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1. 发明申请

US20050221818A1 Dynamic configuration management 有权
标题翻译：动态配置管理
公开(公告)号：US20050221818A1
公开(公告)日：2005-10-06
申请号：US10973727
申请日：2004-10-26
申请人： Steven Johnson , Tri Phan , C. Fagan , Michael D'Annunzio , Ben Forbes , Christopher Payne , Rolf Dietiker
发明人： Steven Johnson , Tri Phan , C. Fagan , Michael D'Annunzio , Ben Forbes , Christopher Payne , Rolf Dietiker
IPC分类号： H04B7/185 , H04W84/06 , H04Q7/20
CPC分类号： H04B7/18506 , H04W84/06
摘要： Configuration of hardware and software onboard a mobile platform may be dynamically managed without significantly impacting a data stream from the mobile platform. Configuration data for equipment and resident software aboard a mobile platform is electronically reported in the form of a part number and a serial number. The configuration data is transferred to a terrestrial database via a mobile communications network. The configuration data is displayed to stakeholders, such as the network-provider enterprise and its customers. Invalid configurations may cause alerts.
摘要翻译：可以动态地管理移动平台上的硬件和软件的配置，而不会显着影响来自移动平台的数据流。移动平台上的设备和驻留软件的配置数据以部件号和序列号的形式进行电子报告。配置数据经由移动通信网络传送到地面数据库。配置数据显示给利益相关者，如网络提供商企业及其客户。无效的配置可能会导致警报。

2. 发明授权

US08800924B2 Aerofoil structure 有权
标题翻译：机翼结构
公开(公告)号：US08800924B2
公开(公告)日：2014-08-12
申请号：US12998913
申请日：2010-01-14
申请人： David Groves , Christopher Payne
发明人： David Groves , Christopher Payne
IPC分类号： B64C3/18 , B21D53/92
CPC分类号： B64C3/22 , Y10T29/49622 , Y10T29/49826
摘要： An aerofoil structure (1) comprising at least two spars (2, 4) spaced apart in a fore and aft direction so as to define a fuel carrying volume between the spars, and at least one longitudinal corrugated reinforcing member (6, 7) disposed between the spars, each reinforcing member being corrugated in the longitudinal direction to form a series of forward ridges (9) on a forward side of the reinforcing member and a series of aft ridges (8) on an aft side of the reinforcing member, wherein each reinforcing member is directly attached by its forward ridges to one of the spars or to the aft ridges of an adjacent one of the reinforcing members, and wherein each reinforcing member is directly attached by its aft ridges to one of the spars or to the forward ridges of an adjacent one of the reinforcing members. Also, a method of manufacturing an aerofoil structure. The reinforcing member(s) may extend substantially the entire length of the structure to reduce the number of manufactured parts of the structure, increase the stiffness of the structure and reduce the weight of the structure.
摘要翻译：一种机翼结构（1），包括沿前后方向间隔开的至少两个翼梁（2,4），以便限定所述翼梁之间的燃料承载体积，以及至少一个纵向波纹状加强构件（6,7）在所述翼梁之间，每个加强构件沿纵向方向波纹形成在所述加强构件的前侧上的一系列前脊（9）和所述加强构件的后侧上的一系列后脊（8），其中每个加强构件通过其前脊直接附接到相邻一个加强构件的翼梁或后脊中，并且其中每个加强构件通过其后脊直接附接到其中一个翼梁或向前相邻一个加强构件的脊。另外，制造机翼结构体的方法。加强构件可以大致延伸该结构的整个长度，以减少结构的制造部件的数量，增加结构的刚度并减小结构的重量。

3. 发明申请

US20120132751A1 AEROFOIL STRUCTURE 有权
标题翻译： AEROFOIL结构
公开(公告)号：US20120132751A1
公开(公告)日：2012-05-31
申请号：US12998913
申请日：2010-01-14
申请人： David Groves , Christopher Payne
发明人： David Groves , Christopher Payne
IPC分类号： B64C3/20 , B64C3/34 , B21D39/03
CPC分类号： B64C3/22 , Y10T29/49622 , Y10T29/49826
摘要： An aerofoil structure (1) comprising at least two spars (2, 4) spaced apart in a fore and aft direction so as to define a fuel carrying volume between the spars, and at least one longitudinal corrugated reinforcing member (6, 7) disposed between the spars, each reinforcing member being corrugated in the longitudinal direction to form a series of forward ridges (9) on a forward side of the reinforcing member and a series of aft ridges (8) on an aft side of the reinforcing member, wherein each reinforcing member is directly attached by its forward ridges to one of the spars or to the aft ridges of an adjacent one of the reinforcing members, and wherein each reinforcing member is directly attached by its aft ridges to one of the spars or to the forward ridges of an adjacent one of the reinforcing members. Also, a method of manufacturing an aerofoil structure. The reinforcing member(s) may extend substantially the entire length of the structure to reduce the number of manufactured parts of the structure, increase the stiffness of the structure and reduce the weight of the structure.
摘要翻译：一种机翼结构（1），包括沿前后方向间隔开的至少两个翼梁（2,4），以便限定所述翼梁之间的燃料承载体积，以及至少一个纵向波纹加强构件（6,7）在所述翼梁之间，每个加强构件沿纵向方向波纹形成在所述加强构件的前侧上的一系列前脊（9）和所述加强构件的后侧上的一系列后脊（8），其中每个加强构件通过其前脊直接附接到相邻一个加强构件的翼梁或后脊中，并且其中每个加强构件通过其后脊直接附接到其中一个翼梁或向前相邻一个加强构件的脊。另外，制造机翼结构体的方法。加强构件可以大致延伸该结构的整个长度，以减少结构的制造部件的数量，增加结构的刚度并减小结构的重量。

4. 植物专利

USPP18654P2 Helianthus plant named ‘SLG DS 05’ 有权
标题翻译：向日葵植物名为“SLG DS 05”
公开(公告)号：USPP18654P2
公开(公告)日：2008-03-25
申请号：US11478052
申请日：2006-06-29
申请人： Christopher Payne
发明人： Christopher Payne
IPC分类号： A01H5/00
CPC分类号： A01H6/14 , A01H5/02
摘要： A new and distinct Helianthus plant cultivar is disclosed, characterized by a compact growth habit, bright yellow ray florets, a dark, purple-brown center and a short node length.
摘要翻译：公开了一种新的和独特的向日葵植物品种，其特征在于生长习性小，亮黄色小花，黑色，紫棕色中心和短节点长度。

5. 发明授权

US09387043B2 Medical master/slave type device for minimally invasive surgery 有权
标题翻译：用于微创手术的医疗主/从型装置
公开(公告)号：US09387043B2
公开(公告)日：2016-07-12
申请号：US14116752
申请日：2012-05-14
申请人： Guang-Zhong Yang , George Mylonas , Christopher Payne
发明人： Guang-Zhong Yang , George Mylonas , Christopher Payne
IPC分类号： B25J19/02 , A61B19/00
CPC分类号： A61B34/30 , A61B34/37 , A61B2034/2048 , A61B2034/2061 , A61B2090/065 , A61B2090/508
摘要： Apparatus for Minimal Invasive Surgery (MIS) comprising a master device, a slave device, a detector for detecting a parameter of, or associated with the slave device, and a shape locking system for locking the shape of the master device in response to a parameter detected by the detector.
摘要翻译：用于最小侵入性手术（MIS）的装置包括主装置，从装置，用于检测从装置的参数或与从装置相关联的检测器，以及用于响应于参数锁定主装置的形状的形状锁定系统由检测器检测。

6. 发明授权

US09169000B2 Leading edge rib assembly 有权
标题翻译：前缘肋组件
公开(公告)号：US09169000B2
公开(公告)日：2015-10-27
申请号：US14232247
申请日：2012-07-06
申请人： Simon Topping , Christopher Payne , Llifon Williams , Martin Mayneord , David Belfourd , Xavier Hue
发明人： Simon Topping , Christopher Payne , Llifon Williams , Martin Mayneord , David Belfourd , Xavier Hue
IPC分类号： B64C13/34 , B64C9/02 , B64C9/22
CPC分类号： B64C13/34 , B64C9/02 , B64C9/22
摘要： An aircraft wing has a main wing element with a spar and a leading edge rib supported by the spar, a high lift device movably mounted to the main wing element, and an actuation mechanism with a drive shaft and a gear train. The gear train has a drive cog carried by the drive shaft, an actuator cog coupled to the high lift device, and one or more intermediate cogs mounted to the rib and coupled in series with the drive cog and the actuator cog so as to transmit torque from the drive cog to the actuator cog which moves the high lift device between a retracted position and an extended position in which the high lift device increases the camber of the wing. Sizes of the cogs in the gear train are selected so that the drive shaft rotates at a higher rate than the high lift device.
摘要翻译：飞机机翼具有带翼梁的主翼元件和由翼梁支撑的前缘肋，可移动地安装到主翼元件的高升降装置以及具有驱动轴和齿轮系的致动机构。齿轮系具有由驱动轴承载的驱动齿轮，联接到高提升装置的致动器齿轮和安装到肋上并与驱动齿轮和致动器齿轮串联耦合的一个或多个中间齿轮，以便传递扭矩从驱动齿轮到致动器齿轮，该致动器齿轮在缩回位置和伸出位置之间移动高升程装置，在该位置，高升力装置增加机翼的外倾角。选择齿轮系中的齿轮的尺寸，使得驱动轴以比高举升装置更高的速度旋转。

7. 发明申请

US20050154718A1 System and method for optimizing search result listings 失效
标题翻译：用于优化搜索结果列表的系统和方法
公开(公告)号：US20050154718A1
公开(公告)日：2005-07-14
申请号：US10805873
申请日：2004-03-22
申请人： Christopher Payne , Eric Watson , Sally Salas , Sreeram Krishnan
发明人： Christopher Payne , Eric Watson , Sally Salas , Sreeram Krishnan
IPC分类号： G06F7/00
CPC分类号： G06F7/00
摘要： A method, system, and computer-accessible medium are provided for optimizing search result listings in a search engine user interface. The system and method provide an automated way of promoting and demoting the placement of a search result listing between more or less desirable locations, based on the listing's performance in a given placement. Promoting and demoting placements is based on a threshold performance for the listing against which the actual performance of a listing is measured. The threshold performance may be advantageously varied to accommodate different revenue and relevance goals for a particular search engine or portion of the search engine's market.
摘要翻译：提供了一种方法，系统和计算机可访问介质，用于优化搜索引擎用户界面中的搜索结果列表。该系统和方法提供了一种自动化方式，根据列表在给定展示位置中的表现，提供和降级搜索结果列表位于多个或多个所需位置之间的位置。宣传和降级展示位置是基于列表的实际性能的衡量标准。可以有利地改变阈值性能以适应特定搜索引擎或搜索引擎市场的一部分的不同收入和相关性目标。

8. 发明申请

US20140231592A1 LEADING EDGE RIB ASSEMBLY 有权
标题翻译：领先的边框总成
公开(公告)号：US20140231592A1
公开(公告)日：2014-08-21
申请号：US14232247
申请日：2012-07-06
申请人： Simon Topping , Christopher Payne , Llifon Williams , Martin Mayneord , David Belfourd , Xavier Hue
发明人： Simon Topping , Christopher Payne , Llifon Williams , Martin Mayneord , David Belfourd , Xavier Hue
IPC分类号： B64C13/34
CPC分类号： B64C13/34 , B64C9/02 , B64C9/22
摘要： An aircraft wing comprising a main wing element with a spar and a leading edge rib which is supported by the spar and extends forward of the spar; a high lift device which is movably mounted to the main wing element; and an actuation mechanism comprising a drive shaft and a gear train. The gear train comprising a drive cog which is carried by the drive shaft, an actuator cog which is coupled to the high lift device, and one or more intermediate cogs which are mounted to the rib and coupled in series with the drive cog and the actuator cog so as to transmit torque from the drive cog to the actuator cog which moves the high lift device between a retracted position and an extended position in which the high lift device increases the camber of the wing. The sizes of the cogs in the gear train are selected so that the drive shaft rotates at a higher rate than the high lift device.
摘要翻译：一种飞机机翼，包括具有翼梁的主翼元件和由翼梁支撑并延伸到翼梁前方的前缘肋骨; 可移动地安装到主翼元件的高升降装置; 以及包括驱动轴和齿轮系的致动机构。齿轮系包括由驱动轴承载的驱动齿轮，联接到高提升装置的致动器齿轮和一个或多个中间齿轮，其安装到肋并与驱动齿轮串联连接，并且致动器齿轮，以便将扭矩从驱动齿轮传递到致动器齿轮，致动器齿轮使高升程装置在缩回位置和伸出位置之间移动，在该位置，高升程装置增加机翼的弯度。选择齿轮系中的齿轮的尺寸，使得驱动轴以比高提升装置更高的速度旋转。

9. 外观设计

USD371969S Bottle 失效
公开(公告)号：USD371969S
公开(公告)日：1996-07-23
申请号：US42950
申请日：1995-08-21
申请人： Federico G. Cabo , Christopher Payne
设计人： Federico G. Cabo , Christopher Payne

10. 发明申请

US20140171964A1 MEDICAL MASTER/SLAVE TYPE DEVICE FOR MINIMALLY INVASIVE SURGERY 有权
标题翻译：医疗大师/从属类型的设备，用于最小的入侵手术
公开(公告)号：US20140171964A1
公开(公告)日：2014-06-19
申请号：US14116752
申请日：2012-05-14
申请人： Guang-Zhong Yang , George Mylonas , Christopher Payne
发明人： Guang-Zhong Yang , George Mylonas , Christopher Payne
IPC分类号： A61B19/00
CPC分类号： A61B34/30 , A61B34/37 , A61B2034/2048 , A61B2034/2061 , A61B2090/065 , A61B2090/508
摘要： Apparatus for Minimal Invasive Surgery (MIS) comprising a master device, a slave device, a detector for detecting a parameter of or associated with the slave device, and a shape locking system for locking the shape of the master device in response to a parameter detected by the detector.
摘要翻译：用于最小侵入性手术（MIS）的装置包括主装置，从装置，用于检测从装置的参数或与从装置相关联的检测器，以及用于响应于检测到的参数来锁定主装置的形状的形状锁定系统由检测器。

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