SAE AS 4831A-2003 Software Interfaces for Ground-Based Monitoring Systems《地基监控系统用的软件接口》.pdf
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1、AEROSPACE STANDARDAS4831REV.AIssued 2001-09Revised 2003-02Superseding AS4831Software Interfaces for Ground-Based Monitoring SystemsFOREWORDThis SAE document seeks to improve the situation whereby current ground-based engine monitoring systems (EMS) cannot readily be integrated into one computing env
2、ironment.Following a consensus by the SAE E-32 Committee on the need for some form of standardization in these systems, ARD50002 was written. It reviewed the situation, laid out several methods of standardization which addressed the problems to varying degrees, and was the vehicle for canvassing the
3、 industry for user views.The result was a clear mandate for standardization and a decision on the degree to which this process should be taken. The consensus was that it is the interfaces between the major functional elements in the EMS which should be standardized, so that elements from different m
4、anufacturers can work together.This document describes the first steps into this standardization.Reaffirmed 2009-10SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely volunta
5、ry, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your writ
6、ten comments and suggestions. Copyright 2009 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permis
7、sion of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/tech
8、nical/standards/AS4831ASAE AS4831 Revision A- 2 -TABLE OF CONTENTS1. SCOPE .42. REFERENCES .42.1 Applicable Documents 42.1.1 SAE Publications 42.2 Glossary42.2.1 Acronyms 42.2.2 Definitions .53. ECM SYSTEM OVERVIEW73.1 Introduction .73.2 Input Interface .73.3 Output Interface 73.4 End-User Tools .93
9、.5 OEM Host System 93.5.1 Input Interface .93.5.2 OEM ECM Host System .93.5.3 OEM Output Reports 103.5.4 Output Interface 104. INPUT INTERFACE SPECIFICATIONS .104.1 Introduction .104.2 The Input Interface114.3 The Input Interface Structure 124.3.1 General Input File Format Requirements134.3.2 Delimi
10、ter Section.134.3.3 Format Section134.3.4 Values Section 144.4 The Input Interface Keys.154.5 Requirements of the OEM Host System for the Input Interface155. OUTPUT INTERFACE SPECIFICATIONS .155.1 Introduction .155.2 Requirements and Structure of the OEM Host System for the Output Interface.165.3 Th
11、e Output Interface Keys 176. EXAMPLE FILES186.1 Input Files .186.1.1 Example of Flight Data Input - One Data Set186.1.2 Example of flight Data Input - Multiple Data Set .19SAE AS4831 Revision A- 3 -TABLE OF CONTENTS (Continued)6.1.3 Example of APU Data Input 206.1.4 Example of a Maintenance Action C
12、ode Input206.1.5 Example of Engine Installation and Removal216.2 Output Files.216.2.1 Example of Flight Data Output216.2.2 Example of Alert Output22SAE AS4831 Revision A- 4 -1. SCOPE:To establish a specification for software input and output interfaces for condition monitoring and performance progra
13、ms used to monitor equipment from multiple manufacturers.The purpose of standardizing these interfaces is to improve operational flexibility and efficiency of monitoring systems as an aid to cost effectiveness (e.g., easier implementation).2. REFERENCES:2.1 Applicable Documents:The following publica
14、tions form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publications shall be the issue in effect on the date of the purchase order. In the event of conflict between the text of this document and references ci
15、ted herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.2.1.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.AIR1873 Guide to Limited E
16、ngine Monitoring Systems for Aircraft Gas Turbine EnginesAIR4175 A Guide for the Development of Ground Station for Condition MonitoringARD50002 A Discussion of Standardization Concepts for Condition Monitoring and Performance Analysis Software2.2 Glossary:2.2.1 Acronyms:ACARS: Aircraft Communication
17、s, Addressing, and Reporting SystemACMS: Aircraft Condition Monitoring SystemADAS: Aircraft Data Acquisition SystemAIMS: Aircraft Information Management System/Aircraft Integrated Monitoring SystemAPU: Auxiliary Power UnitASCII: American Standard Code for Information InterchangeCM: Condition Monitor
18、ingDBMS: Database Management SystemDMU: Data Management UnitECM: Engine Condition MonitoringECS: Environmental Control SystemEMS: Engine Monitoring SystemGUI: Graphical User InterfaceOEM: Original Equipment ManufacturerSQL: Structured Query LanguageSAE AS4831 Revision A- 5 -2.2.2 Definitions:ACCESS
19、METHODS: Methods of accessing data stored in a computer, e.g., indexed, keyed, random, relational or sequential.ALERT: A warning or notification issued based on the analysis of the data, indicating a possible negative change within an engine.ANNOTATION DATA: Narrative text annotating operational exp
20、erience derived from the pilot, maintenance technicians, or engine performance analysts.BASELINE: A set of data defining standard basic operating conditions and performance for a nominal/new engine.BINARY DATA: Variable length strings of binary information, which can represent bit map graphics, comp
21、uter object code, compressed textual data, or digitally recorded data.CHARACTER: A single unit of display or textual data stream (e.g., one letter or one number).COMPRESSION: Mathematical reduction of any volume of digital data (e.g., in a historical plot or time-series data stream).CONFIGURATION DA
22、TA: Data describing where and when engines and modules are installed and removed. The data can be accompanied by hours and cycles information.CONTINUOUSLY RECORDED DATA: Typically, data recorded during exceedance conditions, for a brief duration in real time, encompassing several seconds of multiple
23、 channel engine and/or airframe sensor readings, or data recorded as the operation is in progress, for a length of time dictated by the configuration of the recording system.DATA TYPE: Specific characteristics about representation/storing of data in the computer environment. Following types are cove
24、red: binary, character, field free text, integer, and real number.DERIVED RESULTS OR QUANTITIES: Results from simulation or performance analysis of engine operational measurements which depict the health status or trends in operational performance.EXCEEDANCE: (A flag which indicates that) the value
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