SAE AMS 7819D-2009 Molybdenum Alloy Bars 0 48Ti - 0 09Zr - 0 02C Arc Cast Stress Relieved (UNS R03640)《消除应力的0 48Ti-0 90Zr-0 02C电弧熔铸钼合金棒材》.pdf
《SAE AMS 7819D-2009 Molybdenum Alloy Bars 0 48Ti - 0 09Zr - 0 02C Arc Cast Stress Relieved (UNS R03640)《消除应力的0 48Ti-0 90Zr-0 02C电弧熔铸钼合金棒材》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 7819D-2009 Molybdenum Alloy Bars 0 48Ti - 0 09Zr - 0 02C Arc Cast Stress Relieved (UNS R03640)《消除应力的0 48Ti-0 90Zr-0 02C电弧熔铸钼合金棒材》.pdf(6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 there
2、from, 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 International All rights reserved. No part of this p
3、ublication 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: +1 724-776-497
4、0 (outside USA) 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/AMS7819D AEROSPACE MATERIAL SPECIFICATION AMS7819 REV. D Issued 1964-01 Revised 2
5、009-07 Reaffirmed 2013-10 Superseding AMS7819C Molybdenum Alloy Bars 0.48Ti - 0.09Zr - 0.02C Arc Cast, Stress Relieved (Composition similar to UNS R03640) RATIONALE AMS7819D has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE 1.1 Form This specification covers an arc-cast mo
6、lybdenum alloy in the form of round bars. 1.2 Application These bars have been used typically for parts requiring high modulus and uniform strength up to 2300 F (1260 C) but usage is not limited to such applications. This alloy is not recommended for use in oxidizing atmospheres above 1000 F (540 C)
7、 unless protected by a suitable coating. 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
8、 issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. 2.1 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959,
9、 Tel: 610-832-9585, www.astm.org. ASTM E 8 / E 8M Tension Testing of Metallic Materials ASTM E 92 Vickers Hardness of Metallic Materials ASTM E 350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, and Wrought Iron 2.2 ASME Publications Available from ASME, 22
10、 Law Drive, P.O. Box 2900, Fairfield, NJ 07007-2900, Tel: 973-882-1170, www.asme.org. ASME B46.1 Surface Texture, Surface Roughness, Waviness, and Lay SAE INTERNATIONAL AMS7819D Page 2 of 6 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1; carbon
11、shall be determined in accordance with ASTM E 350, molybdenum by difference, gaseous elements by vacuum fusion, and other metallic elements by spectrographic or other analytical methods acceptable to the purchaser: TABLE 1 - COMPOSITION Element min max Check Analysis Under Min or Over Max Molybdenum
12、 99.25 - - - Titanium 0.40 0.55 0.05 0.05 (500 ppm) Zirconium 0.06 0.12 0.02 0.02 (200 ppm) Carbon 0.010 0.030 0.005 0.005 ( 50 ppm) Iron - 0.020 - 0.002 ( 20 ppm) Silicon - 0.010 - 0.002 ( 20 ppm) Nickel - 0.010 - 0.001 ( 10 ppm) Oxygen - 0.030 (300 ppm) - - Nitrogen - 0.010 (100 ppm) - 0.0005 ( 5
13、ppm) Hydrogen - 0.0005 ( 5 ppm) - - 3.2 Melting Practice Alloy shall be carbon deoxidized and vacuum arc melted using consumable electrode practice. 3.3 Condition Hot-cold worked, descaled, and stress-relieved; when so specified, bars shall be centerless ground before being stress-relieved. The surf
14、ace texture of centerless ground bars shall be 90 microinches (2.3 m) or smoother, determined in accordance with ASME B46.1. 3.4 Properties Bars 0.125 to 4.500 inches (3.00 to 112.50 mm) inclusive, in nominal diameter shall conform to the following requirements: 3.4.1 As-Received 3.4.1.1 Tensile Pro
15、perties Shall be as specified in Table 2, determined in accordance with ASTM E 8 / E 8M with the rate of strain maintained at 0.002 to 0.005 inches/inch per minute (0.002 to 0.005 mm/mm per minute) through the 0.6% offset and 0.002 to 0.05 inches/inch per minute (0.002 to 0.05 mm/mm per minute) abov
16、e the 0.6% offset to fracture. TABLE 2A - TOLERANCES, HOT-COLD WORKED, INCH/POUND UNITS Nominal Diameter Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 4D % 0.125 to 0.875, incl 115 100 18 Over 0.875 to 1.875, incl 100 85 10 Over 1.875 to 2.875, incl 90 80 10 Over 2.875
17、to 3.500, incl 85 75 5 Over 3.500 to 4.500, incl 80 70 5 SAE INTERNATIONAL AMS7819D Page 3 of 6 TABLE 2B - TOLERANCES, HOT-COLD WORKED, SI UNITS Nominal Diameter Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in 4D % 3.00 to 22.00, incl 795 690 18 Over 22.00 to 47.00,
18、incl 690 585 10 Over 47.00 to 72.00, incl 620 550 10 Over 72.00 to 87.50, incl 585 515 5 Over 87.50 to 112.50, incl 550 485 5 3.4.1.2 Hardness Shall be shown in Table 3, determined in accordance with ASTM E 92. TABLE 3 - MAXIMUM HARDNESS Nominal Diameter Inch Nominal Diameter Millimeters Maximum Har
19、dnessHV10 0.125 to 0.875, incl 3.00 to 22.00, incl 320 Over 0.875 to 1.125, incl Over 22.00 to 28.00, incl 310 Over 1.125 to 1.875, incl Over 28.00 to 47.00, incl 300 Over 1.875 to 2.875, incl Over 47.00 to 72.00, incl 290 Over 2.875 to 3.500, incl Over 72.00 to 87.50, incl 285 Over 3.500 to 4.500,
20、incl Over 87.50 to 112.50, incl 280 3.4.2 After High-Temperature Exposure Bars shall meet the tensile property (3.4.1.1) and hardness (3.4.1.2) requirements after being heated in a suitable protective atmosphere to 2100 F 25 (1150 C 15), held at heat for 30 minutes 3, and cooled rapidly. 3.5 Quality
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