首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;ICAS 2008 >DESIGN OF A NOVEL INTELLIGENT DATA MANAGEMENT TOOL FOR HEALTH AND USAGE MONITORING SYSTEMS - DESIGN REQUIREMENTS
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DESIGN OF A NOVEL INTELLIGENT DATA MANAGEMENT TOOL FOR HEALTH AND USAGE MONITORING SYSTEMS - DESIGN REQUIREMENTS

机译:用于健康和使用情况监视系统的新型智能数据管理工具的设计-设计要求

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The utilisation of Health and Usage Monitoring Systems (HUMS) for rotorcraft applications is critical to meet the stringent requirements of rotorcraft airworthiness. The implementation of HUMS systems for automated monitoring and automated inspection has improved safety and reduced maintenance costs associated with fleet management. A HUMS system provides the status of functionality and structural integrity for diagnosis and prognosis of the aircraft components. It encompasses structural & operational health monitoring and usage monitoring of components to provide diagnostic and prognostic analyses. This paper aims to provide a discussion of the design requirements which have been formulated to design a novel HUMS Intelligent Data Management Tool (IDMT) for the Multi-Role Helicopter (MRH) rotorcraft platform. The investigation of HUMS technologies for civil, military & MRH rotorcraft platforms provided the basis to stipulate the high-level design requirements. A parametrical categorisation of the design requirements led to the stipulation of the specific HUMS design parameters based on a holistic analysis. The design parameters will be utilised for integrated HUMS & FMS software development. It is envisaged that the HUMS IDMT will be integrated with the Fleet Management System (FMS) tool to aid the maintenance personnel via increasing efficiency of the current fleet management maintenance practices. Future research work will focus on the formulation and implementation of detailed design requirements & integrated system requirements specifications for HUMS & FMS software.
机译:为了满足旋翼航空器适航性的严格要求,在旋翼航空器应用中使用健康和使用情况监视系统(HUMS)至关重要。 HUMS系统用于自动监控和自动检查的实施提高了安全性并减少了与车队管理相关的维护成本。 HUMS系统提供了功能和结构完整性的状态,用于飞机部件的诊断和预后。它包括结构和运行状况监视以及对组件的使用情况监视,以提供诊断和预后分析。本文旨在提供对设计要求的讨论,这些要求是为多角色直升机(MRH)旋翼飞机平台设计新颖的HUMS智能数据管理工具(IDMT)而制定的。对民用,军用和MRH旋翼飞机平台的HUMS技术的研究为规定高级设计要求奠定了基础。设计要求的参数分类导致了基于整体分析的特定HUMS设计参数的规定。设计参数将用于集成HUMS和FMS软件开发。预计HUMS IDMT将与车队管理系统(FMS)工具集成在一起,以通过提高当前车队管理维护实践的效率来帮助维护人员。未来的研究工作将集中于HUMS和FMS软件的详细设计要求和集成系统要求规范的制定和实施。

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