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QUALIFICATION TEST FOR A C PANEL ADHESIVES
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Develop a qualification test for flammability,of adhesives used in bonded details. Establish similarity of bonded details,APPLICATIONS. Certification of New Parts, International Materials Fire Test Working Group Federal Aviation 2. Administration,October 21 2009,ADHESIVES TASK GROUP. American Airlines,Bombardier,C D Aerospace, International Materials Fire Test Working Group Federal Aviation 3.
Administration,October 21 2009,INDUSTRY PROPOSED METHODS OF COMPLIANCE. INDUSTRY PROPOSED,FOR CERTIFICATION OF INTERIOR MATERIALS. Part 2 Methods That Will Require Supporting Data,25 853 a 25 853 d. Ref Feature Bunsen Burner Heat and Smoke,No Construction Similarity Similarity. Testing detail without Test required if A 2 ft2,BONDED adhesive to Appendix.
28 Possible Test if 1 A 2 ft2,DETAILS F substantiates the. bonded configuration No test required if A 1 ft2,For FAA Qualified Adhesives. International Materials Fire Test Working Group Federal Aviation 4. Administration,October 21 2009,ADHESIVE QUALIFICATION TEST ISSUES. FAR 25 versus Other Measurement Method,Sample Form. Effect of Adherends, Effect of Thickness Does thinner substantiate thicker.
International Materials Fire Test Working Group Federal Aviation 5. Administration,October 21 2009,Example Thermoplastic Thickness Ranges. Peak Heat Release Rate kW m2,Total Heat Release kW min m2. 50 Peak HRR 50,10 Total Heat Release 10,EUROPLEX PPSU Clear. 0 040 080 0 12 0 16 0 20 0 24 0 28,Thickness inches. 0 040 does not substantiate 080,OSU Peak HRR of 0 040 0 16.
International Materials Fire Test Working Group Federal Aviation 6. Administration,October 21 2009,Standard Test,Test Method. Method for,for Measuring,Measuring Flammability,Flammability Properties. Properties of,of Pl astics,Other Solid,Solid Materials. Materials Using,Using Microscale,Microscale Combustion. Combustion Calorimetr y ASTM,Calorimetry ASTM,Oxygen Inlet.
Combustor Flow Meter,Mixing Exhaust,Sample Cup,Purge Gas Inlet. Sample Post,Thermocouple, International Materials Fire Test Working Group Federal Aviation 7. Administration,October 21 2009,THERMAL COMBUSTION PROPERTIES. 500 Peak Heat Release Rate,Heat Release Rate J g K. Heat Release Capacity J g K,hc Total Heat Release J g.
Tp Burning Temperature,Noncombustible Fraction g g. 250 300 350 400 450 500 550 800 850,Temperature C, International Materials Fire Test Working Group Federal Aviation 8. Administration,October 21 2009,HEAT RELEASE CAPACITY VERSUS. Heat Release Capacity c J g K COST OF PLASTICS,1000 PP PE. PMMA Commodity,PS ABS Plastics,PET PPO PAR,POM PSU Engineering.
PC Plastics,PVC PPS PES PVF,rigid Phenolic PEEK,100 PEI LCP PEK Heat. PPSU Resistant,TYPICALLY PAI Plastics,TEST KAPTON,0 1 1 10 100. Materials Cost lb,Truckload Prices 2001, International Materials Fire Test Working Group Federal Aviation 9. Administration,October 21 2009,VERTICAL BUNSEN BURNER TEST 114 plastics. Probability of Passing the UL 94 V 0 Requirement,Probability of Passing VBB p.
0 200 400 600 800 1000 1200 nn 4 46,Heat Release Capacity c J g K. International Materials Fire Test Working Group Federal Aviation 10. Administration,October 21 2009,HAND LAY UP OF ADHESIVE RESIN OSU SAMPLES. Fiberglass reinforced adhesive samples are made by hand lay up. Samples cured between two Teflon coated aluminum plates in heated press. Cured samples trimmed to 6 x 6 for OSU HRR testing. Resulting samples 40 resin by weight, International Materials Fire Test Working Group Federal Aviation 11. Administration,October 21 2009,OSU TESTING OF ADHESIVE RESINS. Peak 2 min,50 kW m2 HRR HR,Resin kW m2 kW min m2,BPA Epoxy 111 44.
BPAE MDA 88 26,BPA Epoxy MDA BPA CE 72 28,BPC Epoxy 48 28. BPA Cyanate Ester,Silicone Resin 33 12,BPC Epoxy BPC CE 13 13. Silicone Resin,BPC Cyanate Ester,Time minutes, International Materials Fire Test Working Group Federal Aviation 12. Administration,October 21 2009,OSU PHRR binned data 101 RESINS AND PLASTICS. Maximum Heat Release Capacity from Curve Fit,200 pHRR 6 4 c R 0 8264.
avg pHRR kW m2,cmax 103 J g K,0 100 200 300 400 500 600 700. International Materials Fire Test Working Group Federal Aviation 13. Administration,October 21 2009,OSU Data for,AIRCRAFT CABIN. 127 121 60 P,F Transform Quantitative Data into,Qualitative Data Using Pass Fail. P 14 CFR 25 853,F HRR 65 kW m2 Pass P,F 4 10 0 40,HRR 65 kW m2 Fail F. Etc Fire Test Working Group,International Materials Federal Aviation 14.
Administration,October 21 2009,OSU PHRR 101 RESINS AND PLASTICS. Probability that pHRR 65 kW m2,Probability of Passing OSU pHRR p. 1 14 CFR 25,0 100 200 300 400 500 600 700,Heat Release Capacity c J g K. International Materials Fire Test Working Group Federal Aviation 15.


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