FORD WSF-M4D628-A-2011 POLYAMIDE (PA) 66 MOLDING COMPOUND 25 % GLASS FIBER REINFORCED FLAME RETARDED TO BE USED WITH FORD WSS-M99P1111-A 《25%玻璃纤维增强阻燃聚酰胺(PA)66模塑材料 与福特WSS-M99P111.pdf

上传人:ideacase155 文档编号:750203 上传时间:2019-01-14 格式:PDF 页数:5 大小:39.71KB
下载 相关 举报
FORD WSF-M4D628-A-2011 POLYAMIDE (PA) 66 MOLDING COMPOUND 25 % GLASS FIBER REINFORCED FLAME RETARDED  TO BE USED WITH FORD WSS-M99P1111-A  《25%玻璃纤维增强阻燃聚酰胺(PA)66模塑材料  与福特WSS-M99P111.pdf_第1页
第1页 / 共5页
FORD WSF-M4D628-A-2011 POLYAMIDE (PA) 66 MOLDING COMPOUND 25 % GLASS FIBER REINFORCED FLAME RETARDED  TO BE USED WITH FORD WSS-M99P1111-A  《25%玻璃纤维增强阻燃聚酰胺(PA)66模塑材料  与福特WSS-M99P111.pdf_第2页
第2页 / 共5页
FORD WSF-M4D628-A-2011 POLYAMIDE (PA) 66 MOLDING COMPOUND 25 % GLASS FIBER REINFORCED FLAME RETARDED  TO BE USED WITH FORD WSS-M99P1111-A  《25%玻璃纤维增强阻燃聚酰胺(PA)66模塑材料  与福特WSS-M99P111.pdf_第3页
第3页 / 共5页
FORD WSF-M4D628-A-2011 POLYAMIDE (PA) 66 MOLDING COMPOUND 25 % GLASS FIBER REINFORCED FLAME RETARDED  TO BE USED WITH FORD WSS-M99P1111-A  《25%玻璃纤维增强阻燃聚酰胺(PA)66模塑材料  与福特WSS-M99P111.pdf_第4页
第4页 / 共5页
FORD WSF-M4D628-A-2011 POLYAMIDE (PA) 66 MOLDING COMPOUND 25 % GLASS FIBER REINFORCED FLAME RETARDED  TO BE USED WITH FORD WSS-M99P1111-A  《25%玻璃纤维增强阻燃聚酰胺(PA)66模塑材料  与福特WSS-M99P111.pdf_第5页
第5页 / 共5页
亲,该文档总共5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 File Control No. Specification Number Date Release No. Release/Revision 2011 10 12 N Status Replaced by WSS-M4D1016-A1 G. Kowalski, NA 1989 08 22 OE00E00107002031 Released WP 3948-a Page 1 of 5 POLYAMIDE (PA) 66 MOLDING COMPOUND, 25 % WSF-M4D628-A GL

2、ASS FIBER REINFORCED, FLAME RETARDED NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by this specification is a type 66 polyamide (nylon) molding compound containing flame retardant and reinforced with 25 % glass fibers. 2. APPLICATION This specification was released originally for mater

3、ial used for ISO relays. NOTICE: This material absorbs and retains moisture. Part design and tolerances must accommodate changes in part dimensions and physical properties due to moisture absorption or loss in the service/assembly environment. 3. REQUIREMENTS 3.1 STATISTICAL PROCESS Suppliers must c

4、onform to the requirements of Ford Quality System Standard Q-101. A mutually acceptable Control Plan as described therein is required for material/source approval. Appropriate statistical tools must be used to analyze process/product data so that variation in the final product is continuously reduce

5、d. 3.2 INFRARED SPECTROPHOTOMETRY AND/OR THERMAL ANALYSIS Ford Motor Company, at its option, may conduct infrared and/or thermal analysis of material/parts supplied to this specification. The IR spectra and thermogram established for initial approval shall constitute the reference standard and shall

6、 be kept on file at the designated material laboratory. All samples shall produce IR spectra and thermograms that correspond to the reference standard when tested under the same conditions. 3.3 CONDITIONING AND TEST CONDITIONS All test values indicated herein are based on material and specimens with

7、 moisture content not exceeding 0.2 % (test according to ISO R 960, Method B/ASTM D 789). ENGINEERING MATERIAL SPECIFICATION WSF-M4D628-A WP 3948-b Page 2 of 5 All test materials immediately after processing have to be sealed in containers that are impermeable to water vapor. If the moisture content

8、 exceeds 0.2 %, condition the material for a minimum of 16 h at 40 - 50 C at a reduced pressure below 133 Pa. Conduct tests in a controlled atmosphere of 23 +/- 2 C and 50 +/- 5 % relative humidity. Individual specimens shall not be removed from closed containers until immediately before testing. 3.

9、4 MOLDING COMPOUND 3.4.1 Glass Fiber Content 22.5 - 27.5 % (ISO 3451/4, at 600 +/- 25 C) 3.4.2 Melt Temperature, min 250 C (ISO 1218, Method B/ASTM D 789) 3.5 MOLDED TEST SPECIMEN 3.5.1 Preparation of Test Specimens Unless otherwise specified all tests shall be carried out on injection molded one-en

10、d gated test specimens. The following dimensions are required: 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 IS

11、O 294. No annealing allowed. 3.5.2 Density 1.54 - 1.60 g/cm (ISO 1183, Method A/ASTM D 792, Method A1) 3.5.3 Tensile Strength at Max Load, min 110 MPa (ISO R 527/ASTM D 638M, 150 min x 10 x 4.0 +/- 0.2 mm specimen, 5 mm/min test speed) 3.5.4 Flexural Modulus, min 7.6 GPa (ISO 178/ASTM D 790M, Method

12、 I, Procedure A, 80 x 10 x 4.0 +/- 0.2 mm specimen, 64 mm support span) 3.5.5. Shear Modulus at 23 C Range TBD MPa/GPa (ASTM D 4065, forced constant amplitude, fixed frequency of 1 Hz +/- 15 %, strain level below 1 %. Specimen approx. 60 x 10 x 4.0 +/- 0.2 mm cut from the center of specimen A.) ENGI

13、NEERING MATERIAL SPECIFICATION WSF-M4D628-A WP 3948-b Page 3 of 5 Additionally, a Shear Modulus vs. Temperature curve shall be plotted for - 50 to + 240 C temperature range, at 5 C minimum intervals. The plotted curve must be within tolerance range shown on page 6. 3.5.6 Impact Strength, Izod, min (

14、ISO 180, Method A/ASTM D 256, Method A, 63.5 x 10 x 4.0 +/- 0.2 mm specimen, 10 specimens for each test) 3.5.6.1 At 23 +/- 2 C 640 J/m 3.5.6.2 At - 40 +/- 2 C TBD J/m 3.5.6.3 At - (TBD) +/- 2 C TBD J/m The test specimens must be conditioned for minimum of 6 h at the above specified temperature prior

15、 to impact test. Low temperature testing shall be done within the cold box, if not possible, test can be conducted outside, but within 5 s. 3.5.7 Heat Deflection Temperature, min (ISO 75/ASTM D 648, 120 x 10 x 4.0 +/- 0.2 mm specimen) 3.5.7.1 At 1.82 MPa 232 C 3.5.7.2 At 0.45 MPa 256 C 3.5.8 Heat Ag

16、ing Performance (ISO 188/ASTM D 573, 1000 h at TBD +/- 2 C. After heat aging test specimens are to be conditioned in a desiccator for 3 - 5 h at 23 +/- 2 C. Unaged property values shall be determined at the time of the aged properties determination) 3.5.8.1 Impact Strength, Izod Change +/- 20 % (Tes

17、t Method per para 3.5.6.1, specimens to be notched before heat aging) 3.6 FLAMMABILITY (ISO 3795) Burn Rate, max 100 mm/minute The specimen size required for material approval is 355 x 100 x 0.8 +/- 0.1 mm with a smooth surface. 3.7 ADDITIONAL REQUIREMENTS Specific requirements for material and/or m

18、anufactured parts shall be specified on the Engineering drawing, Engineering parts specification and/or performance specifications. All critical areas with respect to these properties shall be clearly designated on the Engineering drawing. ENGINEERING MATERIAL SPECIFICATION WSF-M4D628-A WP 3948-b Pa

19、ge 4 of 5 3.8 SUPPLIERS RESPONSIBILITY All materials supplied to this specification must be equivalent in all characteristics to the material upon which approval was originally granted. Prior to making any change in the properties, composition, construction, color, processing or labelling of the mat

20、erial originally approved under this specification, whether or not such changes affect the materials ability to meet the specification requirements, the Supplier shall notify Purchasing, Toxicology and the affected Materials Engineering activity of the proposed changes and obtain the written approva

21、l of the Materials Engineering activity. Test data, test samples and a new code identification are to be submitted with the request. Substance restrictions imposed by law, regulations or Ford, apply to the materials addressed by this document. The restrictions are defined in Engineering Material Spe

22、cification WSS-M99P9999-A1, unless a different suffix (e.g., A2 or A3) is specified on the engineering document for the application. 4. APPROVAL OF MATERIALS Materials defined by this specification must have prior approval by the responsible Materials Engineering activity. Suppliers desiring approva

23、l of their materials shall first obtain an expression of interest from the affected Purchasing, Design and Materials Engineering activity. Upon request, the Supplier shall submit to the affected Materials Engineering activity its own laboratory report to the specification (test results, not nominal

24、values), the material designation and code number, and test specimens for Ford evaluation. Upon approval, the material will be added to the Engineering Material Approved Source List. 5. GENERAL INFORMATION The information below is provided for clarification and assistance in meeting the requirements

25、 to the specification. 5.1 COEFFICIENT OF LINEAR THERMAL EXPANSION 2.4E-5/ C (ASTM D 696) 5.2 MOLD SHRINKAGE (ISO 2577, approx. 150 x 100 x 3.2 +/- 0.2 mm injection molded specimen) 5.2.1 Molding Shrinkage After 48 h at 23 +/- 2 C 0.4 - 0.8 % 5.2.2 Post Shrinkage (Separate specimens required for eac

26、h test) ENGINEERING MATERIAL SPECIFICATION WSF-M4D628-A WP 3948-b Page 5 of 5 After 48 h at 80 C TBD % After 30 min. at 120 C TBD % 5.3 WATER ABSORPTION TBD % (ISO 62, 24 h/ASTM D 570, 24 h, 50 +/- 1 mm diameter, 3.2 +/- 0.2 mm thick specimen) 5.4 IMPACT STRENGTH, IZOD, min (ISO 180, Method A/ASTM D

27、 256, Method A, 63.5 x 10 x 4.0 +/- 0.2 mm specimen, 10 specimens minimum) 5.4.1 After Moisture Conditioning TBD kJ/m The notched specimens shall be immersed for 48 h in distilled water at 50 +/- 1 C and subsequently conditioned for 1 h at 23 +/- 2 C and 50 +/- 5 % relative humidity prior to test and tested under the same conditions within 1 h. Shear Modulus vs. Temperature Plot - TBD

展开阅读全文
相关资源
猜你喜欢
  • ASD-STAN PREN 3375-011 CORR 2-2014 Aerospace series Cable electrical for digital data transmission Part 011 Single braid Star Quad 100 ohms Light weight Type KL Product standard (E.pdf ASD-STAN PREN 3375-011 CORR 2-2014 Aerospace series Cable electrical for digital data transmission Part 011 Single braid Star Quad 100 ohms Light weight Type KL Product standard (E.pdf
  • ASD-STAN PREN 3375-011-2014 Aerospace series Cable electrical for digital data transmission Part 011 Single braid Star Quad 100 ohms Light weight Type KL Product standard (Edition .pdf ASD-STAN PREN 3375-011-2014 Aerospace series Cable electrical for digital data transmission Part 011 Single braid Star Quad 100 ohms Light weight Type KL Product standard (Edition .pdf
  • ASD-STAN PREN 3375-012-2012 Aerospace series Cable electrical for digital data transmission Part 012 Single braid Star Quad 100 ohms 260 Type KH Product standard (Edition P 1).pdf ASD-STAN PREN 3375-012-2012 Aerospace series Cable electrical for digital data transmission Part 012 Single braid Star Quad 100 ohms 260 Type KH Product standard (Edition P 1).pdf
  • ASD-STAN PREN 3376-1989 Aerospace Series Limits of Surface Imperfections of Elastomeric Toroidal Sealing Rings (O-rings) (Issue P 1)《航空航天系列 弹性体环形密封环(O形环)的表面缺陷的限值 第P1版》.pdf ASD-STAN PREN 3376-1989 Aerospace Series Limits of Surface Imperfections of Elastomeric Toroidal Sealing Rings (O-rings) (Issue P 1)《航空航天系列 弹性体环形密封环(O形环)的表面缺陷的限值 第P1版》.pdf
  • ASD-STAN PREN 3377-1989 Aerospace Series Nuts Self-Locking Hexagonal in Heat Resisting Steel FE-PA92HT (A286) Uncoated Classification  1100 MPa 425 Degrees Celsius (Issue P 1)《航空航天.pdf ASD-STAN PREN 3377-1989 Aerospace Series Nuts Self-Locking Hexagonal in Heat Resisting Steel FE-PA92HT (A286) Uncoated Classification 1100 MPa 425 Degrees Celsius (Issue P 1)《航空航天.pdf
  • ASD-STAN PREN 3378-1996 Aerospace Series Titanium TI-P99002 Annealed Wire for Rivet 1 6 mm Less Than or Equal to D Less Than or Equal to 10 mm (Edition P 2)《航空航天系列 1 6mm≤D≤10mm的铆钉用.pdf ASD-STAN PREN 3378-1996 Aerospace Series Titanium TI-P99002 Annealed Wire for Rivet 1 6 mm Less Than or Equal to D Less Than or Equal to 10 mm (Edition P 2)《航空航天系列 1 6mm≤D≤10mm的铆钉用.pdf
  • ASD-STAN PREN 3379-1989 Aerospace Series Bolts Double Hexagon Head Close Tolerance in Heat Resisting Nickel Base Alloy N1-P101HT (Waspaloy) Uncoated for Increased Height Nuts Class.pdf ASD-STAN PREN 3379-1989 Aerospace Series Bolts Double Hexagon Head Close Tolerance in Heat Resisting Nickel Base Alloy N1-P101HT (Waspaloy) Uncoated for Increased Height Nuts Class.pdf
  • ASD-STAN PREN 3380-1990 Aerospace Series Retaining Rings Technical Specification (Issue P 1)《航空航天系列 扣环 技术规范 第P1版》.pdf ASD-STAN PREN 3380-1990 Aerospace Series Retaining Rings Technical Specification (Issue P 1)《航空航天系列 扣环 技术规范 第P1版》.pdf
  • ASD-STAN PREN 3381-1990 Aerospace Series Bolts 100 Degrees Countersunk Normal Head Offset Cruciform-Ribbed Recess Close Tolerance Shank Short Thread in Titanium Anodized MoS 2 Lubr.pdf ASD-STAN PREN 3381-1990 Aerospace Series Bolts 100 Degrees Countersunk Normal Head Offset Cruciform-Ribbed Recess Close Tolerance Shank Short Thread in Titanium Anodized MoS 2 Lubr.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