FORD ESB-M2A113-B-2010 ALUMINUM-FORMABLE SHEET ALLOY TO BE USED WITH FORD WSS-M99P1111-A 《可成型的铝合金板 与标准FORD WSS-M99P1111-A一起使用 》.pdf
《FORD ESB-M2A113-B-2010 ALUMINUM-FORMABLE SHEET ALLOY TO BE USED WITH FORD WSS-M99P1111-A 《可成型的铝合金板 与标准FORD WSS-M99P1111-A一起使用 》.pdf》由会员分享,可在线阅读,更多相关《FORD ESB-M2A113-B-2010 ALUMINUM-FORMABLE SHEET ALLOY TO BE USED WITH FORD WSS-M99P1111-A 《可成型的铝合金板 与标准FORD WSS-M99P1111-A一起使用 》.pdf(3页珍藏版)》请在麦多课文档分享上搜索。
1、 ENGINEERING MATERIAL SPECIFICATIONDate Action Revisions 2010 02 15 N-STATUS No replacement named S. Ryzyi, NA 2005 01 19 Revised Inserted 3.0; Deleted 3.9, 4 1980 06 12 Released AL1-6000-35 Printed copies are uncontrolled Copyright 2010, Ford Global Technologies, LLC Page 1 of 3 ALUMINUM-FORMABLE,
2、SHEET ALLOY ESB-M2A113-B NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by this specification is a formable, heat treatable aluminum sheet alloy (SAE AA X7021). 2. APPLICATION This specification was released originally for material used as bumper reinforcements. CONTROL ITEM - AFFECTS G
3、OVERNMENT REGULATION COMPLIANCE OR CRITICAL VEHICLE FUNCTION AND MUST COMPLY WITH APPLICABLE REQUIREMENTS OF FORD Q-101 OR MANUFACTURING PRACTICE 102 - AREAS MARKED () ARE CONTROL ITEM CHARACTERISTICS - CHANGE IN DESIGN, COMPOSITION OR PROCESSING FROM THE PART PREVIOUSLY APPROVED FOR PRODUCTION REQU
4、IRES PRIOR PRODUCT ENGINEERING APPROVAL. 3. REQUIREMENTS 3.0 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.1 CHEMICAL COMPOSITION (ASTM E 34) Silicon 0.25 max Iron 0
5、.40 max Copper 0.25 max Manganese 0.10 max Magnesium 1.2 - 1.8 Chromium 0.05 max Zinc 5.0 - 6.0 Titanium 0.10 max Zirconium 0.08 - 0.18 Others, Each 0.05 Others, Total 0.15 Aluminum Balance 3.2 MECHANICAL PROPERTIES, “O“ TEMPER (ASTM E 8) Elongation, min 12% ENGINEERING MATERIAL SPECIFICATION ESB-M2
6、A113-B Printed copies are uncontrolled Copyright 2010, Ford Global Technologies, LLC Page 2 of 3 3.3 MECHANICAL PROPERTIES (After heat treating per paragraph 3.5) (ASTM E 8) Yield Strength, min 50,000 psi (345 MPa) Tensile Strength, min 57,000 psi (393 MPa) Elongation, min 8% 3.4 BEND TEST, TRANSVER
7、SE 2T (ASTM E 290) Test samples in the as received condition prior to solution heat treatment, shall pass a 90 bend test at room temperature with the minimum inside bend radius on sheet stock under 0.180 in (4.6 mm) thickness not to exceed the above limits. (T denotes sample thickness.) Note: Somewh
8、at more liberal radii may be required during fabrication of parts. 3.5 HEAT TREAT PROCESS T61 TEMPER As a final operation, all parts must be heat treated using the following sequence: Solution heat treat for 5-10 min at 400 to 470 C. Force air quench to approximately 90 C at a min rate of 3.3 C/s ov
9、er the range 385-200 C. Incubate at room temperature for 8 h min Artificially age as follows: a) Start at room temperature. b) Heat at 55 C/h max between both room temperature incubation step and first step age (c) and between first step age and second step age (d). c) First step: Soak 2 h at 120 +/
10、- 5 C d) Second step: Soak 4 h at 160 +/- 5 C. Note: All temperatures shown above are metal temperature. 3.6 EXCO (ASTM G 34) Master samples of aluminum exhibiting worst case Exco ratings of “EB“ and “EC“ are on file at the BEPE Materials Engineering Office. In case of dispute between standard refer
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