SAE AMS 4949B-2017 Titanium Sheet Laminated Surface Bonded.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/AMS4949B AEROSPACE MATERIAL SPECIFICATION AMS4949 REV. B Issued 2003-07 Reaffirmed 2008-11 Revi
5、sed 2017-04 Superseding AMS4949A Titanium, Sheet, Laminated, Surface Bonded RATIONALE AMS4949B results from a Five-Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers titanium in the form of laminated sheet. 1.2 Application This material has been used typically
6、for shims in which thickness is adjusted by removal of laminations as required, but usage is not limited to such applications. 1.3 Classification Materials are classified as follows: 1.3.1 Type Type I - All laminations Type II - One half laminations Type III - Three quarters laminations 1.3.2 Class
7、Class 1 - 0.002 inch (0.05 mm) thick laminations Class 2 - 0.003 inch (0.075 mm) thick laminations SAE INTERNATIONAL AMS4949 B Page 2 of 6 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 specifi
8、ed herein. The supplier may work to a subsequent revision of a document unless a 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
9、 from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS4901 Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) AMS4907 Titanium Alloy, Sheet, Strip, and Plate
10、 6.0Al - 4.0V, Extra Low Interstitial Annealed AMS4911 Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed ARP1917 Clarification of Terms Used in Aerospace Metals Specifications 2.2 ASQ Publications Available from American Society for Quality, 600 North Plankinton Avenue, Milwaukee, WI 53203,
11、Tel: 800-248-1946 (United States or Canada), 001-800-514-1564 (Mexico), or +1-414-272-8575 (all other locations), www.asq.org. ANSI/ASQC Z1.4 Sampling Procedures and Tables for Inspection by Attributes 3. TECHNICAL REQUIREMENTS 3.1 Composition 3.1.1 Laminations Shall conform to AMS4901 or harder con
12、dition. 3.1.2 Solid Stock When required, shall conform to AMS4907 or AMS4911. 3.1.3 Adhesive Shall be of a composition which will meet the fabrication and quality requirements of this specification. 3.2 Fabrication The laminated shim stock shall consist completely of laminations each 0.002 inch 0.00
13、02 inch (0.05 mm 0.005 mm) thick or 0.003 inch 0.0003 inch (0.08 mm 0.008 mm) thick, or partly of such laminations combined with a single thicker lamination, as ordered, bonded together by an adhesive such that individual laminations may be peeled for adjustment of shim thickness. The thickness of e
14、ach layer of adhesive shall not exceed 0.0003 inch (0.008 mm). 3.2.1 Sheet shall be of the thicknesses and combinations of laminations and solid base shown in Table 1. The existence of the applicable type, class, and nominal thickness shown in Table 1 is not intended to imply that all products descr
15、ibed are commercially available. SAE INTERNATIONAL AMS4949 B Page 3 of 6 Table 1 - Thickness combinations of shim stock Inch Millimeters Type I Class 1 All Laminated, 0.002 Inch (0.05 mm) Laminations Type I Class 2 All Laminated, 0.003 Inch (0.08 mm) Laminations Type II Class 1 Half Solid, Half Lami
16、nated 0.002 Inch (0.05 mm) Laminations Type II Class 2 Half Solid, Half Laminated 0.003 Inch (0.08 mm) Laminations Type III Class 1 Three Quarters Solid, One Quarter Laminated 0.002 Inch (0.05 mm) Laminations Type III Class 2 Three Quarters Solid, One Quarter Laminated 0.003 Inch (0.08 mm) Laminatio
17、ns 0.006 0.15 X 0.008 0.20 X 0.010 0.25 X 0.012 0.31 X 0.015 0.38 X X 0.016 0.41 X X 0.020 0.51 X X 0.021 0.53 X X 0.032 0.81 X X 0.033 0.84 X X 0.047 1.19 X X 0.048 1.22 X X 0.062 1.58 X X X X 0.063 1.60 X X X X 0.078 1.98 X X X X 0.080 2.03 X X X X 0.093 2.37 X X X X 0.094 2.39 X X X X 0.109 2.77
18、X X X X 0.121 3.07 X X X X X X 0.125 3.18 X X X X X X 3.3 Construction 3.3.1 General Requirements Laminations and solid stock, when applicable, shall be bonded together throughout the whole surface area in a manner which will permit peeling of the laminations for adjustment of shim thickness without
19、 the aid of mechanical devices, and without separation of the remaining laminations and solid part. Laminations shall be bonded together in such a manner that any shape can be cut from the material using suitable tools, without separation. Laminations shall remain intact without separation during no
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