SAE AMS 4994A-2006 Titanium Alloy Powdered Metal Products 6Al - 4V Hot Isostatically Pressed Annealed (UNS R56400)《热等静态压力的硬质粉末金属产品的6AL 4V的钛合金》.pdf

《SAE AMS 4994A-2006 Titanium Alloy Powdered Metal Products 6Al - 4V Hot Isostatically Pressed Annealed (UNS R56400)《热等静态压力的硬质粉末金属产品的6AL 4V的钛合金》.pdf》由会员分享，可在线阅读，更多相关《SAE AMS 4994A-2006 Titanium Alloy Powdered Metal Products 6Al - 4V Hot Isostatically Pressed Annealed (UNS R56400)《热等静态压力的硬质粉末金属产品的6AL 4V的钛合金》.pdf（8页珍藏版）》请在麦多课文档分享上搜索。

1、AEROSPACEMATERIAL SPECIFICATIONAMS4994 REV. AIssued 1992-07Revised 2006-03Reaffirmed 2015-03Superseding AMS4994Titanium Alloy Powdered Metal Products6Al - 4VHot Isostatically Pressed, Annealed(Composition similar to UNS R56400)RATIONALEAMS4994A has been reaffirmed to comply with the SAE five-year re

2、view policy._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 ar

3、ising therefrom, 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 o

4、f this publication 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: +1 724-7

5、76-4970 (outside 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/AMS4994A 1. SCOPE: 1.1 Form: This specification covers powdered metal products co

6、nsolidated by hot isostatic pressing (HIP) of titanium alloy powder compacts. 1.2 Application: These products have been used typically for complex-shaped powdered metal products made to near net shape dimensions with properties similar to wrought products, but usage is not limited to such applicatio

7、ns. 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 refere

8、nced document has been cancelled and no superseding document has been specified, the last 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

9、 (outside USA), www.sae.org. AMS 2249 Chemical Check Analysis Limits, Titanium and Titanium Alloys AMS 2750 Pyrometry AMS-STD-2154 Inspection, Ultrasonic, Wrought Metals, Process For AMS 4998 Titanium Alloy Powder, 6Al - 4V, Premium Quality 2.2 ASTM Publications: Available from ASTM International, 1

10、00 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 311 Density Determination for Powder Metallurgy Materials Containing Less than Two Percent Porosity ASTM E 8 Tension Testing of Metallic Materials ASTM E 8M Tension Testing of Metallic Mate

11、rials (Metric) ASTM E 399 Plane-Strain Fracture Toughness of Metallic Materials ASTM E 539 Standard Test Method for X-Ray Emission Spectrometric Analysis of 6AI-4V Titanium Alloy ASTM E 1409 Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Technique ASTM E

12、 1417 Liquid Penetrant Examination ASTM E 1447 Determination of Hydrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Thermal Conductivity Method ASTM E 1742 Radiographic Examination ASTM E 1941 Standard Test Method for Determination of Carbon in Refractory and Reactive Metals and Their A

13、lloys ASTM E 2371 Standard Test Method for Analysis of Titanium and Titanium Alloys by Atomic Emission Plasma Spectrometry 2.3 ANSI Publications: Available from ANSI American National Standards Institute, 25 West 43rd Street, New York, NY 10036, Tel: 212-642-4900, www.ansi.org. ANSI B46.1 Surface Te

14、xture 3. TECHNICAL REQUIREMENTS: 3.1 Powder: The powder used to make products shall conform to AMS 4998 and shall be derived from prealloyed stock. Comminuted hydrided stock is not permitted. SAE INTERNATIONAL AMS4994A Page 2 of 8_ 3.2 Composition: Parts shall conform to the percentages by weight sh

15、own in Table 1; carbon shall be determined in accordance with ASTM E 1941, hydrogen in accordance with ASTM E 1447, oxygen and notrogen in accordance with ASTM E 1409, , and other elements in accordance with ASTM E 539 or ASTM E 2371. Other analytical methods may be used if acceptable to the purchas

16、er. TABLE 1 - Composition Elements min max Aluminum 5.50 6.75 Vanadium 3.50 4.50 Oxygen 0.13 0.20 Iron - 0.30 Carbon - 0.10 Tin (3.2.1) - 0.10 Molybdenum (3.2.1) - 0.10 Copper (3.2.1) - 0.10 Manganese (3.2.1) - 0.10 Zirconium - 0.10 Nitrogen - 0.05 Hydrogen - 0.0125 (125 ppm) Yttrium (3.2.2) - 0.005

17、0 ( 50 ppm) Other Elements, each (3.2.2) - 0.10 Other Elements, total (3.2.2) - 0.30 Titanium remainder 3.2.1 The combined contents of tin, molybdenum, copper, and manganese shall not exceed 0.20%. 3.2.2 Determination not required for routine acceptance. 3.2.3 Check Analysis: Composition variations

18、shall meet the applicable requirements of AMS 2249. 3.3 Condition: Annealed. 3.4 Heat Treatment: Powdered metal products shall be annealed by heating under vacuum or in argon and/or helium to a temperature within the range 1275 to 1600 F (691 to 871 C), holding at the selected temperature within 25

19、F (14 C) for four hours 0.25 and furnace cooling under vacuum or in argon and/or helium. Pyrometry shall be in accordance with AMS 2750. 3.5 Consolidation Process: 3.5.1 Powder shall be compacted in a single gas-hot-isostatic-pressing (HIP) cycle. Pressing parameters of time, temperature, and pressu

20、re shall be selected to provide parts that conform to the requirements of 3.6. SAE INTERNATIONAL AMS4994A Page 3 of 8_ 3.5.2 All consolidation shall be performed below 1750 F (954 C). 3.5.3 When metal containers are used to hold the powder during consolidation, all evidence of the metal container sh

21、all be removed mechanically or chemically before annealing. 3.6 Properties: Powdered metal products shall conform to the following requirements: 3.6.1 Thermally-Induced Porosity (TIP): The degree of TIP in consolidated parts shall not exceed 0.3% or other value agreed upon by the purchaser and vendo

22、r, determined as in 3.6.1.1. 3.6.1.1 A sample weighing 0.01 to 0.1 pound (4.5 to 45.5 grams) shall be cut from an annealed compact. The sample density shall be determined in accordance with ASTM B 311. The sample shall then be heated in a vacuum at 2200 to 2300 F (1204 to 1260 C) and 10-3 Torr maxim

23、um pressure for not less than two hours. No backfilling shall be permitted and vacuum shall be held until temperature falls below 700 F (371 C). The percent change in density expressed as the difference in density divided by the final density and multiplied by 100 shall be defined as the degree of T

24、IP. 3.6.2 Tensile Properties: Shall be as specified in Table 2, determined in accordance with ASTM E 8 or ASTM E 8M. TABLE 2 - Minimum Tensile Properties Property Value Tensile Strength 130 ksi (896 MPa) Yield Strength at 0.2% Offset 120 ksi (827 MPa) Elongation in 4D or 2 Inches (50.8 mm) 10% Reduc

25、tion of Area* 25% *For cylindrical specimens only 3.6.2.1 Requirements for products from which tensile specimens cannot be obtained due to size limits shall be as agreed upon by purchaser and vendor. 3.6.3 Fracture Toughness: When specified, the minimum plane strain fracture toughness shall be 65 ks

26、i (71 MPa ) for any orientation, determined in accordance with ASTM E 399. Location and orientation of specimens shall be as specified on the engineering drawing; if not specified, location and orientation are optional. 3.6.4 Microstructure: The microstructure of finished products in any region shal

27、l be homogeneous and free of inclusions and voids and shall exhibit equiaxed alpha in a transformed beta matrix or equiaxed alpha and elongated alpha in a transformed beta matrix. Continuous alpha along prior beta boundaries or other evidence of beta region exposure, a surface layer of predominantly

28、 alpha phase (alpha case), and/or evidence of prior particle boundaries are not acceptable. Examinations shall be made on etched samples at up to 250X magnification. Edges and corners shall be examined to show consolidation and absence of contamination. SAE INTERNATIONAL AMS4994A Page 4 of 8_ 3.6.5

29、Radiographic Inspection: Shall be in accordance with ASTM E 1742, Quality Level 2, and shall shown no evidence of any high- or low-density inclusions. 3.6.6 Ultrasonic Inspection: When specified, shall be in accordance with AMS-STD-2154, acceptance Class AA. Inspection type, PM standard blocks, and

30、other inspection parameters shall be as agreed upon by purchaser and vendor. 3.6.7 Penetrant Inspection: Product shall be inspected in accordance with ASTM E 1417, Type 1, method optional, sensitivity Level 2. Products with any of the following conditions are not acceptable: Linear indications (leng

31、th = 3 x width). Rounded indications 1/32 inch (0.8 mm) and larger. More than 10 porosity indications in any 1 square inch (645 mm2) area. 3.6.8 Texture: Surface texture shall be 125 microinches (3.18 m) or smoother determined in accordance with ANSI B46.1. 3.7 Quality: Powdered metal products, as r

32、eceived by purchaser, shall be uniform in quality and condition, sound, and free of foreign materials and imperfections detrimental to usage of the parts. 4. QUALITY ASSURANCE PROVISIONS: 4.1 Responsibility for Inspection: The supplier of products shall provide all samples for suppliers tests and sh

33、all 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 product conforms to specified requirements. 4.2 Classification of Tests: Tests for all technical requirements are acceptanc

34、e tests and preproduction tests and shall be performed prior to or on the initial shipment of product to a purchaser, on each lot, when a change in material and/or processing requires reapproval as in 4.4, and when purchaser deems confirmatory testing to be required. 4.3 Sampling and Testing: Shall

35、be as follows; a lot shall be all products of a single design, produced from the same powder lot or blend, compacted in the same consolidation cycle, post compaction heat treated in the same furnace load, and presented for suppliers inspection at one time: 4.3.1 For Acceptance Tests: Specimens shall

36、 be taken from products, prolongations, or material adjacent to the product. Results from the following tests shall be forwarded to purchaser before or with any shipment of product: SAE INTERNATIONAL AMS4994A Page 5 of 8_ 4.3.1.1 One sample from each lot for composition (3.2), thermally induced poro

37、sity (3.6.1), fracture toughness (3.6.3) when specified, microstructure (3.6.4), and surface texture (3.6.8). 4.3.1.2 Two samples from each lot for tensile properties (3.6.2). 4.3.1.3 Each product in each lot for radiographic inspection (3.6.5), ultrasonic inspection (3.6.6) when specified, and pene

38、trant inspection (3.6.7). 4.3.2 For Preproduction Tests: Specimens may be taken from sacrificial powdered metal products, products instrumented for temperature monitoring, and material adjacent to products such as fill tubes. In some cases products shall be augmented with a prolongation specifically

39、 for specimens. Prolongation design and any controls on specimen location and orientation shall be specified on the drawing. Prior to the initial shipment of any product, the supplier shall forward to purchaser the results of a process preproduction program consisting of the following tests and any

40、other tests specified on the drawing or purchase order. 4.3.2.1 One sample from each of two products for composition (3.2) and thermally induced porosity (3.6.1). 4.3.2.2 One sample from one product and five samples from products or prolongations for tensile properties (3.6.2). 4.3.2.3 One sample fr

41、om one product and two samples from products or prolongations for fracture toughness (3.6.3). 4.3.2.4 Two samples from each of three products or prolongations for microstructure (3.6.4). 4.3.2.5 Each product for radiographic inspection (3.6.5), ultrasonic inspection (3.6.6) when required, and penetr

42、ant inspection (3.6.7). 4.3.2.6 One sample from each of three products for surface texture inspection (3.6.8). 4.4 Approval: 4.4.1 The supplier of powdered metal products shall establish a written process description of manufacture and inspection for each product number prior to and during preproduc

43、tion. The description shall include control factors and parameters that provide products meeting the requirements of this specification. Control factors considered proprietary by vendor may be assigned codes within the process description. Each variation in such control factors shall be assigned a m

44、odified code designation. The vendor shall maintain a complete record of all proprietary factors and codes. These factors shall include, but are not limited to, the following: Type and source of powder Compaction concept Mold design (fill tube location) Compaction parameters and sequence, type of ga

45、s, times, temperatures, pressures Post compaction cleaning and annealing methods and annealing parameters Sequence of all chemical and/or heat treatments Inspection procedures, standards, parameters SAE INTERNATIONAL AMS4994A Page 6 of 8_ 4.4.2 Prior to the initial shipment of products of a particul

46、ar design, the supplier shall submit results of preproduction tests and, when requested, a copy of the process description for approval by the cognizant engineering organization. 4.4.3 The supplier shall not change the process description and shall make no significant change to materials, processes,

47、 or controls referenced in the process description, unless the change is approved by the cognizant engineering organization. A significant change is one which in the judgment of the cognizant engineering organization, could affect the properties or performance of the product. 4.5 Reports: 4.5.1 Prior to the initial shipment of product, the supplier shall forward to purchaser the results of a completed preproduction program for approval. The report shall include the results of tests required in 4.3.2 and the process description and c