SAE AIR 4713A-2013 Aerospace - Chlorinated Solvent Contamination of MIL-H-5606 MIL-H-83282 Vehicle Hydraulic Systems《航空航天 MIL-H-5606 MIL-H-83282标准车辆液压系统的氯化溶剂污染》.pdf
《SAE AIR 4713A-2013 Aerospace - Chlorinated Solvent Contamination of MIL-H-5606 MIL-H-83282 Vehicle Hydraulic Systems《航空航天 MIL-H-5606 MIL-H-83282标准车辆液压系统的氯化溶剂污染》.pdf》由会员分享,可在线阅读,更多相关《SAE AIR 4713A-2013 Aerospace - Chlorinated Solvent Contamination of MIL-H-5606 MIL-H-83282 Vehicle Hydraulic Systems《航空航天 MIL-H-5606 MIL-H-83282标准车辆液压系统的氯化溶剂污染》.pdf(13页珍藏版)》请在麦多课文档分享上搜索。
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 ther
2、efrom, 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 2013 SAE International All rights reserved. No part of this
3、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 permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-49
4、70 (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:/www.sae.org/technical/standards/AIR4713AAEROSPACE INFORMATION REPORT AIR4713 REV. A Issued 1992-08 Reaffirmed 20
5、02-05 Stabilized 2013-06 Superseding AIR4713 Aerospace - Chlorinated Solvent Contamination of MIL-H-5606/MIL-H-83282 Vehicle Hydraulic Systems RATIONALE This document has been determined to contain basic and stable technology which is not dynamic in nature. STABILIZED NOTICE This document has been d
6、eclared “Stabilized“ by the A-6C3 Fluids Committee, and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability of technical requirements. Newer technology may exist. Copyright SAE International Provided by IHS under lice
7、nse with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-TABLE OF CONTENTS1. SCOPE . 41.1 Purpose 42. APPLICABLE DOCUMENTS52.1 SAE Publications .52.2 Military Publications .53. FLUID SAMPLE ANALYSIS TECHNIQUES.53.1 Fluid Sample Analysis Techniques 53.2 Specific
8、Analysis Techniques 53.2.1 Gas Chromatography 53.2.2 Microcoulometric Procedure. 63.2.3 X-ray Fluorescence Spectroscopy Method. 64. SOLUBLE CHLORINE CONTAINING CONTAMINANTS.94.1 Potential Contaminant Sources . 95. RECOMMENDATIONS 105.1 Contaminant Allowable Limits105.2 Recommended Chlorine Contamina
9、tion Allowable Limits 105.3 Contamination Removal Methods. 105.3.1 Drain. Refill and Flush 105.3.2 Purification Equipment Method105.4 Recommended Maintenance Practices 11APPENDIX A . 12SAE AIR4713A Page 1 of 12_ Copyright SAE International Provided by IHS under license with SAENot for ResaleNo repro
10、duction or networking permitted without license from IHS-,-,-FOREWORDIn June 1982 a study entitled “Investigation of Air Force MIL-H-5606 Hydraulic System Malfunctions Induced by Chlorine Solvent Contamination“ (AFWAL-TR-82-4027) was issued by the Air Force Wright Aeronautical Laboratories (AFWAL/ML
11、B) and the University of Dayton Research Institute (Bibliography 1). Information in that study reported that in 1975 a large number of C-141 mishaps occurred involving stuck selector valves in landing gear and door systems throughout the Military Airlift Command (MAC). Analysis of hydraulic fluid fr
12、om a problem aircraft hydraulic system revealed the presence of the chlorinated solvent 1,1,2- trichlorotrifluoroethane and water. Auger spectroscopy surface analysis of the stuck valve and spool assembly involved revealed the presence of elements chlorine, oxygen, iron, and carbon. With this proof
13、of chlorinated solvents being the cause of stuck valves in a C-141 mishap, a fleet wide survey of aircraft hydraulic systems was performed to determine the level of chlorinated solvents and water in hydraulic systems. Simultaneously, maintenance overhaul procedures were modified to eliminate the use
14、 of chlorinated solvents as much as possible. A maximum limit was tentatively established for chlorine contamination in C-141 hydraulic systems at 200 parts per million (ppm) chlorine, based on the Navys success with a 200 ppm limit with the P-3 aircraft. Upon establishing this limit, C-141 aircraft
15、 were drained and flushed if their systems exceeded this limit. The use of chlorinated solvents was banned from use in the C-141 hydraulic systems and component overhauls. As a result of that study, a level of 200 ppm maximum allowable chlorine limit was established.a. Summary: Chlorine contaminatio
16、n of aircraft hydraulic fluids has been known to cause considerable amounts of damage to hydraulic flight control systems and their corresponding component parts. In an effort to statistically reveal the origins of, and the damages caused by chlorine contamination, a survey was presented to randomly
17、 selected aerospace corporations and government organizations by the Fluids Panel of Committee A-6. Based on the preliminary data, a problem exists with chlorine contamination in hydraulic systems. Data contained in a follow-up survey identified chlorofluorocarbon based cleaning fluids as the common
18、 chlorine containing fluid in use.The source of the chlorine containing contaminants is primarily solvents used in cleaning/degreasing of aircraft parts. Care must be exercised when such solvents are specified to minimize all opportunities for their being introduced into the hydraulic fluid. Such so
19、lvents are normally miscible with the hydraulic fluid and their presence can only be determined by laboratory analytical techniques such as those outlined in this document.b. Types and Percentages Measured: During 1975 and 1976 hydraulic fluid samples were taken from Air Force aircraft at various ba
20、ses. Aircraft sampled included C-141, B-52, F-105, F-111, F-4, T-38, C-5A, KC-135, F-106 aircraft, and crash accident samples. Also sampled were test stands, servicing carts, and new hydraulic fluids in order to study when and how the chlorinated solvents were introduced into operational hydraulic s
21、ystems. When these initial samples were taken, chlorine content was measured at the various ALC laboratories by x-ray fluorescence techniques which were later recognized to contain possible serious analytical errors. While any particular data point could be in question, the overall trends of chlorin
22、e contamination in hydraulic fluids are considered to be valid.SAE AIR4713A Page 2 of 12_ Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-c. Analysis Results: Of the 250 aircraft fluid samples analyz
23、ed, results are given in parts per million chlorine, number of samples analyzed with that value, and the percentage of the total samples. (1) 300 ppm and above: 1 sample, 1%(2) 200 - 300 ppm: 5 samples, 2%(3) 100 - 199 ppm: 38 samples, 15%(4) 0 - 100 ppm: 205 samples, 82%Of the ground equipment flui
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