FORD WSD-M1A313-A2-2002 STEEL - AUSTENITIC VALVE WROUGHT TO BE USED WITH FORD WSS-M99P1111-A (Shown on WSD-M1A313-A1)《阀门用奥氏体锻造钢 与标准FORD WSS-M99P1111-A一起使用 列于标准WSD-M1A313-A1上》.pdf
《FORD WSD-M1A313-A2-2002 STEEL - AUSTENITIC VALVE WROUGHT TO BE USED WITH FORD WSS-M99P1111-A (Shown on WSD-M1A313-A1)《阀门用奥氏体锻造钢 与标准FORD WSS-M99P1111-A一起使用 列于标准WSD-M1A313-A1上》.pdf》由会员分享,可在线阅读,更多相关《FORD WSD-M1A313-A2-2002 STEEL - AUSTENITIC VALVE WROUGHT TO BE USED WITH FORD WSS-M99P1111-A (Shown on WSD-M1A313-A1)《阀门用奥氏体锻造钢 与标准FORD WSS-M99P1111-A一起使用 列于标准WSD-M1A313-A1上》.pdf(5页珍藏版)》请在麦多课文档分享上搜索。
1、 ENGINEERING MATERIAL SPECIFICATION Material Name Specification Number Date Action Revisions 2002 09 23 Revised Updated and renumbered 1992 11 25 C10261076 Released w. Jones EAO J.C. Webster NAAO Printed copies are uncontrolled Page 1 of 5 Copyright 2002, Ford Global Technologies, Inc. STEEL, AUSTEN
2、ITIC VALVE WROUGHT WSD-M1A313-A1 WSD-M1A313-A2 WSD-M1A313-A3 WSD-M1A313-A4 WSD-M1A313-A5 1. SCOPE The materials defined by this specification are a series of wrought chromium-manganese austenitic steels which develop optimum physical properties by appropriate solution and aging treatments. Controlle
3、d forging and/or stress relieving processing may also be applicable in limited instances. 2. APPLICATION These specifications were released originally for material used for the heads of two piece exhaust valves for reciprocating engines. These materials may also be employed in one piece valve design
4、s where appropriate consideration is given to tip, stem and seat wear properties. Under normal conditions and with appropriate approval (para 3.7) a lower graded material may be substituted by an alternative (see 4.2). 3. REQUIREMENTS 3.1 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppl
5、iers and part producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). ENGINEERING MATERIAL SPECIFICATION WSD-M1A313-A1/A5 Page 2 of 5 Copyright 2002, Ford Global Technologies, Inc. 3.2 CHEMICAL COMPOSITION (WEIGHT %) A1 A2 A3 Carbon * 0.65 - 0.75 0.50
6、- 0.60 0.47 - 0.58 Manganese 5.5 - 6.9 7.0 - 10.00 7.00 - 10.00 Phosphorus 0.04 max 0.05 max 0.05 max Sulphur 0.04 max 0.09 max 0.09 max Silicon 0.45 - 0.85 0.25 max 0.25 max Chromium 20.50 - 22.00 19.50 - 21.50 20.00 - 22.00 Nickel 1.4 - 1.9 1.50 - 2.80 3.25 - 4.50 Nitrogen * 0.18 - 0.28 0.20 - 0.4
7、0 0.38 - 0.50 Tungsten - - - Niobium+Tantalum - - - Molybdenum - - - *Carbon + Nitrogen - - 0.90 min Iron Remainder Remainder Remainder A4 A5 Carbon * 0.48 - 0.58 0.45 - 0.56 Manganese 8.00 - 10.00 8.00 - 10.00 Phosphorus 0.04 max 0.05 max Sulphur 0.035 max 0.03 max Silicon 0.45 max 0.45 max Chromiu
8、m 20.00 - 22.00 20.00 - 22.00 Nickel 3.25 - 4.50 3.5 - 5.0 Nitrogen * 0.38 - 0.50 0.40 - 0.60 Tungsten - 0.8 - 1.5 Niobium+Tantalum 2.00 - 3.00 1.8 - 2.5 Molybdenum - - *Carbon+Nitrogen 0.90 min 0.90 min Iron Remainder Remainder Minor variations to the above composition will be permitted providing a
9、ll other specification and performance criteria are met and the composition is approved at control plan stage. See Para 4.1 for alternative national specifications, where available. 3.3 HEAT TREATMENT High temperature strength, fatigue and corrosion properties are dependent on heat treatment tempera
10、tures and process duration. The supplier must select the best heat treatment compromise for particular component performance. NOTE: Actual times and temperature may be adjusted to meet hardness and microstructural requirements and will be agreed at inception of the control plan. ENGINEERING MATERIAL
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