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1. 发明授权

US08673209B2 Aluminum alloy products having improved property combinations and method for artificially aging same 有权
标题翻译：铝合金产品具有改善的性能组合和人造老化方法
公开(公告)号：US08673209B2
公开(公告)日：2014-03-18
申请号：US11748021
申请日：2007-05-14
申请人： Gary H. Bray , Dhurba J. Chakrabarti , Diana Denzer , Jen Lin , John Newman , Greg Venema , Cagatay Yanar
发明人： Gary H. Bray , Dhurba J. Chakrabarti , Diana Denzer , Jen Lin , John Newman , Greg Venema , Cagatay Yanar
IPC分类号： C22F1/053 , C22C21/10
CPC分类号： B64C3/182 , B64C3/185 , B64C3/187 , B64C3/26 , B64C2001/0081 , C22C21/10 , C22F1/053 , Y02T50/42
摘要： Aluminum alloy products about 4 inches thick or less that possesses the ability to achieve, when solution heat treated, quenched, and artificially aged, and in parts made from the products, an improved combination of strength, fracture toughness and corrosion resistance, the alloy consisting essentially of: about 6.8 to about 8.5 wt. % Zn, about 1.5 to about 2.00 wt. % Mg, about 1.75 to about 2.3 wt. % Cu; about 0.05 to about 0.3 wt. % Zr, less than about 0.1 wt. % Mn, less than about 0.05 wt. % Cr, the balance Al, incidental elements and impurities and a method for making same. The invention alloy is useful in making structural members for commercial airplanes including, but not limited to, upper wing skins and stringers, spar caps, spar webs and ribs of either built-up or integral construction. The invention alloy may be aged by 2 or 3 step practices while exceeding the SCC requirements for applications for which the invention alloy is primarily intended. The flexibility of the invention in this regard is useful for its application in multi-alloy or multi-material systems joined by welding or bonding and subsequently aged.
摘要翻译：约4英寸厚或以下的铝合金产品具有在固溶热处理，淬火和人工老化的同时实现的能力，以及由产品制成的零件中，改进了强度，断裂韧性和耐腐蚀性的组合，该合金组成基本上为：约6.8至约8.5wt。％Zn，约1.5至约2.00wt。％Mg，约1.75至约2.3wt。％Cu; 约0.05至约0.3wt。％Zr，小于约0.1wt。％Mn，小于约0.05wt。％Cr，余量为Al，附带元素和杂质及其制备方法。本发明合金可用于制造商用飞机的结构构件，包括但不限于上部翼皮和桁条，翼梁盖，翼梁腹板和构成或整体结构的肋。本发明合金可以通过2或3步骤的方式老化，同时超过本发明合金主要用途的应用的SCC要求。在这方面，本发明的灵活性对于其在通过焊接或粘合并随后老化而连接的多合金或多材料体系中的应用是有用的。

2. 发明申请

US20080283163A1 Aluminum Alloy Products Having Improved Property Combinations and Method for Artificially Aging Same 有权
标题翻译：具有改进的性能组合的铝合金产品和人造老化的方法相同
公开(公告)号：US20080283163A1
公开(公告)日：2008-11-20
申请号：US11748021
申请日：2007-05-14
申请人： Gary H. Bray , Dhruba J. Chakrabarti , Diana Denzer , Jen Lin , John Newman , Greg Venema , Cagatay Yanar
发明人： Gary H. Bray , Dhruba J. Chakrabarti , Diana Denzer , Jen Lin , John Newman , Greg Venema , Cagatay Yanar
IPC分类号： C22F1/053 , C22C21/10
CPC分类号： B64C3/182 , B64C3/185 , B64C3/187 , B64C3/26 , B64C2001/0081 , C22C21/10 , C22F1/053 , Y02T50/42
摘要： Aluminum alloy products about 4 inches thick or less that possesses the ability to achieve, when solution heat treated, quenched, and artificially aged, and in parts made from the products, an improved combination of strength, fracture toughness and corrosion resistance, the alloy consisting essentially of: about 6.8 to about 8.5 wt. % Zn, about 1.5 to about 2.00 wt. % Mg, about 1.75 to about 2.3 wt. % Cu; about 0.05 to about 0.3 wt. % Zr, less than about 0.1 wt. % Mn, less than about 0.05 wt. % Cr, the balance Al, incidental elements and impurities and a method for making same. The invention alloy is useful in making structural members for commercial airplanes including, but not limited to, upper wing skins and stringers, spar caps, spar webs and ribs of either built-up or integral construction. The invention alloy may be aged by 2 or 3 step practices while exceeding the SCC requirements for applications for which the invention alloy is primarily intended. The flexibility of the invention in this regard is useful for its application in multi-alloy or multi-material systems joined by welding or bonding and subsequently aged.
摘要翻译：约4英寸厚或以下的铝合金产品具有在固溶热处理，淬火和人工老化的同时实现的能力，以及由产品制成的零件中，改进了强度，断裂韧性和耐腐蚀性的组合，该合金组成基本上为：约6.8至约8.5wt。％Zn，约1.5至约2.00wt。％Mg，约1.75至约2.3wt。％Cu; 约0.05至约0.3wt。％Zr，小于约0.1wt。％Mn，小于约0.05wt。％Cr，余量为Al，附带元素和杂质及其制备方法。本发明合金可用于制造商用飞机的结构构件，包括但不限于上部翼皮和桁条，翼梁盖，翼梁腹板和构成或整体结构的肋。本发明合金可以通过2或3步骤的方式老化，同时超过本发明合金主要用途的应用的SCC要求。在这方面，本发明的灵活性对于其在通过焊接或粘合并随后老化而连接的多合金或多材料体系中的应用是有用的。

3. 发明授权

US08840737B2 Aluminum alloy products having improved property combinations and method for artificially aging same 有权
标题翻译：铝合金产品具有改善的性能组合和人造老化方法
公开(公告)号：US08840737B2
公开(公告)日：2014-09-23
申请号：US12152635
申请日：2008-05-14
申请人： Gary H. Bray , Dhruba J. Chakrabarti , Diana K. Denzer , Jen C. Lin , John Newman , Gregory B. Venema , Cagatay Yanar , Julien Boselli
发明人： Gary H. Bray , Dhruba J. Chakrabarti , Diana K. Denzer , Jen C. Lin , John Newman , Gregory B. Venema , Cagatay Yanar , Julien Boselli
IPC分类号： C22C21/10 , B64C3/26 , C22F1/053 , B64C3/18 , B64C1/00
CPC分类号： C22F1/053 , B64C3/182 , B64C3/185 , B64C3/187 , B64C3/26 , B64C2001/0081 , C22C21/10 , Y02T50/42
摘要： Aluminum alloy products about 4 inches thick or less that possesses the ability to achieve, when solution heat treated, quenched, and artificially aged, and in parts made from the products, an improved combination of strength, fracture toughness and corrosion resistance, the alloy consisting essentially of: about 6.8 to about 8.5 wt. % Zn, about 1.5 to about 2.00 wt. % Mg, about 1.75 to about 2.3 wt. % Cu; about 0.05 to about 0.3 wt. % Zr, less than about 0.1 wt. % Mn, less than about 0.05 wt. % Cr, the balance Al, incidental elements and impurities and a method for making same. The instantly disclosed alloys are useful in making structural members for commercial airplanes including, but not limited to, upper wing skins and stringers, spar caps, spar webs and ribs of either built-up or integral construction.
摘要翻译：约4英寸厚或以下的铝合金产品具有在固溶热处理，淬火和人工老化的同时实现的能力，以及由产品制成的零件中，改进了强度，断裂韧性和耐腐蚀性的组合，该合金组成基本上为：约6.8至约8.5wt。％Zn，约1.5至约2.00wt。％Mg，约1.75至约2.3wt。％Cu; 约0.05至约0.3wt。％Zr，小于约0.1wt。％Mn，小于约0.05wt。％Cr，余量为Al，附带元素和杂质及其制备方法。瞬时公开的合金可用于制造商用飞机的结构构件，包括但不限于上部翼皮和桁条，翼梁盖，翼梁腹板和构成或整体结构的肋。

4. 发明申请

US20100037998A1 Aluminum alloy products having improved property combinations and method for artificially aging same 有权
标题翻译：铝合金产品具有改善的性能组合和人造老化方法
公开(公告)号：US20100037998A1
公开(公告)日：2010-02-18
申请号：US12152635
申请日：2008-05-14
申请人： Gary H. Bray , Dhruba J. Chakrabarti , Diana K. Denzer , Jen C. Lin , John Newman , Gregory B. Venema , Cagatay Yanar , Julien Boselli
发明人： Gary H. Bray , Dhruba J. Chakrabarti , Diana K. Denzer , Jen C. Lin , John Newman , Gregory B. Venema , Cagatay Yanar , Julien Boselli
IPC分类号： C22F1/053 , C22C21/10
CPC分类号： C22F1/053 , B64C3/182 , B64C3/185 , B64C3/187 , B64C3/26 , B64C2001/0081 , C22C21/10 , Y02T50/42
摘要： Aluminum alloy products about 4 inches thick or less that possesses the ability to achieve, when solution heat treated, quenched, and artificially aged, and in parts made from the products, an improved combination of strength, fracture toughness and corrosion resistance, the alloy consisting essentially of: about 6.8 to about 8.5 wt. % Zn, about 1.5 to about 2.00 wt. % Mg, about 1.75 to about 2.3 wt. % Cu; about 0.05 to about 0.3 wt. % Zr, less than about 0.1 wt. % Mn, less than about 0.05 wt. % Cr, the balance Al, incidental elements and impurities and a method for making same. The instantly disclosed alloys are useful in making structural members for commercial airplanes including, but not limited to, upper wing skins and stringers, spar caps, spar webs and ribs of either built-up or integral construction.
摘要翻译：约4英寸厚或以下的铝合金产品具有在固溶热处理，淬火和人工老化的同时实现的能力，以及由产品制成的零件中，改进了强度，断裂韧性和耐腐蚀性的组合，该合金组成基本上为：约6.8至约8.5wt。％Zn，约1.5至约2.00wt。％Mg，约1.75至约2.3wt。％Cu; 约0.05至约0.3wt。％Zr，小于约0.1wt。％Mn，小于约0.05wt。％Cr，余量为Al，附带元素和杂质及其制备方法。瞬时公开的合金可用于制造商用飞机的结构构件，包括但不限于上部翼皮和桁条，翼梁盖，翼梁腹板和构成或整体结构的肋。

5. 发明申请

US20060011272A1 2000 Series alloys with enhanced damage tolerance performance for aerospace applications 有权
公开(公告)号：US20060011272A1
公开(公告)日：2006-01-19
申请号：US10893003
申请日：2004-07-15
申请人： Jen Lin , John Newman , Paul Magnusen , Gary Bray
发明人： Jen Lin , John Newman , Paul Magnusen , Gary Bray
IPC分类号： C22C21/12
CPC分类号： C22C21/14 , C22C1/06 , C22C21/12 , C22C21/16 , C22F1/057
摘要： The invention provides a 2000 series aluminum alloy having enhanced damage tolerance, the alloy consisting essentially of about 3.0-4.0 wt % copper; about 0.4-1.1 wt % magnesium; up to about 0.8 wt % silver; up to about 1.0 wt % Zn; up to about 0.25 wt % Zr; up to about 0.9 wt % Mn; up to about 0.5 wt % Fe; and up to about 0.5 wt % Si, the balance substantially aluminum, incidental impurities and elements, said copper and magnesium present in a ratio of about 3.6-5 parts copper to about 1 part magnesium. The alloy is suitable for use in wrought or cast products including those used in aerospace applications, particularly sheet or plate structural members, extrusions and forgings, and provides an improved combination of strength and damage tolerance.

6. 外观设计

USD570213S1 Lid for a disposable drink cup 有权
标题翻译：盖一次性饮料杯
公开(公告)号：USD570213S1
公开(公告)日：2008-06-03
申请号：US29273285
申请日：2007-03-01
申请人： John Newman
设计人： John Newman

7. 发明授权

US5173374A Explosion attenuation system and method for assembly in battery 失效
标题翻译：爆炸衰减系统和电池组装方法
公开(公告)号：US5173374A
公开(公告)日：1992-12-22
申请号：US667970
申请日：1991-03-12
申请人： William H. Tiedemann , Richard R. W. Binder , Daniel J. Cantillon , Allen C. Chapman , Guy D. McDonald , Bryan L. McKinney , John Newman , Richard C. Stone
发明人： William H. Tiedemann , Richard R. W. Binder , Daniel J. Cantillon , Allen C. Chapman , Guy D. McDonald , Bryan L. McKinney , John Newman , Richard C. Stone
IPC分类号： H01M2/12 , H01M10/52
CPC分类号： H01M2/1247 , H01M10/52 , Y10T29/49114
摘要： An electric storage battery according to the invention has a porous explosion attenuating material disposed within a head space of the battery case over the electrode elements. The attenuating material forms a layer or lining on the inner surface of the top wall of the case, and preferably also on the inner surface of the upper ends of each side wall between the electrode elements and the top wall. The interior of the head space remains open. Such an explosion attenuating material is effective to limit pressure build-up resulting from ignition of said gases within the case.
摘要翻译：根据本发明的蓄电池具有在电极元件上设置在电池壳体的顶部空间内的多孔爆炸衰减材料。衰减材料在壳体的顶壁的内表面上形成层或衬里，并且优选地也在电极元件和顶壁之间的每个侧壁的上端的内表面上形成。头部空间的内部保持打开。这种爆炸衰减材料有效地限制由壳体内的所述气体点燃而产生的压力增加。

8. 发明授权

US4649808A Fireplace damper assembly 失效
标题翻译：壁炉风门组件
公开(公告)号：US4649808A
公开(公告)日：1987-03-17
申请号：US816397
申请日：1986-01-06
申请人： Robert Ward , John Newman
发明人： Robert Ward , John Newman
IPC分类号： F23J15/02 , F23L11/00 , F23L17/00 , F23L17/10 , F23L17/02
CPC分类号： F23L11/005 , F23J15/022 , F23L17/005 , F23L17/10 , F23J2213/50
摘要： A damper assembly for sealing a vertical fireplace exhaust including a vertical duct having an outlet communicating with the atmosphere for exhaust of fireplace fumes, mounting means mounted on said vertical duct outlet, a damper downstream of said vertical duct outlet operative to block and open said vertical duct outlet and means to open and close said damper. Easily added improvements include a spark screen assembly downstream of said damper and communicating with said vertical duct outlet, electrical actuation of said damper, automatic control of said actuation by temperature and/or smoke detection means, a fan to provide draft assist, and/or a wind protection hood to provide a better draft.
摘要翻译：一种用于密封垂直壁炉废气的阻尼器组件，其包括具有与大气连通以排出壁炉烟雾的出口的垂直管道，安装在所述垂直管道出口上的安装装置，所述垂直管道出口下游的阻尼器，用于阻塞和打开所述竖直管道出口和打开和关闭所述阻尼器的装置。容易增加的改进包括在所述阻尼器下游并与所述垂直管道出口连通的火花塞组件，所述阻尼器的电致动，通过温度和/或烟雾检测装置的所述致动的自动控制，用于提供助牵引的风扇和/或防风罩提供更好的吃水。

9. 发明授权

US08486865B2 Methods for detecting modification resistant nucleic acids 有权
标题翻译：检测修饰抗性核酸的方法
公开(公告)号：US08486865B2
公开(公告)日：2013-07-16
申请号：US12611817
申请日：2009-11-03
申请人： Jonathan Weissman , Nicholas Ingolia , Sina Ghaemmaghami , John Newman
发明人： Jonathan Weissman , Nicholas Ingolia , Sina Ghaemmaghami , John Newman
IPC分类号： C12Q1/68 , C40B30/00
CPC分类号： C12N15/1041 , C12N15/1034 , C12N15/1093 , C12Q1/6809 , C40B40/08 , C40B50/06
摘要： Methods are provided for, inter alia, detecting nucleic acid molecules resistant to degradation, such as a plurality of RNA molecules bound to a ribosome, using various technologies including deep sequencing.
摘要翻译：提供的方法尤其是使用包括深度测序的各种技术来检测抗降解的核酸分子，例如与核糖体结合的多个RNA分子。

10. 发明授权

US08167038B2 System and method for deflection compensation in power drive system for connection of tubulars 有权
标题翻译：用于连接管道的动力传动系统中的偏转补偿系统和方法
公开(公告)号：US08167038B2
公开(公告)日：2012-05-01
申请号：US12534499
申请日：2009-08-03
申请人： Doyle Boutwell , John Newman , Graham Ruark , Aaron Dauphine
发明人： Doyle Boutwell , John Newman , Graham Ruark , Aaron Dauphine
IPC分类号： E21B47/00
CPC分类号： E21B19/166 , E21B19/165 , E21B47/0006 , Y10T29/49767
摘要： The present invention generally provides methods and apparatus for connecting threaded members while ensuring that a proper connection is made, particularly for premium grade connections. In one embodiment, a method of connecting threaded tubular members for use in a wellbore or a riser system is provided. The method includes the acts of operating a power drive unit, thereby rotating a first threaded tubular member relative to a second threaded tubular member; measuring the rotation of the first threaded tubular member; and compensating the rotation measurement by subtracting a deflection of at least one of: the power drive unit, and one of the tubular members.
摘要翻译：本发明通常提供了用于连接螺纹构件的方法和装置，同时确保进行适当的连接，特别是对于高级连接。在一个实施例中，提供了一种连接用于井筒或立管系统中的螺纹管状构件的方法。该方法包括操作动力驱动单元的动作，从而使第一螺纹管状构件相对于第二螺纹管状构件旋转; 测量第一螺纹管状构件的旋转; 以及通过减去所述动力驱动单元和所述管状构件中的至少一个的偏转来补偿所述旋转测量。

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