SAE AMS 2630C-2010 Inspection Ultrasonic Product Over 0 5 Inch (12 7 mm) Thick《超过0 5 inch(12 7 mm)厚产品超声波检验》.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 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/AMS2630C AEROSPACE MATERIAL SPECIFICATION AMS2630 REV. C Issued 1960-06 Revised 2010-01 Super
5、seding AMS2630B Inspection, Ultrasonic Product Over 0.5 Inch (12.7 mm) Thick RATIONALE AMS2630C revises requirements for qualification (3.1.1), transducers (3.2.2.1), shear wave references (3.2.4.4), special references (3.2.4.6), and gating (3.4.9.1.2), and is a Five Year Review and update of this s
6、pecification. 1. SCOPE 1.1 Purpose This specification covers procedures for ultrasonic inspection, by pulse-echo procedures, of flat, rectangular, round, cylindrical, and contoured products having a thickness or cross-sectional dimension greater than 0.50 inch (12.7 mm), using either contact or imme
7、rsion methods, and using the longitudinal-wave or shear-wave modes or combinations of the two, as necessary. This specification may apply to testing finished machined parts provided the parts can meet the basic testability requirements, such as size, contour, metallurgical structure, and thickness.
8、1.2 Parts with section thickness both over 0.50 inch (12.7 mm) and 0.5 inch (12.7 mm) and under may be tested using this procedure and AMS2632, as applicable. 1.3 Application This procedure has been used typically for locating and defining internal defects such as cracks, voids, laminations, and oth
9、er structural discontinuities which may or may not be exposed to the surface, but usage is not limited to such applications. 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
10、 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 from SAE Inte
11、rnational, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2632 Inspection, Ultrasonic, of Thin Materials, 0.5 Inch (12.7 mm) and Under Cross-Sectional Thickness SAE J300 Crankcase Oil Viscosity Classificatio
12、n 2.2 ASTM Publications SAE AMS2630C Page 2 of 21 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 127 Fabricating and Checking Aluminum Alloy Ultrasonic Standard Reference Blocks ASTM E 317 Evaluating
13、Performance Characteristics of Ultrasonic PulseEcho Testing Systems Without the Use of Electronic Measurement Instruments ASTM E 428 Fabrication and Control of Steel Reference Blocks Used in Ultrasonic Inspection ASTM E 1065 Evaluating Characteristics of Ultrasonic Search Units 2.3 Aerospace Industr
14、ies Association Publications Available from the Aerospace Industries Association, 1000 Wilson Boulevard, Suite 1700, Arlington, VA 22209-3928, www.aia-aerospace.org NAS-410 Nondestructive Testing Personnel Qualification and Certification 2.4 ANSI Publications Available from American National Standar
15、ds Institute, 25 West 43rd Street, New York, NY 10036, Tel: 212-642-4900, www.ansi.org. ANSI B46.1 Surface Texture 2.5 ASNT Publications Available from American Society for Nondestructive Testing, P.O. Box 28518, 1711 Arlingate Lane, Columbus, OH 43228-0518, 800-222-2768 (inside U.S. and Canada), 61
16、4-274-6003 (outside USA), www.asnt.org. SNT-TC-1A Recommended Practice, Personnel Qualification and Certification in Nondestructive Testing 2.6 ATA Publications Available from Air Transport Association of America, 1301 Pennsylvania Avenue, NW - Suite 1100, Washington, DC 20004-1707, Tel: 202-626-400
17、0, www.airlines.org. ATA-105 Guidelines for Training and Qualifying Personnel in Nondestructive Testing 3. TECHNICAL REQUIREMENTS 3.1 Qualification 3.1.1 Personnel Shall be qualified and certified in accordance with NAS-410. Alternate procedures, such as ASNT-TC-1A or ATA-105, may be used if specifi
18、ed on the drawing or purchase order. It is the suppliers responsibility to ensure that personnel are certified and function within the limits of the applicable specification or procedure. 3.1.2 Facilities Shall be subject to survey and approval by purchaser of the inspected product. Ultrasonic test
19、facility equipment shall include, but not be limited to, the basic ultrasonic test instrument, search units (transducers), appropriate ultrasonic references, couplant materials, fixtures, reference specifications, and immersion tanks where applicable. Reference specifications and documentation neces
20、sary to verify the qualification of equipment and test personnel shall be available upon request. SAE AMS2630C Page 3 of 21 3.2 Ultrasonic Test System 3.2.1 Basic Ultrasonic Test Instrument Shall be capable of producing, receiving, amplifying, and displaying on a cathode ray tube (CRT) high frequenc
21、y signals at specific frequencies as required by the test and shall be of a pulse-reflection (echo), pulse-transmission type. The instrument, if required by the test, shall be capable of being adapted with electronic circuitry, such as flaw gates and distance amplitude corrections. A minimum of a 2:
22、1 signal-to-noise ratio is required unless otherwise agreed upon by purchaser and vendor. 3.2.1.1 Instrument Linearity The instrument performance characteristics shall be evaluated in accordance with ASTM E 317 except as follows: 3.2.1.1.1 The calibration block used for evaluating vertical linearity
23、 shall be as shown in Figure 1. 3.2.1.1.2 The vertical linearity plot and the tolerance limits shall be as shown in either Figure 2 or Figure 2A. 3.2.1.1.3 The horizontal linearity check shall be made by plotting signal displacement against known thickness in the range of 1.0 to 5 inches (25.4 to 12
24、7 mm) in 1.0 inch (25.4 mm) increments; the allowable difference in thickness between that indicated by the signal displacement and the actual measured thickness shall be within 3% of the measured thickness of the respective block. Substitute performance checks are permissible when acceptable to pur
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