SAE AIR 5301-2000 Installed Outdoor Engine Testing《户外发动机试验》.pdf
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1、SAE 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 entirelyvoluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefro
2、m, 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 written comments and suggestions.Copyright 2000 Society of Automotive Engineers, Inc.All rights reserved. Printed in U.S.
3、A.TO PLACE A DOCUMENT ORDER: (724) 776-4970 FAX: (724) 776-0790 SAE WEB ADDRESS: http:/www.sae.org400 Commonwealth Drive, Warrendale, PA 15096-0001AEROSPACE INFORMATION REPORTAIR5301Issued 2000-04Installed Outdoor Engine TestingTABLE OF CONTENTS1. SCOPE .31.1 Introduction31.2 Purpose .32. REFERENCES
4、 .32.1 Applicable Documents.33. TECHNICAL BACKGROUND.54. ADVANTAGES .55. DISADVANTAGES .86. ENGINE TEST CRITERIA126.1 Acceptance Tests 127. AIRCRAFT INSTALLED INSTRUMENTATION SYSTEMS .228. EXISTING GROUND-BASED DATA ACQUISITION/INSTRUMENTATION SYSTEMSFOR ON-THE-WING INSTALLED ENGINE TESTING 259. CAP
5、ABILITIES OF ENGINE ON-BOARD-CONDITION-MONITORING SYSTEMS (EOBCMS) .3310. INSTALLATION EFFECTS ON ENGINE PERFORMANCE.35Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-SAE AIR5301 - 2 -TABLE OF CONTENTS
6、 (Continued)11. PROCEDURES, DATA, EQUIPMENT AND PERSONNEL REQUIRED FORON-THE-WING INSTALLED ENGINE TESTING .3612. IMPACT OF ENGINE MODULARITY ON INSTALLED ENGINE TESTING.4213. CONCLUSIONS42APPENDIX A SEA LEVEL STANDARD DAY CORRECTION EQUATIONS 43FIGURE 1 Engine Test Requirement Flow Chart .6FIGURE 2
7、 Alameda Chocks .10FIGURE 3 Turbulence Control Structure 11FIGURE 4 Example Data Sheet for Turbofan Engine Tests.14FIGURE 5 Example Data Sheet for Turboprop Engine Tests 17FIGURE 6 Example Performance Curve for Turbofan Engine .18FIGURE 7 Example Performance Curve for Turbojet Engine 19FIGURE 8 Exam
8、ple Performance Curve for Turboshaft Engine 20FIGURE 9 Example Performance Curve for Turboprop Engine .21FIGURE 10 Maximum Permissible Wind Speed and Orientation for a Twin Engine Aircraft23FIGURE 11 Maximum Permissible Wind Speed and Orientation for a Four Engine Aircraft24FIGURE 12 Typical Turbofa
9、n/Jet and Turboprop Data Displays32FIGURE 13 Inlet and Exhaust Danger Zones - Takeoff Thrust - Twin Engine Aircraft.38FIGURE 14 Forward Thrust at Takeoff Power Engine Inlet and Exhaust Hazard Areas - Four Engine Aircraft 39FIGURE 15 Turboprop Aircraft Engine, Propeller and Noise Hazard Areas 40FIGUR
10、E 16 Helicopter Main and Tail Rotor and Noise Hazard Areas .41TABLE 1 Advantages of On-The-Wing Engine Testing7TABLE 2 Disadvantages of On-The-Wing Engine Testing.9TABLE 3 Power Plant Test List 13TABLE 4 Typical Design Requirements for Electronic Data Display Systems .26TABLE 5 Typical Flight Line T
11、ester Specifications.31TABLE 6 Typical Engine On-Board-Condition-Monitoring System Parametersfor Ground Testing 34Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-SAE AIR5301 - 3 -1. SCOPE:1.1 Introduct
12、ion:This SAE Aerospace Information Report (AIR) was written because of the growing interest in aircraft installed outdoor engine testing by the Federal Aviation Administration, airlines, charter/commercial operators, cargo carriers, engine manufacturers and overhaul and repair stations. This documen
13、t was developed by a broad cross section of personnel from the aviation industry and government agencies and includes information obtained from a survey of a variety of operators of fixed and rotary wing aircraft and research of aircraft and engine maintenance manuals.1.2 Purpose:This document will
14、provide aircraft operators with an overview of current industry on-the-wing engine test practices including advantages/disadvantages derived, test criteria, capabilities of remote ground based test data acquisition/instrumentation and on board condition monitoring systems, aircraft installation effe
15、cts, and a general discussion of procedures, data, equipment and personnel required to perform safe, accurate, on-the-wing engine tests. This information is provided as a guide to help operators decide to initiate, improve, expand or cease performing installed engine testing.2. REFERENCES:2.1 Applic
16、able Documents:The following publications 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. Nothing in this document supersedes appl
17、icable laws and regulations unless a specific exemption has been obtained.2.1.1 SAE ARP1587, Revision A, Gas Turbine Engine Monitoring System Guide, 1993-04-062.1.2 Boeing 767 AMM 71-00-00, PW 4000 Series Engines, November 10, 19922.1.3 Airbus Industries A320 AMM, CFM, 71-00-00, February 19882.1.4 A
18、irbus Industries A310 AMM 71-00-00, CF6-80C2A Engines2.1.5 McDonnell Douglas DC10-30 AMM 71-00-00, CF6-50C2B Engines2.1.6 Boeing 737-200 AMM 71-00-00, JT8D-9/9a/17a Engines2.1.7 Boeing 747-400 AMM 71-00-00, CF6-80C2B Engines, February 10, 19952.1.8 Airbus Industries A300-600 AMM 71-00-00, CF6-80C En
19、gines, December 1, 1989Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-SAE AIR5301 - 4 -2.1.9 NAVAIR 17-15A-89 Technical Manual, Operating Instruction and Intermediate Maintenance with IPB2.1.10 ISO/TA
20、G4/WG3; June 1992, Guide to Expression of Uncertainty in Measurement2.1.11 SAE AIR1871, Lessons Learned from Developmental and Operational Turbine Engine Monitoring Systems, Issued June 1984, Revised January 19882.1.12 SAE AIR1873, Guide to Limited Engine Monitoring Systems for Aircraft Gas Turbine
21、Engines, Issued May 5, 1988, Reaffirmed and under revisions May 19942.1.13 SAE ARD50002, A Discussion of Standardized Concepts for Condition Monitoring and Performance Analysis Software, Issued November 5, 19922.1.14 SAE AIR4061, Guidelines for Integration of Engine Monitoring Functions with On Boar
22、d Aircraft Systems, Issued August 1, 19902.1.15 SAE AIR1839, A Guide to Aircraft Turbine Engine Vibration Monitoring Systems, Issued October 1986, Revised March 10, 19922.1.16 Naval Air Warfare Center, Aircraft Division, Lakehurst, New Jersey, Jet Engine Test Facility Correlation Report. NAS Sigonel
23、la, Italy, A/F37T-19 Turboprop Jet Engine Test Facility,T56-A-14, T56-A-16, and T56-A-425, Engines2.1.17 Naval Air Warfare Center, Aircraft Division, Lakehurst, New Jersey, Jet Engine Test Facility Correlation Report, MCAS Futema, Japan, A/F37T-19 Turboprop Engine Test Facility,T56-A-16 Engines2.1.1
24、8 Pratt all contributing to increased flight safety (Reference 2.1.1). The advantages listed in Table 1 can be realized if the airframe and engine maintenance manuals on-the-wing-test requirements are met. However, there are also many disadvantages that can be encountered which are addressed in Sect
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