专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20050150578A1 Metallurgical product and structure member for aircraft made of Al-Zn-Cu-Mg alloy 审中-公开
标题翻译：由Al-Zn-Cu-Mg合金制成的飞机冶金产品和结构件
公开(公告)号：US20050150578A1
公开(公告)日：2005-07-14
申请号：US11012358
申请日：2004-12-16
申请人： Bernard Bes , Vic Dangerfield , David Dumont , Jean-Christophe Ehrstrom , Timothy Warner
发明人： Bernard Bes , Vic Dangerfield , David Dumont , Jean-Christophe Ehrstrom , Timothy Warner
IPC分类号： C22C21/10 , C22F1/053
CPC分类号： C22C21/10 , C22F1/053
摘要： The present invention relates to a work-hardened product, and particularly a rolled, extruded and/or forged product made of an alloy with composition (% by weight): Zn 6.7-7.3% Cu 1.9-2.5% Mg 1.0-2.0% Zr 0.04-0.15% Fe ≦0.15 Si ≦0.15 other elements ≦0.05 each and ≦0.15 total, remainder aluminium and wherein Mg/Cu
摘要翻译：本发明涉及一种加工硬化产品，特别涉及一种由具有组成（重量％）的合金制成的轧制，挤出和/或锻造产品：Zn 6.7-7.3％Cu 1.9-2.5％Mg 1.0-2.0％Zr 0.04-0.15％Fe <= 0.15 Si <= 0.15其他元素<= 0.05，总共<0.15，余量为铝，其中Mg / Cu <1。该产品优选通过固溶热处理，淬火，冷加工和人造时效处理。冷加工可以通过受控的张力和/或冷转化来实现，例如轧制或拉伸。该产品可以用作例如飞机结构件。

2. 发明授权

US07087317B2 Composite laminated aluminum-glass fiber sandwich panels 有权
标题翻译：复合层压铝玻璃纤维夹层板
公开(公告)号：US07087317B2
公开(公告)日：2006-08-08
申请号：US10669502
申请日：2003-09-25
申请人： Jean-Christophe Ehrstrom , Timothy Warner
发明人： Jean-Christophe Ehrstrom , Timothy Warner
IPC分类号： B32B15/04 , B32B15/08 , B32B15/20
CPC分类号： B64C1/12 , B32B15/08 , B32B15/14 , B64C2001/0072 , Y02T50/43 , Y10T428/12535 , Y10T428/12569 , Y10T428/12736 , Y10T428/12764 , Y10T428/249946 , Y10T428/26 , Y10T428/31522 , Y10T428/31678
摘要： A Glare type composite laminated sandwich panel comprising (i) aluminum (ii) glass fibre with adhesive (iii) aluminum is disclosed. According to the present invention, at least one of the aluminum sheets is preferably made of an aluminum non-heat treatable alloy type Al—Mg with a magnesium content of between 4 and 6%. These sandwich panels have mechanical characteristics similar to sandwich panels comprising sheets with a heat treatable alloy. Panels of the present invention further generally have better corrosion resistance and are less expensive than those made with heat treatable alloys such as 2xxx and 7xxx type alloys.
摘要翻译：公开了一种眩光型复合层压夹层板，其包括（i）铝（ii）具有粘合剂（iii）铝的玻璃纤维。根据本发明，铝板中的至少一个优选由镁含量在4％和6％之间的不可热处理的Al-Mg合金制成。这些夹层板具有类似于包含具有可热处理合金的片材的夹层板的机械特性。本发明的面板通常具有更好的耐腐蚀性，并且比用可热处理的合金如2xxx和7xxx型合金制成的那些更便宜。

3. 发明授权

US07490752B2 Manufacturing method for friction welded aluminum alloy parts 有权
标题翻译：摩擦焊铝合金零件的制造方法
公开(公告)号：US07490752B2
公开(公告)日：2009-02-17
申请号：US10849525
申请日：2004-05-20
申请人： Jean-Christophe Ehrstrom , Timothy Warner
发明人： Jean-Christophe Ehrstrom , Timothy Warner
IPC分类号： B23K20/12
CPC分类号： C22F1/053 , B23K20/122 , B23K2101/18 , B23K2103/10 , C22F1/04 , Y10T428/12493
摘要： A method for manufacturing aluminium alloy parts with precipitation hardening including friction stir welding of at least two elements made from the same alloy or different alloys, solution heat treatment, and quenching of welded parts, in which the elements are subjected to heat treatment before welding at temperature T for at least 2t1, t1 being defined as the minimum treatment duration at temperature T leading to a specific melting peak energy defined by AED equal to less than 1 J/g. A method according to the invention substantially avoids an increase in the grain size following solution heat treatment after welding. The invention further relates to novel aluminum materials as well as uses therefor.
摘要翻译：一种用于制造具有沉淀硬化的铝合金部件的方法，包括由相同合金或不同合金制成的至少两个元件的摩擦搅拌焊接，固溶热处理和焊接部件的淬火，其中元件在焊接之前经受热处理温度T至少为2t1，t1被定义为在温度T下的最小处理持续时间，导致由等于小于1J / g的AED限定的特定熔融峰值能量。根据本发明的方法基本上避免了焊接后的固溶热处理后的晶粒尺寸的增加。本发明还涉及新型铝材料及其用途。

4. 发明申请

US20050037188A1 Composite laminated aluminum-glass fiber sandwich panels 有权
标题翻译：复合层压铝玻璃纤维夹层板
公开(公告)号：US20050037188A1
公开(公告)日：2005-02-17
申请号：US10669502
申请日：2003-09-25
申请人： Jean-Christophe Ehrstrom , Timothy Warner
发明人： Jean-Christophe Ehrstrom , Timothy Warner
IPC分类号： B32B15/08 , B32B15/14 , B64C1/00 , B32B17/02
CPC分类号： B64C1/12 , B32B15/08 , B32B15/14 , B64C2001/0072 , Y02T50/43 , Y10T428/12535 , Y10T428/12569 , Y10T428/12736 , Y10T428/12764 , Y10T428/249946 , Y10T428/26 , Y10T428/31522 , Y10T428/31678
摘要： A Glare type composite laminated sandwich panel comprising (i) aluminum (ii) glass fibre with adhesive (iii) aluminum is disclosed. According to the present invention, at least one of the aluminum sheets is preferably made of an aluminum non-heat treatable alloy type Al—Mg with a magnesium content of between 4 and 6%. These sandwich panels have mechanical characteristics similar to sandwich panels comprising sheets with a heat treatable alloy. Panels of the present invention further generally have better corrosion resistance and are less expensive than those made with heat treatable alloys such as 2xxx and 7xxx type alloys.
摘要翻译：公开了一种眩光型复合层压夹层板，其包括（i）铝（ii）具有粘合剂（iii）铝的玻璃纤维。根据本发明，铝板中的至少一个优选由镁含量在4％和6％之间的不可热处理的Al-Mg合金制成。这些夹层板具有类似于包含具有可热处理合金的片材的夹层板的机械特性。本发明的面板通常具有更好的耐腐蚀性，并且比用可热处理的合金如2xxx和7xxx型合金制成的那些更便宜。

5. 发明申请

US20050011932A1 Manufacturing method for friction welded aluminum alloy parts 有权
标题翻译：摩擦焊铝合金零件的制造方法
公开(公告)号：US20050011932A1
公开(公告)日：2005-01-20
申请号：US10849525
申请日：2004-05-20
申请人： Jean-Christophe Ehrstrom , Timothy Warner
发明人： Jean-Christophe Ehrstrom , Timothy Warner
IPC分类号： B23K20/12 , C22F1/04 , C22F1/053 , C25D5/10
CPC分类号： C22F1/053 , B23K20/122 , B23K2101/18 , B23K2103/10 , C22F1/04 , Y10T428/12493
摘要： A method for manufacturing aluminium alloy parts with precipitation hardening including friction stir welding of at least two elements made from the same alloy or different alloys, solution heat treatment, and quenching of welded parts, in which the elements are subjected to heat treatment before welding at temperature T for at least 2t1, t1 being defined as the minimum treatment duration at temperature T leading to a specific melting peak energy defined by AED equal to less than 1 J/g. A method according to the invention substantially avoids an increase in the grain size following solution heat treatment after welding. The invention further relates to novel aluminum materials as well as uses therefor.
摘要翻译：一种用于制造具有沉淀硬化的铝合金部件的方法，包括由相同合金或不同合金制成的至少两个元件的摩擦搅拌焊接，固溶热处理和焊接部件的淬火，其中元件在焊接之前经受热处理温度T至少为2t1，t1被定义为在温度T下的最小处理持续时间，导致由等于小于1J / g的AED限定的特定熔融峰值能量。根据本发明的方法基本上避免了焊接后的固溶热处理后的晶粒尺寸的增加。本发明还涉及新型铝材料及其用途。

6. 发明申请

US20090184202A1 STRUCTRUAL ELEMENT MADE OF AN ALUMINUM ALLOY INCLUDING AN OPTICAL SENSOR 有权
标题翻译：包含光学传感器的铝合金的结构元件
公开(公告)号：US20090184202A1
公开(公告)日：2009-07-23
申请号：US12050888
申请日：2008-03-18
申请人： Jean-Christophe Ehrstrom , Laurent Cervi , Frank Eberl , Michelle Salvia
发明人： Jean-Christophe Ehrstrom , Laurent Cervi , Frank Eberl , Michelle Salvia
IPC分类号： B64C1/12 , B32B15/04 , B64C3/26 , B21D47/00
CPC分类号： B21K25/00 , B21C23/22 , G01L1/242 , G01M11/083 , G02B6/02057 , G02B6/14 , Y10T29/49616 , Y10T428/249921
摘要： Provided herein is a method for manufacturing a worked product comprising a fiber sensor therein. Also provided is a wrought product comprising a fiber sensor as well as structural elements and other products including fuselage skin and a wing panel.
摘要翻译：本文提供了一种在其中制造包括光纤传感器的加工产品的方法。还提供了一种锻造产品，其包括纤维传感器以及结构元件和包括机身皮肤和翼板的其它产品。

7. 发明申请

US20080265094A1 Structural Element and Method of Manufacture 有权
标题翻译：结构要素和制造方法
公开(公告)号：US20080265094A1
公开(公告)日：2008-10-30
申请号：US12093151
申请日：2006-12-15
申请人： Sjoerd Van Der Veen , Jean-Christophe Ehrstrom , Henri Gerard , Francois Lemaitre
发明人： Sjoerd Van Der Veen , Jean-Christophe Ehrstrom , Henri Gerard , Francois Lemaitre
IPC分类号： B64C3/00 , B21D53/88
CPC分类号： B64C3/185 , B23K20/122 , B23K2101/28 , Y10T29/49622
摘要： In a method for manufacturing a structural element intended for aeronautical construction, at least a first and second metal block are made available, the limit of elasticity under compression of the first metal block being greater than that of the second metal block. The first metal block is machined in such a manner as to obtain a first machined monolithic part which has a first web portion and at least one stringer element whose height is such that a stringer portion extends beyond the first web portion. There is prepared, by shaping the second metal block, at least one second part having at least a second web portion capable of co-operating with the first web portion to form the web. The first monolithic part and the second part are assembled by placing the first and second web portions end-to-end over their entire common length.
摘要翻译：在用于制造用于航空结构的结构元件的方法中，至少第一和第二金属块可用，第一金属块的压缩下的弹性极限大于第二金属块的弹性极限。第一金属块被加工成获得第一加工的整体部分，其具有第一腹板部分和至少一个纵梁元件，其高度使得纵梁部分延伸超出第一腹板部分。通过成形第二金属块来制备至少一个具有至少第二腹板部分的第二部分，该第二腹板部分能够与第一腹板部分协作以形成腹板。通过将第一和第二纤维网部分端对端放置在其整个公共长度上来组装第一整体部分和第二部分。

8. 发明授权

US08091828B2 Structural element and method of manufacture 有权
标题翻译：结构要素及制造方法
公开(公告)号：US08091828B2
公开(公告)日：2012-01-10
申请号：US12093151
申请日：2006-12-15
申请人： Sjoerd Van Der Veen , Jean-Christophe Ehrstrom , Henri Gerard , Francois Lemaitre
发明人： Sjoerd Van Der Veen , Jean-Christophe Ehrstrom , Henri Gerard , Francois Lemaitre
IPC分类号： B64C1/06 , B64C3/18
CPC分类号： B64C3/185 , B23K20/122 , B23K2101/28 , Y10T29/49622
摘要： In a method for manufacturing a structural element intended for aeronautical construction, at least a first and second metal block are made available, the limit of elasticity under compression of the first metal block being greater than that of the second metal block. The first metal block is machined in such a manner as to obtain a first machined monolithic part which has a first web portion and at least one stringer element whose height is such that a stringer portion extends beyond the first web portion. There is prepared, by shaping the second metal block, at least one second part having at least a second web portion capable of co-operating with the first web portion to form the web. The first monolithic part and the second part are assembled by placing the first and second web portions end-to-end over their entire common length.
摘要翻译：在用于制造用于航空结构的结构元件的方法中，至少第一和第二金属块可用，第一金属块的压缩下的弹性极限大于第二金属块的弹性极限。第一金属块被加工成获得第一加工的整体部分，其具有第一腹板部分和至少一个纵梁元件，其高度使得纵梁部分延伸超出第一腹板部分。通过成形第二金属块来制备至少一个具有至少第二腹板部分的第二部分，该第二腹板部分能够与第一腹板部分协作以形成腹板。通过将第一和第二纤维网部分端对端放置在其整个公共长度上来组装第一整体部分和第二部分。

9. 发明授权

US07780802B2 Simplified method for making rolled Al—Zn—Mg alloy products, and resulting products 有权
标题翻译：制造轧制的Al-Zn-Mg合金产品的简化方法以及所得产品
公开(公告)号：US07780802B2
公开(公告)日：2010-08-24
申请号：US10534006
申请日：2003-11-06
申请人： Ronan Dif , Jean-Christophe Ehrstrom , Bernard Grange , Vincent Hochenedel , Hervé Ribes
发明人： Ronan Dif , Jean-Christophe Ehrstrom , Bernard Grange , Vincent Hochenedel , Hervé Ribes
IPC分类号： C22C21/10
CPC分类号： C22C21/10 , C22F1/053
摘要： A process for making Al—Zn—Mg alloy products, and products formed according to such processes are disclosed. The present invention provides a product having an improved compromise between mechanical characteristics and corrosion strength.
摘要翻译：公开了制备Al-Zn-Mg合金产品的方法，以及根据这些方法形成的产品。本发明提供了在机械特性和腐蚀强度之间具有改进的折衷的产品。

10. 发明授权

US08693812B2 Structrual element made of an aluminum alloy including an optical sensor 有权
标题翻译：由包括光学传感器的铝合金制成的结构元件
公开(公告)号：US08693812B2
公开(公告)日：2014-04-08
申请号：US12050888
申请日：2008-03-18
申请人： Jean-Christophe Ehrstrom , Laurent Cervi , Frank Eberl , Michelle Salvia
发明人： Jean-Christophe Ehrstrom , Laurent Cervi , Frank Eberl , Michelle Salvia
IPC分类号： G02B6/00 , G02B6/02
CPC分类号： B21K25/00 , B21C23/22 , G01L1/242 , G01M11/083 , G02B6/02057 , G02B6/14 , Y10T29/49616 , Y10T428/249921
摘要： Provided herein is a method for manufacturing a worked product comprising a fiber sensor therein. Also provided is a wrought product comprising a fiber sensor as well as structural elements and other products including fuselage skin and a wing panel.
摘要翻译：本文提供了一种在其中制造包括光纤传感器的加工产品的方法。还提供了一种锻造产品，其包括纤维传感器以及结构元件和包括机身皮肤和翼板的其它产品。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式