FORD WSS-M2A180-A1-2017 ALUMINUM ALLOY EXTRUSION HEAT TREATABLE STRUCTURAL HIGH STRENGTH 7000 SERIES TO BE USED WITH FORD WSS-M99P1111-A .pdf
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1、 ENGINEERING MATERIAL SPECIFICATION Date Action Revisions Rev. 00 2017 02 16 Released K. Morgan, NA Controlled document at www.MATS Copyright 2017, Ford Global Technologies, LLC Page 1 of 7 ALUMINUM ALLOY, EXTRUSION, HEAT TREATABLE, STRUCTURAL, WSS-M2A180-A1 HIGH STRENGTH, 7000 SERIES 1. SCOPE The m
2、aterial defined by these specifications is for 7000 series, heat treatable extruded aluminum profiles. Ford Motor Company may, at its option and in agreement with the local or regional supplier, define additional and/or restricted technical delivery requirements such as mechanical properties, formin
3、g characteristics, pretreatment, and/or surface texture, for a specific grade and/or part. The defined requirements shall be mandatory and no characteristics shall conflict with these engineering specifications. 2. APPLICATION This specification was released originally for extruded aluminum profiles
4、 for bumper applications. The manufacturing processes used to form these profiles includes but are not limited to rotary bending, push roll bending, stretch bending, stamping, piercing, laser trimming, and machine trimming. 2.1 LIMITATIONS The alloy defined in this specification may be susceptible t
5、o intergranular corrosion or stress corrosion cracking. The yield strength of the material in the part after the artificial aging heat treatment and/or paint baking process is a function of the thermo-mechanical history. The mechanical property values shown in Table 2 apply only to the listed condit
6、ion; individual parts will have different properties, depending on specific processing in the vehicle manufacturing plants. 2.2 DEFINITIONS Variant A1 is a 7000 series structural alloy with gage thicknesses 1.8mm to 5.0mm, typically applied to non-visible structural parts (Class 3) where high streng
7、th and good ductility are required. This alloy will be used for high volume extrusions, which will then be subjected to a prescribed artificial aging heat treatment such that the material achieves desired minimum mechanical properties. 3. REQUIREMENTS 3.1 APPROVED SOURCES This specification requires
8、 the use of approved sources. Only the sources identified on the Ford Approved Source List (ASL) can be used when this specification is listed on the drawing, CAD file, or other documents. The list of approved sources is located within Ford at or available externally through a Ford Materials Engine
9、er. 3.2 CHEMICAL COMPOSITION AND MICROSTRUCTURE (ASTM E34, ASTM E716, ASTM E1251) 3.2.1 Chemical Composition The upper and lower limits of chemical composition of the controlled elements shall be established by the supplier by any of the listed methods and included in the Suppliers Control Plan. In
10、case of dispute, the referee method shall be ASTM E34. ENGINEERING MATERIAL SPECIFICATION WSS-M2A180-A1 Copyright 2017, Ford Global Technologies, LLC Page 2 of 7 The tabulated upper and lower limits of chemical composition for each variant may not agree with those listed in the Aluminum Association
11、“Teal Sheets.“ The values in Table 1 take precedence. Check analyses of cast billets shall be provided as part of the initial material source approval process in a format suitable for upload into the Ford Material Database. Table 1: Chemical Composition (weight percent maximum, unless shown as a ran
12、ge or a minimum; balance Al) A1 Si 0.20 Fe 0.30 Cu 0.05 Mn 0.05 Mg 0.7 1.5 Cr 0.04 Zn 4.8 5.8 Ti 0.03 Zr 0.10 0.25 Other Elements 0.05 Others (total) 0.15 3.3 MECHANICAL PROPERTIES (ASTM B557M, 50 mm gauge length; ISO 6892-1) Mechanical properties are valid in the longitudinal direction parallel to
13、extrusion direction, except as noted. Certification of ongoing production material shall be in accordance with regional and/or local requirements. For the determination of mechanical properties, the material cross sectional area shall be defined as that of the aluminium alloy; contribution of any su
14、rface treatments to the calculated cross-sectional area used for stress calculations is neglected. The test specimen geometry is to be established locally to certify ongoing production material. Yield Strength is defined as 0.2% proof stress. Yield Strength (T81 therefore, the billet change scrap (s
15、tart/change/end) is not useable. Start and end scrap length are to be developed during process development for a new product. Guidelines for usable material and scrap subject to control plan. 3.6.1.2 Longitudinal Welds Longitudinal weld-line integrity shall be assessed per FLTM BB 116-01. Samples ar
16、e to be taken from the front of the extrusion coming from one billet after the prescribed scrap is removed. Actual sampling plan shall be established with Ford materials engineering and based on PFMEA and control plan. 3.7 SURFACE APPEARANCE, CONDITION, AND SURFACE ROUGHNESS 3.7.1 Surface Classifica
17、tion All variants of this specification are suitable for Class 3 applications as defined in ESF75B-11007-(*). (*) latest level 3.7.2 Surface Roughness The surface roughness and associated parameters for a given component are to be defined and recorded, if necessary, by the regional manufacturing act
18、ivity. ENGINEERING MATERIAL SPECIFICATION WSS-M2A180-A1 Copyright 2017, Ford Global Technologies, LLC Page 5 of 7 3.7.3 Final Product Identification Unless an alternate method is agreed upon by the aluminum alloy supplier and the manufacturing activity, the final extruded product shall be identified
19、 as follows per ESDU5A-1B328-(*). This information shall be marked by ink-jet or similar printer, at one meter intervals, in a color as specified by the regional Purchasing activity and shall consist of human readable information in which each piece of information is separated by “ “. The final prod
20、uct should have traceable material identification information including: Part Number Global Product Grade Name Heat Treat Date (yyyy-mm-dd) Extruded Tube Supplier Name Global Supplier Data Base (GSDB) Code Lot Number Stencil Example: 16107K40-A 6XHS yyyy-mm-dd Supplier GSDB A1234567-1 3.8 PAINTABILI
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