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Preliminary studies of riveted joints at feed force

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Języki publikacji
EN
Abstrakty
EN
The aim of the study was to determine the feasibility of riveted joints in composites materials. Static tensile test method was used. In the test one type of glass fabric was used (Interglas 92140) from which two types of composite samples were prepared. In each sample the same type of fiber with the same fiber orientation – 3 layers - was used. The samples had dimensions of 100×100 mm and thickness of approximately 1 mm. The composite probes were located in a metal frame with a screw connection which was made of screws with nominal thread pitch M5. Screws were tightened with constant torque. It was to provide an axial force to the sample during the tensile test. The frame was placed between cross-bars of tensile machine INSTRON 8516. The samples were stretched at a speed of 0.05 mm/s at a distance up to 15 mm. During the tensile test displacement of the samples and pull force were registered. Depending on the fibre orientations and the value of feed force, damage models were described. On the basis of the results the possibility of usage of aluminium rivet nuts connections in composite materials was determined.
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Twórcy
autor
  • Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology, ul. Nowowiejska 24, 00-665 Warszawa, Poland
autor
  • Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology, ul. Nowowiejska 24, 00-665 Warszawa, Poland
  • Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology, ul. Nowowiejska 24, 00-665 Warszawa, Poland
  • Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology, ul. Nowowiejska 24, 00-665 Warszawa, Poland
Bibliografia
  • 1. Colombo C., Vergani L.: Influence of delamination on fatigue properties of a fibreglass composite. Composite Structures. 1; 107, 2014, 325–333.
  • 2. Deng J.H., Tang C., Fu M.W., Zhan Y.R.: Effect of discharge voltage on the deformation of Ti Grade 1 rivet in electromagnetic riveting. Materials Science and Engineering A, 591, 2014, 26–32.
  • 3. Gibson R.F.: Principles of composite material mechanics. 3rd ed. Boca Raton: CRC Press: Taylor & Francis Group, 2012.
  • 4. Cao Z., Cardew-Hall M.: Interference-fit riveting technique in fiber composite laminates. Aerospace Science and Technology, 5; 10(4), 2006, 327–330.
  • 5. Ataş A, Soutis C.: Subcritical damage mechanisms of bolted joints in CFRP composite laminates. Composites Part B: Engineering, 11; 54, 2013, 20–27.
  • 6. Klasztorny M, Nycz D.: Modelling and numerical study of blind rivet nut/bolt joints of composite shell segments. Shell Structures: Theory and Applications, Proceedings of the 10th SSTA 2013 Conference; 2014.
  • 7. Benzarti K, Chataigner S, Quiertant M, Marty C, Aubagnac C.: Accelerated ageing behaviour of the adhesive bond between concrete specimens and CFRP overlays. Constr Build Mater. 2, 25(2), 2011, 523–538.
  • 8. Marques AT. 7 - Fibrous materials reinforced composites production techniques. In: Fangueiro R, editor. Fibrous and Composite Materials for Civil Engineering Applications. Woodhead Publishing, 2011, 191–215.
  • 9. Fazzolari F.A.: A refined dynamic stiffness element for free vibration analysis of cross-ply laminated composite cylindrical and spherical shallow shells. Composites Part B: Engineering, 6, 62, 2014, 143–158.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-d2cf25e7-dc01-44f4-9d88-b7f6cc6bfb27
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