SAE J 549-2015 Preignition Rating of Spark Plugs.pdf
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1、 SURFACE VEHICLE RECOMMENDED PRACTICE J549 MAR2015 Issued 1947-12 Revised 2015-03 Superseding J549 MAR2013 (R) Preignition Rating of Spark Plugs RATIONALE Information updated to reflect current industry practice related to the heat range testing of spark plugs. Key changes are noted below: Deleted r
2、eferences to obsolete U.S Government publications related to lubricating oil and oil for fuel and added applicable SAE document references. Updated section on operating conditions to include engine warm-up procedure. 1. SCOPE This SAE Recommended Practice describes the equipment and procedures used
3、in obtaining preignition ratings of spark plugs. 1.1 The spark plug preignition ratings obtained with the equipment and procedure specified herein are useful for comparative purposes and are not to be considered as absolute values since different numerical values may be obtained in different laborat
4、ories. 2. REFERENCES 2.1 Applicable Documents The following publications form a part of this specification to the extent specified herein. Unless otherwise indicated, the latest issue of SAE publications shall apply. 2.1.1 SAE Publication Available from SAE International, 400 Commonwealth Drive, War
5、rendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. SAE HS840 Manual for the SAE 17.6 Cubic Inch Spark Plug Rating Engine, including Maintenance and Overhaul SAE J1899 Lubricating Oil, Aircraft Piston Engine (Ashless Dispersant) SAE J1966 Lub
6、ricating Oil, Aircraft Piston Engine (Non-dispersant Mineral Oil) SAE J2203 SAE 17.6 Cubic Inch Spark Plug Rating Engine _ 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 entirely
7、 voluntary, 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 revised, reaffirmed, stabilized, or cancelled. S
8、AE invites your written comments and suggestions. Copyright 2015 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
9、prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visi
10、t http:/www.sae.org/technical/standards/J549_201503 SAE INTERNATIONAL J549 Revised MAR2015 Page 2 of 6 3. EQUIPMENT SAE 17.6 engine with the cylinder barrel either knurled or honed, with or without chemically treated surface, and compression piston rings which may or may not be chrome plated. 4. SPE
11、ED The nominal speed is to be 2700 rpm, but is not to be over 2765 rpm when firing, nor below 2670 rpm when motoring. 5. COMPRESSION RATIO 5.6:1. 6. IGNITION SOURCE Magneto or approved alternate. 7. SPARK PLUG INSTALLATION Threads in the spark plug hole opening should conform in size and length to t
12、he standards established by SAE for the rating engine. 7.1 SAE recommended torque values should be used when installing plugs in the engine/bushing. 7.1.1 Reducer bushings or adaptors should not be used. 8. FUEL Although 98% - one degree Benzene, 2% - Specification SAE J1966 SAE 60 NONADDITIVE aviat
13、ion oil, with 0.8 mL/L (3 cc/gal) T.E.L. added has been used as the standard for many years, availability of benzene is becoming highly restricted by virtue of it being a known carcinogen. In lieu of this fact, a number of substitute or alternate fuels are being tested as replacements. Such fuels ar
14、e Toluene or a suitable leaded racing gasoline, which has sufficient octane rating to insure proper operation without a propensity towards spark knock or detonation. It still must be noted that additives such as aviation oil and T.E.L. must be used in those fuels to underwrite cylinder wear and valv
15、e seat longevity. Even with those safeguards in place, the amount of boost required to preignite a plug may be limited by the octane rating of those alternate fuels, which are obtainable. 9. FUEL INJECTION TIMING The fuel injector or injector pump port shall begin to close 60 degrees 5 degrees of cr
16、ankshaft angle After Top Dead Center (ATDC) on the intake stroke. 10. FUEL CIRCULATION RATE 2 L/min 1 L/min (1/2 gal/min 1/4 gal/min). 11. FUEL INJECTION PUMP Using a mechanical fuel injection system, gallery pressure of the fuel injection pump is to be 100 kPa 10 kPa (15 psi 2 psi). However, feed s
17、ystem pressures to an approved alternate electronic fuel injection system could vary widely with type being used. The main requirement is to insure that an adequate pressure is maintained for proper operation. 12. FUEL PRESSURES-INJECTION With a mechanical system, pressure should be 5170 kPa (750 ps
18、i) minimum. When using an approved alternate electronic fuel injection system, the minimum pressure required should be adequate to guarantee sufficient fuel delivery and atomization for engine operation. SAE INTERNATIONAL J549 Revised MAR2015 Page 3 of 6 13. MIXTURE STRENGTH (FUEL TO AIR RATIO) The
19、mixture strength is that which gives maximum thermal plug temperature. 14. COOLANT The coolant should be water plus .26 g/1 L (1 g/gal) of an inhibitor. The total dissolved and suspended solids should not exceed 120 ppm. 15. JACKET INLET TEMPERATURE a. With pressure cooling control - 107 C 3 C (225
20、F 5 F) b. With insert head engine - 88 C 1 C (190 F 2 F) 16. COOLANT FLOW 20 L/min 2 L/min (5 gal/min 1/2 gal/min). 17. CRANKCASE OIL If main and/or rod bearings are silver or suspected of being silver alloy, oil is to be nonadditive SAE J1966, SAE viscosity grade 60 aviation oil. If it is determine
21、d that bearings are not of a silver composition, then either the nonadditive SAE 60 viscosity aviation oil or an additive oil, which complies with SAE J1899 may be used. Included in this are multiviscosity lubricants approved for replacing the SAE viscosity grade 60 aviation oil. 18. OIL PRESSURE a.
22、 In main bearings, 650 kPa 40 kPa (95 psi 5 psi) b. In valve gear, 100 kPa (15 psi) minimum at operating temperature 19. OIL TEMPERATURE 88 C 5 C (190 F 10 F). 20. OIL QUANTITY Oil level is maintained at the center of the oil level sight glass if so equipped without the engine rotating. If a needle
23、valve assembly is used in place of a sight glass, oil must be released when opened. 21. OPERATING CONDITIONS These operating instructions are for use with the 17.6 Spark Plug Rating Engine. It is recognized that individual laboratories will have slightly different operation requirements; however, th
24、e fundamental operations should follow these instructions as closely as possible so that the rating results will be comparable. Only those conditions that affect the rating of the spark plug or the safety of personnel and equipment are specified as required, but recommended procedures or conditions
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