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1.发明授权Method of producing and joining superalloy balls by means of brazing and objects produced with such joints 有权通过钎焊和用这种接头生产的物体制造和接合超级合金球的方法公开(公告)号：US07968207B2
公开(公告)日：2011-06-28
申请号：US11988345
申请日：2006-07-07
申请人： Myriam Douin , Marie-Pierre Bacos , Alexandra Boyer , Aurélie Gregoire , Pierre Josso , Sébastien Mercier , Ariel Moriel , Jason Nadler , Serge Naveos , Catherine Rio
发明人： Myriam Douin , Marie-Pierre Bacos , Alexandra Boyer , Aurélie Gregoire , Pierre Josso , Sébastien Mercier , Ariel Moriel , Jason Nadler , Serge Naveos , Catherine Rio
IPC分类号： B22F3/11 , B22F1/00 , B22F1/02 , G10K11/162
CPC分类号： B22F1/0051 , B22F1/025 , B22F3/1112 , B23K1/0008 , B23K35/02 , B23K35/0244 , Y10T428/12181 , Y10T428/12479 , Y10T428/12493
摘要： The invention relates to a method of producing and joining superalloy balls by means of brazing and to objects produced with such joints. According to one aspect of the invention, an alloy powder covered with a brazing solder is bonded to a spherical core and subsequently transformed into a continuous alloy layer by means of brazing.
摘要翻译： 本发明涉及通过钎焊制造和接合超级合金球的方法以及用这种接头制造的物体。 根据本发明的一个方面，用钎焊焊料覆盖的合金粉末与球形核接合，随后通过钎焊转变为连续的合金层。
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2.发明申请Method of Producing and Joining Superalloy Balls By Means of Brazing and Objects Produced With Such Joints 有权通过钎焊和生产这种接头的物体生产和连接超合金球的方法公开(公告)号：US20090130478A1
公开(公告)日：2009-05-21
申请号：US11988345
申请日：2006-07-07
申请人： Myriam Douin , Marie-Pierre Bacos , Alexandra Boyer , Aurelie Gregoire , Pierre Josso , Sebastien Mercier , Ariel Moriel , Jason Nadler , Serge Naveos , Catherine Rio
发明人： Myriam Douin , Marie-Pierre Bacos , Alexandra Boyer , Aurelie Gregoire , Pierre Josso , Sebastien Mercier , Ariel Moriel , Jason Nadler , Serge Naveos , Catherine Rio
CPC分类号： B22F1/0051 , B22F1/025 , B22F3/1112 , B23K1/0008 , B23K35/02 , B23K35/0244 , Y10T428/12181 , Y10T428/12479 , Y10T428/12493
摘要： The invention relates to a method of producing and joining superalloy balls by means of brazing and to objects produced with such joints. According to the invention, an alloy powder covered with a brazing solder is bonded to a spherical core and subsequently transformed into a continuous alloy layer by means of brazing.
摘要翻译： 本发明涉及通过钎焊制造和接合超级合金球的方法以及用这种接头制造的物体。 根据本发明，用钎焊焊料覆盖的合金粉末与球形核接合，随后通过钎焊转变为连续的合金层。
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公开(公告)号：US07749614B2
公开(公告)日：2010-07-06
申请号：US10566052
申请日：2004-07-15
CPC分类号： B23K1/0008 , B23K20/233 , B23K35/004 , B23K35/005 , B23K35/3033 , B23K2103/14 , B23K2103/18 , B23K2103/26 , Y10T428/12806 , Y10T428/12944 , Y10T428/31678
摘要： The invention relates to a method of brazing a Ti—Al alloy. According to the invention, a layer of nickel (2) is disposed between a part (1) which is made from titanium aluminide and a brazing sheet (3), such as to enable: the aforementioned part (1) to be brazed to another metallic material (4) without the aluminium diffusing from one to the other; and a stable link with good mechanical strength to be produced. The invention can be used for the assembly of aircraft engine parts which are made from titanium aluminide and nickel-based superalloy.
摘要翻译： 本发明涉及一种钎焊Ti-Al合金的方法。 根据本发明，在由铝化钛制成的部分（1）和钎焊片（3）之间设置一层镍（2），以使上述部分（1）钎焊到另一个 金属材料（4），铝不会从一个扩散到另一个; 并具有良好机械强度的稳定连接。 本发明可用于组装由钛铝化物和镍基超级合金制成的飞机发动机部件。
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公开(公告)号：US20070281175A1
公开(公告)日：2007-12-06
申请号：US10566052
申请日：2004-07-15
IPC分类号： B23K20/233 , B23K1/00 , B23K35/00
CPC分类号： B23K1/0008 , B23K20/233 , B23K35/004 , B23K35/005 , B23K35/3033 , B23K2103/14 , B23K2103/18 , B23K2103/26 , Y10T428/12806 , Y10T428/12944 , Y10T428/31678
摘要： The invention relates to a method of brazing a Ti—Al alloy. According to the invention, a layer of nickel (2) is disposed between a part (1) which is made from titanium aluminide and a brazing sheet (3), such as to enable: the aforementioned part (1) to be brazed to another metallic material (4) without the aluminium diffusing from one to the other; and a stable link with good mechanical strength to be produced. The invention can be used for the assembly of aircraft engine parts which are made from titanium aluminide and nickel-based superalloy.
摘要翻译： 本发明涉及一种钎焊Ti-Al合金的方法。 根据本发明，在由铝化钛制成的部分（1）和钎焊片（3）之间设置一层镍（2），以使上述部分（1）钎焊到另一个 金属材料（4），铝不会从一个扩散到另一个; 并具有良好机械强度的稳定连接。 本发明可用于组装由钛铝化物和镍基超级合金制成的飞机发动机部件。
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5.发明授权Process for forming a protective coating containing aluminium and zirconium on a metal 有权在金属上形成含有铝和锆的保护涂层的方法公开(公告)号：US07608301B2
公开(公告)日：2009-10-27
申请号：US10815526
申请日：2004-03-31
申请人： Marie-Pierre Bacos , Pierre Josso , Serge Naveos
发明人： Marie-Pierre Bacos , Pierre Josso , Serge Naveos
摘要： This relates to an improvement to the process of aluminization or activated cementation in which a donor cement containing the aluminium is attacked at high temperature and in a neutral or reducing atmosphere by a gaseous ammonium halide to form a gaseous aluminium halide which decomposes on contact with a nickel-based substrate depositing aluminium metal thereon.According to the invention the aluminium halide is at least partly replaced by a zirconium halide leading to the inclusion of zirconium in the deposit.Improvement in the protection of the hot parts of aircraft engines made of nickel-based superalloy.No figure is to be published.
摘要翻译： 这涉及对铝化或活化胶结过程的改进，其中含有铝的供体水泥在高温下和中性或还原性气氛中被气态卤化铵侵蚀以形成气态卤化铝，其在与 镍基基板上沉积铝金属。 根据本发明，卤化铝至少部分地被卤化锆代替，导致在沉积物中包含锆。 改善镍基超级合金制造的飞机发动机热部件的保护。 没有数字要出版。
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公开(公告)号：US20100221570A1
公开(公告)日：2010-09-02
申请号：US12087025
申请日：2006-12-21
申请人： Jason Nadler , Florin Paun , Pierre Josso , Marie-Pierre Bacos , Stéphane Gasser
发明人： Jason Nadler , Florin Paun , Pierre Josso , Marie-Pierre Bacos , Stéphane Gasser
CPC分类号： G10K11/16 , Y10T29/496 , Y10T29/4998 , Y10T428/12361 , Y10T428/12479 , Y10T428/24628 , Y10T428/249921
摘要： A structural element used for attenuating aviation turbine noise is provided with pores (1, 2) embodied in the form of cylindrical channels which are open on the first ends inside the turbine housing and closed on the opposite ends thereof, wherein the diameter (D) of each channel ranges approximately from 0.1 to 0.3 mm, each channel is remote at least along one part of the length thereof from the closest neighbours at a minimum distance ranging approximately from 0.02 to 0.3 mm and the ratio between the channel length and diameter thereof is of the order of 102.
摘要翻译： 用于衰减航空涡轮机噪声的结构元件设置有以圆柱形通道形式实现的孔（1,2），其在涡轮壳体内的第一端开口并在其相对端封闭，其中直径（D） 每个通道的范围大约为0.1至0.3mm，每个通道至少沿距离最近的邻近部分的距离的一部分距离约0.02至0.3mm的最小距离，并且通道长度和直径之间的比率 的等级为102。
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7.发明申请公开(公告)号：US20070108255A1
公开(公告)日：2007-05-17
申请号：US11482500
申请日：2006-07-07
申请人： Jason Nadler , Pierre Josso , Marie-Pierre Bacos , Florin Paun
发明人： Jason Nadler , Pierre Josso , Marie-Pierre Bacos , Florin Paun
IPC分类号： A47J36/02
CPC分类号： B22F1/0096 , B22F1/0051 , B22F2998/10 , B22F1/0062 , B22F1/0074 , B22F2201/20 , B22F1/0085 , B22F3/1039 , B22F2201/013
摘要： Hollow metal spheres are heated in a high vacuum in the presence of an organic substance, at a temperature at least equal to the melting point of a eutectic between carbon and the metallic constituents of the said spheres.
摘要翻译： 在有机物质存在下，在至少等于碳与所述球体的金属组分之间共晶的熔点的温度下，在高真空中加热空心金属球。
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8.发明授权公开(公告)号：US07544322B2
公开(公告)日：2009-06-09
申请号：US11482500
申请日：2006-07-07
申请人： Jason Nadler , Pierre Josso , Marie-Pierre Bacos , Florin Paun
发明人： Jason Nadler , Pierre Josso , Marie-Pierre Bacos , Florin Paun
CPC分类号： B22F1/0096 , B22F1/0051 , B22F2998/10 , B22F1/0062 , B22F1/0074 , B22F2201/20 , B22F1/0085 , B22F3/1039 , B22F2201/013
摘要： Hollow metal spheres are heated in a high vacuum in the presence of an organic substance, at a temperature at least equal to the melting point of a eutectic between carbon and the metallic constituents of the said spheres.
摘要翻译： 在有机物质存在下，在至少等于碳与所述球体的金属组分之间共晶的熔点的温度下，在高真空中加热空心金属球。
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公开(公告)号：US07963364B2
公开(公告)日：2011-06-21
申请号：US12087025
申请日：2006-12-21
申请人： Jason Nadler , Florin Paun , Pierre Josso , Marie-Pierre Bacos , Stéphane Gasser
发明人： Jason Nadler , Florin Paun , Pierre Josso , Marie-Pierre Bacos , Stéphane Gasser
IPC分类号： G10K11/16
CPC分类号： G10K11/16 , Y10T29/496 , Y10T29/4998 , Y10T428/12361 , Y10T428/12479 , Y10T428/24628 , Y10T428/249921
摘要： A structural element used for attenuating aviation turbine noise is provided with pores (1, 2) embodied in the form of cylindrical channels which are open on the first ends inside the turbine housing and closed on the opposite ends thereof, wherein the diameter (D) of each channel ranges approximately from 0.1 to 0.3 mm, each channel is remote at least along one part of the length thereof from the closest neighbors at a minimum distance ranging approximately from 0.02 to 0.3 mm and the ratio between the channel length and diameter thereof is of the order of 102.
摘要翻译： 用于衰减航空涡轮机噪声的结构元件设置有以圆柱形通道形式实现的孔（1,2），其在涡轮壳体内的第一端开口并在其相对端封闭，其中直径（D） 每个通道的范围大约为0.1至0.3mm，每个通道至少沿距离最近的邻近部分的距离的一部分距离约0.02至0.3mm的最小距离，并且通道长度和直径之间的比率 的等级为102。
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公开(公告)号：US20070071991A1
公开(公告)日：2007-03-29
申请号：US11345807
申请日：2006-02-01
申请人： Marie-Pierre Bacos , Pierre Josso
发明人： Marie-Pierre Bacos , Pierre Josso
CPC分类号： C25D5/34 , C25D5/10 , C25D5/38 , Y10T428/12458 , Y10T428/12743 , Y10T428/1284 , Y10T428/12944
摘要： In order to protect a monocrystalline superalloy rich in rhenium against corrosion whilst avoiding the formation of progressive secondary reaction zones, a layer (3) formed of tungsten and cobalt is deposited on its surface before aluminisation treatment.
摘要翻译： 为了保护富含铼的单晶超合金免受腐蚀，同时避免形成进行的次级反应区，在镀铝处理之前，由钨和钴形成的层（3）沉积在其表面上。
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