SAE AMS 2310F-2006 Qualification Sampling and Testing of Steels for Transverse Tensile Properties《钢横截抗拉性能抽样和试验资格》.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 theref
2、rom, 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 2015 SAE InternationalAll rights reserved. No part of this publi
3、cation 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: +1 724-776-4970 (ou
4、tside USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS2310FAEROSPACEMATERIAL SPECIFICATIONAMS2310 REV. FIssued 1960-11Revised 2006-02Reaffirmed
5、 2015-05Superseding AMS2310EQualification Sampling and Testing of Steelsfor Transverse Tensile PropertiesRATIONALEAMS2310F has been reaffirmed to comply with the SAE five-year review policy.1. SCOPE: This specification covers procedures for sampling and testing aircraft-quality, special aircraft-qua
6、lity, and premium aircraft-quality steels requiring transverse tensile property testing. 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
7、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 ASTM Publications: Available from ASTM International, 100 Barr Harbor Drive
8、, P. O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM A 370 Mechanical Testing of Steel Products 3. TECHNICAL REQUIREMENTS: 3.1 Sampling: Samples shall be selected as in 3.1.1 through 3.1.6. Samples shall be full cross-sections, not less than 3/4 inch (19 mm) thic
9、k, taken from the largest size billet or bar for which the steel is to be qualified but before reduction to under 5 inches (127 mm) in diameter or least distance between parallel sides. Each sample, except those from individual billets or bars, shall be identified with its location in the ingot/reme
10、lt ingot and, when known, the ingot number and the ingot position in the heat. Specimens prepared as in 3.2 and tested as in 3.3 shall meet the specified requirements. 3.1.1 Heat Qualification: When the product of an entire heat is to be qualified, samples shall be taken as follows; sampling is diff
11、erent for heats made from top poured ingots/electrodes and from bottom poured ingots/electrodes: 3.1.1.1 Pouring Sequence Known: When the pouring sequence is known and traceability of billets or bars to ingot/remelt ingot position has been maintained, samples shall be taken from one end of billets o
12、r bars representing the following positions: 3.1.1.2 For Heats Produced From Top Poured Ingots/Electrodes: 3.1.1.2.1 One or Two Ingot Electrodes: Top and bottom of each ingot/remelted ingot. 3.1.1.2.2 Three to Nine Ingots/Electrodes: Top and bottom of the first and last ingot or electrode in the pou
13、ring sequence. 3.1.1.2.3 Ten or More Ingots/Electrodes: Top and bottom of the first, middle, and last ingot or electrode in the pouring sequence. 3.1.1.3 For Heats Produced From Bottom Poured Ingots/Electrodes: For each plate (cluster) poured, a top and a bottom of resulting ingots or remelted ingot
14、s. 3.1.2 Partial Heat Qualification: When the product of only some ingots/electrodes from a heat is to be qualified, samples shall be taken from one end of billets or bars representing the positions in those ingots or remelted ingots specified in 3.1.1.1 when pouring sequence is known. When only a p
15、ortion of an ingot or remelted ingot is to be qualified, samples shall be taken from one end of billets or bars representing the top and bottom of that portion of the ingot or remelted ingot. 3.1.3 Billet or Bar Qualification: If the product of an entire heat is not qualified as in 3.1.1, or the pro
16、duct of a portion of a heat is not qualified as in 3.1.2, or if traceability to ingot/remelt ingot position has not been maintained, samples shall be taken from both ends of each billet or bar to be qualified. SAE INTERNATIONAL AMS2310F Page 2 of 8_ 3.1.4 Multiple Size Qualifications: If the product
17、 of a heat or portion of a heat is qualified at one size, that heat or portion of a heat will be considered qualified for any size of smaller crosssectional area without additional testing if the results of the original tests meet the requirements specified for the smaller size, unless purchaser spe
18、cifies that each size be tested for qualification. 3.1.5 Products from a heat qualified to the requirements of a specification requiring premium aircraft-quality steel may be supplied, without retesting, to a specification requiring aircraft-quality or special aircraft-quality steel of the same basi
19、c composition. 3.1.6 When the material specification requires that samples be forged to specific size for qualification, or when specified by purchaser, the steel shall be forged to that size before cutting samples. 3.2 Specimen Preparation: The samples obtained as in 3.1 shall be heat treated as sp
20、ecified in the material specification. Tensile specimens shall be prepared from the heat treated samples as specified in 3.2.1 or 3.2.2 and tested as in 3.3. 3.2.1 Aircraft-Quality and Special Aircraft-Quality Steels: From each sample from round or square product, two tensile specimens conforming to
21、 ASTM A 370 shall be taken from the locations shown in Figure 1. Specimens from rectangular product having a nominal thickness of 4.5 inches (114 mm) or over shall be taken at the 1/4 and 3/4 width locations at the midpoint of the thickness. For nominal thicknesses under 4.5 inches (114 mm), samples
22、 shall be similarly located in the long-transverse direction. 3.2.1.1 Standard 0.500 inch (12.70 mm) diameter tensile specimens are preferred but sub-size specimens not less than 0.250 inch (6.35 mm) in diameter may be used. The 0.500 inch (12.70 mm) diameter specimen shall be used in any referee te
23、sts. 3.2.2 Premium Aircraft-Quality Steels: Specimens shall be prepared as in 3.2.1 except that the location of specimens from round or square product shall be as shown in Figure 2, and the location of specimens from rectangular product shall be adjacent to the mid-thickness or mid-width line. 3.3 T
24、esting: Each specimen prepared as in 3.2 shall be tested in accordance with ASTM A 370 to determine conformance to specified requirements. 3.3.1 Test Validity: If it can be shown that failure of any specimen to meet specified requirements is due to improper specimen preparation, heat treatment, or t
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