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Guidelines for Integrating Typical Engine Health Management Functions Within Aircraft Systems 飞机系统中典型发动机健康管理功能集成指南
发布日期: 2016-11-12
SAE航空航天信息报告(AIR)4061提供了飞机系统内发动机健康管理(EHM)系统功能集成的最佳实践指南,包括其主发动机和任何辅助动力装置(APU)。本文件概述了EHM通常集成的一些功能,提供了不同飞机遇到的一些系统变化,并提出了与集成有关的一般注意事项。它提供了一个EHM参数覆盖矩阵示例,以显示典型EHM系统可能与之接口的参数类型,提供了对信号和数据处理及检索的深入了解,并提供了按功能划分的典型EHM参数要求视图。在可行的情况下,本文件对军事和商业惯例进行了界定。
SAE Aerospace Information Report (AIR) 4061 provides best practice guidelines for the integration of Engine Health Management (EHM) system functions within aircraft systems to include both its main engine(s) and any Auxiliary Power Unit(s) (APU). This document provides an overview of some of the functions EHM typically integrates, offers some system variations encountered with different aircraft, and suggests general considerations involved with integration. It presents a sample EHM parameter coverage matrix to show the types of parameters with which a typical EHM system might interface, offers insight into signal and data processing and retrieval, and offers a view of typical EHM parameter requirements by function. Where practical, this document delineates between military and commercial practices.
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