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1. 发明申请

US20110206532A1 ELECTROLESS METAL COATINGS 审中-公开
标题翻译：电镀金属涂料
公开(公告)号：US20110206532A1
公开(公告)日：2011-08-25
申请号：US12710691
申请日：2010-02-23
申请人： Francesco Sorbo , Lawrence Bernard Kool , William Clarke Brooks , Massimo Giannozzi , Eugenio Giorni , Thomas Lancsek , Steven Alfred Tysoe , Dennis Michael Gray , Todd Charles Curtis
发明人： Francesco Sorbo , Lawrence Bernard Kool , William Clarke Brooks , Massimo Giannozzi , Eugenio Giorni , Thomas Lancsek , Steven Alfred Tysoe , Dennis Michael Gray , Todd Charles Curtis
IPC分类号： F04D29/24 , B05D3/02 , B32B15/04 , B32B15/01
CPC分类号： C23C18/32 , Y10T428/12944 , Y10T428/31678
摘要： The present invention provides a method for preparing an electroless nickel coating composition that includes (a) coating a substrate with an electroless nickel coating to provide a coated substrate; and (b) subjecting the coated substrate to a heating protocol comprising heating to a temperature in a range from about 550° C. to about 700° C. for a period of from about 7 to about 30 hours. An article made from the method is also provided.
摘要翻译：本发明提供一种制备无电镍涂料组合物的方法，其包括（a）用无电镀镍涂层涂覆基材以提供涂覆的基材; 和（b）使涂覆的基材经受加热方案，包括加热至约550℃至约700℃的温度约7至约30小时。还提供了从该方法制成的文章。

2. 发明申请

US20120312924A1 ICE SHED REDUCTION FOR LEADING EDGE STRUCTURES 审中-公开
标题翻译：用于引导边缘结构的减少冰盖
公开(公告)号：US20120312924A1
公开(公告)日：2012-12-13
申请号：US13590970
申请日：2012-08-21
申请人： Edward Atwood Rainous , Barry Lynn Allmon , Jeffre Gerry Loewe , William Clarke Brooks , Lee Alan Blanton , Courtney James Tudor , Vicky Showalter Budinger
发明人： Edward Atwood Rainous , Barry Lynn Allmon , Jeffre Gerry Loewe , William Clarke Brooks , Lee Alan Blanton , Courtney James Tudor , Vicky Showalter Budinger
IPC分类号： B64D15/00
CPC分类号： B64D15/00 , B64D33/02 , B64D2033/0233 , B64D2033/0286 , F01D9/04 , F01D25/02 , F01D25/162 , F02C7/047 , F05D2300/50212
摘要： A leading edge structure for use in an aerospace vehicle includes a body having a flowpath surface which defines a leading edge adapted to face an air flow during operation, and an opposed inner surface. The body is segmented into a plurality of portions having varying thermal properties and/or mechanical discontinuities, so as to promote stress concentrations in ice attached to the flowpath surface.
摘要翻译：用于航空航天车辆的前缘结构包括具有流动路径表面的主体，其限定了在操作期间适于面对空气流的前缘以及相对的内表面。主体被分割成具有变化的热性能和/或机械不连续性的多个部分，以促进附着在流路表面上的冰中的应力集中。

3. 发明授权

US06454870B1 Chemical removal of a chromium oxide coating from an article 有权
标题翻译：从制品中化学去除氧化铬涂层
公开(公告)号：US06454870B1
公开(公告)日：2002-09-24
申请号：US09994343
申请日：2001-11-26
申请人： William Clarke Brooks
发明人： William Clarke Brooks
IPC分类号： C23G102
CPC分类号： C23C4/02 , C23G1/00 , C23G1/20 , Y02T50/67
摘要： A chromium oxide coating is removed from a surface of an article by cleaning the article in an alkaline degreasing/rust removal solution at a degreasing/rust removal temperature of from about 180° F. to about 200° F., scale conditioning the article in an alkaline permanganate conditioning solution at a scale-conditioning temperature of from about 160° F. to about 200° F., and contacting the article to an acidic stripping solution comprising hydrochloric acid and an etching inhibitor at a stripping temperature of from about 130° F. to about 140° F.
摘要翻译：通过在约180°F至约200°F的脱脂/除锈温度下在碱性脱脂/除锈溶液中清洁该制品，从制品的表面除去氧化铬涂层。在约160°F至约200°F的调温温度下的碱性高锰酸盐调理溶液，并且在约130℃的剥离温度下使制品与包含盐酸和蚀刻抑制剂的酸性剥离溶液接触 F.至约140°F

4. 发明申请

US20090272095A1 ICE SHED REDUCTION FOR LEADING EDGE STRUCTURES 有权
标题翻译：用于引导边缘结构的减少冰盖
公开(公告)号：US20090272095A1
公开(公告)日：2009-11-05
申请号：US12112660
申请日：2008-04-30
申请人： Edward Atwood Rainous , Barry Lynn Allmon , Jeffre Gerry Loewe , William Clarke Brooks , Lee Alan Blanton , Courtney James Tudor , Vicky Showalter Budinger
发明人： Edward Atwood Rainous , Barry Lynn Allmon , Jeffre Gerry Loewe , William Clarke Brooks , Lee Alan Blanton , Courtney James Tudor , Vicky Showalter Budinger
IPC分类号： F02C7/04
CPC分类号： B64D15/00
摘要： A leading edge structure for use in an aerospace vehicle includes a body having a flowpath surface which defines a leading edge adapted to face an air flow during operation; and a metallic icephobic plating comprising nickel applied to at least a portion of the flowpath surface.
摘要翻译：用于航空航天车辆的前缘结构包括具有流动路径表面的主体，其限定在操作期间适于面对空气流的前缘; 以及包含施加到所述流路表面的至少一部分的镍的金属冰敷电镀。

5. 发明授权

US07115171B2 Method for removing engine deposits from turbine components and composition for use in same 有权
标题翻译：用于从涡轮机部件移除发动机沉积物的方法和用于其的组合物
公开(公告)号：US07115171B2
公开(公告)日：2006-10-03
申请号：US11020291
申请日：2004-12-27
申请人： John Matthew Powers , William Clarke Brooks
发明人： John Matthew Powers , William Clarke Brooks
IPC分类号： C23G1/02
CPC分类号： C11D3/046 , C11D3/042 , C11D3/048 , C11D7/08 , C11D7/10 , C11D7/105 , C11D11/0041 , C23G1/10
摘要： A method and cleaning composition for removing engine deposits from turbine components, in particular turbine disks and turbine shafts. This method comprises the following steps: (a) providing a turbine component having a surface with engine deposits thereon, wherein the turbine component comprises a nickel and/or cobalt-containing base metal; and (b) treating the surface of the turbine component with a cleaning composition to convert the engine deposits thereon to a removable smut without substantially etching the base metal of the turbine component. The cleaning composition comprises an aqueous solution that is substantially free of acetic acid and comprising: a nitrate ion source in an amount, by weight of the nitrate ion, of from about 470 to about 710 grams/liter; and a bifluoride ion source in an amount, by weight of the bifluoride ion, of from about 0.5 to about 15 grams/liter. The smut that is formed can be removed from the surface of the turbine component in a manner that does not substantially alter the surface thereof.
摘要翻译：一种用于从涡轮机部件，特别是涡轮盘和涡轮轴中去除发动机沉积物的方法和清洁组合物。该方法包括以下步骤：（a）提供具有其上具有发动机沉积物的表面的涡轮机部件，其中所述涡轮机部件包括含镍和/或钴的贱金属; 和（b）用清洁组合物处理涡轮机部件的表面，以将发动机沉积物转化为可移除的污物，而基本上不会蚀刻涡轮机部件的基体金属。清洁组合物包含基本上不含乙酸的水溶液，其包含：硝酸根离子重量的硝酸根离子源为约470至约710克/升; 和二氟离子源的量为约0.5至约15克/升的二氟离子源。形成的污迹可以以不大体上改变其表面的方式从涡轮机部件的表面移除。

6. 发明授权

US08245981B2 Ice shed reduction for leading edge structures 有权
标题翻译：前缘结构的减少冰川
公开(公告)号：US08245981B2
公开(公告)日：2012-08-21
申请号：US12112733
申请日：2008-04-30
申请人： Edward Atwood Rainous , Barry Lynn Allmon , Jeffre Gerry Loewe , William Clarke Brooks , Lee Alan Blanton , Courtney James Tudor , Vicky Showalter Budinger
发明人： Edward Atwood Rainous , Barry Lynn Allmon , Jeffre Gerry Loewe , William Clarke Brooks , Lee Alan Blanton , Courtney James Tudor , Vicky Showalter Budinger
IPC分类号： B64C21/00 , B64C1/38
CPC分类号： B64D15/00 , B64D33/02 , B64D2033/0233 , B64D2033/0286 , F01D9/04 , F01D25/02 , F01D25/162 , F02C7/047 , F05D2300/50212
摘要： A leading edge structure for use in an aerospace vehicle includes a body having a flowpath surface which defines a leading edge adapted to face an air flow during operation, and an opposed inner surface. The body is segmented into a plurality of portions having varying thermal properties and/or mechanical discontinuities, so as to promote stress concentrations in ice attached to the flowpath surface.
摘要翻译：用于航空航天车辆的前缘结构包括具有流动路径表面的主体，其限定了在操作期间适于面对空气流的前缘以及相对的内表面。主体被分割成具有变化的热性能和/或机械不连续性的多个部分，以促进附着在流路表面上的冰中的应力集中。

7. 发明授权

US08038894B2 Method of selectively stripping an engine-run ceramic coating 有权
标题翻译：选择性剥离发动机运行的陶瓷涂层的方法
公开(公告)号：US08038894B2
公开(公告)日：2011-10-18
申请号：US11564639
申请日：2006-11-29
申请人： William Clarke Brooks
发明人： William Clarke Brooks
IPC分类号： B44C1/22
CPC分类号： C23G1/085 , B24C1/086 , C04B35/486 , C04B35/6306 , C04B2235/3241 , C04B2235/40 , C23F1/16
摘要： A process for selectively stripping a coating from a component of a turbomachine, and particularly a coating having a ceramic matrix that contains metallic particles dispersed therein that render the coating more difficult to remove from the component after the component has been subjected to elevated temperatures during operation of the turbomachine. The process generally includes immersing the component in an aqueous solution containing ferric chloride, nitric acid, and phosphoric acid, for a duration sufficient to attack the metallic particles in the coating. The component is then removed from the aqueous solution and its surface rinsed of the aqueous solution. The immersing and removing steps are then sequentially repeated a sufficient number of times to sufficiently attack the metallic particles to enable the coating to be mechanically removed from the component.
摘要翻译：一种用于从涡轮机组件选择性地剥离涂层的方法，特别是具有包含分散在其中的金属颗粒的陶瓷基体的涂层，其使得在组件在操作期间经受高温之后更难以从组件移除的涡轮机。该方法通常包括将组分浸入含有氯化铁，硝酸和磷酸的水溶液中持续足够时间以侵蚀涂层中的金属颗粒。然后从水溶液中除去组分，并将其表面漂洗水溶液。然后将浸渍和去除步骤顺序地重复足够的次数以充分攻击金属颗粒，以使涂层能够从组件机械地移除。

8. 发明授权

US07992823B2 Ice shed reduction for leading edge structures 有权
标题翻译：前缘结构的减少冰川
公开(公告)号：US07992823B2
公开(公告)日：2011-08-09
申请号：US12112660
申请日：2008-04-30
申请人： Edward Atwood Rainous , Barry Lynn Allmon , Jeffre Gerry Loewe , William Clarke Brooks , Lee Alan Blanton , Courtney James Tudor , Vicky Showalter Budinger
发明人： Edward Atwood Rainous , Barry Lynn Allmon , Jeffre Gerry Loewe , William Clarke Brooks , Lee Alan Blanton , Courtney James Tudor , Vicky Showalter Budinger
IPC分类号： B64D15/00
CPC分类号： B64D15/00
摘要： A leading edge structure for use in an aerospace vehicle includes a body having a flowpath surface which defines a leading edge adapted to face an air flow during operation; and a metallic icephobic plating comprising nickel applied to at least a portion of the flowpath surface.
摘要翻译：用于航空航天车辆的前缘结构包括具有流动路径表面的主体，其限定在操作期间适于面对空气流的前缘; 以及包含施加到所述流路表面的至少一部分的镍的金属冰敷电镀。

9. 发明授权

US07687449B2 Composition for removing engine deposits from turbine components 有权
标题翻译：用于从涡轮机部件移除发动机沉积物的组合物
公开(公告)号：US07687449B2
公开(公告)日：2010-03-30
申请号：US11523643
申请日：2006-09-20
申请人： John Matthew Powers , William Clarke Brooks
发明人： John Matthew Powers , William Clarke Brooks
IPC分类号： C11D7/08 , C11D7/02 , C11D1/00 , C11D3/26
CPC分类号： C11D3/046 , C11D3/042 , C11D3/048 , C11D7/08 , C11D7/10 , C11D7/105 , C11D11/0041 , C23G1/10
摘要： A method and cleaning composition for removing engine deposits from turbine components, in particular turbine disks and turbine shafts. This method comprises the following steps: (a) providing a turbine component having a surface with engine deposits thereon, wherein the turbine component comprises a nickel and/or cobalt-containing base metal; and (b) treating the surface of the turbine component with a cleaning composition to convert the engine deposits thereon to a removable smut without substantially etching the base metal of the turbine component. The cleaning composition comprises an aqueous solution that is substantially free of acetic acid and comprising: a nitrate ion source in an amount, by weight of the nitrate ion, of from about 470 to about 710 grams/liter; and a bifluoride ion source in an amount, by weight of the bifluoride ion, of from about 0.5 to about 15 grams/liter. The smut that is formed can be removed from the surface of the turbine component in a manner that does not substantially alter the surface thereof.
摘要翻译：一种用于从涡轮机部件，特别是涡轮盘和涡轮轴中去除发动机沉积物的方法和清洁组合物。该方法包括以下步骤：（a）提供具有其上具有发动机沉积物的表面的涡轮机部件，其中所述涡轮机部件包括含镍和/或钴的贱金属; 和（b）用清洁组合物处理涡轮机部件的表面，以将发动机沉积物转化为可移除的污物，而基本上不会蚀刻涡轮机部件的基体金属。清洁组合物包含基本上不含乙酸的水溶液，其包含：硝酸根离子重量的硝酸根离子源为约470至约710克/升; 和二氟离子源的量为约0.5至约15克/升的二氟离子源。形成的污迹可以以不大体上改变其表面的方式从涡轮机部件的表面去除。

10. 发明授权

US06379749B2 Method of removing ceramic coatings 有权
标题翻译：去除陶瓷涂层的方法
公开(公告)号：US06379749B2
公开(公告)日：2002-04-30
申请号：US09730373
申请日：2000-12-05
申请人： Robert George Zimmerman, Jr. , William Clarke Brooks , Roger Dale Wustman , John Douglas Evans, Sr.
发明人： Robert George Zimmerman, Jr. , William Clarke Brooks , Roger Dale Wustman , John Douglas Evans, Sr.
IPC分类号： B05D310
CPC分类号： C23G1/10 , B23P2700/06 , C23C4/02
摘要： A method of removing a ceramic coating (18), and particularly zirconia-containing thermal barrier coating (TBC) materials such as yttria-stabilized zirconia (YSZ), that has been either intentionally or unintentionally deposited on the surface of a component (10). The method entails subjecting the ceramic coating (18) to an aqueous solution containing an acid fluoride salt, such as ammonium bifluoride (NH4HF2) or sodium bifluoride (NaHF2), and a corrosion inhibitor. The method is capable of completely removing the ceramic coating (18) without removing or damaging the underlying substrate material, which may include a metallic bond coat (16).
摘要翻译：已经有意或无意沉积在组件（10）的表面上的去除陶瓷涂层（18），特别是含氧化锆的热障涂层（TBC）材料如氧化钇稳定的氧化锆（YSZ）的方法，。该方法需要使陶瓷涂层（18）经受含氟化氢盐如氟化氢铵（NH 4 HF 2）或氟化氢钠（NaHF 2）的水溶液和腐蚀抑制剂。该方法能够完全去除陶瓷涂层（18），而不会移除或损坏可能包括金属粘结涂层（16）的下面的基底材料。

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