SAE AMS 2375E-2017 Control of Forgings Requiring First Article Approval.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/AMS2375E AEROSPACE MATERIAL SPECIFICATION AMS2375 REV. E Issued 1969-05 Reaffirmed 2007-06 Revi
5、sed 2017-07 Superseding AMS2375D Control of Forgings Requiring First Article Approval RATIONALE AMS2375E results from a Five-Year Review and update of this specification that requires hardness surveys and testing (3.2.3.2 and 3.2.3.4) per specifications. 1. SCOPE 1.1 Purpose This specification cover
6、s procedures for obtaining first-article (preproduction) approval of forgings and the controls to be exercised in producing subsequent production forgings. 1.2 Application This procedure has been used typically for forgings which require preproduction approval and where assurance is required that pr
7、oduction lots are of essentially the same metallurgical quality and are produced by the same basic procedures as the forging originally qualified. 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
8、 specified 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 A
9、vailable 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. ARP1917 Clarification of Terms Used in Aerospace Metals Specifications SAE INTERNATIONAL AMS2375E Page 2 of 6 2.2 ASTM Publicat
10、ions 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 A370 Mechanical Testing of Steel Products ASTM E3 Preparation of Metallographic Specimens ASTM E8/E8M Tension Testing of Metallic Materials ASTM E10 B
11、rinell Hardness of Metallic Materials ASTM E18 Rockwell Hardness of Metallic Materials 3. TECHNICAL REQUIREMENTS 3.1 Forging Stock 3.1.1 The forging producer shall determine that the forging stock conforms to the applicable material specification and will yield acceptable forgings. Tests which are c
12、haracteristic of a heat or lot, and that are conducted by the forging stock producer, need not be repeated by the forging producer provided the results of such tests have been supplied by the forging stock producer. 3.1.2 When specified, forging stock shall be procured from sources approved by purch
13、aser of the forgings. 3.2 Preproduction Forgings 3.2.1 Procedure The forging producer shall produce and heat treat to final condition one or more preproduction forgings and shall test a forging or sections thereof to determine conformance to all requirements of the material specification, the drawin
14、g, and any additional requirements specified by purchaser. The preproduction forgings shall be made by the same practices to be used on production forgings and, unless otherwise specified, may be produced as part of the initial production run. A duplicate preproduction forging or the remaining secti
15、on of such forgings shall be submitted to purchaser for confirmatory testing, when requested. 3.2.1.1 When forgings are to be supplied in other than the final heat treated condition, the test forging(s) shall be heat treated to the final heat treated condition of the part. If the as-forged section s
16、ize is too large to achieve proper heat treatment response, the forging, or a section thereof, shall be machined to a configuration of the same equivalent round as that of the heaviest section of the heat treat configuration. 3.2.1.1.1 If the final heat treated condition of the forgings requires a t
17、ensile strength of 200 ksi (1379 MPa) or higher, and the forgings are supplied in a different condition, the producer may excise oversize test coupons from such forgings. Such coupons shall be given the final heat treatment prior to machining to specimen size for testing. 3.2.2 Specimen Locations Th
18、e location(s) of coupons that are to be taken for mechanical property tests and the sections for grain flow examination shall be as specified by purchaser. The forging producer shall perform the required tests on specimens from these locations. If locations are not specified, the forging producer sh
19、all select representative areas for testing and, when required, shall obtain concurrence of purchaser. Mechanical property test specimens shall be taken in the transverse direction whenever practicable unless only longitudinal properties are specified in the material specification. SAE INTERNATIONAL
20、 AMS2375E Page 3 of 6 3.2.3 Properties 3.2.3.1 Grain Flow A representative forging shall be sectioned as indicated on the drawing and the sections suitably etched to show the grain flow. Photographs showing the grain flow pattern shall be made of each section and the photographs shall be identified
21、to indicate the corresponding sections in the forging. The grain flow shall conform to the requirements of the drawing and good forging practice consistent with the part shape, without reentrant flow lines. When the specified alloy is not conducive to good grain flow determination, a substitute allo
22、y or melting practice showing good grain flow and having equivalent forgability shall be substituted and so indicated in the test report. 3.2.3.2 Hardness Hardness surveys in accordance with ASTM A370 for steels or ASTM E10 or ASTM E18 for all metals shall be made across the heaviest section of test
23、 forgings, unless otherwise specified. 3.2.3.3 Microstructure Sections shall be taken from the fully heat-treated forging at the center of the heaviest usable section and at the surface of the heaviest and thinnest sections and prepared for metallographic examination in accordance with ASTM E3. Ther
24、e shall not be any detrimental microstructural abnormalities related to improper forging or heat treating practice or to forging stock quality. Photographs of the microstructures shall be submitted to purchaser and any abnormal microstructural conditions identified. 3.2.3.4 Mechanical Properties Tes
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