FORD WSS-M11G37-A2-2004 DECORATIVE WOOD VENEER EUROPEAN BIRCH-BETULA PENDULA QUARTER CUT TO BE USED WITH FORD WSS-M99P1111-A 《径切割的欧洲白桦(BETULA PENDULA)木制饰面薄板 与标准FORD WSS-M99P1111.pdf

上传人:syndromehi216 文档编号:751189 上传时间:2019-01-14 格式:PDF 页数:2 大小:59.30KB
下载 相关 举报
FORD WSS-M11G37-A2-2004 DECORATIVE WOOD VENEER EUROPEAN BIRCH-BETULA PENDULA QUARTER CUT  TO BE USED WITH FORD WSS-M99P1111-A  《径切割的欧洲白桦(BETULA PENDULA)木制饰面薄板  与标准FORD WSS-M99P1111.pdf_第1页
第1页 / 共2页
FORD WSS-M11G37-A2-2004 DECORATIVE WOOD VENEER EUROPEAN BIRCH-BETULA PENDULA QUARTER CUT  TO BE USED WITH FORD WSS-M99P1111-A  《径切割的欧洲白桦(BETULA PENDULA)木制饰面薄板  与标准FORD WSS-M99P1111.pdf_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述

1、 ENGINEERING MATERIAL SPECIFICATIONDate Action Revisions 2004 11 03 Activated C. Bezant Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 1 of 2 DECORATIVE WOOD VENEER, EUROPEAN BIRCH- WSS-M11G37-A BETULA PENDULA, CROWN CUT DECORATIVE WOOD VENEER EUROPEAN BIRCH- WSS-

2、M11G37-A2 BETULA PENDULA, QUARTER CUT DECORATIVE WOOD VENEER EUROPEAN BIRCH- WSS-M11G37-A3 BETULA PENDULA, MASUR CUT 1. SCOPE These specifications define wood veneers for use as decorative product on interior wood veneer assemblies. A1 = Poplar European Birch, Betula Pendula, Crown Cut A2 = Poplar E

3、uropean Birch, Betula Pendula, Quarter Cut A3 = Poplar European Birch, Betula Pendula, Masur Cut 2. APPLICATION The specifications WSS-M11G37-A1/A2/A3 were released for materials used for wooden decorative automotive components. Application of lacquer and other products will need to be considered to

4、 provide a suitable finished product. 3. REQUIREMENTS Material specification requirements are to be used for initial qualification of materials. When in the fully assembled form the veneer assembly must perform to the Material specification requirements of WSS-M15P34-B1 or as specified on the engine

5、ering drawing. 3.1 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.2 MATERIAL PROPERTIES 3.2.1 Appearance Color, feature and grain to be as per Master samples 3.2.2 Th

6、ickness Nominal thickness - 0.6mm ENGINEERING MATERIAL SPECIFICATIONWSS-M11G37-A/A3Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 2 of 2 3.2.3 Moisture content 11 - 18% 3.2.4 Density A1/A2/A3 596.6 +/- 50 Kgm-33.3 PERFORMANCE PROPERTIES Veneer selected for its attractive appearance should be uniform in thickness, smooth, flat, free from decay and have face grain suitable for the intended face grade.

展开阅读全文
相关资源
猜你喜欢
  • DIN 65110-1984 Aerospace bihexagonal heads for screws and bolts《航空和航天 螺钉和螺栓的十二角头》.pdf DIN 65110-1984 Aerospace bihexagonal heads for screws and bolts《航空和航天 螺钉和螺栓的十二角头》.pdf
  • DIN 65112-1985 Aerospace threaded inserts locked and screw locking technical specification《航空和航天 锁紧和螺纹锁紧的螺纹衬套 技术规范》.pdf DIN 65112-1985 Aerospace threaded inserts locked and screw locking technical specification《航空和航天 锁紧和螺纹锁紧的螺纹衬套 技术规范》.pdf
  • DIN 65113-1990 Aerospace bars and extruded profiles of aluminium and wrought aluminium alloys technical specification inactive for new design《航空航天;铝和铝塑性合金棒和压制型材 技术规范 不适于新结构》.pdf DIN 65113-1990 Aerospace bars and extruded profiles of aluminium and wrought aluminium alloys technical specification inactive for new design《航空航天;铝和铝塑性合金棒和压制型材 技术规范 不适于新结构》.pdf
  • DIN 65115-1986 Aerospace hexagon bolts with waisted shank and MJ thread steel nominal tensile strength 1100 MPa for temperatures up to 235 C《航空和航天 带MJ螺纹、缩颈、标称抗拉强度1100MPa、温度235 ℃以下 .pdf DIN 65115-1986 Aerospace hexagon bolts with waisted shank and MJ thread steel nominal tensile strength 1100 MPa for temperatures up to 235 C《航空和航天 带MJ螺纹、缩颈、标称抗拉强度1100MPa、温度235 ℃以下 .pdf
  • DIN 65116-1980 Aerospace boron fibre reinforced mouldings preparation of test laminates《航空和航天 硼纤维增强的模塑材料 层压试件的制备》.pdf DIN 65116-1980 Aerospace boron fibre reinforced mouldings preparation of test laminates《航空和航天 硼纤维增强的模塑材料 层压试件的制备》.pdf
  • DIN 65117-1980 Aerospace preimpregnated unidirectional boron fibres (BFK-prepreg) dimensions masses《航空和航天 预浸渍单向硼纤维层(BFK-浸渍体),尺寸、质量》.pdf DIN 65117-1980 Aerospace preimpregnated unidirectional boron fibres (BFK-prepreg) dimensions masses《航空和航天 预浸渍单向硼纤维层(BFK-浸渍体),尺寸、质量》.pdf
  • DIN 65118-2010 Welding in aerospace - Welded metallic components - Indications in design documents and general design requirements《航空航天中的焊接 焊接金属组件 设计文件和一般设计要求中的标识》.pdf DIN 65118-2010 Welding in aerospace - Welded metallic components - Indications in design documents and general design requirements《航空航天中的焊接 焊接金属组件 设计文件和一般设计要求中的标识》.pdf
  • DIN 65121-1992 Aerospace bolts screws nuts and associated parts survey and selection for workshop inactive for new design《航空航天 螺栓、螺钉、螺母和有关零件 供车间查看的产品一览表和选用 不适用于新设计》.pdf DIN 65121-1992 Aerospace bolts screws nuts and associated parts survey and selection for workshop inactive for new design《航空航天 螺栓、螺钉、螺母和有关零件 供车间查看的产品一览表和选用 不适用于新设计》.pdf
  • DIN 65122-2017 Aerospace series - Powder for additive manufacturing with powder bed process - Technical delivery specification《航空航天系列 粉床加工的添加剂制造用粉末 交货技术规格》.pdf DIN 65122-2017 Aerospace series - Powder for additive manufacturing with powder bed process - Technical delivery specification《航空航天系列 粉床加工的添加剂制造用粉末 交货技术规格》.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