FORD WSS-M98P3-B-2013 SUN VISOR ASSEMBLY PERFORMANCE TO BE USED WITH FORD WSS-M99P1111-A .pdf
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1、 ENGINEERING MATERIAL SPECIFICATION Date Action Revisions Rev 03 2013 12 03 Revised See Summary of Revisions D. Murtonen FNA 2013 10 09 Revised Editoral- see Summary of Revisions D. Murtonen FNA 2007 07 25 Activated M Dumitrescu, J. W. Williams Controlled document at www.MATS Copyright 2013, Ford Gl
2、obal Technologies, LLC Page 1 of 6 SUN VISOR ASSEMBLY, PERFORMANCE WSS-M98P3-B 1. SCOPE This specification defines the performance requirements for sunvisor assemblies. 2. APPLICATION This specification was released originally for materials used for sun visors. The manufacturing process is not defin
3、ed but they may be covered with vinyl or other polymeric films, knitted or nonwoven fabrics. 2.1 LIMITATIONS All amorphous materials (such as PC, PC/ABS, ABS, SMA, ASA, PPO) should be evaluated for potential incompatibility with other materials that they may come in contact with per FLTM BO 127-03.
4、3. REQUIREMENTS 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). 3.1.1 Vehicle Interior Environment Quality Materials/Component Performance Requirements Materials use
5、d in interior applications must meet the requirements outlined in WSS-M99P2222-D1/latest. 3.1.2 In addition to the requirements listed herein, the assemblies shall meet the additional requirements listed in the Interior Trim System Design Specification (CPSC 01.05.4). Laminated vinyl materials shall
6、 also meet the requirements of WSS-M8P3-E2/E3 or latest. No duplication of testing is required. 3.1.3 Plastic materials must use Ford material specifications and be listed on the Approved Source List. 3.1.4 Testing must be conducted on parts at each prototype and production build phase unless specif
7、ied otherwise by Ford Engineer. See Table 1 for DV/PV testing. 3.2 CONSTRUCTION The construction is not defined but may include wire frames, foam pads or blow molded or injection molded. The part may be covered with a HF welded PVC sheet or other polymeric films, knitted or nonwoven fabric. A mirror
8、 or a printed label is inserted if specified on engineering drawings. Note: Alternative compositions and constructions may be used provided that approval has been given by the appropriate Materials Engineering Activity and is detailed in the Approved Source List. ENGINEERING MATERIAL SPECIFICATION W
9、SS-M98P3-B Copyright 2013, Ford Global Technologies, LLC Page 2 of 6 3.3 COMPRESSION AND RECOVERY After test, the finished part shall not show any visible indentation marks. Test Method: The part shall be indented for one minute with a circular indenter foot of 35.7 mm diameter. Depth of indentation
10、 shall be 50% of part thickness. After release, the part shall recover at standard ambient temperature and humidity for 2 h prior to examination. 3.4 HEAT AGING Rating 4 min (ISO 188/ASTM D 573, ISO 105-A02/AATCC Evaluation Procedure 1, 7 days at 90+/-2 C) Mount the finished part according to vehicl
11、e installation on a suitable fixture and introduce it in car position into a mechanical convection oven. After completion of the heat exposure, condition the part for 24 h minimum at standard atmosphere of 23 +/- 2 C and 50% R.H prior to examination. After test, the part shall not show any color ton
12、e change, change in gloss, or tackiness. Furthermore, no wrinkles or bond line failures are permitted. If applied, the mirror shall not show any distortion or bond line failures. The aged assembly shall not show any change when compared with the original part. 3.5 ENVIRONMENTAL CYCLING Mount the fin
13、ished part according to vehicle installation on a suitable fixture and expose to the required cycling condition. Test Method: Install a complete sun visor using production assembly techniques, in an approved test buck or vehicle, representative of intended production dimensions. Expose the vehicle (
14、with windows open) or test buck to the following environmental cycle: After completion of last cycle condition the part for 24 h minimum at standard atmosphere of 23 +/- 2 C and 50% R.H prior to examination. Automated programmable test cycles based on the listed test conditions may be accepted by pr
15、ior agreement with the affected Materials Engineering Activity. Ramp speed 1 to 5 C per minute. Record actual ramp speed on data sheet. . 5 h at -30 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H. . 5 h at 90 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H. . 16 h at 50 +/- 2 C and 95 +/- 5% R.H. . 30 min at
16、 23 +/- 2 C and 50% R.H. . 5 h at -30 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H. . 5 h at 90 +/- 2 C After test, the part shall not show any color tone change, change in gloss or tackiness. Furthermore, no wrinkles, delamination, cracking or bond line failures are permitted. If applied, the mirror
17、shall not show any distortion or bond line failures. The aged assembly shall not show any change when compared with the original part. ENGINEERING MATERIAL SPECIFICATION WSS-M98P3-B Copyright 2013, Ford Global Technologies, LLC Page 3 of 6 3.6 BOND STRENGTH (applicable to welded or sewn seams) 3.6.1
18、 Original 50 N min 3.6.2 After Environmental Cycling 75% min of original In para 3.5. value Test Method: Specimens 15 mm in width and approx. 150 mm in length shall be cut across the bond line and then clamped in the jaws of a tensile machine in such a manner that the bond line is positioned in the
19、middle of the test sample between the jaws. The maximum breaking strength will be determined using a test speed of 500 mm/min. Report the average of all specimens tested. 3.7 RESISTANCE TO ABRASION 150 cycles (SAE J948, 500 g, CS-10 wheels) No evidence of excessive surface deterioration. The resista
20、nce to abrasion of production materials shall be equal to or better than that exhibited by the sample originally approved by the Materials Engineering Activity. 3.8 RESISTANCE TO SNAGGING 25 cycles (SAE J1530-A, 500 g load, H-18 wheels) (Applicable to nonwoven fabric covered parts only) No evidence
21、of fiber pullout in excess of the material originally approved by Materials Engineering. 3.9 RESISTANCE TO SCUFFING 25 cycles (SAE J365) No evidence of lifting, peeling, excessive scuffing or excessive surface deterioration. The resistance to scuffing of production materials shall be equal to or bet
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