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Investigation of avionic events with use of information from on-board recorders of flight parameters

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The paper discloses opportunities of how information recorded by on-board recorders of flight parameters can be used for investigation of avionic events. An example of the methodical approach is presented of how to verify data acquired from flight recorders, which unambiguously indicates the feasibility of further investigation and analyses of avionic events that may happen to aircrafts. Subsequently the effect of the engine stall is outlined, which enables analysis of those avionic events when the effect of engine(s) stall took place. The paper discloses two cases of avionic events when engine stall was the underlying reason of problems, i.e. when a helicopter entered a stream of exhaust gases produced by a missile launched by that helicopter and when icing of the intake channel occurred in a turbojet engine installed on a helicopter. Investigations of that type are indispensable due to operation constraints and technical conditions of aircrafts operations, where meeting these conditions is the principal requirements in terms of flight safety. This study confirms that opportunities to use data from on-board recorders of flight parameters to find out what was going on with the aircrafts during avionic events are considerable.
Twórcy
  • 3rd Airlift Wing Witkowska Street 8, 62-430 Powidz, Poland tel.: +48 63 2774653, fax: +48 63 2774649
autor
  • Air Force Institute of Technology Księcia Bolesława Street 6, 01-494 Warsaw, Poland tel.: +48 22 6851101, fax: +48 22 8364471
Bibliografia
  • [1] Cieciura, M., Zacharski, J., Probabilistic methods in practical aspects, Warsaw 2009.
  • [2] http://www.focus.pl/jak-to-dziala/zobacz/publikacje/czarna-skrzynka/.
  • [3] Orkisz, M., Impact of the compressor operation control by air bleeding onto the reserve of steady operation, Engineering Transactions, Polish Academy of Sciences, Institute of Fundamental Technical Issues, 1990.
  • [4] Szczepanik, R., Spychała, J., Kowalski, M., Dzięcioł, E., Pawlak, W., Przysowa, R., Perz, M., Analysis of signals generated by rotor blades of rotary fluid flow machines, ITWL, No. V 2497, Warszawa 2006.
  • [5] Szczepanik, R., Szczeciński, S., Investigation of conditions for suction of mechanical contaminants into intakes of turbojet engines, Avionic and Astronautic Technologies, Vol. 3, 1978.
  • [6] Szczepanik, R., Possibilities of stall effect in engines of the “89” series at the moment of missile launching, Technology and Operation, 1980.
  • [7] Wiatrek, R., Theory of avionic engines, Military University of Technology, Warsaw 1983.
  • [8] Wirkowski, P., Impact of alterations in positioning of diving vanes in an axial compressor onto operation of a IC turbojet engine; Scientific Journal of Navy, No. 3 (170), 2007.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-f61f7211-33c3-459c-8de0-8a600938db3b
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