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1. 发明授权

US06258318B1 Weldable, corrosion-resistant AIMG alloys, especially for manufacturing means of transportation 有权
标题翻译：可焊接，耐腐蚀的ALMG合金，特别适用于制造运输工具
公开(公告)号：US06258318B1
公开(公告)日：2001-07-10
申请号：US09530068
申请日：2000-06-14
申请人： Blanka Lenczowski , Rainer Rauh , Dietrich Wieser , Gerhard Tempus
发明人： Blanka Lenczowski , Rainer Rauh , Dietrich Wieser , Gerhard Tempus
IPC分类号： C22C2106
CPC分类号： C22C21/00
摘要： A weldable, corrosion resistant aluminum-magnesium alloy consisting essentially of 3 to 5% by weight magnesium (Mg), 0.05 to 0.15% by weight zirconium (Zr), 0.05 to 0.12% by weight manganese (Mn), 0.01 to 0.2% by weight titanium (Ti), 0.05 to 0.5% by weight of one or more elements selected from the scandium group of the Periodic Table and/or terbium (Tb), wherein at least 0.15% by weight scandium (Sc) is included with or without terbium (Tb) and with or without 0.05 to 0.35% by weight of one or more elements from the lanthanide series, the balance being aluminum (Al), and unavoidable contaminants not exceeding 0.2% by weight silicon (Si).
摘要翻译：一种可焊接的耐腐蚀铝镁合金，其基本上由3至5重量％的镁（Mg），0.05至0.15重量％的锆（Zr），0.05至0.12重量％的锰（Mn），0.01-0.2％的重量的钛（Ti），0.05〜0.5重量％的选自元素周期表钪基和/或铽（Tb）中的一种或多种元素，其中至少0.15重量％的钪（Sc）包括或不含有铽（Tb），以及0.05〜0.35重量％的来自镧系元素的一种或多种元素，余量为铝（Al），不可避免的污染物不超过0.2重量％的硅（Si）。

2. 发明授权

US06315948B1 Weldable anti-corrosive aluminum-magnesium alloy containing a high amount of magnesium, especially for use in automobiles 有权
标题翻译：含镁量高的可焊接防腐铝镁合金，特别适用于汽车
公开(公告)号：US06315948B1
公开(公告)日：2001-11-13
申请号：US09530067
申请日：2000-10-17
申请人： Blanka Lenczowski , Viktor Yelagin , Rainer Rauh , Valeri Zakharov , Yuri Filatov
发明人： Blanka Lenczowski , Viktor Yelagin , Rainer Rauh , Valeri Zakharov , Yuri Filatov
IPC分类号： C22C2106
CPC分类号： C22C21/06
摘要： A weldable, high magnesium-content aluminum-magnesium alloy consisting essentially of at lest 5 to 6% by weight magnesium (Mg), 0.05 to 0.15% by weight zirconium (Zr), 0.7 to 1% by weight manganese (Mn), 0.01 to 0.2% by weight titanium (Ti), 0.005 to 0.5% by weight cerium (Ce), 0.05 to 0.5% by weight of one or more elements selected from the scandium group of the Periodic Table and/or terbium (Tb), wherein at least scandium (Sc) is included with or without terbium (Tb) and with or without 0.05 to 0.45% by weight of an element from the lanthanide series, the balance being aluminum (Al), and unavoidable contaminants not exceeding 0.2% by weight silicon (Si).
摘要翻译：一种可焊接的高镁含量的铝镁合金，其基本上由至少5至6重量％的镁（Mg），0.05至0.15重量％的锆（Zr），0.7至1重量％的锰（Mn），0.01 至0.2重量％的钛（Ti），0.005〜0.5重量％的铈（Ce），0.05〜0.5重量％的选自元素周期表钪基和/或铽（Tb）的一种或多种元素，其中至少钪（Sc）含有或不含铽（Tb），含有或不含有0.05至0.45重量％的来自镧系元素的元素，余量为铝（Al），不可避免的污染物不超过0.2重量％硅（Si）。

3. 发明授权

US06531004B1 Weldable anti-corrosive aluminium-magnesium alloy containing a high amount of magnesium, especially for use in aviation 有权
标题翻译：焊接耐腐蚀的铝镁合金含镁量高，尤其适用于航空
公开(公告)号：US06531004B1
公开(公告)日：2003-03-11
申请号：US09530007
申请日：2000-10-18
申请人： Blanka Lenczowski , Viktor Yelagin , Rainer Rauh , Valeri Zakharov , Yuri Filatov
发明人： Blanka Lenczowski , Viktor Yelagin , Rainer Rauh , Valeri Zakharov , Yuri Filatov
IPC分类号： C22C2106
CPC分类号： C22C21/06
摘要： Weldable, high-magnesium-content aluminum-magnesium alloy consisting of at least 5-6% w/w magnesium (Mg), 0.05-0.15% w/w zirconium (Zr), 0.05-0.12% w/w manganese (Mn), 0.01-0.2% w/w titanium (Ti), 0.05-0.5% w/w of one or more elements from the scandium group and/or terbium (Tb), wherein at least scandium (Sc) is included, 0.1-0.2% w/w copper (Cu) and/or 0.1-0.4% w/w zinc (Zn), along with aluminum (Al), and unavoidable contamination does not exceed 0.1% w/w silicon (Si).
摘要翻译：由镁（Mg），0.05-0.15％w / w锆（Zr），0.05-0.12％w / w锰（Mn）至少为5-6％w / w的可焊接，高镁含量的铝镁合金，，0.01-0.2％w / w钛（Ti），0.05-0.5％w / w的来自钪基和/或铽（Tb）的一种或多种元素，其中至少包含钪（Sc），0.1-0.2 ％w / w铜（Cu）和/或0.1-0.4％w / w锌（Zn）以及铝（Al），不可避免的污染不超过0.1％w / w硅（Si）。

4. 发明申请

US20080115865A1 Aluminum-based alloy and method of fabrication of semiproducts thereof 有权
标题翻译：铝基合金及其半成品的制造方法
公开(公告)号：US20080115865A1
公开(公告)日：2008-05-22
申请号：US12010326
申请日：2008-01-23
申请人： Thomas Pfannen-Mueller , Rainer Rauh , Peter-Juergen Winkler , Roland Lang , Losif Fridlyander , Evgeny Kablov , Vladimir Sandler , Svetlana Borovskikh , Valentin Davydov , Valery Zakharov , Marina Samarina , Viktor Elagin , Leonid Ber
发明人： Thomas Pfannen-Mueller , Rainer Rauh , Peter-Juergen Winkler , Roland Lang , Losif Fridlyander , Evgeny Kablov , Vladimir Sandler , Svetlana Borovskikh , Valentin Davydov , Valery Zakharov , Marina Samarina , Viktor Elagin , Leonid Ber
IPC分类号： C22F1/057
CPC分类号： C22F1/057 , C22C21/14 , C22C21/16 , C22C21/18
摘要： This invention relates to the field of metallurgy, in particular to high strength weldable alloys with low density, of aluminium-copper-lithium system. These alloys can be used in air- and spacecraft engineering. The alloy comprises copper, lithium, zirconium, scandium, silicon, iron, beryllium, and at least one element from the group including magnesium, zinc, manganese, germanium, cerium, yttrium, titanium. A method for fabricating semiproducts is also provided.
摘要翻译：本发明涉及冶金领域，特别涉及铝 - 铜 - 锂系统的低密度高强度可焊合金。这些合金可用于航空和航天器工程。该合金包括铜，锂，锆，钪，硅，铁，铍以及来自镁，锌，锰，锗，铈，钇，钛的至少一种元素。还提供了一种制造半导体的方法。

5. 发明授权

US07597770B2 Aluminum-based alloy and method of fabrication of semiproducts thereof 有权
标题翻译：铝基合金及其半成品的制造方法
公开(公告)号：US07597770B2
公开(公告)日：2009-10-06
申请号：US12010326
申请日：2008-01-23
申请人： Thomas Pfannen-Mueller , Rainer Rauh , Peter-Juergen Winkler , Roland Lang , Iosif Naumovitch Fridlyander , Evgeny Nikolaevitch Kablov , Vladimir Solomonovitch Sandler , Svetlana Nikolaevna Borovskikh , Valentin Georgievitch Davydov , Valery Vladimirovitch Zakharov , Marina Vladimirovna Samarina , Viktor Ignatovitch Elagin , Leonid Borisovitch Ber
发明人： Thomas Pfannen-Mueller , Rainer Rauh , Peter-Juergen Winkler , Roland Lang , Iosif Naumovitch Fridlyander , Evgeny Nikolaevitch Kablov , Vladimir Solomonovitch Sandler , Svetlana Nikolaevna Borovskikh , Valentin Georgievitch Davydov , Valery Vladimirovitch Zakharov , Marina Vladimirovna Samarina , Viktor Ignatovitch Elagin , Leonid Borisovitch Ber
IPC分类号： C22F1/057
CPC分类号： C22F1/057 , C22C21/14 , C22C21/16 , C22C21/18
摘要： This invention relates to the field of metallurgy, in particular to high strength weldable alloys with low density, of aluminium-copper-lithium system. These alloys can be used in air- and spacecraft engineering. The alloy comprises copper, lithium, zirconium, scandium, silicon, iron, beryllium, and at least one element from the group including magnesium, zinc, manganese, germanium, cerium, yttrium, titanium. A method for fabricating semiproducts is also provided.
摘要翻译：本发明涉及冶金领域，特别涉及铝 - 铜 - 锂系统的低密度高强度可焊合金。这些合金可用于航空和航天器工程。该合金包括铜，锂，锆，钪，硅，铁，铍以及来自镁，锌，锰，锗，铈，钇，钛的至少一种元素。还提供了一种制造半导体的方法。

6. 发明申请

US20050271543A1 Aluminum-based alloy and method of fabrication of semiproducts thereof 审中-公开
标题翻译：铝基合金及其半成品的制造方法
公开(公告)号：US20050271543A1
公开(公告)日：2005-12-08
申请号：US10343712
申请日：2001-07-30
申请人： Thomas Pfannen-Mueller , Rainer Rauh , Peter-Juergen Winkler , Roland Lang , Iosif Fridlyander , Evgeny Kablov , Vladimir Sandler , Svetlana Borovskikh , Valentin Davydov , Valery Zakharov , Marina Samarina , Viktor Elagin , Leonid Ber
发明人： Thomas Pfannen-Mueller , Rainer Rauh , Peter-Juergen Winkler , Roland Lang , Iosif Fridlyander , Evgeny Kablov , Vladimir Sandler , Svetlana Borovskikh , Valentin Davydov , Valery Zakharov , Marina Samarina , Viktor Elagin , Leonid Ber
IPC分类号： C22C21/12 , C22C21/14 , C22C21/16 , C22C21/18 , C22F1/00 , C22F1/057 , C22F1/04
CPC分类号： C22F1/057 , C22C21/14 , C22C21/16 , C22C21/18
摘要： This invention relates to the field of metallurgy, in particular to high strength weldable alloy with low density, of aluminium-copper-lithium system. Said invention can be used in air- and spacecraft engineering. The suggested alloy comprises copper, lithium, zirconium, scandium, silicon, iron, beryllium, and at least one element from the group including magnesium, zinc, manganese, germanium, cerium, yttrium, titanium. Also there is suggested the method for fabrication of semiproducts' which method comprising heating the as-cast billet prior to rolling, hot rolling, solid solution treatment and water quenching, stretching and three-stage artificial ageing.
摘要翻译：本发明涉及冶金领域，特别涉及铝 - 铜 - 锂系统的低密度高强度可焊合金。所述发明可用于航空和航天器工程。所提出的合金包括铜，锂，锆，钪，硅，铁，铍以及来自镁，锌，锰，锗，铈，钇，钛的至少一种元素。还提出了半导体制造方法，该方法包括在轧制，热轧，固溶处理和水淬，拉伸和三阶段人工老化之前加热铸坯。

7. 发明授权

US06346132B1 High-strength, high-damping metal material and method of making the same 失效
标题翻译：高强度，高阻尼金属材料及其制造方法
公开(公告)号：US06346132B1
公开(公告)日：2002-02-12
申请号：US09595359
申请日：2000-06-15
申请人： Ulrike Huber , Rainer Rauh , Eduard Arzt
发明人： Ulrike Huber , Rainer Rauh , Eduard Arzt
IPC分类号： B22F102
CPC分类号： B22F1/0003 , B22F2998/00 , C22C1/0416 , C22C49/06 , C22F1/006 , B22F3/14 , B22F3/15 , B22F3/17 , B22F3/20 , C22C47/14
摘要： A composite material includes a metallic second phase dispersed in a metallic matrix material. The metallic second phase has a grain structure that is at least partially martensitic. The second phase material is preferably an alloy of nickel and titanium, each present in the range from 48 to 52 atomic %, optionally in combination with further additives. The second phase particles can be present in the form of granular particles, wires, fibers, whiskers, or layers, making up 5 to 60 vol. % of the overall composite material. The matrix material is preferably an aluminum alloy. The composite material has a high damping capacity and a high tensile strength provided by the matrix, and a high damping capacity provided by the second phase. A method of making the composite material involves mixing a powdery matrix material and a powdery second phase material, and then heat and consolidating the mixture at a temperature of 400 to 700 ° C. and a pressure of 100 to 300 MPa.
摘要翻译：复合材料包括分散在金属基体材料中的金属第二相。金属第二相具有至少部分马氏体的晶粒结构。第二相材料优选为镍和钛的合金，各自存在于48至52原子％的范围内，任选地与其它添加剂组合。第二相颗粒可以粒状颗粒，电线，纤维，晶须或层的形式存在，构成5至60体积％。％的整体复合材料。基质材料优选为铝合金。复合材料具有高的阻尼能力和由基体提供的高拉伸强度，以及由第二相提供的高阻尼能力。制造复合材料的方法包括混合粉末状基体材料和粉末状第二相材料，然后在400-700℃的温度和100-300MPa的压力下加热和固结混合物。

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