SAE AMS 1384A-1991 ACID INHIBITED PHOSPHORIC Aircraft Turbine Engine Components Room Temperature Application《室温下飞机涡轮发动机组件用抑制磷酸》.pdf
《SAE AMS 1384A-1991 ACID INHIBITED PHOSPHORIC Aircraft Turbine Engine Components Room Temperature Application《室温下飞机涡轮发动机组件用抑制磷酸》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 1384A-1991 ACID INHIBITED PHOSPHORIC Aircraft Turbine Engine Components Room Temperature Application《室温下飞机涡轮发动机组件用抑制磷酸》.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、AEROSPACEMATERIAL1 = jA,M;pI;SPECIFICATION IssuedIRevised 1 JUL 1991Superseding AMS 1384ACID, INHIBITED PHOSPHORICAircraft Turbine Engine ComponentsRoom Temperature Application1. SCOPE:1.1 Form:This specification covers an inhibited phosphoric acid in the form of aliquid concentrate or a water solub
2、le powder for dilution with water.1.2 Application:Primarily for derusting of aircraft turbine engine ferrous components andremoval of heat scale and other contamination from the surface of nickelalloys by immersion at room temperature. Should not be used on steel partshaving hardness of 40 HRC or ov
3、er.1.3 Precautions:Inhibited acid may contain chemicals which, if improperly used, could behazardous to the health and safety of operators. Protective clothingincluding eye shields, suitable gloves, and apron should be worn whenpreparing and using acid. Tanks shall be prepared and operated undercond
4、itions of adequate fume extraction and with due regard to the safetyrecommendations of the manufacturer of the acid mixture together with localworkshop safety regulations.SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineer
5、ing 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 at least every five years at which time it may be
6、reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2007 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, r
7、ecording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org RATIONALE This document has been reaffirmed to
8、comply with the SAE 5-year Review policy. Reaffirmed FEB 2007I AMS 1384A SAE AMS 1384A I1.4 Safety - Hazardous Materials:While the materials, methods, applications, and processes described orreferenced in this specification may involve the use of hazardous materials,this specification does not addre
9、ss the hazards which may be involved insuch use. It is the sole responsibility of the user to ensure familiaritywith the safe and proper use of any hazardous materials and to takenecessary precautionary measures to ensure the health and safety of allpersonnel involved.2. APPLICABLE DOCUMENTS:The fol
10、lowing publications form a part of this specification to the extentspecified herein. The latest issue of SAE publications shall apply. Theapplicable issue of other publications shall be the issue in effect on thedate of the purchase order.2.1 SAE Publications:Available from SAE, 400 Commonwealth Dri
11、ve, Warrendale, PA 15096-0001.AMS 2825 Material Safety Data SheetsARP1755 Effect of Cleaning Agents on Aircraft Engine Materials, StockLoss Test Method2.2 ASTM Publications:Available from ASTM, 1916 Race Street, Philadelphia, PA 19103-1187.ASTM D 1568 Sampling and Chemical Analysis of Alkylbenzene S
12、ulfonatesASTM D 2667 Biodegradability of Alkylbenzene Sulfonates2.3 U.S. Government Publications:Available from Standardization Documents Order Desk, Building 4D, 700Robbins Avenue, Philadelphia, PA 19111-5094.MIL-STD-2073-1 - DOD Materiel, Procedures for Development and Application ofPackaging Requ
13、irements3. TECHNICAL REQUIREMENTS:3.1 Composition:Shall be optional with the manufacturer but, when prepared in accordancewith manufacturers instructions, shall form a liquid product, with no solidsediment at room temperature, meeting the requirements of 3.2. Solutionmake up and control shall be in
14、accordance with manufacturers instructionsand purchasers requirements.-2-AMS 1384A SAE AMS 1384A3.2 Properties:The product shall conform to the following requirements; tests shall beperformed in accordance with specified test methods on the product suppliedat the maximum concentration and temperatur
15、e recommended by the manufacturer.3.2.13.2.23.2.3Stock Loss: Test panels of alloys or electrodeposits shalstock loss exceeding 0.000025 inch (0.635 Pm) per surfacedeposited coatings shall not incur stock loss exceeding 0.(2.5 Pm) when tested in accordance with ARP1755, Categoryrequired in ARP1755, s
16、tock loss figures shall be reported.indicate where the product is not recommended for particulsurface coatings.1 not incurand plasma0001 inch1. WhereVendor mayar alloys orSurface Attack: Test panels and bars used for the stock loss test of3.2.1 shall neither exhibit pitting corrosion nor show visual
17、 evidence ofsurface cracks, when examined at 50X magnification under good obliquesurface lighting conditions.Biodegradability: Vendor shall supply evidence that surfactants used inthe product shall be at least 90% biodegradable, determined either inaccordance with ASTM D 2667 where relevant to surfa
18、ctant type or byalternative methods, appropriate to surfactant type, acceptable topurchaser.3.2.3.1 Evidence of surfactant biodegradability does not guarantee that the acidmay be discharged in either concentrated or diluted form into publicwaterways or sewerage systems; manufacturers shall give advi
19、ce on themeans for disposal.3.2.4 Storage Stability: Acid, stored at 25C + 5 (77F + 9) for one year shallshow no visual evidence of deterioration and shall meet all othertechnical requirements.3.2.5 Performance: Acid, prepared and used in accordance with manufacturersinstructions shall, at room temp
20、erature, remove rust from ferrous partsand remove heat scale from nickel alloys. Acid, which meets all othertechnical requirements, shall be tested for cleaning performance in anapproved engine overhaul facility for not less than six months, duringwhich time at least ten turbofan or turbojet engines
21、, or equivalent, shallbe processed with satisfactory results before approval for service use isgranted by the applicable engine manufacturer.3.3 Quality:Acid, as received by purchaser, if a liquid, shall be clear, homogeneous,and free from solid particles and separation and from foreign materialsdet
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAEAMS1384A1991ACIDINHIBITEDPHOSPHORICAIRCRAFTTURBINEENGINECOMPONENTSROOMTEMPERATUREAPPLICATION 室温 下飞机

链接地址:http://www.mydoc123.com/p-1020478.html