首页> 外国专利> REGIME FOR EFFECTIVE HEALTH MONITORING OF HELICOPTER DYNAMIC COMPONENTS

REGIME FOR EFFECTIVE HEALTH MONITORING OF HELICOPTER DYNAMIC COMPONENTS

机译:有效监控直升机动态组件的方法

摘要

Increasing entreaty for both improved effective safety and reduced rotorcraft maintenance and operating cost has marked the way for the Health and Usage monitoring system (HUMS). The health of dynamic components is tersely summarized by a range of condition indicators which relates to specific faults, such as shaft misalignment, gear tooth cracking, bearing faults, rotor unbalance etc. These indicators provide an unblemished depiction of the health of the dynamic components, along with diagnosis of any problems. This invention is about development of a universal regime where the health monitoring data is acquired automatically such that the false warning alert to the ground crew to initiate maintenance action or miss hit in case of actual failure is minimized.
机译:为了提高有效安全性并减少旋翼航空器的维护和运营成本而增加的需求,已经为健康和使用情况监视系统(HUMS)铺平了道路。通过一系列与特定故障(例如轴未对准,齿轮齿裂,轴承故障,转子不平衡等)相关的状态指示器简要总结了动态组件的运行状况。这些指示器提供了对动态组件运行状况的完美描述,以及任何问题的诊断。本发明是关于一种通用机制的发展,在该通用机制中,自动获取健康监测数据,从而使在实际故障情况下对地面人员发起维护行动或误击的错误警告最小化。

著录项

  • 公开/公告号IN2014CH05998A

    专利类型

  • 公开/公告日2016-07-01

    原文格式PDF

  • 申请/专利权人

    申请/专利号IN5998/CHE/2014

  • 发明设计人 HAMID ALI;S SRIDHAR;

    申请日2014-12-01

  • 分类号

  • 国家 IN

  • 入库时间 2022-08-21 14:25:30

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