Entity management system
    2.
    发明授权
    Entity management system 失效
    实体管理系统

    公开(公告)号:US5832224A

    公开(公告)日:1998-11-03

    申请号:US663620

    申请日:1996-06-14

    摘要: A system for managing an assemblage of entities. The entities interface within the assemblage for control of primary information handling functions and further interface with the system to permit the carrying out of management functions. The system includes management modules adapted to carry out management functions by independently interpreting and executing commands, a kernel including a table of dispatch pointers for directing the commands to the respective modules in which they are to be interpreted and executed, and an enroller for enrolling new modules into the system by adding further pointers to the table. In addition, the system includes: a module adapted to independently interpret and execute selected management-related commands; stored records relating to accessed management information, each record indicating an associated time; an information manager, responsive to commands having a time schedule, for retrieving information from the records or accessing information from the entities, including a scheduler for issuing subsidiary accesses or retrievals at possibly multiple times according to the schedule; storage containing domain information defining groups of entities, where the kernel may issue a commands to a group by issuing individual commands to appropriate modules; a common command syntax including fields for identifying the entity and the operation to be performed; a module that stores rules identifying alarm conditions, including a generator for generating rules and an alarm detector for detecting an alarm condition in response to the rules; a module adapted to carry out self-management functions by interpreting and executing commands.

    摘要翻译: 用于管理实体组合的系统。 实体在组合中进行接口,用于控制主要信息处理功能,并与系统进一步接口以允许执行管理功能。 该系统包括适于通过独立地解释和执行命令来执行管理功能的管理模块,包括用于将命令引导到要被解释和执行的相应模块的分派指针表的内核,以及用于登记新的 通过向表中添加更多指针将模块插入系统。 此外,该系统包括:适于独立地解释和执行所选管理相关命令的模块; 与所访问的管理信息相关的存储记录,每个记录指示相关联的时间; 信息管理器,响应于具有时间表的命令,用于从记录中检索信息或从实体访问信息,包括用于根据时间表可能多次发出辅助访问或检索的调度器; 存储包含定义实体组的域信息,其中内核可以通过向适当的模块发出单独的命令来向组发布命令; 包括用于识别实体的字段和要执行的操作的常用命令语法; 存储识别报警条件的规则的模块,包括用于生成规则的发生器和响应于规则检测报警条件的报警检测器; 一个适于通过解释和执行命令执行自我管理功能的模块。

    COMPOSITE AEROSPACE STRUCTURE WITH INTEGRATED CONVEYANCE ELEMENT
    7.
    发明申请
    COMPOSITE AEROSPACE STRUCTURE WITH INTEGRATED CONVEYANCE ELEMENT 审中-公开
    具有集成输送元件的复合气溶胶结构

    公开(公告)号:US20130075539A1

    公开(公告)日:2013-03-28

    申请号:US13245153

    申请日:2011-09-26

    摘要: A composite structure for aerospace applications includes a structural member having multiple composite layers providing a longitudinally extending cavity. A conveyance element is arranged between and integral with the layers. In one example, the structural member provides a gas turbine engine duct or an airframe component. A composite structural assembly is manufactured by providing a first composite layer on a form that corresponds to a cavity. A second form, which may be a conveyance element in one example, is positioned along the first layer. A second composite layer is laid onto the second form and the first composite layer to provide a composite structural member with an integrated conveyance element.

    摘要翻译: 用于航空航天应用的复合结构包括具有提供纵向延伸空腔的多个复合层的结构构件。 传送元件布置在层之间并与层成一体。 在一个示例中,结构构件提供燃气涡轮发动机管道或机身部件。 通过在对应于空腔的形式上提供第一复合层来制造复合结构组件。 在一个示例中可以是传送元件的第二形式沿着第一层定位。 将第二复合层铺设在第二形式和第一复合层上,以提供具有集成输送元件的复合结构构件。

    Monitoring of windows on computers
    8.
    发明授权
    Monitoring of windows on computers 有权
    监控计算机上的窗口

    公开(公告)号:US08214452B2

    公开(公告)日:2012-07-03

    申请号:US11830029

    申请日:2007-07-30

    申请人: Mark J. Seger

    发明人: Mark J. Seger

    IPC分类号: G06F15/16

    CPC分类号: G06F11/30

    摘要: Embodiments include methods, apparatus, and systems for monitoring windows on computers. In one embodiment, movement of a mouse or cursor in a focused window of the computer is analyzed to determine whether an application is properly executing in the computer.

    摘要翻译: 实施例包括用于监视计算机上的窗口的方法,装置和系统。 在一个实施例中,分析计算机的聚焦窗口中的鼠标或光标的运动,以确定应用程序是否在计算机中正确执行。

    Power distribution unit and method of distributing high density power
    9.
    发明授权
    Power distribution unit and method of distributing high density power 有权
    配电单元和分配高密度电源的方法

    公开(公告)号:US09271423B2

    公开(公告)日:2016-02-23

    申请号:US13421233

    申请日:2012-03-15

    IPC分类号: H02J4/00 H05K7/14

    CPC分类号: H05K7/1457 Y10T307/696

    摘要: A power distribution unit includes a first solid state power module comprising a first plurality of solid state power controllers, where the first solid state power module comprises a first set of power characteristics. Also included is a second solid state power module comprising a second plurality of solid state power controllers. The second solid state power module comprises a second set of power characteristics. Also, the first solid state power module and the second solid state power module are interchangeably coupled to a first location of a common chassis.

    摘要翻译: 配电单元包括第一固态功率模块,其包括第一多个固态功率控制器,其中第一固态功率模块包括第一组功率特性。 还包括第二固态功率模块,其包括第二多个固态功率控制器。 第二固态功率模块包括第二组功率特性。 此外,第一固态功率模块和第二固态功率模块可互换地耦合到公共底盘的第一位置。

    MIXED MODE POWER GENERATION ARCHITECTURE
    10.
    发明申请
    MIXED MODE POWER GENERATION ARCHITECTURE 有权
    混合模式发电结构

    公开(公告)号:US20130049366A1

    公开(公告)日:2013-02-28

    申请号:US13222395

    申请日:2011-08-31

    IPC分类号: H02K23/52 B60L1/00

    摘要: An electric power generation system (EPGS) employs both a wild-source generator and a variable and/or constant frequency generator. The wild-source generator is coupled to receive mechanical power from a low-pressure spool on an aircraft engine and to generate in response a wild-source output for consumption by voltage and frequency-tolerant loads. The variable and/or constant frequency generator is coupled to receive mechanical power from a high-pressure spool on the aircraft engine and to generate in response a variable and/or constant frequency output for consumption by voltage and frequency-intolerant loads.

    摘要翻译: 发电系统(EPGS)采用野生源发生器和可变和/或恒定频率发生器。 野生源发生器被耦合以从飞机引擎上的低压线轴接收机械动力,并响应于野生源输出而产生电压和频率承受负载的消耗。 可变和/或恒定频率发生器被耦合以从飞机引擎上的高压线轴接收机械功率,并响应于可变和/或恒定频率输出产生电压和频率不耐受负载的消耗。