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Identyfication pf loads in mechanical structures-helicopter case study

Autorzy
Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This paper presents possibility of identification of loads in mechanical systems based on response measurements during operation. Information of loads is very useful in diagnostic process, if usage of structure is under investigation. State of the art in the field of loads identification is presented. The problem of load identification is defined, and some methods are presented. The paper is focused on the problem of loads identification based on measurements of process parameters or movement parameters for vehicles or airplanes. Two methods are applied to show applicability of this approach in industrial practice; neural network based method and regression model based method. A case study of identification of load of helicopter structure during flight is presented.
Rocznik
Strony
151--160
Opis fizyczny
Bibliogr. 20 poz., rys., wykr.
Twórcy
autor
  • Akademia Górniczo-Hutnicza, al. Mickiewicza 30, 30-059 Kraków
Bibliografia
  • [1] H.R. Busby, D.M. Trujillo. Solution of an inverse dynamics problem using an eigenvalue reduction technique, 23 -Computers and Structures, 25(1), 1990.
  • [2] N.R. Draper, H. Smith. Applied Regression Analysis. Elsevier, Amsterdam, 1971.
  • [3] Z. Engel. Mutual Theorems in Mechanics (in Polish). AGH, Kraków, 2000.
  • [4] J. Giergiel, T. Uhl. Identification of impact forces in mechanical systems. Archives of Machine Design, ADR : XXXVI(2-3), 1989.
  • [5] J. Giergiel, T. Uhl. Identification of the input excitation forces in mechanical structures. The Archives of Transport, 1(1), 1989.
  • [6] D.J. Haas, J. Milano, L. Flitter. Prediction of helicopter component loads using neural networks. Journal of the American Helicopter Society, no. 1, 1995.
  • [7] M. Hackl. Anwendung des Satzes von der wechselseitigen Energie. Acoustica, 58(4), 1985.
  • [8] D. Hall. A multidisciplinary research approach to rotorcraft health and usage monitoring. Presented at the American Helicopter Society 52nd Annual Forum, Washimgton D.C., 1996.
  • [9] J. Li. Application of mutual energy theorem for determining unknown force sources. Proc. of Internotse 88, Avignion, 1988.
  • [10] W. Lisowski, K. Mendrok, T. Uhl. Identification of loads basing on output signal measurement (in Polish). Proc. of 5th Conference on Experimental Methods in design of Machinery, Wrocław-Szklarska Poręba, 2001.
  • [11] L. Ljung. System Identification, Theory for the Users. Prentice Hall, London, 1987.
  • [12] D.P. Schrage, Y.K. Yillikci, S. Liu, J.V.R. Prasad, $.V. Hanagud. Instrumentation of the Yamaha R-50/RMAX helicopter linontar testbed for air loads identification and follow-on research. Journal of the American Helicopter Society, no. 3, 1996.
  • [13] S.S. Simonian. Inverse problems in structural dynamics. Int. Journal on Numerical Methods in Engineering, 17: 357-365, 1981.
  • [14] R. Teal. Regime recognition for MH47E structural usage monitoring. Proceedings of the American Helicopter Society 53 Annual Forum, Virginia Beach, VA, 1267-1284. The Boeing Company, 1997.
  • [15] D.M. Trujillo. Application of dynamic programming to the general inverse problem. Internattonal Journal on Numerical Methods in Engineerring, 23: 613-624, 1987.
  • [16] T. Uhl. Computer Assisted Identification of Mechanical Structures (in Polish). WNT, Warszawa, 1998.
  • [17] T. Uhl. Trends and progress in monitoring and diagnostic systems (in Polish). Pomiary, Automatyka, Kontrola, no. 4, 1999.
  • [18] T. Uhl, J. Pieczara. Application of genetic algorithms for load identification problem. Archives of Transport (in print).
  • [19] A. Wasilak. Investigation of operating conditions of technical objects on example of helicopter SOKOL and its infuence on durability. PhD Thesis, AGH, Kraków, 1998.
  • [20] L. Zion. Predicting fatigue loads using regression diagnostics. Presented at the American Helicopter Society Annual Forum, Washington D.C., 1994.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPB2-0006-0059
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