SAE AMS 4313D-2010 Aluminum Alloy Rolled or Forged Rings 6 3Cu - 0 30Mn - 0 18Zr - 0 10V - 0 06Ti (2219-T351 2219-T352) Solution Heat Treated and Mechanically Stress Relieved (UNS .pdf

《SAE AMS 4313D-2010 Aluminum Alloy Rolled or Forged Rings 6 3Cu - 0 30Mn - 0 18Zr - 0 10V - 0 06Ti (2219-T351 2219-T352) Solution Heat Treated and Mechanically Stress Relieved (UNS .pdf》由会员分享，可在线阅读，更多相关《SAE AMS 4313D-2010 Aluminum Alloy Rolled or Forged Rings 6 3Cu - 0 30Mn - 0 18Zr - 0 10V - 0 06Ti (2219-T351 2219-T352) Solution Heat Treated and Mechanically Stress Relieved (UNS .pdf（7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 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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2010 SAE International All rights reserved. No part of this publication ma

3、y 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 US

4、A) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS4313DAEROSPACEMATERIALSPECIFICATIONAMS4313 REV. D Issued 1977-01 Revised 2010-01 Superseding

5、 AMS4313C Aluminum Alloy, Rolled or Forged Rings 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T351, 2219-T352) Solution Heat Treated and Mechanically Stress Relieved (Composition similar to UNS A92219) RATIONALEAMS4313D removes hardness as a technical requirement and results from a Five Year Revie

6、w and update of this specification.1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of rolled or forged rings. 1.2 Application These rings have been used typically for structural applications requiring good fusion weldability, a combination of good strength and resistance to

7、 stress-corrosion cracking, and for parts requiring good stability during machining, but usage is not limited to such applications. 1.2.1 Certain design and fabrication procedures may cause these rings to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such c

8、onditions. 1.3 Classification Rings covered by this specification are classified by type of mechanical stress relief as follows: Type 1 - Stress relieved by stretching (2219T351) Type 2 - Stress relieved by compression (2219T352) 1.3.1 Either type may be supplied, unless a specific type is ordered.

9、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 specific document issue is specified. When the referenced

10、document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4313D Page 2

11、of 72.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products,

12、Except Forging Stock, and Rolled, Forged, or Flash Welded Rings AMS2770 Heat Treatment of Aluminum and Aluminum Alloys AMS2772 Heat Treatment of Aluminum Alloy Raw Materials AMS2808 Identification, Forgings ARP823 Minimizing Stress-Corrosion for Aerospace Applications in Wrought Heat-Treatable Alumi

13、num Alloy Products2.2 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 B 594 Ultrasonic Inspection of Aluminum-Alloy Products for Aerospace Applications ASTM B 660 Packaging/Packing of A

14、luminum and Magnesium Products ASTM E 3 Preparation of Metallographic Specimens ASTM E 340 Macroetching Metals and Alloys 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355. TABLE 1 - COMPOSITION Element min ma

15、xSiliconIronCopperManganeseMagnesiumZincTitaniumVanadiumZirconiumOther Elements, each Other Elements, total Aluminum-5.80.20-0.020.050.10-remainder0.200.306.80.400.020.100.100.150.250.050.153.2 Condition Rings shall be supplied in the following condition; solution heat treatment shall be performed i

16、n accordance with AMS2772.3.2.1 Type 1 Solution heat treated and stress relieved by stretching to produce a permanent set of 11/2 to 5%. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4313D P

17、age 3 of 73.2.2 Type 2 Solution heat treated and stress relieved by compression to produce a permanent set of 11/2 to 5%. During compression, primary forces shall be applied in the axial direction. 3.3 Properties Rings shall conform to the following requirements, determined in accordance with AMS235

18、5 on the mill produced size. 3.3.1 As Solution Heat Treated and Stress Relieved 3.3.1.1 Hardness Should be not lower than 77 HB/10/500 or 82 HB/10/100 but the rings shall not be rejected on the basis of hardness if the applicable tensile property requirements are met. 3.3.1.2 Grain Size When specifi

19、ed, shall be not larger than 0.030 inch (0.76 mm) in thickness, determined as follows: 3.3.1.2.1 The radial/axial cross-section shall be macroetched in accordance with ASTM E 340 for examination, at not greater than 10X magnification, to select an area representing the largest grain size for metallo

20、graphic examination. The metallographic specimen thus selected shall be prepared in accordance with ASTM E 3. Grain size shall be determined by counting the grains in the radial direction across the microscopic field at approximately 100X magnification, dividing the diameter of the field of view by

21、the number of grains, and dividing the result by the actual magnification used. 3.3.2 After Precipitation Heat Treatment Shall be as follows, determined on rings precipitation heat treated in accordance with AMS2770: 3.3.2.1 Tensile Properties 3.3.2.1.1 Rings with OD to Wall Thickness Ratio Less Tha

22、n 10 Shall be as agreed upon by purchaser and vendor. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4313D Page 4 of 73.3.2.1.2 Rings with OD to Wall Thickness Ratio of 10 or Greater Shall be

23、 as specified in Table 2. Tensile tests are not required in any direction from which a specimen at least 2.375 inches (60.32 mm) in length cannot be obtained. TABLE 2A - MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS Nominal Thickness at Time of Heat TreatmentInches(See 3.3.2.1.2.1) SpecimenOrientatio

24、n(See 3.3.2.1.2.2) TensileStrengthksiYieldStrengthat 0.2% Offset ksiElongationin 4D %Up to 3, incl Over 3 to 4, incl Over 4 to 5, incl Over 5 to 6, incl TangentialAxialRadialTangentialAxialRadialTangentialAxialRadialTangentialAxialRadial60605858585656565454545248.046.044.046.044.042.044.042.040.042.

25、040.040.0643643532532TABLE 2B - MINIMUM TENSILE PROPERTIES, SI UNITS Nominal Thickness at Time of Heat TreatmentMillimeters(See 3.3.2.1.2.1) SpecimenOrientation(See 3.3.2.1.2.2) TensileStrengthMPaYieldStrengthat 0.2% Offset MPaElongationin 4D %Up to 76, incl Over 76 to 102, incl Over 102 to 127, inc

26、l Over 127 to 152, incl TangentialAxialRadialTangentialAxialRadialTangentialAxialRadialTangentialAxialRadial4144144004004003863863863723723723593313173033173032903032902762902762766436435325323.3.2.1.2.1 Thickness shall be the smaller of the wall thickness (one-half the difference between nominal OD

27、 and nominal ID) and height (axial) dimensions. 3.3.2.1.2.2 Tangential requirements apply to specimens machined with axis of specimen tangential to the ring OD (parallel to the direction of rolling). Axial requirements apply to specimens machined with axis of specimen parallel to the ring axis (long

28、 transverse to the direction of rolling). Radial requirements apply to specimens machined with axis of specimen parallel to the radius of the ring (short transverse to the direction of rolling). All specimens shall be machined from the core of the ring. 3.3.2.1.2.3 Elongation requirements do not app

29、ly to test specimens having a gage-length diameter under 0.250 inch (6.35 mm), or located in immediate proximity to an abrupt change in section thickness, or located so that any part of the specimen gage length is located within 0.125 inch (3.18 mm) of the trimmed flash line. Copyright SAE Internati

30、onal Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4313D Page 5 of 73.4 Quality Rings, as received by purchaser, shall be uniform in quality and condition, sound, and free from foreign materials and from imperfections

31、detrimental to usage of the rings. 3.4.1 Each ring shall be ultrasonically inspected in accordance with ASTM B 594 and shall meet the Class A acceptance limits of that specification. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspection The vendor of rings shall supply all samples for ve

32、ndors tests and shall be responsible for the performance of all required tests. Purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary to ensure that the rings conform to specified requirements. 4.2 Classification of Tests All technical requirements are accep

33、tance tests and except for composition shall be performed on each lot. 4.3 Sampling and Testing Shall be in accordance with AMS2355. A lot shall be all rings of the same size solution heat treated in the same batch-furnace load or consecutively in a continuous furnace during an eight-hour period. 4.

34、3.1 Composition One or more samples shall be taken by the producer from each group of ingots poured simultaneously from the same source of molten metal. Complete ingot analysis records shall be available to purchaser at producers facility. 4.3.1.1 Unless compliance with 4.3.1 is established, an anal

35、ysis shall be made for each 4000 pounds (1814 kg) or less of alloy comprising the lot except that not more than one analysis shall be required per piece. 4.3.2 Tensile Properties Except when testing in one or more directions is not required by 3.3.2.1.2, test specimens in the tangential, axial, and

36、radial directions shall be taken from a ring, ring prolongation, or ring segment representing the lot. When ring segments are used for testing, the segments shall be cut from a ring after solution heat treatment and stress-relief. Ring segments shall be included in each precipitation heat treatment

37、furnace load. 4.3.2.1 When requested by purchaser, a minimum of one-half of each ring segment obtained as in 4.3.2 or one-half of each ring prolongation tested shall be submitted to purchaser with the rings represented. 4.3.3 Quality Each ring. 4.3.4 Grain Size One or more radial/axial specimens fro

38、m a ring, ring prolongation, or ring segment representing the lot, when specified. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4313D Page 6 of 74.4 Reports The vendor of rings shall furnis

39、h with each shipment a report stating that the product conforms to the composition, tolerances, and ultrasonic inspection, and showing the numerical results of tests on each inspection lot to determine conformance to the other acceptance test requirements. This report shall include the purchase orde

40、r number, inspection lot number(s), AMS4313D, size, and quantity. The report shall also identify the producer, the product form, and the size of the mill product. 4.5 Resampling and Retesting If any specimen used in the above tests fails to meet the specified requirements, disposition of the rings m

41、ay be based on the results of testing two additional specimens for each original nonconforming specimen. Retest specimens shall be taken from as close as possible to the same location in the same ring or a second ring from the same lot as was the original unacceptable specimen. Failure of any retest

42、 specimen to meet the specified requirements shall be cause for rejection of the rings represented. Results of all tests shall be reported. 5. PREPARATION FOR DELIVERY 5.1 Identification Shall be in accordance with AMS2808. 5.2 Packaging 5.2.1 Rings shall be coated, prior to shipment, with a light,

43、corrosion-inhibiting oil. 5.2.2 Rings shall be prepared for shipment in accordance with ASTM B 660, in compliance with applicable rules and regulations pertaining to the handling, packaging, and transportation of the rings to ensure carrier acceptance and safe delivery. 6. ACKNOWLEDGMENT A vendor sh

44、all mention this specification number and its revision letter in all quotations and when acknowledging purchase orders. 7. REJECTIONS Rings not conforming to this specification, or to modifications authorized by purchaser, will be subject to rejection. 8. NOTES 8.1 A change bar (l) located in the le

45、ft margin is for the convenience of the user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of this specification. An (R) symbol to the left of the document title indicates a complete revision of the specification, including technical revisio

46、ns. Change bars and (R) are not used in original publications, nor in specifications that contain editorial changes only. 8.2 Terms used in AMS are clarified in ARP1917. 8.3 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions and properties in SI uni

47、ts and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information. 8.4 Hardness Should be not lower than 115 HB/10/500 or 120 HB/10/1000 but the rings shall not be rejected on the basis of hardness if the applicable tensile property

48、requirements are met. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4313D Page 7 of 78.5 Purchase orders should specify not less than the following: AMS4313DType of ring when a specific type is required Size or part number of rings desired Quantity of rings desired Whether grain size determination is required (see 3.3.1.2). PREPARED BY AMS COMMITTEE “D“ Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction