SAE AMS 2642D-2010 Structural Examination of Titanium Alloys Etch-Anodize Inspection Procedure《钛合金刻蚀阳极电镀检验规程的结构检查》.pdf
《SAE AMS 2642D-2010 Structural Examination of Titanium Alloys Etch-Anodize Inspection Procedure《钛合金刻蚀阳极电镀检验规程的结构检查》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 2642D-2010 Structural Examination of Titanium Alloys Etch-Anodize Inspection Procedure《钛合金刻蚀阳极电镀检验规程的结构检查》.pdf(6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 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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2010 SAE International All rights reserved. No part of this publication m
3、ay 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: +1 724-776-4970 (outside U
4、SA) 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/AMS2642DAEROSPACEMATERIALSPECIFICATIONAMS2642 REV. D Issued 1972-11 Revised 2010-10Supersedin
5、g AMS2642C Structural Examination of Titanium Alloys Etch-Anodize Inspection Procedure RATIONALE AMS2642D results from a Five Year Review and update of this specification. 1. SCOPE 1.1 Purpose This specification covers a procedure for revealing the macrostructure and microstructure of selected titan
6、ium alloys. 1.2 Application This procedure has been used typically for detecting segregation, inclusions, and other defects in alpha-beta and certain alpha titanium alloys. 1.3 Safety-Hazardous Materials While the materials, methods, applications, and processes described or referenced in this specif
7、ication may involve 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
8、to ensure the health 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
9、 specific document issue 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:
10、 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS4901 Titanium Sheet, Strip, and Plate, Commercially Pure, Annealed, 70.0 ksi (485 MPa) Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without l
11、icense from IHS-,-,-SAE AMS2642D Page 2 of 62.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM E 1447 Determination of Hydrogen in Titanium and Titanium Alloys by the Inert Gas Fusion T
12、hermal Conductivity Method 2.3 ASME Publications Available from American Society of Mechanical Engineers, 22 Law Drive, P.O. Box 2900, Fairfield, NJ 07007-2900, Tel: 973-882-1170, www.asme.org.ASME B46.1 Surface Texture, Roughness, Waviness and Lay 3. TECHNICAL REQUIREMENTS 3.1 Materials and Solutio
13、ns 3.1.1 Etch Solution An aqueous acid salt solution shall be prepared, the concentration of which shall be adjusted to maintain a metal removal rate of 0.00003 to 0.00005 inch (0.76 to 1.27 m) in 80 to 100 seconds after the onset of gas evolution. Operation shall be at room temperature. 3.1.2 Anodi
14、ze Solution An aqueous solution of 13 to 17 ounces/gallon (97 to 127 grams/L) of hydrated trisodium phosphate (Na3PO412H2O)shall be prepared and maintained at 8.5 pH 0.5 at room temperature. See 8.3. 3.1.3 Back Strip Solution An agitated aqueous solution of 42.5 to 51.5 ounces/gallon (320 to 385 gra
15、ms/liter) of nitric acid (technical grade, approximate sp gr 1.42) and 1.3 to 4.7 ounces/gallon (10 to 35 grams per liter) hydroflluoric acid (technical grade, approximate sp gr 1.15) shall be maintained at room temperature. 3.1.4 Specimens for Macrostructure 3.1.4.1 Bars, Extrusions, Plates, and St
16、ock for Forging or Extruding Specimens shall be transverse cross-sections not less than 0.50 inch (12.7 mm) thick, cut from the product to be tested. Specimens from stock for alpha beta forging or alpha beta extrusion shall be heated to a temperature 50 F 25 (28 C 14) degrees below the beta transus
17、as determined for the heat, held at heat for 60 minutes 5, and cooled at a rate equivalent to air cool or faster. Specimens from stock for beta forging or beta extrusion shall be heated to a temperature 50 F 25 (28 C 14) degrees above the beta transus as determined for the heat. Specimens shall be m
18、achined to have surface texture of 70 microinches (1.8 m) AA or finer, determined in accordance with ASME B46.1. 3.1.4.2 Forgings When dimensions permit, forgings shall be machined all over to remove approximately 0.040 inch (1.0 mm) of metal to ensure freedom from alpha case. If forgings are to be
19、inspected by ultrasonic inspection procedures, the configuration used for such inspection is acceptable. Surface roughness shall be 70 microinches (1.8 m) AA or finer, determined in accordance with ASME B46.1. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reprodu
20、ction or networking permitted without license from IHS-,-,-SAE AMS2642D Page 3 of 63.1.4.3 Finished Parts Specimens shall be complete parts. No special preparation is required. 3.2 Equipment 3.2.1 A DC voltage source shall be capable of providing direct current with a maximum of 6% ripple at 30 VDC
21、(under no load) and shall be capable of ramping up the voltage to 30 VDC in 1 to 3 seconds. Automatic control is preferred. The equipment shall include a volt and amp meter. 3.2.2 Fixtures shall be free of distortion, loose fittings, worn areas and corrosion. 3.3 Preparation 3.3.1 Specimens shall be
22、 free from water breaks. If water breaks are observed, parts shall be recleaned and reinspected for water break until no water breaks are observed. See 8.5. 3.3.2 Location of electrical contact points on finished parts shall be acceptable to the cognizant engineering organization. 3.3.3 Areas on fin
23、ished parts that are not to be etch-anodize-inspected shall be protected by a suitable masking material. Such areas shall include inspection areas or surfaces, balance and identification markings applied by electrolytic etching, hardfaced areas, and nontitanium surfaces. 3.3.4 Etch-Anodize Macrostru
24、cture Procedure 3.3.4.1 Specimens shall be immersed for 80 to 100 seconds after the onset of gassing in an agitated acid salt solution in accordance with 3.1.1. Immersed parts shall be agitated to remove entrapped air. Immediately after removal, specimens shall be immersed in clean tap water. Specim
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