SAE AMS 1740-2007 Compound Alkaline Aqueous Cleaner Aircraft Turbine Engine Components《飞行器涡轮发动机元部件用碱性水基清洗剂化合物》.pdf
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1、AEROSPACEMATERIAL SPECIFICATIONAMS1740Issued 2007-07Reaffirmed 2015-04Compound, Alkaline Aqueous CleanerAircraft Turbine Engine ComponentsRATIONALEAMS1740 has been reaffirmed to comply with the SAE five-year review policy._SAE Technical Standards Board Rules provide that: “This report is published b
2、y 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 therefrom, is the sole responsibility of the user.”SAE reviews each technical report
3、 at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2015 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any
4、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: +1 724-776-4970 (outside USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:
5、/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS17401. SCOPE 1.1 Form This specification covers an alkaline aqueous cleaner compound in the form of a liquid concentrate or a water-soluble powder for dilution with wa
6、ter. 1.2 Application This product has been used typically for removing oils, greases, or other soils from aircraft turbine engine parts by immersion in a solution of the compound at elevated temperature or spray cleaned in a parts washer, but usage is not limited to such applications. Restrictions f
7、or cleaning titanium parts may be imposed by the engine manufacturer. 1.3 Classification Compounds conforming to this specification are classified as follows: Type 1 - Liquid concentrate Type 2 - Water-soluble powder 1.3.1 Type 1 shall be supplied unless Type 2 is ordered. 1.4 Precautions Cleaner co
8、mpound may contain chemicals which, if improperly used, could be hazardous to the health and safety of operators. Protective clothing including eye shields, suitable gloves, and apron should be worn when preparing and using compound. Tanks shall be prepared and operated under conditions of adequate
9、fume extraction and with due regard to the safety recommendations of the manufacturer of the compound together with local workshop safety regulations. 1.5 Safety - Hazardous Materials While the materials, methods, applications, and processes described or referenced in this specification may involve
10、the use of hazardous materials, this specification does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health
11、 and safety of all personnel involved. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document i
12、ssue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (insid
13、e USA and Canada) or 724-776-4970 (outside USA), www.sae.org. ARP1755 Effect of Cleaning Agents on Aircraft Engine Materials, Stock Loss Test Method 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www
14、.astm.org. ASTM D 1568 Sampling and Chemical Analysis of Alkylbenzene Sulfonates ASTM D 2667 Biodegradability of Alkylbenzene Sulfonates ASTM F 945 Stress Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials 3. TECHNICAL REQUIREMENTS 3.1 Composition The composition of the compound shal
15、l be optional with the manufacturer except that, when prepared for use, the solution shall be alkaline. When prepared in accordance with manufacturers instructions, the compound shall form a homogeneous solution, with no solid sediment at room temperature and shall meet the applicable requirements o
16、f 3.2. 3.2 PropertIes The compound shall conform to the following requirements; tests shall be performed in accordance with specified test methods on the product supplied at the maximum concentration and temperature recommended by the manufacturer. 3.2.1 Stock Loss Test panels of alloys or electrode
17、posits shall not incur stock loss exceeding 0.000025 inch (0.635 m) per surface and plasma deposited coatings shall not incur stock loss exceeding 0.0001 inch (2.5 m), when tested in accordance with ARP1755, Category 10. Stock loss figures shall be reported for all materials specified in ARP1755, Ca
18、tegory 10. Vendor shall indicate where compound is not recommended for particular alloys or coatings. 3.2.2 Surface Attack Test panels and bars used for the stock loss test of 3.2.1 shall neither exhibit pitting corrosion nor show visual evidence of degradation, when examined at 50X magnification un
19、der good oblique surface lighting conditions. SAE INTERNATIONAL AMS1740 Page 2 of 5_ 3.2.3 Hot Corrosion Cleaner shall neither produce visual corrosion nor localized microscopic corrosion where the depth of attack is greater than 0.0003 inch (0.0075 mm), determined in accordance with 3.2.3.1 on the
20、alloys shown in Table 1. TABLE 1 - HOT CORROSION PARAMETERS Panel Material Bake Temperature F Bake Temperature CAMS 4025 Aluminum Alloy 399 204 AMS 4037 Aluminum Alloy 399 204 AMS 4911 Titanium Alloy 900 482 AMS 4916 Titanium Alloy 900 482 AMS 5040 Carbon Steel, nickel- cadmium plated as in AMS 2416
21、 849 454 AMS 5040 Carbon Steel, coated with MIL-C-81751, Type I, Class 750 399 AMS 5504 Stainless Steel 1051 566 AMS 5510 Stainless Steel 1600 871 AMS 5536 Nickel Alloy 1600 871 AMS 5544 Nickel Alloy 1600 871 AMS 5608 Cobalt Alloy 1600 871 3.2.3.1 Degrease two 1 0.5 0.05 inch (25 13 1.3 mm) panels o
22、f each alloy using absorbent paper tissue and wiping with a suitable solvent and then with isopropanol. After drying at ambient temperature for 60 minutes 5, immerse one panel of each type in cleaning compound for 15 seconds, and air dry. Bake both panels of each type for 8 hours 0.1 at the indicate
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