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AIRCRAFT ENGINE MONITORING SYSTEM VALIDATION INSTRUMENT

机译:飞机发动机监测系统验证仪器

摘要

FIELD: test equipment.;SUBSTANCE: group of inventions relates to an instrument of aircraft engine monitoring system validation, a monitoring system and a monitoring system validation method. Validation instrument contains test means (13), processing means (11), analysis means (12) adapted to evaluate the validation of the monitoring system. System for monitoring an aircraft engine assembly comprises at least one validation instrument and is configured to receive surveillance data and output a diagnostic result of the condition of said unit. Validation method consists in performing tests to assess validation of monitoring system, wherein collecting observation data related to aircraft engine assembly, calculating current value of quality factor on current amount of observation data, estimating probabilistic reliability, estimating minimum amount of observation data to achieve preset reliability criterion.;EFFECT: reduced time of data processing and increased reliability of monitoring system.;11 cl, 6 dwg
机译:飞机发动机监控系统验证仪器,监控系统和监控系统验证方法技术领域本发明涉及飞机发动机监控系统验证仪器,监控系统和监控系统验证方法。验证仪器包括适于评估监测系统有效性的测试装置(13),处理装置(11),分析装置(12)。用于监视飞机发动机组件的系统包括至少一个验证仪器,并且被配置为接收监视数据并输出所述单元的状况的诊断结果。验证方法包括执行测试以评估监视系统的有效性,其中收集与飞机发动机组件有关的观测数据,根据当前观测数据量计算品质因数的当前值,估算概率可靠性,估算最小观测数据量以达到预设的可靠性效果:减少数据处理时间并提高监视系统的可靠性。; 11 cl,6 dwg

著录项

  • 公开/公告号RU2684225C2

    专利类型

  • 公开/公告日2019-04-04

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号RU20170119421

  • 发明设计人 LACAILLE JEROME (FR);

    申请日2015-10-28

  • 分类号G05B23/02;G01M15/14;G06F17/50;

  • 国家 RU

  • 入库时间 2022-08-21 11:46:17

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