FORD WSB-M11P53-A-1992 PERFORMANCE REQUIREMENTS ADHESIVE FOR BONDING PLASTIC BUMPER GUIDE BRACKETS TO BUMPER FASCIA《用于将塑料保险杠导架粘附到保险杠横梁上的胶粘剂的性能要求》.pdf
《FORD WSB-M11P53-A-1992 PERFORMANCE REQUIREMENTS ADHESIVE FOR BONDING PLASTIC BUMPER GUIDE BRACKETS TO BUMPER FASCIA《用于将塑料保险杠导架粘附到保险杠横梁上的胶粘剂的性能要求》.pdf》由会员分享,可在线阅读,更多相关《FORD WSB-M11P53-A-1992 PERFORMANCE REQUIREMENTS ADHESIVE FOR BONDING PLASTIC BUMPER GUIDE BRACKETS TO BUMPER FASCIA《用于将塑料保险杠导架粘附到保险杠横梁上的胶粘剂的性能要求》.pdf(7页珍藏版)》请在麦多课文档分享上搜索。
1、 ENGINEERING MATERIAL SPECIFICATIONMaterial Name Specification NumberDate Release No. Release/Revision1992 05 29 NB00E10197527000 Released W.Curtiss E.RezendesWP 3948-a Page 1 of 7 PERFORMANCE REQUIREMENTS, ADHESIVE FOR BONDING WSB-M11P53-APLASTIC BUMPER GUIDE BRACKETS TO BUMPER FASCIA1. SCOPEThis s
2、 pecification defines the performance requirements of an adhesive oradhesive system for bonding plastic bumper guide bracket s to bumper fascia.2. APPLICATIONTh is specification was released originally for adhesives used tostructurally bond plastic bumper guide brackets to bumper fascia.This specifi
3、cation does not describe initial adhesive cu re conditions. Theprocedures for assembly bonding shall be prescribed in accordance toadhesive manufacturer and part supplier recommendations.Mate rials meeting this performance specification are identified on theCorporate Approved Source List.Compl iance
4、 with this performance specification does not guarantee thestr uctural adhesive will function for all potential applications on ave hicle. The specific design condition should be evaluated by a planttrial or laboratory simulation prior to release of the material.3. REQUIREMENTS3.1 STATISTICAL PROCES
5、SSupplie 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 product is con
6、tinuously reduced.3.2 CONDITIONING AND TEST CONDITIONSAll test values indicated herein are based on ma terial 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.EN
7、GINEERING MATERIAL SPECIFICATIONWSB-M11P53-AWP 3948-b Page 2 of 7 3.3 SHEAR ADHESION Minimum load specified or(SAE J1523, with details below) substrate breakageSubject bonded test assemblies to the following exposures:. Normal (not aged), min(Condition for 30 minutes at specifiedtemperature prior to
8、 test)3.3.1 Test at 23 +/- 2 C 4000 kPa3.3.2 Test at 90 +/- 2 C 900 kPa3.3.3 Test at - 30 +/- 1 C 4000 kPa. Environmental Aged, min3.3.4 1000 h heat age at 90 +/- 2 C 3000 kPa3.3.5 1000 h humidity at 38 +/- 2 C and 1000 kPa98 +/- 2 % R.H.3.3.6 1000 h water immersion described 1000 kPaper FLTM BI 104
9、-013.3.7 240 h salt spray described per 2500 kPaASTM B 1173.3.8 10 thermal cycles 4000 kPa4 h at 9 0 +/- 2 C, 4 h humidity (38 +/- 2 C and 98 +/- 2 %R.H.), 16 h at - 30 +/- 1 C.Test Method:. Prepare a minimum of 5 test assemblies per test condition. Testsubstr ates shall consist of 100 x 25 x 3 mm c
10、oupons identified inpara 5.1. Bond t est coupons and condition at 23 +/- 2 C until full adhesivecure. (Reference para 5.2). Subject test assemblies to the environments listed above. Allow test assemblies to condition 24 h minimum after en vironmentalexposure before pull test. Conduct shear pull test
11、 on a te nsile tester at a rate of 13 mm perminute . Report peak load at failure and indicate type of failuremode.ENGINEERING MATERIAL SPECIFICATIONWSB-M11P53-AWP 3948-b Page 3 of 7 3.4 CREEP RESISTANCE No slippage(ASTM D 1780)Test Method: Prepare three tes t samples per para 3.3, apply a 4.5 kgdead
12、 weight load to test samples and expose to 90 +/- 2 C for 24 h.3.5 MANDREL BEND FLEXIBILITY No cracking or adhesion loss tosubstrateTest Method:. Apply a 250 x 13 x 3 mm ribbon of adhesive centered lengthwise ontwo 250 x 50 x 3 mm panels identified in para 5.1. Condition test panels after adhesive a
13、pplication at 23 +/- 2 Cuntil full cure. (Reference para 5.2). Conduct 60 d eg mandrel bend test at 23 +/- 2 C and - 30 +/- 1 Cover a 50 mm diameter mandrel. Substrate is in contact withmandrel during test. Repeat above procedure on test assemblies heat aged at 70 +/- 2 Cfor 2 weeks.3.6 COLD SLAM RE
14、SISTANCE No cracking, adhesion or cohesion(FLTM BV 101-02, 10 cycles of failure6 slams per cycle at- 30 +/- 1 C, 3 samplesminimum) . Prepare test assemblies as illustrated in Figure I. Test substratesshall consist of 100 x 250 x 3 mm panels identified in para 5.1. Cond ition test assemblies after bo
15、nding at 23 +/- 2 C untiladhesive full cure. (Reference para 5.2). Mechan ically attach bonded test assembly to a 300 x 300 x 0.76 mmCRS base panel. Centrally locate test assembly on base panel. Conduct test as outlined per FL TM BV 101-02 following steps 9, 10,and 11 . Position panel in slam fixtur
16、e with test assembly facinginward. Subject each test assembly to 10 cycles of 6 slams percycle at - 30 +/- 1 C.ENGINEERING MATERIAL SPECIFICATIONWSB-M11P53-AWP 3948-b Page 4 of 7 3.7 REVERSE IMPACT PLAQUE TEST Test p laques shall exhibit no less(FLTM BO 117-02) than 8 0 % of the impact resistanceof
17、the control plaques and failuremode must be ductileTest Method:. Impact test samples must be inj ection molded 127 x 127 mm or 101.6x 101.6 mm plaques with smooth surfaces and 2.54 mm thick. Prepar e five test samples with adhesive applied to one side, 1.02mm thic k, covering at least a 76.2 mm diam
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