要： A method of sealing gaps between a bucket dovetail and a rotor disk dovetail slot in which the bucket dovetail is adapted to be received, the method comprising applying a resin material to selected areas of the bucket dovetail; and inserting the bucket dovetail into the dovetail slot.
摘要翻译：一种密封桶燕尾榫和转子盘燕尾槽之间的间隙的方法，其中铲斗鸠尾形适合于其中，该方法包括将树脂材料施加到铲斗燕尾榫的选定区域; 并将铲斗燕尾榫插入燕尾槽。

3. 发明授权

US08157525B2 Methods and apparatus relating to turbine airfoil cooling apertures 有权
标题翻译：与涡轮机翼型冷却孔相关的方法和装置
公开(公告)号：US08157525B2
公开(公告)日：2012-04-17
申请号：US12274553
申请日：2008-11-20
申请人： Robert A. Brittingham , Paul S. Dimascio
发明人： Robert A. Brittingham , Paul S. Dimascio
IPC分类号： F01D5/08 , F01D5/18 , B21D53/78
CPC分类号： F01D5/189 , F05D2260/202 , Y02T50/671 , Y02T50/676 , Y10T29/49341
摘要： An airfoil assembly for a turbine engine, that may comprise: an airfoil that includes at least one panel opening formed therein; and an aperture panel that includes at least one cooling aperture; wherein the panel opening and the aperture panel are configured such that, upon installation of the aperture panel within the panel opening, a substantially smooth outer surface of the airfoil is formed and at least one of the cooling apertures of the aperture panel forms an exit passageway from at least one hollow internal cavity within the airfoil.
摘要翻译：一种用于涡轮发动机的翼型组件，其可以包括：翼型件，其包括形成在其中的至少一个板开口; 以及孔板，其包括至少一个冷却孔; 其中所述面板开口和所述开口面板被构造成使得在将所述开口面板安装在所述面板开口内时，形成所述翼型件的大致平滑的外表面，并且所述孔板的至少一个所述冷却孔形成出口通道从翼型内的至少一个中空内腔。

4. 发明申请

US20090116533A1 Method and apparatus for testing and evaluating machine components under simulated in-situ thermal operating conditions 审中-公开
标题翻译：在模拟原位热操作条件下测试和评估机器部件的方法和装置
公开(公告)号：US20090116533A1
公开(公告)日：2009-05-07
申请号：US11979431
申请日：2007-11-02
申请人： Matthew J. O'Connell , Christopher E. Thompson , Paul S. Dimascio
发明人： Matthew J. O'Connell , Christopher E. Thompson , Paul S. Dimascio
IPC分类号： G01N25/72 , G01N29/14 , G01N19/08
CPC分类号： G01N25/72 , G01N29/14
摘要： A method and apparatus is described for enabling the testing and evaluation of industrial machine components and, in particular, gas turbine engine components, under simulated in-situ thermal operating conditions for effectively evaluating new component designs and repair techniques. A specimen machine component/part is placed in a test chamber and cyclically heated and cooled while being monitored to obtain information regarding the initiation and propagation of a crack within the structure of the component. Information regarding the number of heating and cooling cycles sustained by the component until crack initiation and information indicating the rate of crack propagation are acquired and compared over multiple heating-cooling cycles to evaluate components and repair techniques. In one example implementation, the component is monitored during cyclic heating-cooling for spontaneous acoustic emissions and acoustic emission waveform data is recorded and analyzed to determine crack initiation and/or propagation.
摘要翻译：描述了一种方法和装置，用于在模拟的原位热操作条件下实现工业机器部件，特别是燃气涡轮发动机部件的测试和评估，以有效地评估新的部件设计和修理技术。将样品机组件/部件放置在测试室中并在被监视的同时循环地加热和冷却以获得关于部件结构内的裂纹的引发和传播的信息。获得关于部件直到裂纹开始持续的加热和冷却循环的数量以及指示裂纹扩展速率的信息的信息，并在多个加热 - 冷却循环中进行比较以评估部件和修复技术。在一个示例实施方案中，在循环加热 - 冷却期间监测组件以进行自发声发射，并且记录和分析声发射波形数据以确定裂纹发生和/或传播。

5. 发明授权

US4014146A Jamb mounting assembly 失效
标题翻译： Jamb安装组件
公开(公告)号：US4014146A
公开(公告)日：1977-03-29
申请号：US608443
申请日：1975-08-28
申请人： Paul S. DiMascio , John D. DiMascio
发明人： Paul S. DiMascio , John D. DiMascio
IPC分类号： E06B1/60 , E06B1/62 , E06B1/64 , E06B1/02
CPC分类号： E06B1/6015 , E06B1/64 , E06B2001/622
摘要： An adjustable bracket for mounting a jamb to an adjacent framing member. The mounting assembly comprises at least one L-shaped member, an inner leg of which is secured to the back of the jamb. The outer leg of the member can be nailed to the surrounding framing to locate and support the jamb.In one embodiment, a pair of telescoping L-shaped members are provided, one of which is secured to the jamb while the other slides within it. The members are advantageously formed with stiffening means at the apexes, and can be formed with detents for engaging the opposite edges of a hollow molding strip.In another embodiment, the brackets engage one side of the molding strip, the other side thereof being forced into a slot extending along the door jamb. A retainer is described which aids in retaining the molding lip in the jamb slot.
摘要翻译：用于将侧柱安装到相邻框架构件的可调节支架。安装组件包括至少一个L形构件，其内腿固定在侧柱的后部。成员的外腿可以钉在周围的框架上，以定位和支撑侧柱。

6. 发明申请

US20110165433A1 Erosion and corrosion resistant coating system for compressor 审中-公开
标题翻译：耐腐蚀和耐腐蚀的压缩机涂层系统
公开(公告)号：US20110165433A1
公开(公告)日：2011-07-07
申请号：US12654843
申请日：2010-01-06
申请人： Surinder S. Pabla , Krishnamurthy Anand , Paul S. Dimascio , Stuart S. Collins , James A. Ruud , Suchismita Sanyal
发明人： Surinder S. Pabla , Krishnamurthy Anand , Paul S. Dimascio , Stuart S. Collins , James A. Ruud , Suchismita Sanyal
IPC分类号： B32B15/04 , B05D1/36 , C09D1/00
CPC分类号： C23C18/1662 , C23C18/1651 , C23C18/48 , C23C30/00 , F01D5/288 , Y10T428/12493
摘要： Process for providing a protective coating to a metal surface by applying a nickel or tantalum plate layer to the surface and dispersing particles of a hard material such as diamond, alumina, vanadium nitride, tantalum carbide and/or tungsten carbide within the nickel or tantalum plate layer as the plating is occurring.
摘要翻译：通过将镍或钽板层施加到表面并将硬质材料如金刚石，氧化铝，氮化钒，碳化钽和/或碳化钨的颗粒分散在镍或钽板内的方式向金属表面提供保护涂层发生电镀层。

7. 发明申请

US20130261034A1 COATING FOR TURBOMACHINERY 审中-公开
标题翻译：涂装用于涡轮机
公开(公告)号：US20130261034A1
公开(公告)日：2013-10-03
申请号：US12504837
申请日：2009-07-17
申请人： David V. Bucci , Paul S. Dimascio , Surinder S. Pabla , Jesse C. Moses
发明人： David V. Bucci , Paul S. Dimascio , Surinder S. Pabla , Jesse C. Moses
IPC分类号： C10M125/02
CPC分类号： C10M125/02 , C10M103/02 , C10M111/02 , C10M111/04 , C10M2201/0413 , C10M2201/1023 , C10N2230/06 , C10N2240/12 , C10N2250/18
摘要： A coating for turbomachinery comprises graphite-based sold film lubricant material.
摘要翻译：用于涡轮机械的涂层包括基于石墨的销售膜润滑剂材料。

8. 发明授权

US07842402B2 Machine components and methods of fabricating 有权
标题翻译：机械部件和制造方法
公开(公告)号：US07842402B2
公开(公告)日：2010-11-30
申请号：US11395633
申请日：2006-03-31
申请人： Ganjiang Feng , Paul S. Dimascio , Jon C. Schaeffer
发明人： Ganjiang Feng , Paul S. Dimascio , Jon C. Schaeffer
IPC分类号： B32B15/04
CPC分类号： F01D5/288 , C23C4/073 , C23C4/11 , C23C4/129 , C23C4/18 , C23C30/00 , F05D2230/311 , F05D2300/611 , Y10T428/12493 , Y10T428/12611 , Y10T428/12944 , Y10T428/31678
摘要： A thermal barrier coating (TBC) system is provided. The system includes at least one thermal barrier coating (TBC) bond coat layer formed over a substrate surface region. The TBC bond coat layer includes at least one TBC bond coat material. The TBC bond coat material is a nickel-chromium-aluminum-yttrium (NiCrAlY) composition that also includes silicon (Si), hafnium (Hf) and less than 10 weight percent (wt %) cobalt (Co). The TBC system further includes at least one top coat layer formed over the TBC bond coat layer.
摘要翻译：提供了一种隔热涂层（TBC）系统。该系统包括在衬底表面区域上形成的至少一个热障涂层（TBC）粘合涂层。 TBC粘合涂层包括至少一种TBC粘结涂层材料。 TBC粘合涂层材料是还包括硅（Si），铪（Hf）和小于10重量％（重量％）钴（Co）的镍 - 铬 - 铝 - 钇（NiCrAlY）组合物。 TBC系统还包括形成在TBC粘结涂层上的至少一个顶涂层。

9. 发明申请

US20100124499A1 METHODS AND APPARATUS RELATING TO TURBINE AIRFOIL COOLING APERTURES 有权
标题翻译：关于涡轮机空气冷却孔的方法和装置
公开(公告)号：US20100124499A1
公开(公告)日：2010-05-20
申请号：US12274553
申请日：2008-11-20
申请人： Robert A. Brittingham , Paul S. Dimascio
发明人： Robert A. Brittingham , Paul S. Dimascio
IPC分类号： F01D5/08
CPC分类号： F01D5/189 , F05D2260/202 , Y02T50/671 , Y02T50/676 , Y10T29/49341
摘要： An airfoil assembly for a turbine engine, that may comprise: an airfoil that includes at least one panel opening formed therein; and an aperture panel that includes at least one cooling aperture; wherein the panel opening and the aperture panel are configured such that, upon installation of the aperture panel within the panel opening, a substantially smooth outer surface of the airfoil is formed and at least one of the cooling apertures of the aperture panel forms an exit passageway from at least one hollow internal cavity within the airfoil.
摘要翻译：一种用于涡轮发动机的翼型组件，其可以包括：翼型件，其包括形成在其中的至少一个板开口; 以及孔板，其包括至少一个冷却孔; 其中所述面板开口和所述开口面板被构造成使得在将所述开口面板安装在所述面板开口内时，形成所述翼型件的大致平滑的外表面，并且所述孔板的至少一个所述冷却孔形成出口通道从翼型内的至少一个中空内腔。

10. 发明申请

US20100119871A1 Machine components and methods of fabricating 有权
公开(公告)号：US20100119871A1
公开(公告)日：2010-05-13
申请号：US11395633
申请日：2006-03-31
申请人： Ganjiang Feng , Paul S. Dimascio , Jon C. Schaeffer
发明人： Ganjiang Feng , Paul S. Dimascio , Jon C. Schaeffer
IPC分类号： B32B15/01 , B05D1/36 , C23C4/08 , B05D7/00 , B32B15/04
CPC分类号： F01D5/288 , C23C4/073 , C23C4/11 , C23C4/129 , C23C4/18 , C23C30/00 , F05D2230/311 , F05D2300/611 , Y10T428/12493 , Y10T428/12611 , Y10T428/12944 , Y10T428/31678
摘要： A thermal barrier coating (TBC) system is provided. The system includes at least one thermal barrier coating (TBC) bond coat layer formed over a substrate surface region. The TBC bond coat layer includes at least one TBC bond coat material. The TBC bond coat material is a nickel-chromium-aluminum-yttrium (NiCrAlY) composition that also includes silicon (Si), hafnium (Hf) and less than 10 weight percent (wt %) cobalt (Co). The TBC system further includes at least one top coat layer formed over the TBC bond coat layer.

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