FORD WSS-M4D981-A-2013 THERMOPLASTIC ELASTOMERIC MOLDING COMPOUND FOR PAINTED AIRBAG COVERS TO BE USED WITH FORD WSS-M99P1111-A .pdf

上传人:jobexamine331 文档编号:753752 上传时间:2019-01-14 格式:PDF 页数:3 大小:49.45KB
下载 相关 举报
FORD WSS-M4D981-A-2013 THERMOPLASTIC ELASTOMERIC MOLDING COMPOUND FOR PAINTED AIRBAG COVERS  TO BE USED WITH FORD WSS-M99P1111-A  .pdf_第1页
第1页 / 共3页
FORD WSS-M4D981-A-2013 THERMOPLASTIC ELASTOMERIC MOLDING COMPOUND FOR PAINTED AIRBAG COVERS  TO BE USED WITH FORD WSS-M99P1111-A  .pdf_第2页
第2页 / 共3页
FORD WSS-M4D981-A-2013 THERMOPLASTIC ELASTOMERIC MOLDING COMPOUND FOR PAINTED AIRBAG COVERS  TO BE USED WITH FORD WSS-M99P1111-A  .pdf_第3页
第3页 / 共3页
亲,该文档总共3页,全部预览完了,如果喜欢就下载吧!
资源描述

1、 ENGINEERING MATERIAL SPECIFICATION Date Action Revisions 2013 04 26 N Status Replaced by WSS-M4D981-B1 T. Nover, EU 2006 07 21 Revised Inserted 3.0; Deleted 3.1, 3.2, 3.3, 3.7, 3.8 & 4 2001 11 27 Activated L. Hess L. Soreide Controlled document at www.MATS Copyright 2013, Ford Global Technologies,

2、LLC Page 1 of 3 THERMOPLASTIC ELASTOMERIC MOLDING COMPOUND, WSS-M4D981-A FOR PAINTED AIRBAG COVERS WSS-M4D981-A2 NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by these specifications is a thermoplastic polyolefinic elastomer. 2. APPLICATION These specifications were released originally

3、 to be used as a painted airbag cover. The first surface must be painted with a ultraviolet and heat resistant paint (WSS-M15J13-A). Parts produced from materials of the specification must also meet the appropriate passenger and driver side airbag System Design Specification (SDS). 3. REQUIREMENTS M

4、aterial specification requirements are to be used for initial qualification of materials. 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). 3.1.1 All requirements of t

5、his specification, identified by symbol (s), shall be met with data representing 3 sigma values. 3.4 MOLDED TEST SPECIMEN 3.4.1 Preparation of Test Specimens Unless otherwise specified all tests shall be carried out on injection molded one-end gated test specimens. The following dimensions are requi

6、red: A. 150 min x 10 x 4.0 +/- 0.2 mm (Tensile Bar, ISO 3167) B. 120 x 10 x 4.0 +/- 0.2 mm Specimens with shorter dimensions shall be cut from the center portion of the test specimen A and/or B. The specimens shall be prepared according to ISO 294. No annealing allowed. A A2 (s) 3.4.2 Density, g/cm3

7、 0.87 - 0.90 0.87-0.89 (ISO 1183, Method A) ENGINEERING MATERIAL SPECIFICATION WSS-M4D981-A/A2 Copyright 2013, Ford Global Technologies, LLC Page 2 of 3 A A2 (s) 3.4.3 Hardness, Durometer D 35 48 (ISO 868, 10 s dwell, +/- 5) (s) 3.4.4 Tensile Strength at Max Load, min, MPA 8.5 11 (ISO R 527, 150 min

8、 x 10 x 4.0 +/- 0.2 mm specimen, 50 mm/minute test speed) (s) 3.4.4.1 Elongation at Break, min, % 440 440 (Test Method according to para 3.4.4) (s) 3.4.5 Flexural Modulus, min, MPa 170 260 (ISO 178, 80 x 10 x 4.0 +/- 0.2 mm specimen, 2 mm/minute test speed, 64 mm support span) (s) 3.4.6 Heat Aging P

9、erformance (ISO 188, except 120 +/- 50 air changes/h, 1000 h at 110 +/- 2 C. Unaged property values shall be determined at the time of the aged properties determination) 3.4.6.1 Tensile Strength at Change, % +/- 25 +/- 25 (Test Method per para 3.4.4) 3.4.6.2 Elongation at Break,Change, % +/- 25 +/-

10、25 (Test Method per para 3.4.4) 3.5 FOGGING (SAE J1756, 3 h at 100 C heating, 21 C cooling plate, post test conditioning 1 h and 16 h) Fog Number, min 70 70 Formation of clear film, droplets or crystals is cause for rejection. 3.6 FLAMMABILITY (ISO 3795) Burn Rate, max, mm/min 100 100 The specimen s

11、ize required for material approval is 355 x 100 x 0.8 +/- 0.1 mm with a smooth surface. ENGINEERING MATERIAL SPECIFICATION WSS-M4D981-A/A2 Copyright 2013, Ford Global Technologies, LLC Page 3 of 3 5. GENERAL INFORMATION The information given below is provided for clarification and assistance in meet

12、ing the requirements of these specifications. 5.1 COEFFICIENT OF LINEAR THERMAL EXPANSION (ISO 11359-2(TMA), -30 to 100 C) A A2 Parallel to Flow 4.6-05 5.0-05 Across Flow 4.9-05 4.9-05 5.2 MOLD SHRINKAGE, % (ISO 2577, approximately 150 x 100 x 3.2 +/- 0.2 mm injection molded specimen) 5.2.1 Molding

13、Shrinkage . After 48 h at 23 +/- 2 C 0.5/0.6 0.6/1.0 5.2.2 Post Shrinkage (Separate specimens required for each test) . After 30 min. at 80 C 0.6/0.7 0.7/1.1 . After 60 minutes at 120 C 0.7/0.8 0.8/1.2 5.3 MULTI AXIAL IMPACT AT MAX LOAD, ave (ASTM D 3763, 100 x 100 x 2.5 +/- 0.2 mm edge gated inject

14、ion molded specimens) Test velocity at initial contact with the test specimen shall be 6.7 m/s and must not change by more that 10% during the impact event. Load energy and velocity are to be recorded as a function of displacement. 5.3.1 At 23 C 26 J 27 J 5.3.2 At -40 C 24 J 28 J 5.4 RECYCLING CODE TEO

展开阅读全文
相关资源
猜你喜欢
  • EN 2584-2001 en Aerospace Series - Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner - Narrow Series - Elevated Load at Ambient Temperature - Dimens.pdf EN 2584-2001 en Aerospace Series - Bearings Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner - Narrow Series - Elevated Load at Ambient Temperature - Dimens.pdf
  • EN 2585-2001 en Aerospace series - Bearings spherical plain in corrosion resisting steel with self-lubricating liner - Wide series - Elevated load at ambient temperature - Dimensio.pdf EN 2585-2001 en Aerospace series - Bearings spherical plain in corrosion resisting steel with self-lubricating liner - Wide series - Elevated load at ambient temperature - Dimensio.pdf
  • EN 2586-1991 en Washers Lock for Flight Control Rods - Dimensions《航空航天系列 飞行驾驶杆用锁紧垫片尺寸》.pdf EN 2586-1991 en Washers Lock for Flight Control Rods - Dimensions《航空航天系列 飞行驾驶杆用锁紧垫片尺寸》.pdf
  • EN 2587-1990 en Rod Ends Adjustable Double Fork and Threaded Shank Dimensions and Loads《航空航天系列 两端均为叉端、杆部有螺纹的可调整的操纵杆 尺寸和负荷》.pdf EN 2587-1990 en Rod Ends Adjustable Double Fork and Threaded Shank Dimensions and Loads《航空航天系列 两端均为叉端、杆部有螺纹的可调整的操纵杆 尺寸和负荷》.pdf
  • EN 2588-2006 en Aerospace series - Bearings Spherical Plain in Corrosion Resisting Steel with Assembly Slots - Dimensions and Loads《航空航天系列 带装配槽的耐蚀钢普通球面轴承 尺寸和负荷》.pdf EN 2588-2006 en Aerospace series - Bearings Spherical Plain in Corrosion Resisting Steel with Assembly Slots - Dimensions and Loads《航空航天系列 带装配槽的耐蚀钢普通球面轴承 尺寸和负荷》.pdf
  • EN 2589-2017 en Aerospace series - Steel - Sheet and strip cold rolled - Thickness 0 1 mm less than or equal to a less than or equal to 3 mm - Dimensions《航空航天系列-钢片和带冷轧厚度0 1mm小于或等于a.pdf EN 2589-2017 en Aerospace series - Steel - Sheet and strip cold rolled - Thickness 0 1 mm less than or equal to a less than or equal to 3 mm - Dimensions《航空航天系列-钢片和带冷轧厚度0 1mm小于或等于a.pdf
  • EN 259-1-2001 en Wallcoverings in Roll Form - Heavy Duty Wallcoverings - Part 1 Specifications《卷式墙面饰层 重负载墙面饰层 第1部分 规范》.pdf EN 259-1-2001 en Wallcoverings in Roll Form - Heavy Duty Wallcoverings - Part 1 Specifications《卷式墙面饰层 重负载墙面饰层 第1部分 规范》.pdf
  • EN 259-2-2001 en Wallcoverings in Roll Form - Heavy Duty Wallcoverings - Part 2 Determination of Impact Resistance《卷式墙面饰层 重负载墙面饰层 第2部分 耐冲击性测定》.pdf EN 259-2-2001 en Wallcoverings in Roll Form - Heavy Duty Wallcoverings - Part 2 Determination of Impact Resistance《卷式墙面饰层 重负载墙面饰层 第2部分 耐冲击性测定》.pdf
  • EN 2590-2017 en Aerospace series - Steel - Sheets and plates hot rolled - Dimensions《航空航天系列-钢片和带热轧-尺寸》.pdf EN 2590-2017 en Aerospace series - Steel - Sheets and plates hot rolled - Dimensions《航空航天系列-钢片和带热轧-尺寸》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1