SAE AMS 2629E-2017 Fluid Jet Reference.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 entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising there
2、from, 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. SAE invites your written comments and suggestions. Copyright 2017 SAE International All rights reserved. No part of this p
3、ublication 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 permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-497
4、0 (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 visit http:/standards.sae.org/AMS2629E AEROSPACE MATERIAL SPECIFICATION AMS2629 REV. E Issued 1989-07 Reaffirmed 2001-01 Revi
5、sed 2017-02Superseding AMS2629D Fluid, Jet Reference RATIONALE Revise fuel composition to adjusted/spiked Jet A Fuel per SAE G-9 committee discussion. Change will reduce cost, ease production, and maximize consistency with in-service fuel composition. Reverted to AMS2629B sulfur and mercaptan levels
6、 to address levels in global fuel supply. Reduced icing inhibitor concentration to current fuel specification limits. Corrected aromatic blend constituent volume percents. 1. SCOPE 1.1 Form This specification covers a mixture of liquid hydrocarbons and soluble additives. 1.2 Application To provide a
7、 standard composition, simulating aviation jet engine fuel. This fluid is intended for use in laboratory tests involving compatibility and interaction with aircraft materials, but usage is not limited to such applications. 1.3 Classification Jet reference fluid shall be classified as follows: Type 1
8、 Liquid hydrocarbons without the addition of metal ions. Type 1 fluid is intended for all material compatibility tests except chalking evaluations. Type 2 Liquid hydrocarbons with a controlled concentration of metal ions. Type 2 fluid is intended for chalking evaluations. 1.3.1 Type 1 shall be suppl
9、ied unless Type 2 is ordered. 1.4 Safety - Hazardous Materials Shall be in accordance with AS5502 (1.1). 2. APPLICABLE DOCUMENTS Shall be in accordance with AS5502 (Section 2). SAE INTERNATIONAL AMS2629E Page 2 of 7 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warre
10、ndale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AS5502 Standard Requirements for Aerospace Sealants and Adhesion Promoters 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken,
11、PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM D130 Standard Test Method for Corrosiveness to Copper from Petroleum Products by Copper Strip Test ASTM D156 Standard Test Method for Saybolt Color Of Petroleum Products (Saybolt Chromometer Method) ASTM D664 Standard Test Method for Acid Number o
12、f Petroleum Products by Potentiometric Titration ASTM D1094 Standard Test Method for Water Reaction of Aviation Fuels ASTM D1266 Standard Test Method for Sulfur in Petroleum Products (Lamp Method) ASTM D1319 Standard Test Method for Hydrocarbon Types in Liquid Petroleum Products by Fluorescent Indic
13、ator Adsorption ASTM D1655 Standard Specification for Aviation Turbine Fuels ASTM D2622 Standard Test Method for Sulfur in Petroleum Products by Wavelength Dispersive X-Ray Fluorescence Spectrometry ASTM D3227 Standard Test Method for (Thiol Mercaptan) Sulfur in Gasoline, Kerosine, Aviation Turbine,
14、 and Distillate Fuels (Potentiometric Method) ASTM D3242 Standard Test Method for Acidity in Aviation Turbine Fuel ASTM D4294 Standard Test Method for Sulfur in Petroleum and Petroleum Products by Energy Dispersive X-ray Fluorescence Spectrometry ASTM D5006 Standard Test Method for Measurement of Fu
15、el System Icing Inhibitors (Ether Type) in Aviation Fuels ASTM D6379 Standard Test Method for Determination of Aromatic Hydrocarbon Types in Aviation Fuels and Petroleum Distillates - High Performance Liquid Chromatography Method with Refractive Index Detection 2.3 U.S. Government Publications Copie
16、s of these documents are available online at http:/quicksearch.dla.mil. MIL-PRF-25017 Inhibitor, Corrosion / Lubricity Improver, Fuel Soluble MIL-DTL-85470 Inhibitor, Icing, Fuel System, High Flash NATO Code Number S-1745 SAE INTERNATIONAL AMS2629E Page 3 of 7 3. TECHNICAL REQUIREMENTS 3.1 Standard
17、Tolerances Unless otherwise specified, standard tolerances shown in Table 1 shall apply: Table 1 - Standard tolerances Measurement Units Tolerance Temperature 2 F (1 C) Day 2 hours Hour 5 minutes Minute 10 seconds Inches (mm) 0.010 inch (0.25 mm) 3.2 Material 3.2.1 Type 1 Fluid The individual hydroc
18、arbon and aromatic constituents of Type 1 fluid shall conform to the percentages by volume shown in Table 2 determined by wet chemical methods or by other analytical methods acceptable to purchaser. The total volume or mass percent of all fluid constituents shall conform to the percentages shown in
19、Table 2, independent of initial Jet A constituent values, determined in accordance with the indicated test procedures. Table 2 - Fluid composition Constituents Volume % Mass % Test Procedures Jet A Fuel1Total 73.8 1 ASTM D1655 (Remainder) Aromatics Total 25 12ASTM D1319 or ASTM D6379 Sulfur Di-Tert-
20、Butyl Disulfide (CAS 110-06-5) 1.0230.42 0.02 ASTM D4294, ASTM D1266, or ASTM D2622 Mercaptan 1-Decanethiol (CAS 143-10-2) 0.02630.005 0.0005 ASTM D3227 Fuel System Icing Inhibitor MIL-DTL-85470 0.11 0.02 ASTM D5006 Lubricity Improver/Corrosion Inhibitor4MIL-PRF-25017 0.0017 0.0002 1 Jet A fuel leve
21、ls of the constituents listed should be verified before addition of reference fluid components. Final fluid composition must meet Table 2 requirements. 2 Aromatic content of as-received Jet A fuel shall be adjusted to the required volume percent by adding the aromatic blend identified in Table 3. 3V
22、olume percent provided as estimate to achieve mass percent; mass percent shall be measured. 4Unicor J was used in initial test program. SAE INTERNATIONAL AMS2629E Page 4 of 7 Table 3 - Aromatic blend Constituents5, 6Volume % Aromatic 100 30% 0.5% Aromatic 150 60% 0.5% Aromatic 200 10% 0.5% 5Aromatic
23、 100, 150, and 200 manufactured and distributed by ExxonMobil. 6Aromatic products marketed under the tradename Solvesso outside of North America. 3.2.1.1 The fluid shall be stored out of contact with light in containers which are inert to the fluid ingredients (see 5.1.1). 3.2.1.2 The fluid shall be
24、 stored below 80 F (27 C). Refrigeration at 40 F (4 C) of the fuel is not required, but is recommended to maximize constituent stability. 3.2.2 Type 2 Fluid Type 2 fluid shall be produced by blending the individual components of Type 1 fluid in amber glass containers and then adding 0.50 ppm by weig
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