Abstract
This paper reports on experimental and numerical studies of the effects of bolt preloads, viscoelasticity, and external applied static and dynamic loads on bolt load relaxation in a unidirectional carbon/epoxy composite bolted joint. Experimental measurements of bolt-connected joints in three-point bending specimens were employed in the studies, and relaxation was observed to depend on the initial preload and external dynamic applied loads. It was observed that for any magnitude of external load the bolt load relaxation decreases with increasing initial preload. These findings emphasize the importance of the magnitude of the preload. It was concluded that only about 1/3 of the bolt force relaxation in the composite joints could be attributed to viscoelastic behavior of the polymer matrix in the composite, and the remaining 2/3 of the relaxation is likely caused by other mechanisms such as bolt thread slip, plasticity and/or external excitation. This paper also briefly reviews some relevant relaxation studies found in the literature for mechanically fastened composite and hybrid joints, as well as the effects of environmental conditions such as temperature and moisture on joint relaxation, and points out some gaps where more research needs to be carried out to understand the behavior of such joints.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Griffiths B (2005) Boeing sets pace for composite usage in large civil aircraft. High-Perform Composite 13:68–71
Weber A (2010) Composite joining pros and cons. Assembly 53(6):38–43
Broughton W, Crocker LE, Gower MRL (2002) Design requirements for bonded and bolted composite structure. National Physical Laboratory Materials Center, NPL report MATC(A)65, Jan 2002
Thoppul SD, Finegan J, Gibson RF (2009) Mechanics of mechanically fastened joints in polymer-matrix composite structures – A review. Compos Sci Technol 69(3–4):301–329
Torque limits for standard threaded fasteners (1993) MSFC-STD-486, NASA Marshall Space Flight Center
Zhao Y, Ford D, Richardson S (2001) Torque limit for fasteners in composites, Technical Report, NASA/MSFC/ED23
Thomas FP, Zhao Y (2005) Torque limits for composites joined with mechanical fasteners, AIAA 2005–2351. In: Proceeding 46th AIAA/ASME/AHS/ASCE/ASC structural dynamics and materials conference AIAA, Reston, VA
Thomas FP (2006) Experimental observation for determining the maximum torque values to apply to composite components mechanically joined with fasteners (MSFC center Director’s discretionary fund report, project No. 03–13). NASA/TM-2006-214323
McCarthy MA, Lawlor P, O’Donnell C, Harris K, Kelly P, Cunningham JP (2005) Measurement of bolt pre-load in torqued composite joints. Strain 41:109–112
Shivakumar KN, Crews JH Jr (1983) Bolt clampup relaxation in a graphite/epoxy laminate. Long-term behavior of composites, ASTM symposium, Williamsburg, ASTM STP 813, pp 5–22
Shivakumar KN, Crews JH Jr (1982) An equation for bolt clamp-up relaxation in transient environments. Compos Technol Rev 4(4):132–135
Schmitt RR, Horn WJ (1990) Viscoelastic relaxation in bolted thermoplastic composite joints. In: 35th international SAMPE symposium and exhibition, was published by SAMPE, Covina, CA pp 1336–1347
Horn WJ, Schmitt RR (1993) Relaxation in bolted thermoplastic composite joints. AIAA J 3(3):485–494
Zhao H, Gibson RF (1995) Influence of clamping force relaxation on vibration damping measurements for polymer composite cantilever beams. In: Proceedings SEM spring conference, Grand Rapids, pp 735–738
Chen H-S (2001) The static and fatigue strength of bolted joints in composites with hygrothermal cycling. Compos Struct 52(3–4):295–306
Chen HS, Kung HK (2002) A hygrothermal sensitivity evaluation on the clamp-up torque of bolted composite joint. In: Sun CT, Kim H (eds) Proceedings of the American Society for composites 17th technical conference, CRC Press LLC
Niu MC (1992) Composite airframe structures practical design information and data, 1st edn. Conmilit Press LTD, Hong Kong, pp 301–302
Monogram Aerospace Fasteners Online catalog, Access on Jan. 31, 2012. Jan. 31, 2012, http://www.monogramaerospace.com/files/active/0/Monogram%20Catalog.pdf
Raju KS, Kumar B, Kolachalamma A, Buhrman AJ (2005) Blind-fastener applications in composite structures: NIAR/Industry/State of Kansas (NIS). NIS 05–003
Kolachalama A, Raju KS (2006) Viscoelastic clamp-up relaxation of blind fastener joints in composites. In: 2nd annual symposium: graduate research and scholarly projects conference proceedings held at Wichita State University, Wichita, 28 Apr 2006
Caccese V, Berube KA, Fernandez J, Melo D, Kabche JP (2009) Influence of stress relaxation on clamp-up force in hybrid composite-to-metal bolted joints. Compos Struct 89:285–293
Pelletier KN, Caccese V, Berube KA (2005) Influence of stress relaxation in hybrid composite/metal bolted connections. Report No. UM-MACH-RPT-01-02, Prepared for the Office of Naval Research under grant No. N00014-01-1-0916
Fernandez M, Caccese V, Vel SS (2009) Effect of temperature and viscoelastic creep on the clamp-up load in hybrid composite/metal bolted joints. Report No. C-2004-015-RPT-03, Prepared for the Office of Naval Research under grant No. N00014-05-1-0735
Caccese V, Mewer R, Vel SS (2004) Detection of bolt load loss in hybrid composite/metal bolted connections. Eng Struct 26:895–906
Bickford JH (1995) An introduction to the design and behavior of bolted joints, 3rd edn. CRC Press, Taylor and Francis, Boca Raton
Thoppul SD, Gibson RF, Ibrahim RA (2008) Phenomenological modeling and numerical simulation of relaxation in bolted composite joints. J Compos Mater 42(17):1709–1729
Hypermesh® V 5.0, User’s manual, Altair Engineering, Inc
ABAQUS® V 6.3, User’s Manual and Theory Manual, Hibbit, Karlson and Sorensen, Inc
Ireman T (1998) Three-dimensional stress analysis of bolted single-lap composite joints. Compos Struct 43:195–216
Gibson RF (2011) Principles of composite material mechanics, 3rd edn. CRC Press, Taylor and Francis Group, Boca Raton
Beckwith SW (1984) Viscoelastic creep behavior of filament-wound case materials. J Spacecr Rocket 21(6):546–552
Acknowledgements
Most of the work reported here was done in the Advanced Composites Research Laboratory at Wayne State University under the sponsorship of the U.S. Air Force Office of Scientific Research grant No. FA9550-04-1-0042. The program manager was Dr. Victor Guirguitui.
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2013 The Society for Experimental Mechanics, Inc.
About this paper
Cite this paper
Gibson, R.F., Thoppul, S.D. (2013). Experimental and Numerical Characterization of Relaxation in Bolted Composite Joints. In: Patterson, E., Backman, D., Cloud, G. (eds) Composite Materials and Joining Technologies for Composites, Volume 7. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, New York, NY. https://doi.org/10.1007/978-1-4614-4553-1_5
Download citation
DOI: https://doi.org/10.1007/978-1-4614-4553-1_5
Published:
Publisher Name: Springer, New York, NY
Print ISBN: 978-1-4614-4552-4
Online ISBN: 978-1-4614-4553-1
eBook Packages: EngineeringEngineering (R0)