GMW GMW3164-2011 Cast Stainless Steel for High Temperature Components Issue 3 English [Replaced GMW GMW3164]《高温部件的铸造不锈钢 第3次出版(英文版本)[代替 GMW GMW3164]》.pdf
《GMW GMW3164-2011 Cast Stainless Steel for High Temperature Components Issue 3 English [Replaced GMW GMW3164]《高温部件的铸造不锈钢 第3次出版(英文版本)[代替 GMW GMW3164]》.pdf》由会员分享,可在线阅读,更多相关《GMW GMW3164-2011 Cast Stainless Steel for High Temperature Components Issue 3 English [Replaced GMW GMW3164]《高温部件的铸造不锈钢 第3次出版(英文版本)[代替 GMW GMW3164]》.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、 WORLDWIDE ENGINEERING STANDARDS Material Specification GMW3164 Cast Stainless Steel for High Temperature Components Copyright 2011 General Motors Company All Rights Reserved August 2011 Originating Department: North American Engineering Standards Page 1 of 6 1 Scope This material standard applies t
2、o those grades of stainless steel castings used in automotive and allied industries requiring high temperature heat resistant service. This standard specifies compositional requirements for the casting. Any specific material property required from a particular casting or section of that casting shal
3、l be identified on the engineering drawing. Wrought stainless steels are discussed in GMW3161. 1.1 Material Description. Cast stainless steel has excellent strength, ductility and heat resistance. Steel castings can be welded and are easily adapted to other steel fabrications. GMW3164 grades, their
4、approximate upper use temperatures, and matrix microstructures are listed in Table 1. Table 1: GMW3164 Grades, Upper Use Temperatures and Matrix Microstructures Grade Upper Use Temperature (C) Note 1 Matrix Microstructure Cr17Si 950 Ferritic Cr20Ni10Nb 950 Austenitic Cr25Ni21NbW 975 Austenitic Cr26N
5、i26W2Nb 1000 Austenitic Ni38Cr18SiNb 1020 Austenitic Cr26Ni14Nb2 1025 Austenitic Cr25Ni20Si 1050 Austenitic Cr26Ni22W3Nb 1050 Austenitic Note 1: Upper use temperatures are based on oxidation temperature limits and are approximate. These temperatures are guides only. 1.2 Symbols. Not applicable. 1.3
6、Typical Applications. Stainless steel castings described in this specification are primarily used for exhaust manifolds and turbo charger housings requiring high temperature heat resistance. 2 References Note: Only the latest approved standards are applicable unless otherwise specified. 2.1 External
7、 Standards/Specifications. ANSI/AWS A5.9 DIN EN 10295 ISO 6892 ASTM A751 ISO 6506 2.2 GM Standards/Specifications. GMW3059 GMW14058 GMW3161 2.3 Additional References. TMC003 Material Safety Data Sheet guidance documents (available at ). Copyright General Motors Company Provided by IHS under license
8、with General Motors CompanyNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-GM WORLDWIDE ENGINEERING STANDARDS GMW3164 Copyright 2011 General Motors Company All Rights Reserved August 2011 Page 2 of 6 3 Requirements 3.1 Requirements on Delivery. 3.1.1 Chemical Requi
9、rements. The chemical composition is a mandatory requirement. Chemical composition is used as the mandatory requirement since it will most accurately reflect material performance at elevated temperature. The chemical compositional requirements are shown in Table 2. A chemical analysis of each metal
10、heat shall be made by the foundry from a representative test sample that is taken during pouring. The chemical analysis shall conform to the requirements specified for the respective grade listed in Table 2 when tested per ASTM A751. Table 2: Mandatory Chemical Composition (in % by Mass) Grade C Si
11、Mn Cr Ni Mo W Nb S P N Fe Cr17Si 0.25 to 0.45 1.00 to 2.00 1.0 max. 17.0 to 20.0 0.9 max. 0.50 max. 1.5 to 2.00 0.60 max. 0.05 max. 0.04 max. - Bal Cr20Ni10Nb 0.25 to 0.50 2.00 max. 1.5 max. 19.0 to 23.0 9.0 to 14.0 0.50 max. 0.60 max. 1.2 to 1.8 0.15 max. 0.04 max. - Bal Cr25Ni21NbW 0.25 to 0.35 1.
12、50 max. 1.5 max. 23.0 to 27.0 20.5 to 22.0 - 0.50 to 2.00 1.00 to 2.00 0.10 max. 0.04 max. - Bal Cr26Ni26W2Nb 0.25 to 0.35 1.50 max. 1.5 max. 23.0 to 28.0 24.0 to 28.0 - 1.50 to 3.00 1.00 to 2.00 0.10 max. 0.04 max. - Bal Ni38Cr18SiNb 0.30 to 0.50 1.00 to 2.50 2.0 max. 18.0 to 21.0 36.0 to 39.0 0.50
13、 max. 0.60 max. 1.20 to 1.80 0.04 max. 0.04 max. - Bal Cr26Ni14Nb2 0.40 to 0.50 0.80 to 1.25 0.75 to 1.10 24.0 to 27.0 12.0 to 15.0 0.50 max. - 1.70 to 2.10 0.11 to 0.15 0.04 max. 0.08 to 0.40 Bal Cr25Ni20Si 0.30 to 0.50 1.00 to 2.50 2.0 max. 24.0 to 27.0 19.0 to 22.0 0.50 max. 0.60 max. 0.60 max. 0
14、.04 max. 0.04 max. - Bal Cr26Ni22W3Nb 0.35 to 0.45 2.00 max. 2.0 max. 23.0 to 28.0 20.5 to 23.0 - 1.50 to 4.00 0.50 to 2.00 0.10 max. 0.04 max. - Bal Note: max. = maximum 3.1.2 Mechanical Properties. Mandatory room temperature mechanical properties (at 23 5 C) associated with each grade via separate
15、ly cast and machined test samples are listed in Table 3. Additional mechanical property testing on the casting itself, excluding hardness testing, may be conducted by agreement between the purchaser and the supplier. Any mechanical property testing on the casting shall have the test locations noted
16、on the drawing and sampling plan agreed upon by the purchaser and the supplier. Table 3: Mandatory Mechanical Properties at Room Temperature (23 5 C) Grade Tensile Strength (MPa) Minimum Yield Strength (MPa) Minimum Elongation (%) Minimum Hardness HBW Note 1 Cr17Si 450 345 0.5 200 to 280 Cr20Ni10Nb
17、450 230 5 165 to 235 Cr25Ni21NbW 490 235 5 165 to 235 Cr26Ni26W2Nb 490 235 5 165 to 235 Ni38Cr18SiNb 420 220 4 160 to 230 Cr26Ni14Nb2 515 240 7 187 to 214 Cr25Ni20Si 450 220 8 170 to 240 Cr26Ni22W3Nb 490 235 2 165 to 235 Note 1: Hardness values use a 10 mm ball and a 3000 kg load. Reference ISO 6506
18、 for minimum thicknesses required when using this diameter and load. Copyright General Motors Company Provided by IHS under license with General Motors CompanyNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-GM WORLDWIDE ENGINEERING STANDARDS GMW3164 Copyright 2011
19、General Motors Company All Rights Reserved August 2011 Page 3 of 6 3.1.2.1 Hardness. Brinell hardness shall be taken in accordance with ISO 6506. The material hardness range, described in Table 3, is a mandatory requirement and is measured on the prepared smooth casting surface. Other hardness metho
20、ds, such as cast surface penetrators, can be used if these methods are validated against ISO 6506 and are agreed upon by supplier and customer. 3.1.2.2 Tensile Properties. Mandatory tensile properties shall be measured on specimens machined from separately cast samples. Thickness of the cast test sa
21、mple shall be similar to critical casting sections per ISO 6892. 3.1.2.2.1 The separately cast samples shall be poured into molds made from sand aggregate that is similar to the aggregate used in production molds. Samples shall cool in the mold until their surfaces are a completely gray color with n
22、o tint of red observable. The samples can then be removed from the mold and allowed to air cool. 3.1.2.2.2 Porosity, shrink or other discontinuities within a test piece represent an invalid test, thus the data must be discarded. The evaluation of such discontinuities shall be done at a magnification
23、 not exceeding 100x. 3.1.3 Physical Requirements. Reference values for physical properties are shown in Appendix A. These properties have been gathered from textbooks and are meant to be used for comparative purposes only. 3.1.4 Additional Requirements. 3.1.4.1 Casting Requirements. Castings shall c
24、onform to the dimensions and tolerances specified on the casting drawing. Harmful discontinuities, e.g., sand and slag inclusions, cold laps, scabs, porosity, etc., that may be detrimental to subsequent processing or to the service performance are not permitted. Casting surfaces shall be smooth and
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