SAE AMS-QQ-A-250 30A-2013 Aluminum Alloy 2219 Plate and Sheet《2219铝合金 板材和带材》.pdf

《SAE AMS-QQ-A-250 30A-2013 Aluminum Alloy 2219 Plate and Sheet《2219铝合金 板材和带材》.pdf》由会员分享，可在线阅读，更多相关《SAE AMS-QQ-A-250 30A-2013 Aluminum Alloy 2219 Plate and Sheet《2219铝合金 板材和带材》.pdf（9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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2013 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 (out

4、side 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/AMSQQA250/30AAEROSPACE MATERIAL SPECIFICATIONAMS-QQ-A-250/30 REV. AIssued 1997-08Reaffirmed 2

5、010-05Stabilized 2013-12Superseding AMS-QQ-A-250/30Aluminum Alloy 2219, Plate and SheetA92219RATIONALEAMS-QQ-A-250/30A results from a five year review of this specification.STABILIZATION NOTICEAMS-QQ-A-250/30A has been declared “STABILIZED“ by AMS Committee D. This document will no longer be updated

6、 and may no longer represent standard industry practice. The last technical update of this document occurred in August 1997. Users of this document should refer any certification issues (e.g. exceptions listed on the certification report) to the cognizant engineering organization for their dispositi

7、on. CAUTION: In many cases the purchaser is not the cognizant engineering organization (i.e. purchaser may be a sub tier supplier).AMS Committee D recommends that the following technically equivalent (e.g. properties, fit, form, function) specifications be used for future procurement. This listing d

8、oes not constitute authority to substitute these specifications for the“STABILIZED” specification.AMS4031 Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-0) Annealed or when specified, “As Fabricated” (2219-F)AMS4601 Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.0

9、6Ti - 0.10V - 0.18Zr Solution Heat Treated, Cold Worked and Naturally Aged (2219 -T31/-T351)AMS4599 Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution and Precipitation Heat Treated (2219 -T81/-T851)AMS4600 Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10

10、V - 0.18Zr Solution Heat Treated, Cold Worked (8%) and Naturally Aged (2219 -T37)AMS4613 Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution Heat Treated, Cold Worked (8%) and Precipitation Heat Treated (2219 -T87)Copyright SAE International Provided by IHS under licens

11、e with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE INTERNATIONAL AMS-QQ-A-250/30A Page 1 of 8 NOTICEThis document has been taken directly from Federal Specification QQ-A-250/30A, Amendment 1, and contains only minor editorial and format changes required

12、to bring it into conformance with the publishing requirements of SAE technical standards.The original Federal Specification was adopted as an SAE standard under the provisions of the SAE Technical Standards Board (TSB) Rules and Regulations (TSB 001) pertaining to accelerated adoption of government

13、specifications and standards. TSB rules provide for (a) the publication of portions of unrevised government specifications and standards without consensus voting at the SAE Committee level, (b) the use of the existing government specification or standard format, and (c) the exclusion of any qualifie

14、d product list (QPL) sections.The complete requirements for procuring 2219 aluminum alloy plate and sheet described herein shall consist of this document and the latest issue of AMS-QQ-A-250.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking

15、 permitted without license from IHS-,-,-SAE INTERNATIONAL AMS-QQ-A-250/30A Page 2 of 8 1. SCOPE AND CLASSIFICATION:1.1 Scope: This specification covers the specific requirements for 2219 aluminum alloy plate and sheet.1.2 Classification: 1.2.1 Tempers: The plate and sheet are classified in one of th

16、e following tempers as specified (See 6.3 and 6.4): O, T31, T37, T62, T81, T87, T351, T851, or F temper. Definitions of these tempers are specified in AMS-QQ-A-250.2. APPLICABLE DOCUMENTS: See AMS-QQ-A-250.3. REQUIREMENTS: 3.1 Chemical Composition: 3.1.1 The chemical composition shall conform to the

17、 requirements specified in Table I.TABLE I. Chemical Composition 1/PercentElement minimum maximumCopper 5.8 6.8Manganese 0.20 0.40Zirconium 0.10 0.25Vanadium 0.05 0.15Titanium 0.02 0.10Iron - 0.30Silicon - 0.20Zinc - 0.10Magnesium - 0.02Other Elements, each - 0.05Other Elements, total - 0.15Aluminum

18、 remainder1/ Analysis shall routinely be made only for the elements specifically mentioned in Table I. If, however, the presence of other elements is indicated or suspected in amounts greater than the specified limits, further analysis shall be made to determine that these elements are not present i

19、n excess of specified limits.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE INTERNATIONAL AMS-QQ-A-250/30A Page 3 of 8 3.2 Mechanical Properties: 3.2.1 Mechanical Properties of Material as Suppl

20、ied: The mechanical properties perpendicular to the direction of final rolling, except for material under 9 inches in width, shall conform to the requirements of Table II for the temper specified. For material under 9 inches in width, the mechanical properties parallel to the direction of final roll

21、ing shall conform to the requirements of Table II for the temper specified.TABLE II. Mechanical Properties (See 6.7) TemperThicknessInchesTensile StrengthminimumksiYield Strengthat 0.2 percentOffsetminimumksiElongation in2 inches 1/ or4 times D 2/minimumpercentO 0.020 - 2.000 32.0 (max) 16.0 (max) 1

22、2T310.020 - 0.039 46.0 29.0 80.040 - 0.249 46.0 28.0 10T3510.250 - 2.000 46.0 28.0 102.001 - 3.000 44.0 28.0 103.001 - 4.000 42.0 27.0 94.001 - 5.000 40.0 26.0 95.001 - 6.000 39.0 25.0 80.020 - 0.039 49.0 38.0 60.040 - 2.500 49.0 37.0 6T37 2.501 - 3.000 47.0 36.0 63.001 - 4.000 45.0 35.0 54.001 - 5.

23、000 43.0 34.0 4T62 3/0.020 - 0.039 54.0 36.0 60.040 - 0.249 54.0 36.0 70.250 - 1.000 54.0 36.0 81.001 - 2.000 54.0 36.0 7T810.020 - 0.039 62.0 46.0 60.040 - 0.249 62.0 46.0 7T8510.250 - 1.000 62.0 46.0 81.001 - 2.000 62.0 46.0 72.001 - 3.000 62.0 45.0 63.001 - 4.000 60.0 44.0 54.001 - 5.000 59.0 43.

24、0 55.001 - 6.000 57.0 42.0 4Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE INTERNATIONAL AMS-QQ-A-250/30A Page 4 of 8 3.2.2 Mechanical Properties After Heat Treatment: In addition to conforming

25、to requirements of 3.2.1, material in the tempers identified in the following paragraphs shall, after having been processed to tempers also identified therein, have properties conforming to those specified in Table II, as applicable.3.2.2.1 Material in the Annealed (O) and As-Fabricated (F) Tempers:

26、 Material in the O or F tempers, without the subsequent imposition of cold work or forming operations, shall, after proper solution and artificial aging treatments, develop the properties specified for the T62 temper (See 6.2).3.2.2.2 Material in the T31, T351, T81, and T851 Tempers: Material in the

27、 T31, T351, T81, and T851 tempers shall, without the subsequent imposition of cold work or forming operations, be heat treatable to the properties specified for the T62 temper. Such capability shall be demonstrated when specified (See 6.2 and 6.4).3.2.2.3 Material in the T31, T351, and T37 Tempers:

28、Material in the T31, T351, and T37 tempers shall be precipitation heat treatable to the properties specified for the T81, T851, and T87 tempers, respectively. Such capability shall be demonstrated when specified (See 6.4).T870.020 - 0.039 64.0 52.0 50.040 - 0.249 64.0 52.0 60.250 - 1.000 64.0 51.0 7

29、1.001 - 3.000 64.0 51.0 63.001 - 4.000 62.0 50.0 44.001 - 5.000 61.0 49.0 3FAl 4/4/ 4/1/ Not required for material 1/2 inch or less in width.2/ D represents specimen diameter.3/ Material in the T62 temper is a user heat-treated condition and is not available from the material producer.4/ No requirem

30、ents.TABLE II. Mechanical Properties (See 6.7) (Continued)TemperThicknessInchesTensile StrengthminimumksiYield Strengthat 0.2 percentOffsetminimumksiElongation in2 inches 1/ or4 times D 2/minimumpercentCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or

31、 networking permitted without license from IHS-,-,-SAE INTERNATIONAL AMS-QQ-A-250/30A Page 5 of 8 3.2.3 Bend Test: Bend specimens taken from material shall be capable of withstanding without cracking the bend test specified in AMS-QQ-A-250. The values for bend factor N are given in Table III.3.3 Int

32、ernal Defects: When specified (See 6.4), plate shall be ultrasonically inspected (See AMS-QQ-A-250). Acceptance limits shall be as specified in Table IV.3.4 Resistance to Stress-Corrosion Cracking: Plate 0.750 inch and over in thickness supplied in the T851 and T87 tempers or in the T351 and T37 tem

33、pers and aged to the T851 and T87 tempers shall exhibit no stress-corrosion cracking when subjected to the test specified in 4.3. Frequency of testing shall be in accordance withAMS-QQ-A-250. When specified (See 6.4), plate 0.750 inch and thicker, without prior cold work or forming, heat-treated to

34、the T62 temper shall exhibit no stress-corrosion cracking when subjected to the test specified in 4.3 (See 6.2).TABLE III. Bend Test Factor “N“.Thickness, Inch O temper0.020 - 0.250 40.251 - 0.750 60.751 - 1.000 8TABLE IV. Ultrasonic Discontinuity Acceptance Limits 1/Thickness,inchesMaximum Weightpe

35、r Piece,pounds 2/DiscontinuityClass 3/0.500 - 1.499 2,000 B1.500 - 3.000 2,000 A3.001 - 4.500 2,000 B4.501 - 6.000 4/4/1/ Discontinuities in excess of those listed in Table IV may be allowed, subject to approval of the procuring activity, if it is established that they will be removed by machining o

36、r that they are in non-critical areas.2/ Class for weights in excess of those shown shall be as agreed upon between the user and supplier.3/ The discontinuity class limits are defined in MIL-I-8950.4/ Shall be as agreed upon by purchaser and supplier.Copyright SAE International Provided by IHS under

37、 license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE INTERNATIONAL AMS-QQ-A-250/30A Page 6 of 8 3.5 Marking: In addition to the marking required in AMS-QQ-A-250, sheet and plate in the T81, T87, and T851 tempers shall be identified by an inspection

38、lot number marked in at least one location on each piece.4. QUALITY ASSURANCE PROVISIONS: See AMS-QQ-A-250 and the following:4.1 Heat Treatment: 4.1.1 Aging Period Before Testing: Specimens in the T31, T351, and T37 tempers shall not be required to be tested within 4 days after completion of the hea

39、t treatment. If the manufacturer so elects, samples may be tested after less than 4 days aging; but if they fail to meet specified properties, the test samples may be discarded and additional specimens may be tested after 4 days aging. These specimens shall be taken from the same locations in the pr

40、oduction lot or sample from which the prior specimens were taken.4.2 Mechanical Tests After Heat Treatment: 4.2.1 Number of Tests After Heat Treatment: From material in each temper of those specified for heat treatment capability demonstrations in 3.2.2 and 6.2, an additional number of specimens equ

41、al to that required in AMS-QQ-A-250 shall be taken and tested after heat treatment to each temper specified to determine conformance to 3.2.2.4.3 Stress-Corrosion Cracking Test: Samples of plate in the thicknesses and tempers identified in 3.4 shall be taken in accordance with AMS-QQ-A-250. Test spe

42、cimens shall be selected in a manner that will permit application of the specified tensile stress in the short-transverse direction with respect to grain flow. Specimens shall be stressed in tension in the short-transverse direction and be held at constant strain. The stress level shall be 75 percen

43、t of the long-transverse yield strength. The specimens shall be subjected to the stress-corrosion test specified in AMS-QQ-A-250.4.4 Records: It is the responsibility of the contractor that all test results be recorded, identified as to inspection lot, and preserved after completion of the contract

44、or purchase order. The records shall be made available to the procuring activity upon request.5. PREPARATION FOR DELIVERY: See AMS-QQ-A-250.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE INTERNA

45、TIONAL AMS-QQ-A-250/30A Page 7 of 8 6. NOTES:6.1 Intended Use: Aluminum alloy 2219 plate and sheet is intended for use where elevated temperature strength is required. This alloy is also noted for its good weldability and stress-corrosion resistance in the artificially aged tempers. Use of material

46、in the T31, T351, and T37 tempers is not recommended for finished products when optimum corrosion resistance is required.6.2 Properties After Heat Treatment: Mechanical and corrosion properties of producer-supplied material are certified for the temper of material supplied. The producers capability

47、demonstration is not evidence that user-treated material conforms to property requirements of a given temper. Frequently, user-heat-treated material may develop a lower level of properties, especially if any cold, warm, or hot work is introduced prior to solution heat treatment. The user should be h

48、eld responsible for demonstrating that his processing meets strength and corrosion requirements.6.3 Temper: Tempers T351 and T851 are available in plate only.6.4 Ordering Data: Purchasers should select the preferred options permitted herein and include the following information in procurement documents:Title, number, and date of this specification.Form, quantity, and temper required (See 1.2.1).Dimensions required.Requirements for sizes not specifically covered (See AMS-QQ-A-250).Whether ultrasonic inspect