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TOOL FOR VALIDATING A SYSTEM FOR MONITORING AN AIRCRAFT ENGINE

机译:验证飞机发动机系统的工具

摘要

A tool for validation of a system for monitoring at least one piece of equipment in an aircraft engine, also comprising a computer configured to: collect observation data related to the equipment, calculate a current value of at least one quality indicator on a current quantity of observation data, estimate the probability that the current value of the quality indicator reaches a predetermined reliability criterion, thus forming a probabilistic reliability law, and estimate a minimum quantity of observation data from the probabilistic reliability law, starting from which the value of the quality indicator reaches a predetermined reliability criterion with a probability exceeding a predetermined value.
机译:一种用于验证用于监视飞机发动机中的至少一件设备的系统的工具,该工具还包括计算机,该计算机被配置为:收集与该设备有关的观察数据,计算至少一个质量指示器的当前值。观测数据,估计质量指标的当前值达到预定可靠性标准的概率,从而形成概率可靠性定律,并从概率可靠性定律估计最小量的观测数据,从此开始质量指标的值以超过预定值的概率达到预定的可靠性标准。

著录项

  • 公开/公告号EP3215903B1

    专利类型

  • 公开/公告日2019-12-18

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号EP20150798515

  • 发明设计人 LACAILLE JÉRÔME HENRI NOËL;

    申请日2015-10-28

  • 分类号G05B23/02;B64D45;F01D17/02;G07C5/08;B64F5/60;F01D21;

  • 国家 EP

  • 入库时间 2022-08-21 11:41:58

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