FORD WSB-M7H54-A-1994 TAPE FASTENER NYLON LOOP KNITTED UNNAPPED《不起绒针织尼龙圈式紧固件用胶带》.pdf

上传人:bonesoil321 文档编号:749240 上传时间:2019-01-14 格式:PDF 页数:4 大小:14.69KB
下载 相关 举报
FORD WSB-M7H54-A-1994 TAPE FASTENER NYLON LOOP KNITTED UNNAPPED《不起绒针织尼龙圈式紧固件用胶带》.pdf_第1页
第1页 / 共4页
FORD WSB-M7H54-A-1994 TAPE FASTENER NYLON LOOP KNITTED UNNAPPED《不起绒针织尼龙圈式紧固件用胶带》.pdf_第2页
第2页 / 共4页
FORD WSB-M7H54-A-1994 TAPE FASTENER NYLON LOOP KNITTED UNNAPPED《不起绒针织尼龙圈式紧固件用胶带》.pdf_第3页
第3页 / 共4页
FORD WSB-M7H54-A-1994 TAPE FASTENER NYLON LOOP KNITTED UNNAPPED《不起绒针织尼龙圈式紧固件用胶带》.pdf_第4页
第4页 / 共4页
亲,该文档总共4页,全部预览完了,如果喜欢就下载吧!
资源描述

1、 ENGINEERING MATERIAL SPECIFICATIONMaterial Name Specification NumberDate Release No. Released1994 07 16 NB00I10043054340 Released D.Henrickson AJS BCFWP 3948-a Page 1 of 4 TAPE, FASTENER, NYLON LOOP, KNITTED, UNNAPPED WSB-M7H54-A1. SCOPEThe ma terial defined by this specification is an unnapped, kn

2、itted, nylonloop tape fastener with polyester backing.2. APPLICATIONThis specification was released originally for material sewn to seam jointson the interior of seat trim covers. This loop fastener joins togetherwith a hook fastener secured to the foam seat cushion pad.3. REQUIREMENTS3.1 STATISTICA

3、L PROCESSSupplie rs must conform to the requirements of Ford Quality SystemStand ard Q-101. A mutually acceptable Control Plan as describedtherein is required for material/source approval. Appropriatestatist ical tools must be used to analyze process/product data sothat variation in the final produc

4、t is continuously reduced.3.2 INFRARED SPECTROPHOTOMETRY AND/OR THERMAL ANALYSISFord Motor Company, at its option, may conduct infrared and/ortherma l analysis of material/parts supplied to this specification.The IR spectra and thermograms established for i nitial approval shallconst itute the refer

5、ence standard and shall be kept on file at thedesignated material laboratory. All samples sha ll produce IR spectraand thermograms that correspond to the reference standard when testedunder the same conditions.3.3 CONDITIONING AND TEST CONDITIONSAll test values indicated herein are based on ma teria

6、l conditioned ina control led atmosphere of 23 +/- 2 C and 50 +/- 5 % relativehumidity for not less than 24 h prior to testing and tested under thesame conditions unless otherwise specified.ENGINEERING MATERIAL SPECIFICATIONWSB-M7H54-AWP 3948-b Page 2 of 4 3.4 CONSTRUCTION AND YARN DESCRIPTION(ASTM

7、D 3887 and ASTM D 1244)The loop tape is knit with uncut upright loops w hich provide a matingengagement for the hook tape.3.4.1 Loop 22 tex Nylon 65 rows/cm3.4.2 BackingWarp 33 tex Texturizedpolyester13 picks/cmFill 33 tex Texturizedpolyester6 rows/cm3.5 BREAKING STRENGTH, warp only, min 10 N/mm wid

8、th(ASTM D 5034, 305 mm/minutejaw speed, avg. of 5 samples)Test samples for paragraphs 3.6, 3.7, and 3.8 ar e prepared by joining25 mm w ide strips of material and ESB-M7H4-A1 or equivalent hookfastener as noted.3.6 SHEAR STRENGTH, min 45 kPa(ASTM D 5034, with 50 mm hookto loop overlay, 305 mm/minute

9、 jawspeed, avg. of 5 samples)3.7 PEEL STRENGTH, min 150 N/m width(ASTM D 413, Machine method, jawspeed 305 mm/minute, avg. of 5samples)3.8 TENSION STRENGTH, min 35 kPa(Avg. of 5 samples)Test Method: Staple 25 x 75 mm pieces of materi al and ESB-M7H4-A1 oreq uivalent hook material to flat foundation

10、boards. Mate these 2pieces together with a 36 N roller so that a 25 x 25 mm area of thehook and loop is in contact with one another. S eparate these samplesin a tensile testing machine with a jaw speed of 305 mm/minute, andthe direction of load perpendicular to the plane of the samples.3.9 SHRINKAGE

11、, warp, max 3.0 %(FLTM BN 105-01)ENGINEERING MATERIAL SPECIFICATIONWSB-M7H54-AWP 3948-b Page 3 of 4 3.10 FOGGING(FLTM BO 116-03)Fog Number, min 60Formati on of a clear film, droplets or crystals is cause forrejection.3.11 FUNCTIONAL APPROVALMaterials being evaluated for approval to this s pecificati

12、on shall besubject ed to a production trial. Functional trial results must beapproved by the affected assembly operation and Design Engineering.Results shall be made available to the responsible MaterialsEngineering Activity prior to material approval and release.3.12 ADDITIONAL REQUIREMENTSSpecific

13、 requirements for material and/or manufa ctured parts shall bespecified on the Engineering drawing, Engineerin g parts specificationand/or performance specifications. All critical areas with respectto these properties shall be clearly designated on the engineeringdrawing.3.13 SUPPLIERS RESPONSIBILIT

14、YAll materials supplied to this specification must be equivalent inal l characteristics to the material upon which approval wasoriginally granted.Pri or to making any change in the properties, composition,constr uction, color, processing or labeling of the materialorig inally approved under this spe

15、cification, whether or not suchchange s affect the materials ability to meet the specificationrequir ements, the Supplier shall notify Purchasing, Toxicology andthe affected Materials Engineering activity of the proposed changesand obtain the written approval of the Materials Engineeringactivity. Te

16、st data, t est samples and a new code identification areto be submitted with the request.Substance restrictions imposed by law, regulations or Ford, apply tothe materials addressed by this document. The restrictions aredefined in Engineering Material Specification WSS-M99P9999-A1.ENGINEERING MATERIA

17、L SPECIFICATIONWSB-M7H54-AWP 3948-b Page 4 of 4 4. APPROVAL OF MATERIALSMat erials defined by this specification must have prior approval by theresp onsible Materials Engineering activity. Suppliers desiring approvalof thei r materials shall first obtain an expression of interest from theaffec ted P

18、urchasing, Design and Materials Engineering activity. Uponrequest, the Supplier shall submit to the affected Materials Engineeringactivity a completed copy of their laboratory test reports, signed by aqualified and authorized representative of the test faci lity, demonstratingful l compliance with a

19、ll the requirements of this specification (testresults, not nominal values), the material designation a nd code number, andtes t specimens for Ford evaluation. Fords engineering approval of amateri al will be based on its performance to this specification and on anassessment of suitability for i ntended processes and/or applications. Uponapprov al, the material will be added to the Engineering Material ApprovedSource List.

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 3521-1998 Aerospace Series Steel FE-PL2106 (30CrNiMo8) Air Melted Hardened and Tempered Bar for Machining De Less Than or Equal to 150 mm 900 MPa Less Than or Equal to R.pdf AECMA PREN 3521-1998 Aerospace Series Steel FE-PL2106 (30CrNiMo8) Air Melted Hardened and Tempered Bar for Machining De Less Than or Equal to 150 mm 900 MPa Less Than or Equal to R.pdf
  • AECMA PREN 3522-1988 Aerospace Series Steel FE-PL79 Softened Reference Heat Treatment Carburized Hardened and Tempered Forging Stock De Less Than or Equal to 200 mm Issue P 1《航空航天系.pdf AECMA PREN 3522-1988 Aerospace Series Steel FE-PL79 Softened Reference Heat Treatment Carburized Hardened and Tempered Forging Stock De Less Than or Equal to 200 mm Issue P 1《航空航天系.pdf
  • AECMA PREN 3523-1999 Aerospace Series Steel FE-PL1505 (15CrMoV6) Air Melted Hardened and Tempered Bar for Machining De Less Than or Equal to 100 mm 1 080 MPa Less Than or Equal to .pdf AECMA PREN 3523-1999 Aerospace Series Steel FE-PL1505 (15CrMoV6) Air Melted Hardened and Tempered Bar for Machining De Less Than or Equal to 100 mm 1 080 MPa Less Than or Equal to .pdf
  • AECMA PREN 3524-1999 Aerospace Series Steel FE-PL1505 (15CrMoV6) Air Melted Hardened and Tempered Sheet and Strip 2 mm Less Than or Equal to a Less Than or Equal to 6 mm 1 080 MPa .pdf AECMA PREN 3524-1999 Aerospace Series Steel FE-PL1505 (15CrMoV6) Air Melted Hardened and Tempered Sheet and Strip 2 mm Less Than or Equal to a Less Than or Equal to 6 mm 1 080 MPa .pdf
  • AECMA PREN 3525-1999 Aerospace Series Steel FE-PL1505 (15CrMoV6) Air Melted Hardened and Tempered Plate 6 mm Less Than or Equal to a Less Than or Equal to 20 mm 1 080 MPa Less Than航.pdf AECMA PREN 3525-1999 Aerospace Series Steel FE-PL1505 (15CrMoV6) Air Melted Hardened and Tempered Plate 6 mm Less Than or Equal to a Less Than or Equal to 20 mm 1 080 MPa Less Than航.pdf
  • AECMA PREN 3526-1999 Aerospace Series Steel FE-PL1505 (15CrMoV6) Air Melted Hardened and Tempered Sheet and Strip 0 5 mm Less Than or Equal to a Less Than or Equal to 6 mm 980 MPa t.pdf AECMA PREN 3526-1999 Aerospace Series Steel FE-PL1505 (15CrMoV6) Air Melted Hardened and Tempered Sheet and Strip 0 5 mm Less Than or Equal to a Less Than or Equal to 6 mm 980 MPa t.pdf
  • AECMA PREN 3527-1998 Aerospace Series Steel FE-PL1504 (33CrMoV12) Air Melted Softened Forging Stock a or D Less Than or Equal to 300 mm Edition P2《航空航天系列.钢 FE-PL1504(33CrMoV12) 空气熔.pdf AECMA PREN 3527-1998 Aerospace Series Steel FE-PL1504 (33CrMoV12) Air Melted Softened Forging Stock a or D Less Than or Equal to 300 mm Edition P2《航空航天系列.钢 FE-PL1504(33CrMoV12) 空气熔.pdf
  • AECMA PREN 3528-1988 Aerospace Series Steel FE-PA95 Solution Treated and Precipitation Treatment 1750 Less Than or Equal to Rm Less Than or Equal to 2000 MPa Bar for Machining De L.pdf AECMA PREN 3528-1988 Aerospace Series Steel FE-PA95 Solution Treated and Precipitation Treatment 1750 Less Than or Equal to Rm Less Than or Equal to 2000 MPa Bar for Machining De L.pdf
  • AECMA PREN 3529-1999 Aerospace Series Steel FE-PM2701 (X2NiCoMo18-8-5) Vacuum Induction Melted and Vacuum Arc Remelted Solution Treated and Precipitation Treated Forgings a or D Ler.pdf AECMA PREN 3529-1999 Aerospace Series Steel FE-PM2701 (X2NiCoMo18-8-5) Vacuum Induction Melted and Vacuum Arc Remelted Solution Treated and Precipitation Treated Forgings a or D Ler.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