CFRP/titanium hybrid material for improving composite bolted joints

Composite Structures

Volumn 83, Issue 4, 2008, Pages 368-380

  Kolesnikov, B ^a   Herbeck, L ^a   Fink, A ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

Bolted joint; Carbon fiber reinforced plastics (CFRP); Fiber metal laminate (FML); Hybrid titanium composite laminate (HTCL); Lamella coupling

Indexed keywords

CARBON FIBER REINFORCED PLASTICS; HYBRID MATERIALS; LAMINATED COMPOSITES; LIGHT WEIGHT STRUCTURES; TITANIUM;

FIBER-METAL LAMINATE; HYBRID TITANIUM COMPOSITE LAMINATE; LAMELLA COUPLING;

BOLTED JOINTS;

BENDING; CARBON FIBER; FIBER REINFORCED COMPOSITE; SHEAR PROPERTY; STRUCTURAL ANALYSIS;

EID: 38849200966     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2007.05.010     Document Type: Article

References (51)

1. Niu M.C.Y. Composite airframe structures, second published (1996), Conmilit Press Ltd., Hong Kong
2. Kupke M, Kolax M. CFRP-fuselage - ensuring future competitiveness. In: Material & process technology - the driver for tomorrow's improved performance. Proceeding of the 25th jubilee international SAMPE Europe conference 2004 of the Society for the Advancement of Materials and Process Engineering Paris EXPO 2004, Porte de Versailles, Paris, 30 March-1 April, 2004. p. 432-7.
3. Airbus A380. In: Jane's All the World's Aircraft 2005-2006. p. 241-6.
4. The new-technology Boeing 787 Dreamliner, which makes extensive use of composite materials, promises to revolutionize commercial air travel. In: Aviation week & space technology market supplement, 14 March, 2005. p. S1-31.
5. Mecham M. Evolution and revolution. In: Aviation week & space technology, 28 March, 2005. p. 46-7.
6. Niu M.C.Y. Airframe structural design. Ninth printing (1997), Conmilit Press Ltd., Hong Kong
7. Jarfall LE. Optimum design of joints: the stress severity factor concept. In: Aircraft faticue - design, operational and economic aspects. 5th ICAF Symposium Melbourne, Australia, 22-24 May, 1967.
8. ESA PSS-03-203 Structural materials handbook. Polymer composites. vol. 1. European Space Agency; July, 1993.
9. Collings T.A. The strength of bolted joints in multi-directional CFRP laminates. Composites January (1977) 43-55
10. Godwin E.W., and Matthews F.L. A review of the strength of joints in fibre-reinforced plastics. Part 1. Mechanically fastened joints. Composites July (1980) 155-160
11. Xiong Y, Poon C. A design model for composite joints with multiple fasteners. Institute for Aerospace Research, Aeronautical note IAR-AN-80, NRC No. 32165, Ottawa, August, 1994.
12. Hollmann K. Failure analysis of bolted composite joints exhibiting in-plane failure modes. J Compos Mater 30 3 (1996) 358-383
13. Hung C.L., and Chang F.K. Strength envelope of bolted composite joints under bypass loads. J Compos Mater 30 13 (1996) 1402-1435
14. Oh J.H., Kim Y.G., and Lee D.G. Optimum bolted joints for hybrid composite materials. Compos Struct 38 1-4 (1997) 329-341
15. Camanho P.P., and Matthews F.L. Delamination onset prediction in mechanically fastened joints in composite laminates. J Compos Mater 33 10 (1999) 906-927
16. Dano M.L., Gendron G., and Picard A. Stress and failure analysis of mechanically fastened joints in composite laminates. Compos Struct 50 (2000) 287-296
17. Starikov R., and Schön J. Quasi-static behaviour of composite joints with protruding-head bolts. Compos Struct 51 (2001) 411-425
18. Hanauska J., Kradinov V., and Madenci E. A composite double-lap joint with staggered bolts: an experimental and analytical investigation. Compos Struct 54 (2001) 3-15
19. Lawlor V.P., McCarthy M.A., and Stanley W.F. An experimental study of bolt-hole clearance effects in double-lap, multi-bolt composite joints. Compos Struct 71 (2005) 176-190
20. Kradinov V., Madenci E., and Ambur D.R. Application of genetic algorithm for optimum design of bolted composite lap joints. Compos Struct 77 (2007) 148-159
21. Müller J. Spannungsverteilung an gelochten über einen Bolzen belasteten Stäben aus kohlenstofffaserverstärktem Kunststoff. ETH Zürich, Dissertation, 1975.
22. Eisenmann J.R., and Leonhardt J.L. Improving composite bolted joint efficiency by laminate tailoring. In: Kedward K.T. (Ed). Joining of composite materials. ASTM STP 749 (1981), American Society for Testing and Materials 117-130
23. Li R., Kelly D., and Crosky A. Strength improvement by fibre steering around a pin loaded hole. Compos Struct 57 (2002) 377-383
24. Öry H, Reimerdes HG. Faserverbundwerkstoffe. Vorlesung an der RWTH, Aachen, 1989.
25. Kradinov V., Madenci E., and Ambur D.R. Bolted lap joints of laminates with varying thickness and metallic inserts. Compos Struct 68 (2005) 75-85
26. Grüniger G. Möglichkeiten der Krafteinleitung in faserverstärkte Bauteile. Kohlenstoff- und aramidfaserverstärkte Kunststoffe (1977), VDI-Verlag, Düsseldorf 123-154
27. Hart-Smith L.J. Mechanically fastened joints for advanced composites - phenomenological considerations and simple analysis. Fibrous composites in structural design (1980), Plenum Press, New York and London 543-574
28. Kolesnikov B, Herrmann AS, Pabsch A, Wilmes H. Patentschrift DE 199 25 953 C 1. Bolzenverbindung für Faserverbundstrukturen, Patentinhaber DLR, 7 September, 2000.
29. Kolesnikov B, Herbeck L. Patentschrift DE 10 2004 045 845 B3. Faserverbundstruktur mit einer Bolzenverbindung und Herstellungsverfahren dafür, Patentinhaber DLR, 15 Dezember, 2005.
30. Nadler MA, Yoshino SY, Darms FJ. Boron/epoxy support strut for non-integral cryogenic tankage. In: Materials and processes, 15th SAMPE symposium, vol. 15, Los Angeles, 1969. p. 179-207.
31. Abibov AL, Vasiliev VV, Kutjinov VF, Sirotkin OS. Designing of dot connections of details from composite materials. In: Designing, evaluation and tests of structural parts from composite materials, Issue 1, Moscow: TsAGI; 1973. p. 144-51 [in Russian].
32. Henze E, Schneider H, Preuß T. Statische Berechnung eines CFK-Flügelmodells (Biege-Torsionskasten) mit der Methode der finiten Elemente und Vergleich mit Versuchswerten. In: Jahrestagung der DGLR, 17-19 September, 1974 Kiel, Vortrag Nr. 74-1187, Bericht von Dornier.
33. Vorobei V.V., and Sirotkin O.S. Joining of structures made from composite materials (1985), Machinostroenie, Moscow [in Russian]
34. Gunjaev G.M., Shelesina G.F., and Iltshenko S.I. Metal laminates with aluminium and titanium alloys. Aviation materials and technologies (2002), VIAM, Moscow 50-58 [in Russian]
35. Kolesnikov B, Herbeck L, Fink A. Fortschrittliche Verbindungstechniken von Faserverbunden. In: DGLR-Kongress, Dresden, Band II, 20-23 September, 2004. p. 1419-28.
36. Vlot A., and Gunnink J.G. Fibre metal laminates an introduction (2001), Kluwer Academic Publishers, Dordrecht-Boston-London
37. Westre WN, et al. Titanium-polymer hybrid laminates. Patent No. US006114050A, the Boeing Company, Seattle, 5 September, 2000.
38. Li E., and Johnson W.S. An investigation into the fatigue of a hybrid titanium composite laminate. J Compos Technol Res, JCTRER 20 1 (1998) 3-12
39. Cortes P., and Cantwell W.J. The tensile and fatigue properties of carbon fiber-reinforced PEEK-titanium fiber-metal laminates. J Reinf Plast Compos 23 15 (2004) 1615-1623
40. Fink A., Kolesnikov B., and Wilmes H. CFRP/titanium: improving composite structure coupling. JEC-Composites February-March 7 (2004) 64-67
41. Kolesnikov B. Trennstellenproblematik und experimentelle Untersuchungen von CFK/Titan-Laminaten (ILS, Zug- Druck- und Lochleibungsfestigkeiten), Interner Bericht IB 131-99/66, DLR, Braunschweig, 1999.
42. AITM 1.0010, issue 2. Determination of compression strength after impact. Airbus Industrie Test Method. June, 1994.
43. DIN 29971. Unidirektionalgelege-Prepreg aus Kohlenstofffasern und Epoxiharz, Luft- und Raumfahrt, July, 1986.
44. Darkov AW, Spiro GS. Strength of materials, Wisshaja Shkola, Moscow, 1969 [in Russian].
45. Engler E., and Hadcock R. Development of boron-epoxy tubular struts for a one-third scale shuttle booster thrust structure. Space shuttle materials (1971), SAMPE, Huntesville 83-98 October
46. Grimes G.C., Jeans L.L., and Demuts E. Sensitivity of bonded and joints in composites to load/environmental spectrum variations. Fibrous composites in structural design (1980), Plenum Press, New York and London 619-644
47. Althof W, Müller J. Untersuchungen an geklebten und lösbaren Verbindungen von faserverstärkten Kunststoffen. Kunststoffe 80, München, 1970. p. 911-6.
48. Kolesnikov B, Wilmes H, Herrmann AS, Pabsch A. Verbundmaterial mit einem verstärkten Verbindungsbereich. Europäisches Patent Nr. 1082217, Europäische Patentschrift EP 1 082 217 B1, Patentblatt 2002/23, Patentinhaber DLR, 5 July 2002.
49. HSB, Handbuch Struktur Berechnung, 12571-01, DASA - AIRBUS, 1995, p. 3.
50. Michaeli W., Huybrechts D., and Wegener M. Dimensionieren mit Faserverbundkunststoffen: Einführung und praktische Hilfen (1994), Carl Hanser Verlag, München-Wien
51. Lowak H., de Jonge J.B., Franz J., and Schütz D. MINITWIST, a shortened version of TWIST. NLR MP 79018 U (1979), National Aerospace Laboratory NLR, Amsterdam, The Netherlands 1 May