ARMY A-A-52549-1996 NICKEL BASE ALLOY SHEET CORROSION-AND HEAT-RESISTANT (METRIC)《公制腐蚀和耐热板的镍基合金》.pdf
《ARMY A-A-52549-1996 NICKEL BASE ALLOY SHEET CORROSION-AND HEAT-RESISTANT (METRIC)《公制腐蚀和耐热板的镍基合金》.pdf》由会员分享,可在线阅读,更多相关《ARMY A-A-52549-1996 NICKEL BASE ALLOY SHEET CORROSION-AND HEAT-RESISTANT (METRIC)《公制腐蚀和耐热板的镍基合金》.pdf(4页珍藏版)》请在麦多课文档分享上搜索。
1、METRIC March 15. 1996 SUPERSEDING 30 March 1988 A-A-52549 MIL-N-62623 (AT) COMMERCIAL ITEM DESCRIPTION NICKEL BASE ALLOY, SHEET, CORROSION- AND HEAT-RESISTANT (METRIC) The General Services Administration has authorized the use of this commercial item description (CID) for all federal agencies. 1. SC
2、OPE. This CID covers sheet stock of a corrosion- and heat-resistant nickel base alloy, referred to herein as “alloy“. This alloy is intended primarily for parts requiring good corrosion- and oxidation-resistance at temperatures up to approximately 1093 degrees Celsius (OC). Alloy may be used where s
3、uch parts require welding. 2. SALIENT CHARACTERISTICS 2.1 Materials. Materials shall be uniform in quality and condition, clean, sound, and free from foreign materials and internal and external imperfections detrimental to fabrication or performance of parts. Conformance to these requirements shall
4、be established by visual inspection for surface quality of the final product and metallographic examination of the structure. The use of recovered materials made in compliance with regulatory requirements is acceptable provided that all requirements of this CID are met (see 3.1). 2.1.1 Delivew condi
5、tion. Unless otherwise specified (see 6.2), the alloy shall be delivered cold rolled and bright annealed in a protective atmosphere, such as hydrogen. The use of dissociated ammonia or N2/H2 mixtures is prohibited. The product may be leveled after the last anneal to enhance flatness of the product.
6、_. Beneficial comments, recommendations, additions, deletions, clarifications, etc. and any other data which may improve this document should be sent by letter to: U.S. Army Tank-automotive and Armaments Command, ATTN: AMSTA-TR-EBLUE, Warren, MI 48397-5000. AMSC NJA FSC 9630 DISTRIBUTION STATEMENT A
7、. Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- A-A-52549 9999974 0170078 989 A-A-52549 2.1.2 Chemical composition. The alloy shall be nickel-chrome, solid solution strengthened, Unified Numb
8、ering System (UNS) N06625, in the form of sheet stock. The chemical composition of the alloy shall conform to the percentage by weight of each element as specified in ASTM B443 or equivalent. Determination of cobalt is not required for routine acceptance. 2.2 Design and construction. 2.2.1 Thickness
9、. Alloy shall be not greater than 0.5 1 millimeter (mm) thick. 2.2.2 Grain size. The grain size of the alloy shall be ASTM Micro-Grain Size #5 or finer in accordance with ASTM El 12. 2.2.3 Surface discoloration. Unless otherwise specified (see 6.2), there shall be no evidence of surface discoloratio
10、n present on the alloy. 2.3 Performance. 2.3.1 Tensile properties. The tensile properties of the alloy shall be as follows when the alloy is tested in accordance with ASTM ES: a. Ultimate strength: Not less than 724 megapascals (ma) b. Yield strength at 0.2 percent (%) offset: 331 to 393 MPa c. Elon
11、gation in 50.8 mm: Not less than 35% 2.3.2 Stress rupture. Alloy shall not fail in less than 23 hours and elongation shall be not less than 15% in 50.8 mm when the alloy is subjected to a continuous axial load of 114 MPa in accordance with ASTM E139 at a temperature of 816 2 3C. 2.3.3 Bending. Alloy
12、 shall withstand, without cracking, bending at room temperature through an angle of 180 degrees around a diameter equal to the nominal thickness of the alloy, with the axis of the bend parallel to the direction of rolling. 2.4 Identification markings. Identification markings shall be permanent and l
13、egible and shall include, as a minimum, the manufacturers identification code (CAGE), the heat number, the alloy nominal thickness, and the part identification number (PIN) (see 6.3). When identification marking is performed directly on the alloy, the marking fluid shall have no deleterious effect o
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