Method of modelling nonlinear bearing stiffness of composite laminates plates in the area of installation of the fastener for static strength analysis


Аuthors

Arkhipov P. A.

,

e-mail: p.a.arkhipov@yandex.ru

Abstract

The article considers methods for modeling fasteners in finite element models developed for static strength analysis. It presents a method for modeling nonlinear bearing stiffness of composite laminates (balanced and symmetric) plates in the area of fastener installation for solving static strength problems. 
Two CBUSH elements (in terms of the MSC.NASTRAN software package) are used to model the bearing stiffness of composite laminates plates:
1.    Element CBUSH №1 model linear bearing stiffness;
2.    Element CBUSH №2 model nonlinear bearing stiffness, which obtained from results of testing according to ASTM D5961. 
The algorithm for calculation linear bearing stiffness for element CBUSH element №1 consists of three consecutive steps: 
1.    Calculation the linear bearing stiffness for a typical finite element model of a plate and a bolt using three-dimensional finite elements; 
2.    Calculation the linear bearing stiffness for a finite element model of a plate, corresponding to a typical modeling zone of a fastener of the finite element model of the part; 
3.    Calculating linear bearing stiffness for element CBUSH №1 as the difference between the linear bearing stiffness, which obtained from finite element model with three-dimensional elements, and the linear bearing stiffness, which obtained using a finite element model of a typical zone of a fastener in the finite element model of the part. 
Element CBUSH №2 uses a displacement-force graph that is developed from the results of testing the plate material according to ASTM D 5961.
It presents the calculation of the test task with the presentation of the results with the existing version of modeling fasteners and its modification according to the presented method. 
The presented approach allows for a reasonable calculation of the loads on the fasteners of a multi-bolt connection and the fasteners of non-load-bearing elements to load-bearing elements of the structure under loads close to the ultimate according to the criterion of bearing under the fastener.

Keywords:

fastener; finite element model; bearing stiffness; composite laminate plate

References

  1. MSC Nastran Quick reference guide, May 2013, Version 2013
  2. Alexander Rutman, Adrian Viisoreanu, John A. Parady, Jr. Fasteners Modeling for MSC.Nastran Finite Element Analysis, SAE International and the American Institute of Aeronautics and Astronautics 2000, 18 p. DOI: 10.2514/6.2000-5585
  3. Alexander Rutman, Chris Boshers, John Parady, Larry Pearce Fastener Modeling for Joining Composite Parts, Virtual Product Development Conference, 2009, 22 p. 
  4. Tarichko V. I., Shalupina P. I. On the issue of dynamic loading of supporting structures of special wheeled chassis, Vestnik Kontserna VKO «Almaz – Antei», 2019, no. №4, p. 73-83
  5. R.S. Martins, S.P. Ernani, A. Lorentz Influence of Types of Discrete Modelling of Fasteners in FEM Models, NAFEMS World Congress, 2017, 26p.
  6. Borovskaya Ya. S., Grishin V. I., Kacharava I. N., Naumov S. M. Study of strength of multi-row metal-composite joints, Uchenye Zapiski TsAGI, 2013, v. XLIV, № 4, p. 80 - 90.
  7. Borovskaya Ya. S., Grishin V. I., Popov D. V. On the determination of shear forces in bolts of multi-row metal-composite joints, Uchenye Zapiski TsAGI, 2010, v. XLI, № 6, p. 72 - 79.
  8. Bogoslovskii S.E., Martirosov M.I. Numerical and analytical calculation of critical stress for reinforced shell for stability problem solving, Izvestiya Tul'skogo gosudarstvennogo universiteta. Tekhnicheskie nauki, 2020, p. 481 – 490
  9. Polonik E.N., Surenskii E.A., Fedotov A.A. Avtomatizatsiya raschetov ustalostnoi dolgovechnosti mekhanicheskikh soedinenii elementov aviakonstruktsii, Trudy MAI, no. № 92, 2017, 22 с., URL: https://trudymai.ru/published.php?ID=76755
  10. Dudar'kov Yu. I., Limonin M. V., Naumov S. M., Osipyan E. E. Virtual simulation of experiment at static trials of the aircraft primary structure panels, Kosmicheskie apparaty i tekhnologii, 2015, p. 32 - 39
  11. Vashurin A.S., Orlov L.N. Numerical and experimental evaluation of the passive safety of a crew bus body made of sandwich panels, Mashinostroenie, 2014, p.46 – 54
  12. Alyab'ev A.F., Fedotov M.V., Kolesnikov A.B. Examination of the strength properties of the cargo platform frame of a wheel forwarder, Nauchnyi zhurnal KubGAU, 2021, no. №174, 13 p., DOI: 10.21515/1990-4665-174-003
  13. Strekoz A.V., Sidorenko V.V., Ledovskikh I.V. Analysis of the stress-strain state (SSS) of ailerons from polymer composite materials (PCM) using the finite element method (FEM), Izvestiya Yuzhnogo federal'nogo universiteta. Tekhnicheskie nauki, 2019, p. 122 – 133, DOI: 10.23683/2311-3103-2019-6-122-133
  14. R.S. Martins, M.T. Santos, E.S. Palma Fastening analysis using low fidelity finite element models, 31st Congress of the International Council of the Aeronautical Sciences, 2018, 10 p.
  15. Geoff Morris Defining a standard formula and test-method for fastener flexibility in lap-joints, PhD thesis, Technical University Delft  2004, The Netherlands.
  16. Heimo Huth Influence of fastener flexibility on the prediction of load transfer and fatigue life for multiple-row joints, In ASTM, editor, Fatigue in Mechanically Fastened Composite and Metallic Joints, 1986, 30 p.
  17. S. Rosenfeld, M. B. Tate Preliminary investigation on loads carried by individual joints, NACA-TN-1051, Technical report, 1946, 74 p.
  18. Swift T. Development of fail-safe design features of the dc-10, Damage tolerance in aircraft structures, ASTM STP486, American society for Testing and Materials, 1971, pp. 164-214. DOI: 10.1520/STP26678S
  19. Endogur A.I., Kravcov V.A., Soloshenko V.N. Principy racional'nogo proektirovanija aviacionnyh konstrukcij s primeneniem kompozicionnyh materialov, Trudy MAI, no. № 72, 2014, 13 p., URL: https://trudymai.ru/published.php?ID=47572
  20. Endogur A.I., Kravcov V.A. Ideologija proektirovanija aviacionnyh konstrukcij iz polimernyh kompozicionnyh materialov, Trudy MAI, no. № 81, 2015, 13 p., URL: https://trudymai.ru/published.php?ID=57755
  21. Arkhipov P.A. Method of modelling nonlinear bearing stiffness of metal plates in the area of installation of the fastener for static strength analysis, Trudy MAI, no. № 140, 2025, 34 p., URL: https://trudymai.ru/published.php?ID=184052

Download

mai.ru — informational site MAI

Copyright © 2000-2026 by MAI

Вход