FORD WSS-M3H83-A2-2015 CARPET MOLDABLE FLATNEEDLED POLYESTER FACE 340 g m2 BACKED WITH RECLAIMED SYNTHETIC FIBER TO BE USED WITH FORD WSS-M99P1111-A .pdf

上传人:arrownail386 文档编号:753389 上传时间:2019-01-14 格式:PDF 页数:3 大小:33.28KB
下载 相关 举报
FORD WSS-M3H83-A2-2015 CARPET MOLDABLE FLATNEEDLED POLYESTER FACE 340 g m2 BACKED WITH RECLAIMED SYNTHETIC FIBER  TO BE USED WITH FORD WSS-M99P1111-A  .pdf_第1页
第1页 / 共3页
FORD WSS-M3H83-A2-2015 CARPET MOLDABLE FLATNEEDLED POLYESTER FACE 340 g m2 BACKED WITH RECLAIMED SYNTHETIC FIBER  TO BE USED WITH FORD WSS-M99P1111-A  .pdf_第2页
第2页 / 共3页
FORD WSS-M3H83-A2-2015 CARPET MOLDABLE FLATNEEDLED POLYESTER FACE 340 g m2 BACKED WITH RECLAIMED SYNTHETIC FIBER  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 Material Name Specification Number Date Action Revisions Rev 01 2015 07 02 N Status No replacement or future use. L. Sinclair, NA 2002 08 30 Revised L. Soreide Page 1 of 3 Copyright 2015, Ford Global Technologies, Inc. CARPET, MOLDABLE, FLATNEEDLED POLYESTER FACE,

2、 WSS-M3H83-A2 340 g/m2, BACKED WITH RECLAIMED SYNTHETIC FIBER NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by this specification is a scrimless integrated mat consisting of a base reclaimed synthetic fiber pad with a flat needled polyester fiber face, uniformly needled together to for

3、m a composite product. 2. APPLICATION This specification was released originally for material used as molded convertible sides for the S197. 3. REQUIREMENTS In addition to the requirements listed herein, the end-item carpet assembly (molded or otherwise fabricated), shall meet all the applicable req

4、uirements of WSS-M15P32-C TRIM ASSEMBLY, ENCLOSED LUGGAGE COMPARTMENT COVERING PERFORMANCE SPECIFICATION, with 600 cycles as the required number of cycles for paragraph 3.9.1 and excluding paragraph 3.8.2 unless otherwise specified on the Engineering Document. 3.1 STANDARD REQUIREMENTS FOR PRODUCTIO

5、N MATERIALS Material suppliers and part producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.2 SAMPLE SELECTION All evaluations shall be conducted of test specimens taken from production representative molded carpet assemblies. Test specimens for

6、strength properties shall be taken from molded or stressed areas of the carpet assembly. 3.3 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 Formation of clear film, droplets or crystals is cause for rejection. ENGINEERING MATERIA

7、L SPECIFICATION WSS-M3H83-A2 Page 2 of 3 Copyright 2015, Ford Global Technologies, Inc. 3.4 APPEARANCE (FLTM BN 109-01) The color, pattern and finish shall match the approved Design Center master sample, or shall be as specified on the engineering drawing. 3.5 COMPOSITION (ASTM D 276) Face Fiber 100

8、 Polyester Base Pad 50% polypropylene fibers and 50% acrylic fibers or other synthetics 3.6 DYE METHOD Solution dyed or equivalent 3.7 CONSTRUCTION 3.7.1 Fiber Size & Description 6- 18 dtex (ASTM D 1244) 50.6 101.2mm 3.7.2 Thickness, min As specified on engineering drawing. (ASTM D 418) *Prior to m

9、olding 3.7.3 Needle Gage, min 3.5 rows/cm 3.8 WEIGHT, Min, g/m2 (ASTM D 418) Face Fiber 340 Base Pad As specified on the engineering drawing. 3.9 PHYSICAL PROPERTIES (roll goods) 3.9.1 Breaking Strength, N, min, (ASTM D 1682, Grab Method) MD and AMD 650 3.9.2 Heat Shrinkage, max 3.0% (FLTM BN 105-01

10、) ENGINEERING MATERIAL SPECIFICATION WSS-M3H83-A2 Page 3 of 3 Copyright 2015, Ford Global Technologies, Inc. 3.9.3 Trapezoidal Tear, N, min, (FLTM BN 122-01) MD 135 AMD 180 3.9.4 Adhesion of Surface Fiber to Base Pad, min (ASTM D 413, Machine Method, Strip Specimens Type A, sample size 150 X 50 mm,

11、average of 4 samples in each direction, jaw speed 305 mm/minute) The pull necessary to separate the carpet and the pad, or the internal strength of the pad shall be as follows: Original 13 N Cycled (FLTM BN 113-01) 13 N Cycled samples shall be exposed to alternating humidity, cold and heat aging cycles per FLTM BN 113-01. Upon completion of the cycle aging, samples shall be conditioned for one hour at the standard laboratory conditions specified in paragraph 3.3 prior to testing. 3.10 FLAMMABILITY (ISO 3795/SAE J369) Burn Rate, max 100 mm/minute

展开阅读全文
相关资源
猜你喜欢
  • EN 2155-14-1993 en Aerospace Series - Test Methods for Transparent Materials for Aircraft Glazing - Part 14 Determination of the 1 10 Vicat Softening Temperature《航空航天系列 飞行器上门窗玻璃用透明.pdf EN 2155-14-1993 en Aerospace Series - Test Methods for Transparent Materials for Aircraft Glazing - Part 14 Determination of the 1 10 Vicat Softening Temperature《航空航天系列 飞行器上门窗玻璃用透明.pdf
  • EN 2155-2-1993 en Aerospace Series Test Methods for Transparent Materials for Aircraft Glazing Part 2 Determination of Water Absorption《航空航天系列 飞机窗透明料试验方法 第2部分 吸水性的测定》.pdf EN 2155-2-1993 en Aerospace Series Test Methods for Transparent Materials for Aircraft Glazing Part 2 Determination of Water Absorption《航空航天系列 飞机窗透明料试验方法 第2部分 吸水性的测定》.pdf
  • EN 2155-21-1989 en Aerospace series Test Methods for Transparent Materials for Aircraft Glazing Part 21 Determination of Resistance to Crack Propagation (K Factor)《航空航天系列 飞机窗透明料试验方.pdf EN 2155-21-1989 en Aerospace series Test Methods for Transparent Materials for Aircraft Glazing Part 21 Determination of Resistance to Crack Propagation (K Factor)《航空航天系列 飞机窗透明料试验方.pdf
  • EN 2155-3-1993 en Aerospace Series Test Methods for Transparent Materials for Aircraft Glazing Part 3  Determination of Refractive Index《航空航天系列 航空器上釉透明材料的试验方法 第3部分 折射系数的测定》.pdf EN 2155-3-1993 en Aerospace Series Test Methods for Transparent Materials for Aircraft Glazing Part 3 Determination of Refractive Index《航空航天系列 航空器上釉透明材料的试验方法 第3部分 折射系数的测定》.pdf
  • EN 2155-5-1989 en Test Methods for Transparent Materials for Aircraft Glazing Part 5 Determination of Visible Light Transmission《航空航天系列 飞行器玻璃窗透明材料试验方法 第5部分 可见光透射测定》.pdf EN 2155-5-1989 en Test Methods for Transparent Materials for Aircraft Glazing Part 5 Determination of Visible Light Transmission《航空航天系列 飞行器玻璃窗透明材料试验方法 第5部分 可见光透射测定》.pdf
  • EN 2155-7-1997 en Aerospace Series - Test Methods for Transparent Materials for Aircraft Glazing - Part 7 Determination of Optical Deviation《航空航天系列 飞机门窗玻璃用透明材料的试验方法 第7部分 光偏移的测定》.pdf EN 2155-7-1997 en Aerospace Series - Test Methods for Transparent Materials for Aircraft Glazing - Part 7 Determination of Optical Deviation《航空航天系列 飞机门窗玻璃用透明材料的试验方法 第7部分 光偏移的测定》.pdf
  • EN 2155-8-1989 en Test Method for Transparent Materials for Aircraft Glazing Part 8 Determination of Optical Distortion《航空航天系列 飞行器玻璃窗透明材料试验方法 第8部分 光学畸变测定》.pdf EN 2155-8-1989 en Test Method for Transparent Materials for Aircraft Glazing Part 8 Determination of Optical Distortion《航空航天系列 飞行器玻璃窗透明材料试验方法 第8部分 光学畸变测定》.pdf
  • EN 2155-9-1989 en Test Methods for Transparent Materials for Aircraft Glazing Part 9 Determination of Haze《航空航天系列 飞行器玻璃窗透明材料试验方法 第9部分 薄雾测定》.pdf EN 2155-9-1989 en Test Methods for Transparent Materials for Aircraft Glazing Part 9 Determination of Haze《航空航天系列 飞行器玻璃窗透明材料试验方法 第9部分 薄雾测定》.pdf
  • EN 2157-1-1993 en Aerospace Series Steel Forging Stock and Forgings Technical Specifications Part 1 - General Requirements《航空航天系列 钢 锻坯和锻件的技术规范 第1部分 一般要求》.pdf EN 2157-1-1993 en Aerospace Series Steel Forging Stock and Forgings Technical Specifications Part 1 - General Requirements《航空航天系列 钢 锻坯和锻件的技术规范 第1部分 一般要求》.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