Forming and drilling of fiber metal laminates – A review
Source abstract
Abstract
In aviation industries, most of the stiffened structural components are manufactured by forming and laminating process. Combination of several conventional manufacturing processes is required in modern industries in hybrid laminate production. Fiber metal laminates undergo various joining process during assembly of aero-structures. Among them, forming and drilling are often required during assembly. Understanding the significance of various process parameters enables quality production and assembly of fiber metal laminates structures. Many researchers explored the cause and effect of few parameters and mechanisms which significantly alter the quality of form and drill. This review describes the progress in forming and drilling of fiber metal laminates for aerospace applications. Especially towards the process parameters, defects and their causes along with the preferred solutions recommended by the researcher society in forming and drilling processes. Numerous factors have controlled the quality of forming and drilling processes. Due to the machining parameters, different failure modes will occur in different layup of the laminates. To overcome the failures in machining/forming of fiber metal laminates, choosing the optimum parameter for the selection based procedure is needed to improve quality of fiber metal laminates.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Advanced machining processes and optimization · Advanced Machining and Optimization Techniques · Mechanical Behavior of Composites
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Center for Composite Materials, Department of Mechanical Engineering, Kalasalingam Academy of Research and Education, Krishnankoil, India
References (91)
Show source-provided references
1. 10.1016/j.paerosci.2005.02.00410.1016/j.paerosci.2005.02.004 ↗
2. Vlot A, Vogelesang LB and De Vries TJ. Towards application of fibre metal laminates in large aircraft. Aircraft Eng Aerosp Tech 1999; 71: 558–570.10.1108/00022669910303711 ↗
3. 10.1016/S0924-0136(00)00411-810.1016/S0924-0136(00)00411-8 ↗
4. 10.1016/S0924-0136(96)02652-010.1016/S0924-0136(96)02652-0 ↗
5. 10.1016/j.proeng.2013.12.04910.1016/j.proeng.2013.12.049 ↗
6. 10.1007/s11837-005-0067-410.1007/s11837-005-0067-4 ↗
7. 10.1016/j.compstruct.2011.01.01810.1016/j.compstruct.2011.01.018 ↗
8. 10.1016/j.compstruct.2011.11.02410.1016/j.compstruct.2011.11.024 ↗
9. Mosse L · Mater Res · 2005 · 8 · 649
10. 10.1016/0734-743X(96)89050-610.1016/0734-743X(96)89050-6 ↗
11. 10.1007/s10443-009-9119-110.1007/s10443-009-9119-1 ↗
12. 10.1016/j.compstruct.2009.06.00610.1016/j.compstruct.2009.06.006 ↗
13. 10.1016/j.msea.2005.02.09310.1016/j.msea.2005.02.093 ↗
14. Pärnänen T, Kanerva M, Sarlin E and Saarela O. Debonding and impact damage in stainless steel fibre metal laminates prior to metal fracture. Compos Struct 2015; 119: 777–786.10.1016/j.compstruct.2014.09.056 ↗
15. Bagnoli F, Bernabei M, Figueroa-Gordon D and Irving PE. The response of aluminium/GLARE hybrid materials to impact and to in-plane fatigue. Mat Sci Eng A - Struct 2009; 523: 118–124.10.1016/j.msea.2009.05.055 ↗
16. Pärnänen T, Alderliesten R, Rans C, Brander T and Saarela O. Applicability of AZ31B-H24 magnesium in fibre metal laminates – an experimental impact research. Compos Part A Appl Sci Manuf 2012; 43: 1578–1586.10.1016/j.compositesa.2012.04.008 ↗
17. 10.1016/j.msea.2008.07.04110.1016/j.msea.2008.07.041 ↗
18. Yeh PC, Chang PY, Wang J, Yang JM, Wu PH and Liu MC. Bearing strength of commingled boron/glass fiber reinforced aluminum laminates. Compos Struct 2012; 94: 3160–3173.10.1016/j.compstruct.2012.05.001 ↗
19. 10.1016/S0266-3538(00)00002-610.1016/S0266-3538(00)00002-6 ↗
20. Vo TP, Guan ZW, Cantwell WJ and Schleyer GK. Modelling of the low-impulse blast behaviour of fibre–metal laminates based on different aluminium alloys. Compos Part B Eng 2013; 44: 141–151.10.1016/j.compositesb.2012.06.013 ↗
21. 10.1016/j.compstruct.2012.08.05010.1016/j.compstruct.2012.08.050 ↗
22. Hausmann J, Naghipour P, Schulze K. Analytical and numerical residual stress models for fiber metal laminates – comparison and application. Procedia Materials Science 2013; 2: 68–73.10.1016/j.mspro.2013.02.009 ↗
23. Moussavi-Torshizi SE, Dariushi S, Sadighi M and Safarpour P. A study on tensile properties of a novel fiber/metal laminates. Mater Sci Eng A 2010; 527: 4920–4925.10.1016/j.msea.2010.04.028 ↗
24. 10.1016/j.ast.2013.12.00510.1016/j.ast.2013.12.005 ↗
25. Xue J, Wang WX, Zhang JZ and Wu SJ. Progressive failure analysis of the fiber metal laminates based on chopped carbon fiber strands. J Reinf Plast Compos 2015; 34: 364–376.10.1177/0731684415571659 ↗
26. Hu YB, Li HG, Cai L, et al. Preparation and properties of Fibre–Metal Laminates based on carbon fibre reinforced PMR polyimide. Mech Eng 2015; 69: 587–591.10.1016/j.compositesb.2014.11.011 ↗
27. Cortes P and Cantwell WJ. The Tensile and Fatigue Properties of Carbon Fiber-reinforced PEEK-Titanium Fiber-metal Laminates. J Reinf Plast Comp 2004; 23: 1615–1623.10.1177/0731684404039796 ↗
28. 10.1023/A:102152001988010.1023/A:1021520019880 ↗
29. Lin CT, Kao PW and Yang FS. Fatigue behaviour of carbon fibre-reinforced aluminium laminates. Composite 1991; 22: 135–141.10.1016/0010-4361(91)90672-4 ↗
30. Almeida RS, Damato CA, Botelho EC, Pardini LC and Rezende MC. Effect of surface treatment on fatigue behavior of metal/carbon fiber laminates. J Mater Sci 2008; 43: 3173–3179.10.1007/s10853-008-2528-y ↗
31. Sun Z, Shi S, Hu X, Chen H and Wong Z. Adhesive joints between carbon fiber and aluminum foam reinforced by surface-treated aramid fibers. Polym Compos 2015; 36: 192–197.10.1002/pc.22929 ↗
32. 10.1016/j.proeng.2013.09.13110.1016/j.proeng.2013.09.131 ↗
33. Kweon JH, Jung JW, Kim TH, Choi JH and Kim DH. Failure of carbon composite-to-aluminum joints with combined mechanical fastening and adhesive bonding. Compos Struct 2006; 75: 192–198.10.1016/j.compstruct.2006.04.013 ↗
34. Wang WX, Matsubara T, Takao Y, Yasuda K and Hayashi R. Effects of curing conditions on the short time co-cure of CFRP–steel hybrid laminates. J Reinf Plast Comp 2015; 34: 819–829.10.1177/0731684415582281 ↗
35. Hundley JM, Hahn HT, Yang JM and Facciano AB. Multiscale modeling of metal-composite interfaces in titanium-graphite fiber metal laminates Part II: continuum scale. J Compos Mater 2011; 46: 1235–1249.10.1177/0021998311416685 ↗
36. 10.1016/j.mechmat.2009.03.00210.1016/j.mechmat.2009.03.002 ↗
37. Lee BE, Park ET, Kim J, Kang BS and Song WJ. Analytical evaluation on uniaxial tensile deformation behavior of fiber metal laminate based on SRPP and its experimental confirmation. Compos Part B-Eng 2014; 67: 154–159.10.1016/j.compositesb.2014.06.031 ↗
38. Kalyanasundaram S, DharMalingam S, Venkatesan S and Sexton A. Effect of process parameters during forming of self-reinforced – PP based fiber metal laminate. Compos Struct 2013; 97: 332–337.10.1016/j.compstruct.2012.08.053 ↗
39. 10.1016/j.compstruct.2011.08.00410.1016/j.compstruct.2011.08.004 ↗
40. Santulli C, Kuan HT, Sarasini F, De Rosa IM and Cantwell WJ. Damage characterisation on PP-hemp/aluminium fibre – metal laminates using acoustic emission. J Compos Mater 2012; 47: 2265–2274.10.1177/0021998312457098 ↗
41. Kuan HTN, Cantwell WJ, Hazizan MA and Santulli C. The fracture properties of environmental-friendly fiber metal laminates. J Reinf Plast Compos 2011; 30: 499–508.10.1177/0731684411398536 ↗
42. Watkins KG, Edwardson SP, Magee J, et al. Laser forming of aerospace alloys. In: Proceedings of the SAE Aerospace Manufacturing Technology Conference , 2001 (Aerospace Congress, Seattle, 2001), Paper No. 2001-01-2610.10.4271/2001-01-2610 ↗
43. Jeyasingh JJV, Anjaneyulu C, Gopinath S and Venkitakrishna PV. Numerical Simulation of Deep Drawing manufacturing process using flexible Die and Rigid Die Techniques. J Mach Form Technol. 2000; 7: 942–945.
44. Pattanaik LN. · J Mach Form Technol · 2013 · 5 · 29
45. Kamble N · J Mach Form Technol · 2016 · 8 · 41
46. Fernandes JL · J Mach Form Technol Form Technol · 2009 · 1 · 21
47. Hufenbach W, Dobrzański LA, Gude M, Konieczny J and Czulak A. Optimisation of the rivet joints of the CFRP composite material and aluminium alloy. J Achiev Mater Manuf Eng 2007; 20: 119–122.
48. Campos Rubio J, Abrao AM, Faria PE, Esteves Correia A, Paulo Davim J. Effects of high speed in the drilling of glass fibre reinforced plastic: Evaluation of the delamination factor. Int J Mach Tool Manu 2008; 48: 715–720.10.1016/j.ijmachtools.2007.10.015 ↗
49. 10.1016/S0007-8506(07)61703-X10.1016/S0007-8506(07)61703-X ↗
50. Goo C-S · J Manuf Technol Res · 2011 · 3 · 167
51. Gaitonde VN · J Manuf Technol Res · 2005 · 7 · 115
52. Markopoulos AP · J Manuf Technol Res · 2010 · 2 · 17
53. Shaikh V · J Manuf Technol Res · 2008 · 2 · 1
54. Carey C, Cantwell WJ, Dearden G, Edwards KR, Edwardson SP and Watkins KG. Low power laser forming of glass fibre based fibre metal laminates. Laser Assisted Net Shape Engineering 5, LANE 2007, 645-655.
55. Lasers Eng · 2005 · 15 · 233
56. 10.1016/j.jmatprotec.2005.09.00210.1016/j.jmatprotec.2005.09.002 ↗
57. Dharmalingam S · J Eng Technol · 2013 · 4 · 147
58. Russig C, Bambach M, Hirt G and Holtmann N. Shot peen forming of fiber metal laminates on the example of GLARE (R). Int J Mater Form 2014; 7: 425–438.10.1007/s12289-013-1137-8 ↗
59. 10.1016/S0020-7683(01)00144-510.1016/S0020-7683(01)00144-5 ↗
60. Pawar OA, Gaikhe YS, Tewari A, Sundaram R and Joshi SS. Analysis of hole quality in drilling GLARE fiber metal laminates. Compos Struct 2015; 123: 350–365.10.1016/j.compstruct.2014.12.056 ↗
61. Abrao AM, Faria PE, Campos Rubio JC, Reis P and Paulo Davim J. Drilling of fiber reinforced plastics: A review. J Mater Process Tech 2007; 186: 1–7.10.1016/j.jmatprotec.2006.11.146 ↗
62. Wang X, Kwon PY, Sturtevant C, Kim DDW and Lantrip J. Comparative tool wear study based on drilling experiments on CFRp/Ti stack and its individual layers. Wear 2014; 317: 265–276.10.1016/j.wear.2014.05.007 ↗
63. 10.1007/s12541-012-0140-110.1007/s12541-012-0140-1 ↗
64. Kuo CL, Soo SL, Aspinwall DK, et al. The effect of cutting speed and feed rate on hole surface integrity in single-shot drilling of metallic-composite stacks. Procedia CIRP 2014; 13: 405–410.10.1016/j.procir.2014.04.069 ↗
65. Durão LMP, Gonçalves DJS, Tavares JMRS, Albuquerque VHCD, Vieira AA and Marques AT. Drilling tool geometry evaluation for reinforced composite laminates. Compos Struct 2010; 92: 1545–1550.10.1016/j.compstruct.2009.10.035 ↗
66. 10.1016/j.ijmachtools.2009.08.00210.1016/j.ijmachtools.2009.08.002 ↗
67. Davim JP, Reis P. Drilling carbon fiber reinforced plastics manufactured by autoclave—experimental and statistical study. Mater Design 2003; 24: 315–324.10.1016/S0261-3069(03)00062-1 ↗
68. Ashrafi SA, Sharif S, Farid AA and Yahya MY. Performance evaluation of carbide tools in drilling CFRP-Al stacks. J Compos Mater 2013; 48: 2071–2084.10.1177/0021998313494429 ↗
69. Montoya M, Calamaz M, Gehin D and Girot F. Evaluation of the performance of coated and uncoated carbide tools in drilling thick CFRP/aluminium alloy stacks. Int J Adv Manuf Technol 2013; 68: 2111–2120.10.1007/s00170-013-4817-0 ↗
70. 10.1016/S0261-3069(03)00062-110.1016/S0261-3069(03)00062-1 ↗
71. Piquet R, Ferret B, Lachaud F and Swider P. Experimental analysis of drilling damage in thin carbon/epoxy plate using special drills. Comps Part A- Appl S 2000; 31: 1107–1115.10.1016/S1359-835X(00)00069-5 ↗
72. 10.1016/j.ijmachtools.2004.09.01210.1016/j.ijmachtools.2004.09.012 ↗
73. Ramulu M, Pahuja R, Hashish MA and Isvilonanda V. In: Abrasive waterjet machining effects on kerf quality in thin fiber metal laminate 2015 WJTA-IMCA conference and expo, New Orleans, LO, 2–4 November 2015.
74. Park KH, Beal A, Kim DDW, Kwon P and Lantrip J. Tool wear in drilling of composite/titanium stacks using carbide and polycrystalline diamond tools. Wear 2011; 271: 2826–2835.10.1016/j.wear.2011.05.038 ↗
75. 10.1016/j.proeng.2013.09.13310.1016/j.proeng.2013.09.133 ↗
76. Durão LMP, Tavares JMRS, Albuquerque VHCD, Marques AT, Magalhães AG and Vieira AA. Tool effects on hybrid laminates drilling. Mater Manuf Process 2010; 25: 476–481.10.1080/10426910903229354 ↗
77. Zitoune R, Collombet F, Lachaud F, Piquet R, Pasquet P. Experiment-calculation comparison of the cutting conditions representative of the long fiber composite drilling phase. Compos Sci Technol 2005; 65: 455–466.10.1016/j.compscitech.2004.09.028 ↗
78. 10.1016/1359-835X(95)00013-R10.1016/1359-835X(95)00013-R ↗
79. 10.1016/j.compstruct.2009.10.01010.1016/j.compstruct.2009.10.010 ↗
80. 10.1016/S0007-8506(07)61472-310.1016/S0007-8506(07)61472-3 ↗
81. Wertheim R, Hanan UB, Ihlenfeldt S, Stoll A, Treppe F and Wabner M. Acoustic emission for controlling drill position in fiber-reinforced plastic and metal stacks. CIRP Ann Manuf Technol 2012; 61: 75–78.10.1016/j.cirp.2012.03.003 ↗
82. 10.1016/j.ijmachtools.2012.01.01310.1016/j.ijmachtools.2012.01.013 ↗
83. 10.4028/www.scientific.net/AMR.325.36910.4028/www.scientific.net/AMR.325.369 ↗
84. 10.1080/10910344.2013.80609810.1080/10910344.2013.806098 ↗
85. 10.1177/030932471349308210.1177/0309324713493082 ↗
86. 10.1016/j.compstruct.2015.02.08010.1016/j.compstruct.2015.02.080 ↗
87. 10.1016/j.ijmachtools.2005.01.00910.1016/j.ijmachtools.2005.01.009 ↗
88. 10.1046/j.1460-2695.2000.00250.x10.1046/j.1460-2695.2000.00250.x ↗
89. 10.1016/j.compositesb.2012.07.05710.1016/j.compositesb.2012.07.057 ↗
90. Krishnaraj V, Prabukarthi A, Ramanathan A, et al. Optimization of machining parameters at high speed drilling of carbon fiber reinforced plastic (CFRP) laminates. Compos Part B 2012; 43: 1791–1799.10.1016/j.compositesb.2012.01.007 ↗
91. Pinho LV, Carou D, Davim JP. Comparative study of the performance of diamond-coated drills on the delamination in drilling of carbon fiber reinforced plastics: assessing the influence of the temperature of the drill. J Compos Mater 2015; 50: 179–189.10.1177/0021998315571973 ↗