SAE AMS 4355-2015 Aluminum Alloy Discontinuously Reinforced Hot Isostatically Pressed Shapes 2124A SiC 25p (3 m) (T1P).pdf

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 (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/AMS4355AEROSPACEMATERIAL SPECIFICATIONAMS4355Issued 2015-12Aluminum Alloy, Discontinuously Re

5、inforced Hot Isostatically Pressed Shapes2124A/SiC/25p (3Pm) (T1P)RATIONALEAMS4355 is a new specification for aluminum alloy hot isostatically pressed shapes produced from 2124A discontinuously reinforced with silicon carbide particulates.1. SCOPE1.1 Form This specification covers discontinuously re

6、inforced aluminum alloy (DRA) metal matrix composites (MMC) made by mechanical alloying of the 2124A powder and SiC particulate, which is then consolidated by Hot Isostatic Pressing (HIP) into shapes less than 62 in2(0.04 m2) cross-section (see 8.11). 1.2 Application HIPed shapes have been used typi

7、cally for structural applications requiring high static strength, fatigue strength and high elastic modulus, but usage is not limited to such applications. HIPed shapes may also be used as input to forging and extrusion processes.2. APPLICABLE DOCUMENTSA change bar (l) located in the left margin is

8、for the convenience of the user in locating areas where technical revisions, not editorial changes, have been made to the previous issue of this document. An (R) symbol to the left of the document title indicates a complete revision of the document, including technical revisions. Change bars and (R)

9、 are not used in original publications, nor in documents that contain editorial changes only.2.1 SAE Publications Available 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.AMS2355 Quali

10、ty Assurance, Sampling and Testing, Aluminum Alloys and Magnesium Alloy, Wrought Products(Except Forging Stock), and Rolled, Forged, or Flash Welded RingsAMS2750 PyrometrySAE INTERNATIONAL AMS4355 Page 2 of 62.2 ANSI Accredited PublicationsCopies of these documents are available online at http:/webs

11、tore.ansi.org/.ANSI B46.1 Surface Texture, Surface Roughness, Waviness and Lay2.3 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 B311 Density of Powder Metallurgy (PM) Materials Contain

12、ing Less Than Two Percent PorosityASTM B660 Packaging/Packing of Aluminum and Magnesium ProductsASTM B666/B666M Identification Marking of Aluminum and Magnesium ProductsASTM E8/E8M Tension Testing of Metallic Materials2.4 FEPAAvailable from Federation of the European Producers of Abrasives www.fepa-

13、abrasives.org.FEPA-42-GB3. TECHNICAL REQUIREMENTS 3.1 Aluminum Matrix Composition Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355. Table 1 2124A CompositionElement Min maxSilicon - 0.20Iron - 0.30Copper 3.8 4.9Magnesium 1.2 1.8Manganese 0.30 0.9Chro

14、mium - 0.10Zinc - 0.25Titanium - 0.15Oxygen - 0.6Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainder3.2 Reinforcement Type and Volume Fraction 3.2.1 Reinforcement Shall consist of silicon carbide particulate (SiCp) having the following characteristics:Mean Diameter 3 micrometer

15、 determined in accordance with F1200 from the FEPA-42-GB.3.2.2 Reinforcement Volume Fraction The content of silicon carbide particulate shall be 25% 0.5% by volume determined through conversion from measured input material weights.SAE INTERNATIONAL AMS4355 Page 3 of 63.2.3 The aluminum matrix alloy

16、and reinforcement particulate shall be mechanically alloyed to produce a uniform distribution of the reinforcement particulate within the resultant discontinuously reinforced aluminum powder.3.3 Condition Hot Isostatically Pressed (see 8.4), and air cooled to T1P condition.3.3.1 Surface ConditionIf

17、no surface finish is specifed, the material shall be furnished with an as-sawn, as HIP, and/or machined surface. Machined surfaces shall have surface finish no greater than 125 Ra inch (3.2 m), determined in accordance with ANSI B46.1.3.4 Response to T4P/T42P Heat TreatmentSamples taken from the mat

18、erial (see 4.3) shall be solution heat treated followed by a cold water quench and naturally aged to the T4P/T42P condition (see 8.6). Pyrometry shall be in accordance with AMS2750.3.4.1 Tensile Properties A sample with less than 1 in2(645 mm2) cross-section from a lot shall be heat treated to the T

19、4P/T42P condition, and shall have the properties shown in Table 2.Table 2 - Minimum tensile propertiesProperty ValueTensile Strength 70.0 ksi (470 MPa)Yield Strength 64.0 ksi (430 MPa)Strain to Failure 1%3.4.1.1 Properties for sizes larger than 62 in2shall be as agreed between purchaser and producer

20、.3.4.2 Density Shall be within the range of 2.88 to 2.91 g/cm (0.104 to 0.105 lb/inch) determined using a water displacement method in accordance with ASTM B311; measurement may be made on the product or a sample after HIP or a sample after heat treatment.3.5 Quality HIPed shapes, as received by pur

21、chaser, shall be uniform in quality and condition, sound, and free from imperfections detrimental to usage of the shapes.3.6 Tolerances Shall conform to +0.25/-0.000 inch (+6.35/-0.00 mm), unless specified by agreement between purchaser and supplier(see 8.3).SAE INTERNATIONAL AMS4355 Page 4 of 64. Q

22、UALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspection The vendor of HIPed shape shall supply all samples for vendors 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 en

23、sure that the HIPed blanks conforms to specified requirements.4.2 Classification of Tests All technical requirements are acceptance tests and shall be performed on each lot or each powder blend, as applicable.4.3 Sampling and Testing Shall be in accordance with the following: a lot shall consist of

24、all shapes manufactured from a specific powder blend and HIPd together in a single cycle. Mechanical properties shall be determined using samples (see 3.4.1) taken from a sample shape (component) or from material produced as an integral part (prolongation) of a shape (component) from the lot.4.3.1 T

25、ensile PropertiesOne tensile specimen from any location of a lot.4.3.1.1 Tensile specimens shall be machined from a sample heat treated to the T4P/T42P condition (see 8.6). 4.3.1.2 Tensile testing shall be done in accordance with ASTM E8/8M. 4.3.2 DensityOne sample from each lot (see 3.4.1.1) unless

26、 a sampling plan has been agreed upon by purchaser and vendor.4.3.3 DimensionsEach piece, unless a sampling plan has been agreed upon by purchaser and vendor.4.4 Reports The vendor of the product shall furnish with each shipment a report stating that the product conforms to the composition of the ma

27、trix and the volume fraction of the reinforcement component, and showing the numerical results of tests on each lot to determine conformance to the other acceptance test requirements. This report shall include the purchase order number, lot number, AMS4355, serial numbers, when specified, part numbe

28、r when applicable, as Hiped cross section area, and quantity. 4.4.1 Properties for sizes larger than 62 in2shall be as agreed between purchaser and producer.4.5 Resampling and Retesting If any specimen used in the above tests fails to meet the specified requirements, disposition of the product may b

29、e based on the results of testing two additional specimens for each original nonconforming specimen. Failure of any retest specimen to meet the specified requirements shall be cause for rejection of the product represented. SAE INTERNATIONAL AMS4355 Page 5 of 65. PREPARATION AND DELIVERY 5.1 Identif

30、ication Shall be in accordance with ASTM B666/B666M.5.2 SerializationWhen specified (see 8.11), each HIPed shape shall be serialized with a unique, non-repeating serial number.5.3 Packaging The product shall be prepared for shipment in accordance with in ASTM B660 and in compliance with applicable r

31、ules and regulations pertaining to the handling, packaging, and transportation of the product to ensure carrier acceptance and safe delivery.6. ACKNOWLEDGMENT A vendor shall mention this specification number in all quotations and when acknowledging purchase orders.7. REJECTIONS Product not conformin

32、g to this specification, or to modifications authorized by purchaser, will be subject to rejection.8. NOTES 8.1 Revision IndicatorA change bar (l) located in the left margin is for the convenience of the user in locating areas where technical revisions, not editorial changes, have been made to the p

33、revious issue of this document. An (R) symbol to the left of the document title indicates a complete revision of the document, including technical revisions. Change bars and (R) are not used in original publications, nor in documents that contain editorial changes only.8.2 ANSI H35.5, Nomenclature S

34、ystem for Aluminum Metal Matrix Composite Materials, is used to describe the matrix composition, type, volume fraction, and composition of the reinforcement materials and temper as 2124A/SiC/25p-T4P.8.3 Drawings shall be interpreted in accordance with ANSI Y14.5M, Dimension and Tolerance.8.4 Materia

35、l is supplied in the T1P condition for ease of machining and then subsequently T4P/T42P heat treated for strength.8.5 Recommended HIP Parameters 940 F 27 F (505 C 15 C ), 6 ksi (45 MPa) minimum, 1 hour minimum.8.6 Recommended Heat Treatment Parameters (1 inch (25 mm) x 1 inch (25 mm) Maximum Section

36、 Thickness)Solution Treatment: 940 F 9 F (505 C 5 C) for 1 hour minimumQuench: Cold Water Quench 73 F 9 F (23 C 5 C), Transfer Time 7 seconds maximumT4P/T42P Natural Aging at ambient temperature for 100 hours minimum.8.7 Electrical Conductivity Typical conductivity range of 24.5 to 30.0% IACS for As

37、 HIPed product (T1P).SAE INTERNATIONAL AMS4355 Page 6 of 68.8 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions and properties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented

38、only for information.8.9 Terms used in AMS are clarified in ARP1917.8.10 With the exceptions of density and particulate size, dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions and properties in SI units and the Celsius temperatures are shown as the

39、 approximate equivalents of the primary units and are presented only for information. Density is in units of gram/centimeter and particulate size is in micrometer.8.11 Purchase documents should specify not less than the following:AMS4355Dimensions of HIPed Shapes desiredSerialization, if required (see 5.2)Quantity of HIPed Shapes desiredProperty and acceptance requirements from the cognizant engineering organization applicable to sizes outside the range listed in 3.4.1.1Part number, if applicable.PREPARED BY AMS COMMITTEE “D“