首页> 外国专利> DEVICE FOR DETECTING ANOMALIES BY ACOUSTIC ANALYSIS OF AN AIRCRAFT TURBOMACHINE

DEVICE FOR DETECTING ANOMALIES BY ACOUSTIC ANALYSIS OF AN AIRCRAFT TURBOMACHINE

机译:通过飞机涡轮机的声学分析检测异常的装置

摘要

The invention relates to a device (DISP) for detecting anomalies by acoustic analysis of an aircraft turbomachine (TURBO) (AERO), characterized in that it is not loaded and comprises: - At least one mobile module (MOD) comprising: o Acoustic signal acquisition means (MDAC) for the turbomachine (TURBO); o processing means (MDTT) of said signals adapted to generate a damage report (RAP_END); o transmission means (MDTM) of said damage report (RAP_END); a server (SERV) able to exchange data with the at least one module (MOD), said server (SERV) comprising: receiving means (MDR) for the damage report (RAP_END); storage means (MDS) adapted to store said damage report (RAP_END).
机译:本发明涉及一种用于通过飞机涡轮机(TURBO)(AERO)的声学分析来检测异常的设备(DISP),其特征在于,该设备未装载并且包括:-至少一个移动模块(MOD),其包括:o声信号涡轮机(TURBO)的采集装置(MDAC);所述信号的处理装置(MDTT),适于产生损坏报告(RAP_END); o所述损害报告(RAP_END)的传输方式(MDTM);一服务器(SERV),能够与至少一个模块(MOD)交换数据,所述服务器(SERV)包括:用于损坏报告(RAP_END)的接收装置(MDR);以及存储装置(MDS),适于存储所述损坏报告(RAP_END)。

著录项

  • 公开/公告号FR2987443A1

    专利类型

  • 公开/公告日2013-08-30

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号FR20120051713

  • 发明设计人 JEROME HENRI NOEL LACAILLE;

    申请日2012-02-24

  • 分类号G01M15/14;G01H3;

  • 国家 FR

  • 入库时间 2022-08-21 16:20:59

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