FORD WSS-M1A365-A20-2017 STEEL SHEET HOT ROLLED LOW CARBON TO BE USED WITH FORD WSS-M99P1111-A (Shown on FORD WSS-M1A365-A11).pdf
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1、 ENGINEERING MATERIAL SPECIFICATION Date Action Revisions Rev. 1 2017 09 06 Revised See Summary of Revisions I. Liu, AP 2012 01 10 Released D. Jordan, NA, A. Toennessen, EU Controlled document at www.MATS Copyright 2017, Ford Global Technologies, LLC Page 1 of 9 STEEL, SHEET, COLD ROLLED, LOW CARBON
2、 WSS-M1A365-A11 STEEL, SHEET, COLD ROLLED, LOW CARBON, WSS-M1A365-A12 GENERAL FORMABILITY STEEL, SHEET, COLD ROLLED, LOW CARBON, WSS-M1A365-A13 IMPROVED FORMABILITY STEEL, SHEET, COLD ROLLED, LOW CARBON, WSS-M1A365-A14 HIGH FORMABILITY STEEL, SHEET, COLD ROLLED, LOW CARBON, WSS-M1A365-A15 EXTRA HIGH
3、 FORMABILITY STEEL, SHEET, HOT ROLLED, LOW CARBON WSS-M1A365-A20 STEEL, SHEET, HOT ROLLED, LOW CARBON, WSS-M1A365-A21 GENERAL FORMABILITY STEEL, SHEET, HOT ROLLED, LOW CARBON, WSS-M1A365-A22 IMPROVED FORMABILITY STEEL, SHEET, HOT ROLLED, LOW CARBON, WSS-M1A365-A23 HIGH FORMABILITY 1. SCOPE The mater
4、ials defined by these Global specifications are fully killed, fine grained, low carbon steel sheet, with specified minimum yield strength between 110 and 240 MPa and good forming, joining, and painting characteristics. The steel sheet may achieve its final thickness by cold rolling, hot rolling, con
5、tinuous thin-strip casting, or other means. All requirements of the specific variant are to be met regardless of the final thickness reduction method. Hot rolled flat products are usually supplied in thicknesses greater than 1.8 mm, for uncoated products in a pickled and oiled condition. Specificati
6、on WSS-M1P94-A shall be used where pre-coating by the steel supplier is required. All requirements of the specific variant are to be met with or without pre-coating, except as noted in these specifications or as noted as exceptions on the Engineering Drawing. ENGINEERING MATERIAL SPECIFICATION WSS-M
7、1A365-A11/A23 Copyright 2017, Ford Global Technologies, LLC Page 2 of 9 2. APPLICATION These Global specifications were released originally for automotive body and chassis parts. 2.1 LIMITATIONS Common Global Grade Names are provided for information purposes and are not intended to be used on Engine
8、ering Drawings or CAD files. Not all grade / gauge / width / coating combinations are available. Contact Product Development Materials Engineering for assistance or Global Materials and Fastener Standards () for help in locating the responsible engineer. Material supplied to these specifications may
9、 contain titanium or other transition metals as alloying additions. Such alloyed steels, if subsequently surface treated by a nitrocarburising and/or oxidizing process, risk becoming embrittled due to the formation of ultrafine TiN or other precipitates. Accordingly, special consideration should be
10、given to low carbon steel that contains intentional additions of titanium or other transition metals for parts that may be subjected to nitrocarburising and/or oxidizing processes. 3. REQUIREMENTS Note: Drawing Precedence Any part specific exceptions or restrictions of requirements listed in paragra
11、ph 3 shall be recorded on the part drawing and have to be considered in all engineering testing and attribute confirmation checklists. 3.1 APPROVED SOURCES This specification requires the use of approved sources. Only the sources identified on the Ford Approved Source List (ASL) can be used when thi
12、s 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 Engineer. See also paragraph 4.1. 3.2 CHEMICAL COMPOSITION AND MICROSTRUCTURE (ASTM E112, JIS G0320, ISO 4967 / ASTM E45) 3
13、.2.1 Chemical Composition The upper and lower limits of chemical composition of the controlled elements shall be established by the supplier and included in the suppliers Control Plan. Guidelines for chemical composition are provided in section 4.4. Heat and/or check analyses shall be provided as pa
14、rt of the initial material source approval process in a format suitable for upload into the Ford Material Database. 3.2.2 Microstructure The grain size number shall be established as part of the initial material source approval process and shall be consistent (within 1 unit) throughout the thickness
15、 of the sheet. The steel sheet shall be free from internal defects that adversely affect manufacturing or part functionality. Examples of defects may include: pipe laminations, non-metallic inclusions, segregation, and blowholes. Non-metallic inclusion content shall not exceed a rating of 2.0 for th
16、in and 2.0 for heavy when tested in accordance with ASTM E45 Method D, Plate I-r, by analysis at 100X. ENGINEERING MATERIAL SPECIFICATION WSS-M1A365-A11/A23 Copyright 2017, Ford Global Technologies, LLC Page 3 of 9 3.3 MECHANICAL PROPERTIES (ASTM E8M, ASTM E517, ISO 6892-1, ISO 10113, ISO 10275,JIS
17、Z2241,JIS Z2254) For initial approval requirements see paragraph 4.1. Mechanical properties are valid in both the transverse and longitudinal directions. Certification of ongoing production material shall be in accordance with regional and/or local requirements. It is acceptable to certify material
18、for shipment using only one test direction. However, disputes will be settled using longitudinal, transverse and diagonal test bars sampled from the suspect material. For the determination of mechanical properties, the material cross sectional area shall be defined as that of the steel substrate onl
19、y; contribution of any metallic and/or organic coating to the calculated cross-sectional area used for stress calculations is neglected. (i.e. Zn, e-coat and/or paint are not included). This method of determining the cross sectional area of the test bar will be used as the referee method in all case
20、s where the mechanical properties of the incoming material are in dispute. Yield Strength is defined as lower yield stress or 0.2% proof stress (for materials without marked yield point). ASTM Total Elongation is measured with an ASTM (50 mm) test bar (ASTM E 8M). EN Total Elongation is measured wit
21、h an ISO II (80 mm) test bar (ISO 6892-1). JIS Total Elongation is measured with a JIS #5 test bar (JIS Z 2241). Plastic Strain Ratio (r-value) is defined for a specific test direction with respect to the rolling direction. It is measured at 20% total elongation (or maximum uniform elongation if les
22、s than 20%). See ASTM E 517, ISO 10113, or JIS Z 2254. Average Plastic Strain Ratio (ravg) is calculated as a weighted average of the individual r-values, i.e., ( 0o + 90o + 2 x 45o ) / 4. For grades with ravg requirements, data is collected for initial source approval. Ongoing certification to ravg
23、 requirements is not required for all coils. However, disputes will be settled using longitudinal, transverse and diagonal test bars sampled from the suspect material. Strain Hardening Exponent (n-value) is measured over the range 10-20% strain (or 10% to end of uniform elongation if less than 20%).
24、 See ASTM E 646 or ISO 10275. n-value measurements only valid for material up to 6.4 mm. For gauges over 6.4 mm n-values are not required. Bend testing shall be performed to ASTM E290. Using a V-Bend test setup through a 90 bend angle. Other test setups may be acceptable at the discretion of the reg
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