AN EVENT ANALYSIS APPARATUS, AN EVENT ANALYSIS METHOD, AND AN EVENT ANALYSIS PROGRAM
    2.
    发明公开
    AN EVENT ANALYSIS APPARATUS, AN EVENT ANALYSIS METHOD, AND AN EVENT ANALYSIS PROGRAM 审中-公开
    事件分析装置,事件分析方法和事件分析程序

    公开(公告)号:EP3165984A1

    公开(公告)日:2017-05-10

    申请号:EP16197256.7

    申请日:2016-11-04

    IPC分类号: G05B23/02

    摘要: An event analysis device includes: a one or more event collector configured to collect event log data representing an operation history by a DCS operator; an event analyzer configured to analyze the event log data, and to extract one or more basic unit operations or one or more unit operations representing an operation method based on operations of the DCS operator or an operation intention based on operations of the DCS operator; an operation sequence extractor configured to extract one or more operation sequences which the one or more basic unit operations or the one or more unit operations are aligned in accordance with time order in every service time period; an operation clusterer configured to cluster the operation sequences based on similarity among the operation sequences extracted in every service time period; and an operation procedure generator configured to analyze the operation sequences clustered in same type, and to estimate a structure of the operation procedure based on the operation of the DCS operator.

    摘要翻译: 事件分析设备包括:一个或多个事件收集器,被配置为收集表示DCS操作员的操作历史的事件日志数据; 事件分析器,被配置为分析事件日志数据,并且基于DCS操作员的操作或基于DCS操作员的操作的操作意图提取表示操作方法的一个或多个基本单元操作或一个或多个单元操作; 操作序列提取器,被配置为在每个服务时间段中按照时间顺序提取所述一个或多个基本单元操作或所述一个或多个单元操作对齐的一个或多个操作序列; 操作分组器,被配置为基于在每个服务时间段中提取的操作序列之间的相似性来聚类操作序列; 以及操作过程生成器,被配置为分析聚类在相同类型中的操作序列,并且基于DCS操作员的操作来估计操作过程的结构。

    AIRCRAFT LRU DATA COLLECTION AND RELIABILITY PREDICTION
    6.
    发明公开
    AIRCRAFT LRU DATA COLLECTION AND RELIABILITY PREDICTION 审中-公开
    FLUGZEUG-LRU-DATENSAMMLUNG UNDZUVERLÄSSIGKEITSVORHERSAGE

    公开(公告)号:EP3065016A1

    公开(公告)日:2016-09-07

    申请号:EP16156364.8

    申请日:2016-02-18

    发明人: SZETO, Roland

    IPC分类号: G05B23/02 G07C5/08

    摘要: A remote computing system is described that includes at least one processor and at least one module. The at least one module is operable by the at least one processor to receive first operational data collected by a first line-replaceable-unit of a first aircraft during flight operations of the first aircraft, and receive second operational data collected by at least one second line-replaceable-unit of at least one second aircraft during flight operations of the at least one second aircraft. The at least one module is further operable by the at least one processor to predict, based at least in part on the first operational data and the second operational data, a failure condition associated with the first line-replaceable-unit of the first aircraft, and output, based on the impending failure condition, an indication of the predicted failure condition.

    摘要翻译: 描述了包括至少一个处理器和至少一个模块的远程计算系统。 所述至少一个模块可由所述至少一个处理器操作以在所述第一飞行器的飞行操作期间接收由所述第一飞行器的第一线路可更换单元收集的第一操作数据,并且接收由至少一秒钟收集的第二操作数据 在所述至少一个第二飞行器的飞行操作期间,所述至少一个第二飞机的线路可更换单元。 所述至少一个模块可由所述至少一个处理器进一步操作,至少部分地基于所述第一操作数据和所述第二操作数据来预测与所述第一飞行器的第一线路可替换单元相关联的故障状况, 并且基于即将发生的故障条件输出预测的故障状态的指示。

    VERFAHREN ZUR AUTOMATISCHEN ÜBERWACHUNG ZUMINDEST EINER KOMPONENTE EINES PHYSIKALISCHEN SYSTEMS
    7.
    发明公开
    VERFAHREN ZUR AUTOMATISCHEN ÜBERWACHUNG ZUMINDEST EINER KOMPONENTE EINES PHYSIKALISCHEN SYSTEMS 有权
    一种用于自动监测至少一个组件的物理系统

    公开(公告)号:EP2652716A1

    公开(公告)日:2013-10-23

    申请号:EP11788055.9

    申请日:2011-11-21

    发明人: HAINZL, Stefan

    IPC分类号: G07C3/08 G07C5/08 G05B23/02

    摘要: The invention relates to a method for automatically monitoring at least one component of a physical system; wherein at least one sensor of the component outputs an electrical signal via a measuring chain, said signal being read and processed and saved in a file as data in a data set; wherein the data of the data set are then checked in a first checking step for errors that could have been caused by a prior processing of the data; wherein the data of the data set are then brought into the physical context of the at least one sensor in a second checking step and checked for errors that could have been caused by damage to the reception of the physical and/or system-related conditions of the elements of the measuring chain; wherein the data of the data set can then optionally (if a plurality of sensors are present, if said sensors are to be considered equivalent due to the system, such as due to close proximity on or in the monitored physical system) checked in the context of the equivalent neighbors thereof in a third checking step for errors that could arise from damage to the conditions of similarity and/or dependency; wherein the data of the data are then brought into the context of the component in a third or fourth checking step and checked for errors that could arise from damage to the physical and/or system-related conditions of the component; and wherein the individual errors indicated are then checked against each other in a fourth or fifth checking step and either rejected or output as an error message with reference to the source of the error.

    Redundant actuator control system
    8.
    发明公开
    Redundant actuator control system 审中-公开
    冗余致动器控制系统

    公开(公告)号:EP2381322A3

    公开(公告)日:2013-09-18

    申请号:EP11163677.5

    申请日:2011-04-26

    摘要: An operation control apparatus includes a command generation portion that generates a command signal for commanding operation of a control surface, and first and second monitoring portions that monitor an abnormality of operation of first and second control portions, respectively, of the actuator control apparatus. The actuator control apparatus includes first and second control portions that generate a control signal for an actuator for driving the control surface and that are different in design, and a switching unit that switches the connection to the actuator from one of the first and second control portions to the other, when an abnormality is detected by the first and second monitoring portions. Accordingly, it is possible to monitor a generic failure, and realize redundancy enabling control of the overall operation of the actuator, from start to finish, when a generic failure has occurred, thus realizing further simplification and streamlining of the configuration.

    Electronic device integrity monitoring apparatus
    9.
    发明公开
    Electronic device integrity monitoring apparatus 有权
    Vorrichtung zurÜberwachungderIntegritäteiner elektronischen Vorrichtung

    公开(公告)号:EP2492770A2

    公开(公告)日:2012-08-29

    申请号:EP12155006.5

    申请日:2012-02-10

    发明人: NAKAGAWA, Shingo

    IPC分类号: G05B23/02 B64C13/00

    摘要: A storage unit stores a first reference value of an input/output electric signal into/from control unit and a second reference value of an input/output electric signal into/from a monitoring unit. If the amount of deviation between the input/output electric signal into/from the control unit and the first reference value exceeds a threshold value, a first caution signal output unit detects degradation of the control unit and outputs a caution signal. If the amount of deviation between the input/output electric signal into/from the monitoring unit and the second reference value exceeds a threshold value, a second caution signal output unit detects degradation of the monitoring unit and outputs a caution signal. The first and second reference values are acquired and stored in the storage unit in a period between completion of production of the control unit and the monitoring unit and start of the operation thereof.

    摘要翻译: 存储单元将输入/输出电信号的第一参考值存储到控制单元中,并将输入/输出电信号的第二参考值存储到监控单元中。 如果进入/从控制单元的输入/输出电信号与第一参考值之间的偏差量超过阈值,则第一警告信号输出单元检测控制单元的劣化并输出警告信号。 如果进入监控单元的输入/输出电信号与第二参考值之间的偏差量超过阈值,则第二警告信号输出单元检测监视单元的劣化并输出警告信号。 第一和第二参考值在控制单元的生产完成和监视单元之间的时间段中被获取并存储在存储单元中并开始其操作。

    MONITORING OF BLADE FREQUENCIES OF A WIND TURBINE
    10.
    发明公开
    MONITORING OF BLADE FREQUENCIES OF A WIND TURBINE 审中-公开
    ÜBERWACHUNGDER SCHAUFELFREQUENZEN EINER WINDTURBINE

    公开(公告)号:EP2195527A2

    公开(公告)日:2010-06-16

    申请号:EP08804671.9

    申请日:2008-09-24

    IPC分类号: F03D11/00

    摘要: By the invention one or more bolt gauges (6) each with a built-in load cell (LC, not shown) are positioned on a blade bolt or a bearing bolt between a pitch bearing and a nut and tensioned by the nut at the inside or the outside of a hub of a wind turbine. The bolt gauge then outputs a signal descending both from the tension from the bolt/nut connection and the tension from the blade when the blade is vibrated due to wind forces and the rotation of the blade when the hub of the wind turbine is rotating. Further a severe and alarming change in each blade frequency is monitored as each blade frequency is compared to the other blade frequencies and an alarm is set and/or the wind turbine is stopped if a given level is reached.

    摘要翻译: 每个具有内置称重传感器的一个或多个螺栓量规位于叶片螺栓或变桨轴承和紧固装置之间的轴承螺栓上,并且通过固定装置在风力涡轮机的轮毂的内部或外部张紧 。 然后,当风力涡轮机的轮毂旋转时,由于风力和叶片的旋转,当叶片振动时,螺栓计量器输出来自螺栓/固定装置连接的张力和来自叶片的张力的信号。