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1. 发明授权

US09730339B2 Common bus structure for avionics and satellites (CBSAS) 有权
公开(公告)号：US09730339B2
公开(公告)日：2017-08-08
申请号：US15084181
申请日：2016-03-29
申请人： Edmund David Burke
发明人： Edmund David Burke
IPC分类号： B64G1/66 , B64G1/40 , B64G1/24 , H05K5/00 , G05D1/08 , B64G1/42 , B64D27/00 , H01Q1/28 , H05K9/00
CPC分类号： H05K5/0021 , B64D27/00 , B64G1/24 , B64G1/40 , B64G1/425 , B64G1/66 , G05D1/08 , H01Q1/28 , H05K9/0007
摘要： A Common Bus Structure for Avionics and Satellites (CBSAS) (10) as shown in FIG. 1 is comprised of a module lid (14), module floor (38), module stack base (16), module compression bolts (22) and stackable modules (12). Stackable modules (12) are sub-dividable to create module scaled chamber volumes (45) individually as required, while stackable modules (12) simultaneously create at least one collectively continuous raceway sealed chamber volume (44) perpendicular to individual stackable modules (12) in the vertical direction where no module floor (38) is present, in order to internally electrically interconnect the contents of any stackable module (12) with the contents of any other stackable module (12) via internal connector raceway system (24). Raceway sealed chamber volume (44) therefore collectively and continuously traverses all present stackable modules (12) positioned between module lid (14) and module stack base (16). Modules are interchangeable and inter-connectable in any order, and contain all required electronic or mechanical components required for CBSAS (10) to function as a single box consolidated avionics system that is equally functional in the atmosphere or the vacuum of space, while also being fully functional as a single complete stand-alone satellite system. CBSAS (10) enables a paradigm shift in the aerospace industry whereby all legacy and current multiple black-box systems on aerospace platforms such as missiles, rockets, satellites and aircraft are extremely inefficient when compared to the size, weight and power attributes of CBSAS (10). The ability for CBSAS (10) to be instantly employable as either a single box consolidated avionics system for use within the atmosphere or in space while also being fully functional as a stand-alone satellite enables a hardware, firmware and software capability never before manifested in the aerospace industry.

2. 发明申请

US20170141369A1 Advanced Lithium Polymer System (ALPS) 审中-公开
公开(公告)号：US20170141369A1
公开(公告)日：2017-05-18
申请号：US14249646
申请日：2014-04-10
申请人： Edmund David Burke
发明人： Edmund David Burke
IPC分类号： H01M2/10 , H01M10/0565 , H01M10/615 , G01R31/36 , H01M2/34 , H01M10/625 , B64G1/42 , B64G1/10 , H01M10/0525 , H01M10/48
CPC分类号： H01M2/1094 , B64G1/10 , B64G1/42 , G01R31/3679 , H01M2/0275 , H01M2/1077 , H01M2/34 , H01M10/052 , H01M10/0525 , H01M10/0565 , H01M10/482 , H01M10/486 , H01M10/615 , H01M10/625 , H01M2010/4271 , H01M2200/00 , H01M2220/20 , Y02E60/122
摘要： An advanced power system employing lithium polymer pouch cells which operates in all environments from atmospheric pressures, upward and through to the harsh and demanding realm of a space vacuum, including any aerospace related environments of launch, flight or operation for satellites, missiles, rockets, aircraft, or on any vehicle where size and weight may or may not be of critical importance but where power output is desired to be maximized, this invention is an new manifestation, arrangement, combination, architecture and application of lithium polymer battery technology in the form of an advanced lithium polymer system (ALPS) for aerospace or similar environments that require an architecture resulting in the never-before contemplated, attempted or demonstrated integrated combination of attributes of safety, modularity, scalability, expandability, deployability, employability, practicality, intelligence control and radiation hardening, while being comprised of any number of stacked flat lithium polymer battery cells physically arranged and integrated within a constraining packaging enclosure that maximizes safety and power density while mitigating the debilitating effects of shock, vibration, thermal cycle, vacuum, radiation and electromagnetic interference while simultaneously communicating electronically with a battery management system that provides instant autonomous cell protection, balancing and electronically isolated real-time monitoring of all individual cell parameters of voltage, current, temperature, state of charge and internal resistance to prevent battery catastrophic thermal runaway events caused by cell electrolyte leakage, overcharge and internal defects while simultaneously being capable of interfacing with a hardwired graphical human interface and remote telemetry system that monitors and displays all cell parameters with visibility down to the individual cell level allowing for cell parameter data to be continually monitored and archived and used to characterize and screen out cells in a particular cell manufacturing lot, and also to identify in real-time via prognostic software if a particular cell is entering a non-acceptable condition prior to displaying hazardous behavior which could result in a hazardous condition.

3. 发明申请

US20160324019A1 COMMON BUS STRUCTURE FOR AVIONICS AND SATELLITES (CBSAS) 审中-公开
公开(公告)号：US20160324019A1
公开(公告)日：2016-11-03
申请号：US15084181
申请日：2016-03-29
申请人： Edmund David Burke
发明人： Edmund David Burke
IPC分类号： H05K5/00 , B64G1/66 , B64G1/40 , H01Q1/28 , B64G1/24 , B64D27/00 , H05K5/03 , G05D1/08 , B64G1/42
CPC分类号： H05K5/0021 , B64D27/00 , B64G1/24 , B64G1/40 , B64G1/425 , B64G1/66 , G05D1/08 , H01Q1/28 , H05K9/0007
摘要： A Common Bus Structure for Avionics and Satellites (CBSAS) (10) as shown in FIG. 1 is comprised of a module lid (14), module floor (38), module stack base (16), module bolts (22) and stackable modules (12). Stackable modules (12) are sub-dividable to create module sealed chamber volumes (45) individually as required, while stackable modules (12) simultaneously create at least one collectively continuous raceway sealed chamber volume (44) perpendicular to individual stackable modules (12) in the vertical direction where no module floor (38) is present, in order to internally electrically interconnect the contents of any stackable module (12) with the contents of any other stackable module (12) via internal connector raceway system (24). Raceway sealed chamber volume (44) therefore collectively and continuously traverses all present stackable modules (12) positioned between module lid (14) and module stack base (16). Modules are interchangeable and inter-connectable in any order, and contain all required electronic or mechanical components required for CBSAS (10) to function as a single box consolidated avionics system that is equally functional in the atmosphere or the vacuum of space, while also being fully functional as a single complete stand-alone satellite system. CBSAS (10) enables a paradigm shift in the aerospace industry whereby all legacy and current multiple black-box systems on aerospace platforms such as missiles, rockets, satellites and aircraft are extremely inefficient when compared to the size, weight and power attributes of CBSAS (10). The ability for CBSAS (10) to be instantly employable as either a single box consolidated avionics system for use within the atmosphere or in space while also being fully functional as a stand-alone satellite enables a hardware, firmware and software capability never before manifested in the aerospace industry.

4. 外观设计

USD691469S1 Container 有权
公开(公告)号：USD691469S1
公开(公告)日：2013-10-15
申请号：US29419483
申请日：2012-04-27
申请人： Niketa Mohler , Kristina Lambros , Shelley Markoulis , Piaras Valdis de Cleir , David Burke , Andrew Bunner , Jordan French
设计人： Niketa Mohler , Kristina Lambros , Shelley Markoulis , Piaras Valdis de Cleir , David Burke , Andrew Bunner , Jordan French

5. 发明申请

US20120013115A1 Educational Tool 审中-公开
标题翻译：教育工具
公开(公告)号：US20120013115A1
公开(公告)日：2012-01-19
申请号：US12836522
申请日：2010-07-14
申请人： Gregory David Burke , Jo-Jo Wai Yan Burke
发明人： Gregory David Burke , Jo-Jo Wai Yan Burke
IPC分类号： B42F21/00
CPC分类号： B42F21/04 , B42D1/007 , B42D1/008 , G09B1/00 , G09B5/062
摘要： An educational tool is described including a number of pages, at least some of which bear elements of page information; a number of tabs are associated with the pages, at least some of which bear elements of tab information; wherein the elements of tab information on each tab define criteria for identifying at least one corresponding element of page information borne on the page with which each tab is associated.
摘要翻译：描述了一种教育工具，其中包括多页，至少其中一些页面具有页面信息的元素; 许多选项卡与页面相关联，其中至少一些选项卡具有制表信息的元素; 其中每个标签上的标签信息的元素定义用于标识每个标签与之相关联的页面上承载的页面信息的至少一个对应元素的标准。

6. 发明授权

US07958567B2 Low protrusion safety fastener for ballistic helmet 有权
标题翻译：防弹头盔低突出安全紧固件
公开(公告)号：US07958567B2
公开(公告)日：2011-06-14
申请号：US11207469
申请日：2005-08-19
申请人： Brad Sutter , Charles F. Acker , David Burke
发明人： Brad Sutter , Charles F. Acker , David Burke
IPC分类号： A42B3/00
CPC分类号： A42B3/04
摘要： A safety fastener for mounting fitting equipment such as suspension and retention systems onto a ballistic helmet. The nut portion of the fastener fits substantially within a grommet that is attached to a strap that forms part of the suspension or retention systems. The nut retains, rather than clamps, the grommet to the helmet. The grommet can be pulled off the nut. The pull-out force is less than the fastener fracture force. The configuration of the fastener allows ballistic threat energy to be absorbed by helmet deformation and delamination along with grommet pull-out to provide energy dissipation in stages which avoids the creation of secondary projectiles from the fastener itself.
摘要翻译：一种安全紧固件，用于将诸如悬挂和保持系统的装配设备安装到防弹头盔上。紧固件的螺母部分基本上配合在附接到形成悬挂或保持系统的一部分的带的索环中。螺母保留，而不是夹具，索环到头盔。护环可以从螺母上拉下来。拔出力小于紧固件的断裂力。紧固件的配置允许弹道威胁能量通过头盔变形和分层以及索环拉出来吸收，以提供阶段性的能量耗散，从而避免从紧固件本身产生二次射弹。

7. 发明申请

US20090040554A1 System and method of processing print order requests 失效
标题翻译：处理打印订单请求的系统和方法
公开(公告)号：US20090040554A1
公开(公告)日：2009-02-12
申请号：US12221813
申请日：2008-08-07
申请人： David Burke , Brian Deane , Paul McDonnell , Dermot Heslin
发明人： David Burke , Brian Deane , Paul McDonnell , Dermot Heslin
IPC分类号： G06F3/12
CPC分类号： G06Q10/06 , G06F3/1204 , G06F3/126 , G06F3/1288 , G06Q10/10
摘要： This invention relates to a system and method of processing print order requests in a print system comprising a central print controller, a plurality of remote print customers and a plurality of remote print suppliers, the central print controller being connected to the plurality of remote print customers and the plurality of remote print suppliers by way of a communications network. Print customers transmit their print order requests to one central print controller. The central print controller will have information relating to a number of print suppliers stored in the central print controller database and can ascertain which of the print suppliers is the most suitable print supplier for executing a particular order. The central print controller is able to obtain the different protocols and data formats used in the proprietary database systems of the print supplier from its own central print controller database and may then format the print order request into a format suitable for receipt by the print supplier.
摘要翻译：本发明涉及一种在包括中央打印控制器，多个远程打印客户和多个远程打印供应商的打印系统中处理打印订单请求的系统和方法，所述中央打印控制器连接到多个远程打印客户和多个远程打印供应商通过通信网络。打印客户将其打印订单请求发送到一个中央打印控制器。中央打印控制器将具有与中央打印控制器数据库中存储的多个打印供应商有关的信息，并且可以确定哪些打印供应商是用于执行特定订单的最合适的打印供应商。中央打印控制器能够从其自己的中央打印控制器数据库获得在打印供应商的专有数据库系统中使用的不同协议和数据格式，然后可以将打印订单请求格式化成适合于打印供应商接收的格式。

8. 发明申请

US20080295215A1 Integrated Wearable Costume and Storage Case 审中-公开
标题翻译：集成可穿戴服装和存储案例
公开(公告)号：US20080295215A1
公开(公告)日：2008-12-04
申请号：US11754956
申请日：2007-05-29
申请人： David Burke , Ronald Shostack
发明人： David Burke , Ronald Shostack
IPC分类号： A41D1/00 , A45F4/02
CPC分类号： A45F4/02 , A41D11/00 , A41D15/04 , A45F3/04 , A45F5/06
摘要： A combination backpack and garment carrying apparatus is disclosed. The combination backpack and garment carrying apparatus includes a back plate, a cover, a frame, and garment segments. These pieces combined together create a combination backpack and garment carrying apparatus that allows the wearer to easily access, store, and carry a costume. The wearer activates a switch on the combination backpack and garment carrying apparatus and opens the lids allowing the garment segments to fall out and be pulled over the wearer's arms, legs, and head.
摘要翻译：公开了组合背包和服装运输装置。组合背包和服装运送装置包括背板，盖，框架和衣服部分。这些组合在一起形成组合的背包和服装承载装置，其允许穿戴者容易地进入，存放和携带服装。佩戴者激活组合背包和服装输送装置上的开关，并打开盖子，允许衣服部分脱落并被拉过佩戴者的手臂，腿部和头部。

9. 发明申请

US20080098802A1 SYSTEM AND METHOD FOR ANALYTE MEASUREMENT 有权
标题翻译：用于分析测量的系统和方法
公开(公告)号：US20080098802A1
公开(公告)日：2008-05-01
申请号：US11970952
申请日：2008-01-08
申请人： David Burke , Lance Kuhn , Terry Beaty , Vladimir Svetnik
发明人： David Burke , Lance Kuhn , Terry Beaty , Vladimir Svetnik
IPC分类号： G01N33/487
CPC分类号： G01N27/3274 , Y10T436/11 , Y10T436/112499 , Y10T436/115831 , Y10T436/12 , Y10T436/142222 , Y10T436/143333 , Y10T436/144444 , Y10T436/203332
摘要： A method of measuring an analyte in a biological fluid comprises applying an excitation signal having a DC component and an AC component. The AC and DC responses are measured; a corrected DC response is determined using the AC response; and a concentration of the analyte is determined based upon the corrected DC response. Other methods and devices are disclosed.
摘要翻译：测量生物流体中的分析物的方法包括施加具有DC分量和AC分量的激发信号。测量AC和DC响应; 使用AC响应确定校正的DC响应; 并且基于校正的DC响应确定分析物的浓度。公开了其它方法和装置。

10. 发明授权

US07234714B2 Roll control system for a motor vehicle 有权
标题翻译：汽车滚动控制系统
公开(公告)号：US07234714B2
公开(公告)日：2007-06-26
申请号：US10483166
申请日：2002-07-04
申请人： Philippe Germain , David Burke
发明人： Philippe Germain , David Burke
IPC分类号： B60G21/055
CPC分类号： B60G21/055 , B60G17/0162 , B60G21/0553 , B60G2202/135 , B60G2204/122 , B60G2400/204 , B60G2400/41 , B60G2800/012 , B60G2800/24 , B60G2800/9122 , F16F9/535 , F16F9/58 , F16F13/06
摘要： (57) A roll control system (20) for installation between axially aligned wheels of a motor vehicle, the roll control system comprising a torsion bar (22); a damper (24) attached to one end (28) of the torsion bar and attachable to one of the wheels; and attachment means (25) attached to the other end (29) of the torsion bar and attachable to the other wheel; wherein the damper comprises an axially extending cylindrical housing (52); a piston (34) slidably mounted inside the housing; a piston rod (58) connected to the piston, extending out of one end (55) of the housing, and movable in an axial direction relative to the housing; a floating piston (35) slidably mounted in the housing between the piston and the other end of the housing; a compensation chamber (37) between the floating piston and the other end (54) of the housing containing a first pressurised fluid; a compression chamber (30) between the floating piston and the piston containing a second pressurised fluid; a rebound chamber (32) between the piston and the one end of the housing containing the second pressurised fluid; valve means (36) on the piston allowing restricted flow of the second pressurised fluid between the compression chamber and the rebound chamber; a rebound stop (60) positioned in the rebound chamber between the piston and the one end of the housing and providing a spring-effect on the movement of the piston towards the one end of the housing; and a compression stop (62) providing a spring-effect on the movement of the piston towards the floating piston. Provides an improved passive roll controle system.
摘要翻译：（57）一种用于安装在机动车辆的轴向对齐的车轮之间的滚动控制系统（20），所述滚动控制系统包括扭杆（22）; 安装在所述扭杆的一端（28）上并可附接到所述车轮之一的阻尼器（24）; 以及附接到所述扭杆的另一端（29）并可附接到另一个车轮的附接装置（25）其中所述阻尼器包括轴向延伸的圆柱形壳体（52）; 可滑动地安装在所述壳体内的活塞（34）活塞杆（58），其连接到所述活塞，从所述壳体的一端（55）延伸出并且能够相对于所述壳体在轴向方向上移动; 浮动活塞（35），其可滑动地安装在所述壳体中的所述活塞和所述壳体的另一端之间; 在所述浮动活塞和所述壳体的另一端（54）之间的补偿室（37）包含第一加压流体; 在所述浮动活塞和所述活塞之间的压缩室（30）包含第二加压流体; 在所述活塞和所述壳体的包含所述第二加压流体的所述一端之间的回弹室（32）活塞上的阀装置（36）允许第二加压流体在压缩室和回弹室之间受到限制的流动; 位于所述活塞和所述壳体的一端之间的所述回弹室中的回弹挡块（60），并且对所述活塞朝向所述壳体的一端的运动提供弹簧效应; 以及对活塞朝向浮动活塞的运动提供弹簧效应的压缩止挡件（62）。提供了一种改进的无源滚动控制系统。

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