Advertisement

Aerotecnica Missili & Spazio

, Volume 97, Issue 2, pp 85–95 | Cite as

Design of a Fuselage-Mounted Main Landing Gear of a Medium-Size Civil Transport Aircraft

  • A. Nuti
  • F. Bertini
  • V. Cipolla
  • G. Di Rito
Article

Abstract

The subject of the present paper is the design of an innovative fuselage mounted main landing gear, developed for a PrandtlPlane architecture civil transport aircraft with a capacity of about 300 passengers. The paper presents the conceptual design and a preliminary sizing of landing gear structural components and actuation systems, in order to get an estimation of weight and of the required stowage. The adopted design methodology makes use of dynamic modelling and multibody simulation from the very first design stages, with the aim of providing efficient and flexible tools for a preliminary evaluation of performances, as well as enabling to easily update and adapt the design to further modifications. To develop the activity, the multibody dynamics of the landing gear (modelled using Simpack software) has been integrated via co-simulation with dynamic models developed in the Matlab/Simulink environment.

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. 1.
    A. Frediani, G. Montanari, “Best Wing System: An Exact Solution of the Prandtl’s Problem”, Variational Analysis and Aerospace Engineering, 2009.Google Scholar
  2. 2.
    A. Frediani, V. Cipolla, K. Abu Salem, V. Binante, Picchi Scardaoni, “On the Preliminary Design of PrandtlPlane Civil Transport Aircraft”, 7th EUCASS conference, 2017, Milan, Italy.Google Scholar
  3. 3.
    R. Cavallaro, L. Demasi, “Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future”, Progress in Aerospace Sciences, Vol. 87, 2016, pp. 1–93.CrossRefGoogle Scholar
  4. 4.
    S.F.N. Jenkins, “Landing Gear Design and Development”, Proceedings of the Institution of Mechanical Engineers, Vol. 203, No. 1, 1989, pp. 67–73.CrossRefGoogle Scholar
  5. 5.
    J. Roskam, “Airplane Design: Part IV — Layout Design of Landing Gear and Systems”, 1986.Google Scholar
  6. 6.
    D.P. Raymer, “Aircraft Design: A Conceptual Approach”, 1989.Google Scholar
  7. 7.
    N.S. Currey, “Aircraft Landing Gear Design: Principles and Practices”, 1988.CrossRefGoogle Scholar
  8. 8.
    European Aviation Safety Agency, “Certification Specifications and Acceptable Means of Compliance for Large Aeroplanes CS-25”.Google Scholar
  9. 9.
    M. Howse, “All electric aircraft”, IEEE Power Engineering Journal, Vol. 17, No. 4, 2003, pp. 35–37.CrossRefGoogle Scholar
  10. 10.
    J.A. Rosero, J.A. Ortega, E. Aldabas, and L. Romeral, “Moving towards a more electric aircraft”, IEEE Aerospace and Electronic Systems Magazine, Vol. 22, No. 3, 2007, pp. 3–9.CrossRefGoogle Scholar
  11. 11.
    J.C. Shaw, S.D.A. Fletcher, P.J. Norman, and S.J. Galloway, “More electric power system concepts for an environmentally responsible aircraft (N+2)”, Proceedings of 47th International, Universities Power Engineering Conference (UPEC), 2012, London, United Kingdom, pp. 1–6.Google Scholar
  12. 12.
    F. Bertini and A. Nuti, “Design and Dynamic Modelling of a Fuselage-Mounted Main Landing Gear for a PrandtlPlane Civil Transport Aircraft”, Master Thesis, University of Pisa, 2018.Google Scholar
  13. 13.
    A.P. Garshin, V.I. Kulik and A.S. Nilov, “Braking friction materials based on fiber-reinforced composites with carbon and ceramic matrices”, Refractories and Industrial Ceramics, Vol. 49, No. 5, 2008, pp. 391–396.CrossRefGoogle Scholar
  14. 14.
    J.C. Maré, “Aerospace Actuators, Signal-by-Wire and Power-by-Wire”, Vol. 2, 2017.Google Scholar
  15. 15.
    G. Di Rito, R. Galatolo, and F. Schettini, “Experimental and simulation study of the dynamics of an electromechanical landing gear actuator”, Proceedings of the 30th International Council of the Aeronautical Sciences (ICAS), 2016, Daejeon, South Korea.Google Scholar
  16. 16.
    A. Garcia, I. Cusidò, J.A. Rosero, J.A. Ortega, and L. Romeral, “Reliable electro-mechanical actuators in aircraft”, IEEE Aerospace and Electronic Systems Magazine, 2008, pp. 19–25.Google Scholar
  17. 17.
    E. Balaban, P. Bansal, P. Stoelting, A. Saxena, K.F. Goebel and S. Curran, “A diagnostic approach for electromechanical actuators in aerospace systems”, Proceedings of the 2009 IEEE Aerospace Conference, 2009, pp. 1–10.Google Scholar
  18. 18.
    G. Di Rito and F. Schettini, “Health monitoring of electromechanical flight actuators via position-tracking predictive models”, Advances in Mechanical Engineering, Vol. 10, No. 4, 2018, pp. 1–12.Google Scholar
  19. 19.
    L. Venkatakrishnan, N. Karthikeyan and K. Mejia, “Experimental Studies on a Rudimentary Four Wheel Landing Gear”, AIAA Journal, Vol. 50, No. 11, 2012, pp. 2435–2447.CrossRefGoogle Scholar
  20. 20.
    A.A. Shabana, “Dynamics of Multibody Systems”, 3rd ed., 2005.CrossRefGoogle Scholar
  21. 21.
    W. Schiehlen (ed.), “Multibody Systems Handbook”, 1990.CrossRefGoogle Scholar
  22. 22.
    E. Bakker, L. Nyborg, and H.B. Pacejka, “Tyre Modelling for Use in Vehicle Dynamics Studies”, SAE Technical Paper, No. 870421, 1987.Google Scholar
  23. 23.
    H.B. Pacejka, “Tire and Vehicle Dynamics”, 3rd ed., 2012.Google Scholar

Copyright information

© AIDAA Associazione Italiana di Aeronautica e Astronautica 2018

Authors and Affiliations

  • A. Nuti
    • 1
  • F. Bertini
    • 1
  • V. Cipolla
    • 1
  • G. Di Rito
    • 1
  1. 1.Department of Civil and Industrial Engineering - Aerospace DivisionUniversity of PisaUK

Personalised recommendations