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Tytuł artykułu

Modelling of helicopter main rotor aerodynamic loads in manoeuvres

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EN
Abstrakty
EN
The article discusses the method of modelling of the helicopter main rotor aerodynamic loads during steady state flight and manoeuvres. The ability to determine these loads was created by taking into account the motion of each blade relative to the hinges and was a result of the applied method of aerodynamic loads calculating. The first part of the work discusses the basic relationships that were used to build the mathematical model of helicopter flight. The focus was also on the method of calculating of the aerodynamic forces generated by the rotor blades. The results of simulations dedicated to the "jump to hover" manoeuvre were discussed, showing the possibilities of analysing aerodynamic loads occurring in unsteady flights. The main rotor is considered separately in an “autonomous” way and treated as a source of averaged forces and moments transferred to the hub. The motion of individual blades is neglected, and their aerodynamic characteristics are radically simplified. The motion of individual blades is neglected, and their aerodynamic characteristics are radically simplified. This can lead to significant errors when attempting to model dynamic helicopter manoeuvres. The more complex model of helicopter dynamics is discussed.
Słowa kluczowe
Twórcy
  • Polish Air Force Academy Dywizjonu 303 Street 35, 08-521 Deblin, Poland tel.: +48 81 5517423, fax: +48 81 5517417
  • Air Force Institute of Technology Ksiecia Boleslawa Street 6, 01-494 Warsaw, Poland tel.: +48 261 851302, fax: +48 261 851313
Bibliografia
  • [1] Bazow, D. I., Helicopter Aerodynamics, “Mashinostroyenie” Publishing House, Moscow 1969.
  • [2] Bieriestow, L. М., Modeling of Helicopter Dynamics in Flight, “Mahinostroyenie” Publishing House, Moscow 1978.
  • [3] Bramwell, A. R. S., Helicopter Dynamics, Edward Arnold Publishers Ltd., London 1986.
  • [4] Ćwik, D., Kowalski, M., Steżycki, P., Impact of work of turbine adaptive engines for the natural environment, Journal of KONES, DOI: 10.5604/01.3001.0012.7848, Vol. 25, No. 4, pp. 509-516, Warsaw 2018.
  • [5] Garrard, W. L., Liebst, B., Design of a Murtivariable Helicopter Flight Control Qualities Enhancement, Journal of the American Helicopter Society, Vol. 4, No. 4, 1990.
  • [6] Gessow, A., Aerodynamics of the Helicopter, Frederick Ungar Publishing Co., New York 1985.
  • [7] Jankowski, A., Kowalski, M., Start-up Processes’ Efficiency of Turbine Jet Engines, Journal of KONBiN, DOI 10.1515/jok-2016-0041, No. 40, pp. 63-72, 2016.
  • [8] Jankowski, K., Physical and Mathematical Modeling of Helicopter Dynamic Spatial Motion, Ph.D. Thesis, Warsaw University of Technology, Warsaw 1982.
  • [9] Jesaułow, S. J. et all., Helicopter as a Control Object, “Mashinostroyenie” Publishing House, Moscow, 1977.
  • [10] Kim, F. D., Celi, R., Tischler, M., High-Order State Space Simulation Models of Helicopter Flight Mechanics, Journal of the American Helicopter Society, Vol. 38/4, 1993.
  • [11] Kowaleczko, G., Analysis of the Spatial Dynamics of Helicopter Motion Taking Into Account the Influence of Autopilot, Ph.D. Thesis, Military University of Technology, Warsaw 1992.
  • [12] Kowaleczko, G., Inverse Problem in Aircraft Flight Dynamics, Military University of Technology, Warsaw 2003.
  • [13] Kowaleczko, G., Modeling of Dynamics of Flying Objects, Publishing House of the Air Force Institute of Technology, Warsaw 2018.
  • [14] Kowaleczko, G., Nonlinear Dynamics of Helicopter Spatial Motion, Military University of Technology, Warsaw 1998.
  • [15] Kowalski, M., Application of the phase reproduction method to the analysis of an avionic event on board of the W-3 "Sokół" helicopter, Journal of KONES, Vol. 18, No. 1, pp. 301-310, Warsaw 2011.
  • [16] Kowalski, M., Noise emission level versus the structure of the aircraft turbine engine, Journal of KONES, DOI: 10.5604/12314005.1138603, Vol. 19, No. 4, pp. 325-332, Warsaw 2012.
  • [17] Kowalski, M., Waślicki, P., Żak, J., Selected aspects of the maintenance system optimisation of the Polish Armed Forces helicopters, Journal of KONES, DOI: 10.5604/01.3001.0012.4320, Vol. 25, No. 3, pp. 99-109, Warsaw 2018.
  • [18] Mil, M. L., et al., Helicopters – Calculation and Design, “Mahinostroyenie” Publishing House, Moscow 1966.
  • [19] Padfield, G. D., Helicopter Flight Dynamics, Blackwell Publishing Ltd., 2007.
  • [20] Payne, P. R., Helicopter Dynamics and Aerodynamics, Sir Isaac Pitman and Sons Ltd., London 1959.
  • [21] Rutherford, S., Thomson, D., Helicopter Inverse Simulation Incorporating an Individual Blade Rotor Model, 20th Congress of the International Council of the Aeronautical Sciences, ICAS-96-1.2.1.
  • [22] Szabelski, K., et all., Introduction to Helicopter Construction, Transport and Communication Publishers, Warsaw 1995.
  • [23] Szumański, K., Pilot-Helicopter Transgression, Habilitation Thesis, Warsaw University of Technology, Warsaw 1986.
Uwagi
Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-2254ec6a-cc8b-48bb-86b3-d525c326947f
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