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 2012 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: 724-776-4970 (outside USA)
4、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/AMSQQA367D AEROSPACE MATERIAL SPECIFICATION AMS-QQ-A-367 REV. D Issued 2000-09 Revised 2012-04 Su
5、perseding AMS-QQ-A-367C Aluminum Alloy Forgings RATIONALE AMS-QQ-A-367D was revised to permit the use of longitudinal specimens if long transverse specimens cannot be taken from a given forging (4.9). NOTICE The initial SAE publication of this document was taken directly from U.S. Military Specifica
6、tion QQ-A-367H, Notice 1, Amendment 2. This SAE Standard may retain the same part numbers established by the original military document. Any requirements associated with Qualified Products Lists (QPL) may continue to be mandatory for DoD contracts. Requirements relating to QPLs have not been adopted
7、 by the SAE for this standard and are not part of this SAE document. 1. SCOPE AND CLASSIFICATION 1.1 This specification has previously been widely used and may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, considers this specif
8、ication non-current and does not recommend this specification for future use in new design. 1.2 Scope This specification covers aluminum alloy die forgings and hand forgings. 1.3 Classification 1.3.1 Composition Aluminum alloy forgings covered by this specification shall be the alloy number and comp
9、ositions as specified in Table 1. 1.3.2 Form Aluminum alloy forgings shall be furnished in the form of die forgings or hand forgings, as specified. If the method is not specified, manufacturers may use any method of forging most convenient. SAE AMS-QQ-A-367D Page 2 of 19 1.3.3 Temper Forgings shall
10、be supplied in the temper specified in the order or contract. Forgings supplied in the T652 or T852 tempers shall be solution heat treated, stress relieved by compression to produce a permanent set of 1 to 5 percent, and artificially aged. Forgings in 7049 and 7075 alloy supplied in the T73 or T7352
11、 temper shall be solution heat treated and aged in a manner to develop the mechanical properties shown in Tables 2, 3, and 5, and shall be capable of passing the test for resistance to stress-corrosion cracking 4.4.3. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date
12、 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 document has been cancelled and no superseding document has been specified, the la
13、st published issue of that document shall apply. 2.1 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 A
14、lloys and Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2430 Shot Peening, Automatic AMS2772 Heat Treatment of Aluminum Alloy Raw Materials AMS-STD-2154 Inspection, Ultrasonic, Wrought Metals, Process for 2.2 ASTM Publications Available from A
15、STM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 557 Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM E 1282 Chemical Composit
16、ions and Selecting Sampling Practices and Quantitative Analysis Methods for Metals, Ores, and Related Materials ASTM E 1417 Liquid Penetrant Testing ASTM G 44 Exposure of Metals and Alloys by Alternate Immersion in Neutral 3.5% Sodium Chloride Solution 2.3 U.S. Government Publications Available from
17、 the Document Automation and Production Service (DAPS), Building 4/D, 700 Robbins Avenue, Philadelphia, PA 19111-5094, Tel: 215-697-6257, http:/assist.daps.dla.mil/quicksearch/. FED-STD-123 Marking for Shipment (Civil Agencies) MIL-STD-129 Military Marking for Shipment and Storage SAE AMS-QQ-A-367D
18、Page 3 of 19 2.4 Aluminum Association Publications Available from the Aluminum Association Inc., 1525 Wilson Blvd., Suite 600, Arlington, VA 22209, Tel: (703) 358-2960, www.aluminum.org. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys
19、 (known as the “Teal Sheets”) TABLE 1 - CHEMICAL COMPOSITION LIMITS (NOTE 1) PERCENT MAXIMUM, EXCEPT WHERE INDICATED AS RANGE Alloy No. Silicon Iron Copper Manganese Magnesium Chromium Zinc Titanium Nickel Other Elements(Note 2) Aluminum 2014 0.50-1.2 0.7 3.9-5.0 0.40-1.2 0.20-0.8 0.10 0.25 0.15 - 0
20、.05 remainder 2018 0.9 1.0 3.5-4.5 0.20 0.45-0.9 0.10 0.25 - 1.7-2.3 0.05 remainder 2025 0.50-1.2 1.0 3.9-5.0 0.40-1.2 0.05 0.10 0.25 0.15 - 0.05 remainder 2218 0.9 1.0 3.5-4.5 0.20 1.2-1.8 0.10 0.25 - 1.7-2.3 0.05 remainder 2219 0.20 0.30 5.8-6.8 0.20-0.40 0.02 - 0.10 0.02-0.10 - 0.05 (Note 3) rema
21、inder 2618 0.25 0.9-1.3 1.9-2.7 - 1.3-1.8 - 0.10 0.04-0.10 0.9-1.2 0.05 remainder 4032 11.0-13.5 1.0 0.50-1.3 - 0.8-1.3 0.10 0.25 - 0.50-1.3 0.05 remainder 5083 0.40 0.40 0.10 0.040-1.0 4.0-4.9 0.05-0.25 0.25 0.15 - 0.05 remainder 6061 0.40-0.8 0.7 0.15-0.40 0.15 0.8-1.2 0.04-0.35 0.25 0.15 - 0.05 r
22、emainder 6066 0.9-1.8 0.50 0.7-1.2 0.6-1.1 0.8-1.4 0.40 0.25 0.20 - 0.05 remainder 6151 0.6-1.2 1.0 0.35 0.20 0.45-0.8 0.15-0.35 0.25 0.15 - 0.05 remainder 7049 0.25 0.35 1.2-1.9 0.20 2.0-2.9 0.10-0.22 7.2-8.2 0.10 - 0.05 remainder 7075 0.40 0.5 1.2-2.0 0.30 2.1-2.9 0.18-0.28 5.1-6.1 0.20 - 0.05 rem
23、ainder 7076 0.40 0.6 0.30-1.0 0.30-0.8 1.2-2.0 - 7.0-8.0 0.20 - 0.05 remainder 7079 0.30 0.40 0.40-0.8 0.10-0.30 2.9-3.7 0.10-0.25 3.8-4.8 0.10 - 0.05 remainder 1/ Analysis shall be made only for the elements specifically mentioned in the above table. If, however, the presence of other elements is i
24、ndicated in the course of routine analysis, further analysis shall be made to determine that these other elements are not present in excess of the limits specified. 2/ Total of all elements not specified shall not exceed 0.15 percent. 3/ Vanadium 0.05-0.15 and zirconium 0.10-0.25. 4/ In the case of
25、a discrepancy in the values listed in Table 1 with those listed in the International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys (known as the “Teal Sheets”), the composition limits registered with the Aluminum Association and published in the
26、“Teal Sheets” shall apply. 3. REQUIREMENTS 3.1 Forgings shall produced by hammering or pressing from a cast ingot or from as-fabricated (rolled, hand forged, or extruded) stock of suitable quality and of composition as specified in Table 1. Whether the forgings are produced from cast ingot or wrough
27、t stock, the material shall be sufficiently worked upon completion of forging operations to produce a thoroughly wrought structure. 3.2 Chemical Composition 3.2.1 The chemical composition of the forgings shall be as specified in Table 1. 3.3 Mechanical Properties 3.3.1 Die Forgings The mechanical pr
28、operties of test specimens taken as specified in 4.2.3.1 shall be as specified in Tables 2 and 3. SAE AMS-QQ-A-367D Page 4 of 19 TABLE 2 - MECHANICAL PROPERTIES OF DIE FORGINGS AND SEPARATELY FORGED TEST BARS - TEST SPECIMEN PARALLEL TO FORGING FLOW (GRAIN) LINES Alloy No. Temper (Note 3) Maximum He
29、at Treat Section Thickness Inches Tensile Strength (Note 2) Minimum ksi Yield Strength (Note 2) at 0.2 percent Offset Minimum ksi Elongation in 2 inches or 4D (Note 1), Minimum Forging Percent Elongation in 2 inches or 4D (Note 1), Minimum Test Coupon (Forged) Percent 2014 T4 4 55.0 30.0 11 16 2014
30、T6 Up thru 1 65.0 56.0 6 8 Over 1 thru 2 65.0 56.0 6 (Note 4) Over 2 thru 3 65.0 55.0 6 (Note 4) Over 3 thru 4 63.0 55.0 6 (Note 4) 2018 T61 4 55.0 40.0 7 10 2025 T6 4 52.0 33.0 11 16 2218 T61 4 55.0 40.0 7 10 2219 T6 4 58.0 38.0 8 10 2618 T61 4 58.0 45.0 4 6 4032 T6 4 52.0 42.0 3 5 5083 H111 (Note
31、6) 4 42.0 22.0 14 16 5083 H112 (Note 6) 4 40.0 18.0 16 16 6061 T6 4 38.0 35.0 7 10 6066 T6 4 50.0 45.0 8 12 6151 T6 4 44.0 37.0 10 14 7049 T73 Up thru 2 72.0 62.0 7 10 Over 2 thru 4 71.0 61.0 7 10 Over 4 thru 5 70.0 60.0 7 10 7075 T6 Up thru 1 75.0 64.0 7 10 Over 1 thru 2 74.0 63.0 7 (Note 4) Over 2
32、 thru 3 74.0 63.0 7 (Note 4) Over 3 thru 4 73.0 62.0 7 (Note 4) 7075 T73 Up thru 3 66.0 56.0 7 10 Over 3 thru 4 64.0 55.0 7 10 7075 T7352 Up thru 3 66.0 56.0 7 10 Over 3 thru 4 64.0 53.0 7 10 7076 T61 4 70.0 60.0 10 14 7079 T6 Up thru 1 72.0 62.0 7 10 Over 1 thru 2 72.0 62.0 7 (Note 4) Over 2 thru 3
33、 71.0 61.0 7 (Note 4) Over 3 thru 4 71.0 61.0 7 (Note 4) Over 4 thru 5 70.0 60.0 7 (Note 4) Over 5 thru 6 70.0 59.0 7 (Note 4) 1/ D is diameter of test specimen. 2/ Tensile and yield strength test requirements may be waived for material in any direction in which the dimension is less than 2 inches b
34、ecause of the difficulty to obtain a tension test specimen suitable for routine control testing. 3/ Die forgings in some configurations of these alloys can be purchased in the heat treated and mechanically stress relieved T652 temper conforming to the mechanical properties requirements specified for
35、 the T6 temper. 4/ When separately forged coupons are used to verify acceptability of forgings in the indicated thicknesses, the properties shown for thicknesses “Up thru 1 inch“, including the test coupon elongation, apply. 5/ As-forged thickness. When forgings are machined prior to heat treatment
36、the properties will also apply to the machined heat treat thickness provided the machined thickness is not less than one-half the original (as-forged) thickness. 6/ Maximum section thickness to which mechanical properties apply (non-heat-treatable-alloys). SAE AMS-QQ-A-367D Page 5 of 19 TABLE 3 - ME
37、CHANICAL PROPERTIES OF DIE FORGINGS - SPECIMENS NOT PARALLEL TO FORGING FLOW LINES Alloy No. Temper (Note 3) Maximum Heat Treat Section Thickness Inches Tensile Strength (Note 2) Minimum ksi Yield Strength at 0.2 percent Offset Minimum ksi Elongation in 2 inches or 4D (Note 1), Minimum 2014 T6 Up th
38、ru 1 64.0 55.0 3 Over 1 thru 2 64.0 55.0 2 Over 2 thru 3 63.0 54.0 2 Over 3 thru 4 63.0 54.0 2 2219 T6 4 56.0 36.0 4 2618 T61 4 55.0 42.0 4 5083 (Note 4) H111 4 39.0 20.0 12 5083 (Note 4) H112 4 39.0 16.0 14 6061 T6 4 38.0 35.0 5 6151 T6 4 44.0 37.0 6 7049 T73 Up thru 1 71.0 61.0 3 Over 1 thru 3 70.
39、0 60.0 3 Over 3 thru 4 70.0 60.0 2 Over 4 thru 5 68.0 58.0 2 7075 T6 Up thru 1 71.0 61.0 3 Over 1 thru 2 71.0 61.0 3 Over 2 thru 3 70.0 60.0 3 Over 3 thru 4 70.0 60.0 2 7075 T73 Up thru 3 62.0 53.0 3 Over 3 thru 4 61.0 52.0 2 7075 T7352 Up thru 3 62.0 51.0 3 Over 3 thru 4 61.0 49.0 2 7076 T61 4 67.0
40、 58.0 3 7079 T6 Up thru 1 71.0 61.0 5 Over 1 thru 2 70.0 60.0 5 Over 2 thru 3 70.0 60.0 4 Over 3 thru 4 70.0 60.0 4 Over 4 thru 5 68.0 58.0 3 Over 5 thru 6 68.0 58.0 3 1/ D is diameter of test specimen. 2/ Tensile and yield strength test requirements may be waived for material in any direction in wh
41、ich the dimension is less than 2 inches because of the difficulty to obtain a tension test specimen suitable for routine control testing. 3/ Die forgings in some configurations of these alloys can be purchased in the heat treated and mechanically stress relieved T652 temper conforming to the mechani
42、cal properties requirements specified for the T6 temper. 4/ Maximum section thickness to which mechanical properties apply (non-heat-treatable-alloys). 3.3.1.1 A forging representing the first production lot of forgings produced from new or significantly reworked dies, significantly changed forging
43、production procedures, or from significantly changed stock (See 3.1), shall be tested in accordance with 4.2.3.1. 3.3.1.2 If test specimens are taken from forgings of the alloys listed in Table 3 so that the axis is not substantially parallel (within plus or minus 15 degrees) to the metal flow lines
44、 in the specimen, the mechanical properties shall conform to the requirements of Table 3 except that the elongation requirements shall be as specified by the procuring activity for test specimens taken so that the reduced section (1) is in immediate proximity to an abrupt change in section thickness
45、; or (2) intersects the parting plane within 1/4 inch of the flash line. SAE AMS-QQ-A-367D Page 6 of 19 3.3.2 Hand Forgings The mechanical properties of hand forgings of 2014-T6, T652; 7049-T73; 7075-T6, T652, T73; 7079-T6, T652; 6061-T6 or T652; 2618-T61; 2219-T6, T852; and 5083-H111, H112 determin
46、ed from specimens taken in accordance with 4.2.3.2 shall conform to the applicable properties specified in Tables 4 through 11. 3.3.2.1 The properties in Tables 4, 5, 6, 7, 8, and 9 apply to hand forgings that are essentially rectangular in cross section. The requirements of long-transverse and shor
47、t-transverse properties apply also to the squares even though both transverse dimensions are equal length. The cross-sectional grain direction, perpendicular to the longitudinal direction, of hexagons and rounds shall be considered the long transverse grain direction. The direction of the long trans
48、verse properties shall be identified as required in 3.7. Biscuits, octagons, rings, and contour hand forgings are considered to be special purpose forgings (See 3.3.3). TABLE 4 - MECHANICAL PROPERTIES OF ALLOY 2014 HAND FORGINGS (NOTE 1) Temper Thickness (Notes 4,5) Inches Axis of Test Specimen Tens
49、ile Strength (Note 2) Minimum ksi Yield Strength (Note 2) Minimum ksi Elongation (Note 2) in 2 inches or 4D (Note 3) Minimum Percent T6 Up thru 2 Longitudinal 65.0 56.0 8 Long Transverse 65.0 56.0 3 Over 2 thru 3 Longitudinal 64.0 56.0 8 Long Transverse 64.0 55.0 3 Short Transverse 62.0 55.0 2 Over 3 thru 4 Longitudinal 63.0 55.0 8 Long Transverse 63.0 55.0 3 Short Transverse 61.0 54.0 2 Over 4 thru 5 Longitudinal 62.0 54.0 7 Long Transverse 62.0 54.0 2 Short Transverse 60.0 53.0 1 Over 5 thru 6 Longitudinal 61.0 53.0 7 Long Transverse 61.0 53.0 2 Sh
