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1. 发明授权

US06805750B1 Surface preparation process for deposition of ceramic coating 失效
标题翻译：陶瓷涂层沉积的表面处理工艺
公开(公告)号：US06805750B1
公开(公告)日：2004-10-19
申请号：US09274127
申请日：1999-03-23
申请人： Raymond P. Ristau , Sudhangshu Bose , Alan D. Cetel
发明人： Raymond P. Ristau , Sudhangshu Bose , Alan D. Cetel
IPC分类号： B08B304
CPC分类号： C23C14/028 , C23C8/10 , C23C14/02 , C23C14/021
摘要： A method of surface cleaning and controlled oxidation of superalloys is described. The method provides a thin homogeneous layer of relatively pure alpha alumina which is suited to receive and adhere to a subsequent vapor deposited coating.
摘要翻译：描述了超级合金的表面清洁和受控氧化的方法。该方法提供了相当纯的α氧化铝的薄均匀层，其适于接收和粘附到随后的气相沉积涂层。

2. 发明申请

US20110256421A1 METALLIC COATING FOR SINGLE CRYSTAL ALLOYS 审中-公开
标题翻译：金属涂层用于单晶合金
公开(公告)号：US20110256421A1
公开(公告)日：2011-10-20
申请号：US12761667
申请日：2010-04-16
申请人： Sudhangshu Bose , Alan D. Cetel , David A. Litton , Michael J. Maloney , Venkatarama K. Seetharaman , Shiela Woodard
发明人： Sudhangshu Bose , Alan D. Cetel , David A. Litton , Michael J. Maloney , Venkatarama K. Seetharaman , Shiela Woodard
IPC分类号： B32B15/01 , C22C19/05
CPC分类号： C22C19/056 , B32B15/01 , C22C19/057 , C23C4/08 , C23C28/00 , C23C30/00 , C30B29/52 , Y10T428/12944
摘要： A metallic coating for use in a high temperature application is created from a nickel base alloy containing from 5.0 to 10.5 wt % aluminum, from 4.0 to 15 wt % chromium, from 2.0 to 8.0 wt % tungsten, from 3.0 to 10 wt % tantalum, and the balance nickel. The metallic coating has particular utility in protecting single crystal superalloys used in high temperature applications such as turbine engine components.
摘要翻译：用于高温应用的金属涂层由含有5.0至10.5重量％的铝，4.0至15重量％的铬，2.0至8.0重量％的钨，3.0至10重量％的钽的镍基合金产生，余量为镍。金属涂层在保护用于高温应用例如涡轮发动机部件的单晶超合金中具有特别的用途。

3. 发明授权

US06725540B2 Method for repairing turbine engine components 有权
标题翻译：修理涡轮发动机部件的方法
公开(公告)号：US06725540B2
公开(公告)日：2004-04-27
申请号：US10094702
申请日：2002-03-09
申请人： Sudhangshu Bose , Alan D. Cetel , Peter J. Draghi , Norman Pietruska
发明人： Sudhangshu Bose , Alan D. Cetel , Peter J. Draghi , Norman Pietruska
IPC分类号： B23P1500
CPC分类号： C23G1/20 , B23P6/007 , C23C10/02 , Y10T29/49318 , Y10T29/49336 , Y10T29/49726 , Y10T29/49737 , Y10T29/49746
摘要： The present invention relates to a method for repairing turbine engine components, such as vanes and blades, which have airfoils. The method broadly comprises removing oxidation debris from portions of the component by blending areas exhibiting thermal barrier coating spall and/or oxidation damage, removing a ceramic insulating layer from the component, and blending surfaces of the component where nicks, dents, and/or cracks are located. If the component has a depleted aluminum zone, the depleted zone is either removed or replenished. Further, a tip portion of the component, if damaged, is restored and tip abrasives are applied to restore the component's cutting ability. Thereafter, a ceramic coating is applied to the component.
摘要翻译：本发明涉及一种用于修理具有翼型的涡轮发动机部件（例如叶片和叶片）的方法。该方法广泛地包括通过混合具有热障涂层剥落和/或氧化损伤的区域来除去部件的部分的氧化碎屑，从该组件中除去陶瓷绝缘层，以及混合表面，其中缺口，凹痕和/或裂纹位于。如果组件具有耗尽的铝区，则耗尽的区域被去除或补充。此外，如果损坏的部件的尖端部分被恢复，并且施加尖端磨料以恢复部件的切割能力。此后，将陶瓷涂层施加到部件上。

4. 发明授权

US06833203B2 Thermal barrier coating utilizing a dispersion strengthened metallic bond coat 有权
公开(公告)号：US06833203B2
公开(公告)日：2004-12-21
申请号：US10212928
申请日：2002-08-05
申请人： Sudhangshu Bose , Daniel A. Bales , Mark T. Ucasz , Merritt W. Wight , Steven M. Burns , Tyrus E. Royal
发明人： Sudhangshu Bose , Daniel A. Bales , Mark T. Ucasz , Merritt W. Wight , Steven M. Burns , Tyrus E. Royal
IPC分类号： B32B1504
CPC分类号： C23C4/06 , C23C4/12 , C23C4/18 , C23C8/02 , C23C8/28 , C23C14/06 , Y10T428/12458 , Y10T428/12535 , Y10T428/12576 , Y10T428/12611 , Y10T428/12618 , Y10T428/12771 , Y10T428/12937 , Y10T428/12944 , Y10T428/25 , Y10T428/252 , Y10T428/256 , Y10T428/257 , Y10T428/26
摘要： The present invention relates to an overlay coating which has improved strength properties. The overlay coating comprises a deposited layer of MCrAlY material containing discrete nitride particles therein. The nitride particles are present in a volume fraction in the range of 0.1% to 15.0% and have a particle size in the range of from 0.1 microns to 10.0 microns. The coating may also have oxide particles dispersed therein.

5. 发明申请

US20050053799A1 Thermal barrier coating utilizing a dispersion strengthened metallic bond coat 有权
标题翻译：使用分散强化金属粘结涂层的热障涂层
公开(公告)号：US20050053799A1
公开(公告)日：2005-03-10
申请号：US10922009
申请日：2004-08-19
申请人： Sudhangshu Bose , Daniel Bales , Mark Ucasz , Merritt Wight , Steven Burns , Tyrus Royal
发明人： Sudhangshu Bose , Daniel Bales , Mark Ucasz , Merritt Wight , Steven Burns , Tyrus Royal
IPC分类号： F01D5/28 , C23C4/06 , C23C4/12 , C23C4/18 , C23C8/02 , C23C8/28 , C23C14/06 , C23C16/00 , C23C28/00 , F02C7/00 , B32B15/00
CPC分类号： C23C4/06 , C23C4/12 , C23C4/18 , C23C8/02 , C23C8/28 , C23C14/06 , Y10T428/12458 , Y10T428/12535 , Y10T428/12576 , Y10T428/12611 , Y10T428/12618 , Y10T428/12771 , Y10T428/12937 , Y10T428/12944 , Y10T428/25 , Y10T428/252 , Y10T428/256 , Y10T428/257 , Y10T428/26
摘要： The present invention relates to an overlay coating which has improved strength properties. The overlay coating comprises a deposited layer of MCrAlY material containing discrete nitride particles therein. The nitride particles are present in a volume fraction in the range of 0.1% to 15.0% and have a particle size in the range of from 0.1 microns to 10.0 microns. The coating may also have oxide particles dispersed therein.
摘要翻译：本发明涉及具有改善的强度性能的覆盖涂层。覆盖涂层包括其中包含离散的氮化物颗粒的MCrAlY材料的沉积层。氮化物颗粒存在于0.1％至15.0％范围内的体积分数中，并且具有在0.1微米至10.0微米范围内的粒度。涂层也可以具有分散在其中的氧化物颗粒。

6. 发明授权

US06605556B1 High temperature composite material formed from nanostructured powders 失效
标题翻译：由纳米结构粉末形成的高温复合材料
公开(公告)号：US06605556B1
公开(公告)日：2003-08-12
申请号：US08476497
申请日：1995-06-07
申请人： Sudhangshu Bose
发明人： Sudhangshu Bose
IPC分类号： C04B3580
CPC分类号： C04B35/80
摘要： The present invention relates to high temperature composite materials formed from nano-sized powders suitable for use in the manufacture of jet engine components. The composite materials consist essentially of a matrix formed from a powdered material having a particle size in the range of from about 1 to about 100 nanometers and a plurality of reinforcing fibers embedded within the matrix and comprising from about 20% to about 40% by volume of the composite material. The method of manufacturing the composite materials broadly comprises the steps of mixing the powdered material with the reinforcing fibers and consolidating the mixture to form the composite material.
摘要翻译：本发明涉及由适用于制造喷气发动机部件的纳米尺寸粉末形成的高温复合材料。复合材料基本上由由粒度在约1至约100纳米范围内的粉末材料形成的基质和嵌入基质内的多个增强纤维组成，并且包含约20体积％至约40体积％的复合材料。制造复合材料的方法广泛地包括将粉末材料与增强纤维混合并固结混合物以形成复合材料的步骤。

7. 发明授权

US08367964B2 Repair methods involving conductive heat resistance welding 有权
标题翻译：导电耐热焊接修补方法
公开(公告)号：US08367964B2
公开(公告)日：2013-02-05
申请号：US12186602
申请日：2008-08-06
申请人： Nicole Sullivan , John H. Hughes , James J. Moor , David A. Rutz , Sudhangshu Bose
发明人： Nicole Sullivan , John H. Hughes , James J. Moor , David A. Rutz , Sudhangshu Bose
IPC分类号： B23K11/00 , B23K31/02
CPC分类号： F01D5/005 , B23K9/04 , B23K9/167 , B23K31/02 , B23P6/007 , B23P6/045 , F05D2230/232 , Y10T29/49318
摘要： Repair methods involving conductive heat resistance welding includes repairing a crack of a gas turbine engine component using a conductive heat resistance welding technique and a welding technique other than conductive heat resistance welding.
摘要翻译：涉及导电耐热焊接的修理方法包括使用导电耐热焊接技术和不同于导电耐热焊接的焊接技术来修复燃气轮机发动机部件的裂纹。

8. 发明授权

US5304031A Outer air seal for a gas turbine engine 失效
标题翻译：燃气轮机的外气密封
公开(公告)号：US5304031A
公开(公告)日：1994-04-19
申请号：US28771
申请日：1993-02-25
申请人： Sudhangshu Bose
发明人： Sudhangshu Bose
IPC分类号： C23C16/04 , C23C16/32 , C23C16/44 , F01D11/12 , F01D11/08
CPC分类号： C23C16/045 , C23C16/325 , C23C16/4418 , F01D11/122 , F05D2300/21 , F05D2300/603 , Y10S277/937 , Y10S277/943 , Y10T428/31678
摘要： An uncooled turbine outer air is comprised of a combination of monolithic ceramics with high temperature capability and oxidation and creep resistance, and a fiber reinforced ceramic composite with high fracture toughness. In a preferred embodiment of the invention, a fiber reinforced ceramic composite of silicon carbide and aluminum borosilicate is infiltrated by chemically vapor deposited silicon carbide. The infiltration process is continued until the composite develops a monolithic layer of silicon carbide. An additional layer is deposited on the monolithic ceramic to provide additional thermal protection.
摘要翻译：未冷却的涡轮机外部空气由具有高温能力和抗氧化和抗蠕变性的整体式陶瓷的组合以及具有高断裂韧性的纤维增强陶瓷复合材料组成。在本发明的优选实施方案中，碳化硅和硼硅酸铝的纤维增强陶瓷复合材料被化学气相沉积的碳化硅渗透。渗透过程继续进行，直到复合材料开发出碳化硅的整体层。另外的一层沉积在单片陶瓷上以提供额外的热保护。

9. 发明授权

US4985316A Corrosion resistant fuel cell substrates 失效
标题翻译：耐腐蚀燃料电池基板
公开(公告)号：US4985316A
公开(公告)日：1991-01-15
申请号：US432335
申请日：1989-11-03
申请人： Sudhangshu Bose , Michael E. Gorman
发明人： Sudhangshu Bose , Michael E. Gorman
IPC分类号： C04B35/524 , H01M4/96
CPC分类号： H01M4/96 , C04B35/524 , Y10T428/30
摘要： A porous substrate of a fuel cell electrode assembly is formed by producing a fibrous carbon precursor web by means of a conventional wet paper-making process. The precursor web is then dried and saturated with a wet resinous binder which will carbonize when heated. Substantially the entirety of all of the carbon fibers in the web are thus coated with the binder, and substantially all of the inter-fiber junctures in the web will also be coated with the binder. The saturated web is then dried, and heat treated to convert the binder to a glassy carbon which exhibits superior resistance to corrosion.
摘要翻译：燃料电池电极组件的多孔基底是通过常规的湿法造纸工艺生产纤维状碳前体纤维网而形成的。然后将前体纤维网干燥并用湿树脂粘合剂饱和，该粘合剂将在加热时碳化。因此，幅材中基本上全部的碳纤维都被粘合剂涂覆，并且幅材中基本上所有的纤维间接合面也将被粘合剂涂覆。然后干燥饱和纤维网，并进行热处理以将粘合剂转化为显示出优异的耐腐蚀性的玻璃碳。

10. 发明申请

US20090114797A1 REFRACTORY METAL CORE COATINGS 有权
标题翻译：耐火金属核心涂层
公开(公告)号：US20090114797A1
公开(公告)日：2009-05-07
申请号：US10685631
申请日：2003-10-15
申请人： James T. Beals , Joshua Persky , Dilip M. Shah , Venkat Seetharaman , Sudhangshu Bose , Jacob Snyder , Keith Santeler , Carl Verner , Stephen D. Murray , John J. Marcin , Dinesh Gupta , Daniel A. Bales , Daniel Francis Paulonis , Glenn Cotnoir , John Wiedemer
发明人： James T. Beals , Joshua Persky , Dilip M. Shah , Venkat Seetharaman , Sudhangshu Bose , Jacob Snyder , Keith Santeler , Carl Verner , Stephen D. Murray , John J. Marcin , Dinesh Gupta , Daniel A. Bales , Daniel Francis Paulonis , Glenn Cotnoir , John Wiedemer
IPC分类号： B28B7/28
CPC分类号： B22C9/10
摘要： A refractory metal core for use in a casting system has a coating for providing oxidation resistance during shell fire and protection against reaction/dissolution during casting. In a first embodiment, the coating includes at least one oxide and a silicon containing material. In a second embodiment, the coating includes an oxide selected from the group of calcia, magnesia, alumina, zirconia, chromia, yttria, silica, hafnia, and mixtures thereof. In a third embodiment, the coating includes a nitride selected from the group of silicon nitride, sialon, titanium nitride, and mixtures thereof. Other coating embodiments are described in the disclosure.
摘要翻译：用于铸造系统的难熔金属芯具有用于在壳体火焰期间提供抗氧化性和防止铸造期间的反应/溶解的涂层。在第一实施例中，涂层包括至少一种氧化物和含硅材料。在第二个实施方案中，涂层包括选自氧化钙，氧化镁，氧化铝，氧化锆，氧化铬，氧化钇，二氧化硅，铪和其混合物的氧化物。在第三实施例中，涂层包括选自氮化硅，赛隆，氮化钛及其混合物的氮化物。在本公开中描述了其它涂层实施例。

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