Title: Laser Angle of Incidence Effects on In-Situ Consolidation of Automated Fiber Placement of Polyaryletherketone Composites
Authors: Brian W. Grimsley, Tyler B. Hudson, Roberto J. Cano, Jamie C. Shiflett, Christopher J. Stelter, Christopher J. Wohl, Rodolfo I. Ledesma, Thammaia Sreekantamurthy, Jin Ho Kang, John P. Nancarrow, Ryan F. Jordan, and Jake H. Rower
DOI: 10.33599/nasampe/s.24.0178
Abstract: NASA and Electroimpact, Inc. ®†† in conjunction with other U.S. industry partners are performing research as a part of the NASA High-rate Composites for Aircraft Manufacturing (HiCAM) Project to fabricate thermoplastic panels using automated fiber placement (AFP) to increase manufacturing rates of aircraft structural composites. This work focuses on evaluating the in-situ consolidation AFP of thermoplastics (ICAT) process. Previous studies of the ICAT process using semi-crystalline, polyaryletherketone (PAEK) slit-tape have resulted in an adequate degree of intimate contact between plies; however, the resulting interlaminar strength have been less than laminates fabricated in an autoclave. To improve these properties, the effect of reducing the laser angle of incidence (AoI) during placement to increase the degree of auto-hesion was evaluated. The AoI of the laser assisted AFP head was varied between 12° and 16° to fabricate multiple quasi-isotropic and unidirectional test panels. Physics-based thermal models developed at the NASA Langley Research Center were utilized to predict the temperature profile. Laminate processing temperature was measured experimentally, and panel quality was evaluated by both non-destructive evaluation (NDE) as well as destructively by photo-microscopy. The effect on interlaminar strength was determined by short beam strength testing. Test results of carbon fiber laminates fabricated by ICAT using polyetheretherketone (PEEK), polyetherketoneketone (PEKK), and low-melt polyaryletherketone (LM-PAEK) at various laser angles of incidence, placement temperatures and placement speeds are presented.
References: 1.Lian, E, Lovingfoss, R., and V. Tanoto; “Qualification Material Property Data Report of Medium Toughness PAEK thermoplastics Toray (Formerly TenCate) Cetex TC1225 (LM PAEK) T700GC 12K T1E Unidirectional Tape, 145 gsm 34% RC,” NCAMP Test Report Number: CAM-RP-2019-036 Rev A; 2021 2.O’Brien, T.K., and RH. Martin; ”Round-Robin Testing for Mode I Interlaminar Toughness of Composite Materials,” Journal of Composites Technology & Research, Vol. 15, No. 4, 1993, pp. 269-281. DOI: 10.1520/CTR10379J 3.Corveleyn, S., Lachaud, F., Berthet., F., and C. Rossignol; “Long-term creep behavior of a short carbon fiber-reinforced PEEK at high temperature: Experimental and modeling approach,” Journal of Composite Structure, Vol. 290, 15 June 2022, doi.org/10.1016/j.compstruct.2022.115485 4.Rubin, A.M., Fox, J.R., and R.D. Wilkerson; ”Continuous Molding of Thermoplastic Laminates,” U.S.Patent Application Publication# 20110206906A1,The Boeing Company, 2011. 5.Dara, P.H. and A.C. Loos;”Thermoplastic Matrix Composite Processing Model,” Graduate Dissertation, Virginia Polytechnic Institute, CCMS-85-10, 1985. 6.P.C. deGennes: “Reptation of a Polymer Chain in the Presence of Fixed Obstacles,” Journal of Chemical Physics, VOL:55, No.572 (1971); DOI: 10.1063/1.1675789 7.Wool, R. P. and O'Conner, K. M., ""A Theory of Crack Healing in Polymers,"" Journal of Applied Phvsics. 52(10), p.5953-5963, 1981 8.Wool, R. P. and O'Conner, K. M., ""Time Dependence of Crack Healing,"" Journal of Polvmer Science. Polvmer Letters Edition. Vol 20, p.7-16,1982. 9.Donough, M.J., Shafaq, St.John, N.A., Phillip, A.W., and B.G. Prusty; “Process modelling of In-situ Consolidated Thermoplastic Composite by Automated Fibre Placement – A review,”- Journal of Composites: Part A, Vol163,(2022),DOI: doi.org/10.1016/ j.compositesa.2022.107179. 10.Heil, Joseph P.; Wadsworth, Mark A.; Dando, Kerrick R.; Jones, Ron E.; Tymes, Matt; Slater, Sam J.; Bahr, Rodney E.; Bearden, Bryan T.; “Thermoplastic Composite Rate Enhanced Stiffened Skin: A Case Study,”SAMPE Journal, Vol. 59,p.9, (2023), DOI: 10.33599/SJ.v59no6.01. 11.Lamontia, M. A., Gruber,M. B., Waibel, B. J., Cope, R. D., and A. B. Hulcher, Conformable Compaction System used in Automated Fiber Placement of Large Composite Aerospace Structures,” Proceedings of the 23rd SAMPE EUROPE Conference, (2002); DOI: 20030065867. 12.Tierney, J., and J. W. Gillespie, Jr; “Modeling of In Situ Strength Development for the Thermoplastic Composite Tow Placement Process,” Journal of Composite Materials, Vol 40, No. 16, (2006); DOI:10.1177/0021998306060162. 13.Grimsley, B.W., Cano, R.J., Hudson, T.B., Palmieri, F.P, Wohl, C.J., Ledesma, R.I., Sreekantamurthy, T., Stelter, C.J., Assadi, M.D., Jordan, R.F., Rower, J.H., Edahl, R.A., Shiflett, J.C., Connell, J.W., and Brian J. Jensen;” In-Situ Consolidation Automated Fiber Placement of Thermoplastic Composites for High-Rate Aircraft Manufacturing,” SAMPE Conference, May 2022. ISBN: 978-193455141-7. 14.Hudson, T. B., C. T. Dolph, G. M. Grose, R. J. Cano, R. F. Jordan, C. J. Wohl, R. I. Ledesma and B. W. Grimsley, ""Thermal Response of Thermoplastic Composite Tape During In-situ Consolidation Automated Fiber Placement Using a Laser Heat Source,"" in SAMPE 2023, 2023. doi:10.33599/nasampe/s.23.0101. 15.Cano, R.J., Grimsley, B.W., Hudson, T.B., Shiflett, J.C., Wohl, C.J., Ledesma, R.I., Sreekantamurthy, T., Stelter, C.J., Kang, J.H., Nancarrow, J.P., Jordan, R.F., and J.H. Rower;” Composites from In-situ Consolidation Automated Fiber Placement of Thermoplastis for High-rate Aircraft Manufacturing,” SAMPE Conference, May 2024 (in-press). 16.Agarwal, V.; “The Role of Molecular Mobility in the Consolidation and Bonding of Thermoplastic Composite Materials,” Doctoral Dissertation, The University of Deleware; (1991). 17.Agarwal, V., S. I. Guqeri, R. L. McCullough and J. M. Schultz; ""Thermal Characterization of Laser-Assisted Consolidation Process,"" Journal of Thermoplastic Composite Materials, Vol 5, No. 2:pp115-135, (1992). DOI:10.1177/089270579200500203 18.Bastien, L.J., and J.W. Gillespie; “A Non-Isothermal Healing Model for Strength and Toughness of Fusion Bonded Joints of Amorphous Thermoplastics,” Polymer Engineering and Science, , Vol. 31, No. 24; pp.1720-1730.(1991); DOI: 10.1002/pen.760312406 19.Dara, P.H. and A.C.Loos: “Thermoplastic Matrix Composite Processing Model,” Virginia Polytechnic Institute, CCMS-85-10. (1985) 20.Yang, F. and R. Pitchumani; “Nonisothermal Healing and Interlaminar Bond Strength Evolution During Thermoplastic Matrix Composites Processing,” Journal of. Polymer Composites, Vol. 24, No. 2; pp: 263–278; (2003); DOI:10.1177/0021998306060162 21.Pitchumani, R., Don, R.C., Gillespie, Jr., J.W. and S. Ranganathan; “Analysis of On-Line Consolidation during the Thermoplastic Tow-placement Process,”Book Chapter In: Alam, M.K. and Pitchumani, R. (eds), Heat and Mass Transfer in Composites Processing, ASME Press. (1994). 22.Stelter, C.J., Sreekantamurphy, T., Hudson, T.B., and B.W. Grimsley; “Thermal Modelling of the In-situ Consolidation of Automated Fiber Placement of Themoplastic Composites,” SAMPE Conference, May 2024 (in-press).
Conference: SAMPE 2024
Publication Date: 2024/05/20
SKU: TP24-0000000178
Pages: 19
Price: $38.00
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