SAE AMS 5629 H1000-2015 Steel Corrosion-Resistant Bars Wire Forgings Rings and Extrusions 13Cr - 8 0Ni - 2 2Mo - 1 1Al Vacuum Induction Plus Consumable Electrode Melted Solution He.pdf
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1、AEROSPACE MATERIAL SPECIFICATION AMS5629/H1000 REV. A Issued 2014-12 Revised 2015-04 Superseding AMS5629/H1000 Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 13Cr - 8.0Ni - 2.2Mo - 1.1Al Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Precipitation H
2、ardened (H1000) (Composition similar to UNS S13800) RATIONALE AMS5629/H1000A results from a limited scope ballot to correct errors in Table 3B. 1. SCOPE 1.1 Form This specification covers a corrosion-resistant steel product in the solution and precipitation heat treated (H1000) condition. 1.1.1 The
3、aged product may be supplied directly by a mill or by a producer other than the mill. The latter would be accomplished by precipitation heat treatment of solution treated material previously certified to AMS5629. The entity assuming responsibility for the aging operation is designated the producer o
4、f AMS5629/H1000. 1.1.2 This specification covers products up to 12 inches (305 mm) and under in nominal diameter, thickness or for hexagons, least distance between parallel sides (See 8.3). 1.2 Application These products have been used typically for parts requiring corrosion resistance and high stre
5、ngth up to 600 F (316 C) with good ductility and strength in the transverse direction in large section sizes, but usage is not limited to such applications (See 8.1). 1.3 Classification Melting practice classification shall be in accordance with AMS5629. 2. APPLICABLE DOCUMENTS The issue of the foll
6、owing 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 referenced document has been cancelled and no supersedin
7、g document has been specified, the last published issue of that document shall apply. _ 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 a
8、nd suitability for any particular use, including any patent infringement arising 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 an
9、d suggestions. Copyright 2015 SAE International All rights reserved. No part of 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
10、 PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (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/stand
11、ards/AMS5629/H1000A SAE INTERNATIONAL AMS5629/H1000A Page 2 of 5 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. AMS2750 Pyrometry AMS2759/3 Heat Treatme
12、nt, Precipitation-Hardening Corrosion-Resistant and Maraging Steel Parts AMS5629 Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 13Cr - 8.0Ni - 2.2Mo - 1.1Al, Vacuum Induction Plus Consumable Electrode Melted, Solution Heat Treated, Precipitation Hardenable AMS-H-6875 Heat Tr
13、eatment of Steel Raw Materials 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall be in accordance with AMS5629. 3.2 Melting Practice and Delta Ferrite Class Shall be in accordance with AMS5629. 3.3 Condition Shall be in accordance with AMS5629, and the following: 3.3.1 The product shall be supplied in
14、 the precipitation hardened (H1000) heat treat condition. 3.3.1.1 If stress relieving is requested by the purchaser, heat treatment shall be performed by heating to 900 F 25 F (482 C 14 C) and soaking for at least 1 hour plus 1 hour additional for each inch (25 mm) of thickness or fraction thereof g
15、reater than 1 inch (25 mm). When load thermocouples are used, the soaking time shall be at least 1 hour. Heat treated tolerances stated in AMS2241 will be applied if stress relieving after aging is requested. 3.3.1.2 Bar shall not be cut from plate (See also 4.3.1). 3.4 Heat Treatment Shall be in ac
16、cordance with AMS5629 and the following: 3.4.1 Precipitation Heat Treatment Shall be in accordance with the requirements applicable to either AMS-H-6875 and AMS2750, or AMS2759/3 at the vendors option, except acceptance testing and criteria shall be as specified in 3.5.1.3. Precipitation heat treatm
17、ent processed in batch-type furnaces shall have Type B instrumentation. Continuous-type furnaces shall comply with the pyrometry requirements of AMS2750. When the product is precipitation heat treated by an entity other than the mill producer of the AMS5629 certified product, the heat treatment sour
18、ce shall be accredited by a recognized industry agency for stainless steel heat treatment acceptable to the purchaser. 3.5 Properties 3.5.1 All products shall conform to the following requirements: 3.5.1.1 Macrostructure Shall be in accordance with AMS5629. SAE INTERNATIONAL AMS5629/H1000A Page 3 of
19、 5 3.5.1.2 Microstructure Shall be in accordance with AMS5629. 3.5.1.3 Tensile Properties Shall be in accordance with the following: 3.5.1.3.1 Product, 12 inches (305 mm) and under in nominal diameter, thickness or for hexagons, least distance between parallel sides, shall be as shown in Table 3. Pr
20、operties for larger sizes shall be as agreed upon between purchaser and vendor. Tensile testing shall be performed in accordance with ASTM A370. Table 3A - Tensile properties, inch/pound units (1) Condition Specimen Orientation Tensile Strength ksi Minimum Yield Strength at 0.2% Offset ksi Minimum E
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