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Impact Loads and Crash Safety of the Cockpit of a Composite Glider

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
One major problem associated with gliding is the safety of the crew during landings in the country outside the airfield. The analysis of glider-accident statistics shows that such out-landings may significantly influence the safety. Therefore, of vital importance are the crashworthiness properties of the glider fuselage structure. The subject of the study was the PW-5 glider fuselage made of composites and subjected to high loads typical of glider crashes. The aim was to provide experimental data for validation of a numerical model of the cockpit-pilot system during impact. Two experimental tests with the composite glider cockpit were performed using a typical car-crash track. During the first test the cockpit with a dummy inside was crashed onto the ground at the angle of 45 degrees at a speed of 55 km/h. Accelerations and deformations at chosen points in the cockpit as well as signals coming from the dummy sensors and forces in the seat belts were recorded. The second test was an impact into a concrete wall at a speed of about 80 km/h. The full-scale tests were accompanied by a number of quasi-static and dynamic laboratory tests on samples of composite material. The experimental tests provided valuable results for the parametrical identification of a simulation model developed using the MADYMO software.
Rocznik
Tom
Strony
39--55
Opis fizyczny
Bibliogr. 14 poz., fot., rys., tab., wykr.
Twórcy
  • Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics plac Politechniki 1, 00-661, Warsaw, Poland
  • Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics plac Politechniki 1, 00-661, Warsaw, Poland
  • Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics plac Politechniki 1, 00-661, Warsaw, Poland
  • Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics plac Politechniki 1, 00-661, Warsaw, Poland
Bibliografia
  • [1] Annual safety review 2019, EASA – European Aviation Safety Agency,
  • [2] AVSCOM, Aircraft Crash Survival Design Guide, AD-218 434, Vol. 1. Design Criteria and Check List, 1989.
  • [3] Bureau of Investigation and Analysis for Civil Aviation Safety, Glider accidents 1999-2001 Study, France, 2001.
  • [4] Civil Aviation Office, Analiza stanu bezpieczeñstwa lotów i skoków spadochronowych w lotnictwie cywilnym RP w 2003 roku, Warsaw, Poland, 2004.
  • [5] European Aviation Safety Agency, CS22. Sailplanes and Powered Sailplanes.
  • [6] European Commission, European Vehicle Passive Safety Network 2. Report Task 5.6: Aircraft Safety, 5th Framework Programme, Competitive and Sustainable Growth Programme, Land Transport and Marine Technologies, Contract G3RTCT2001-05074, 25 February 2004.
  • [7] Lindstedt L., Rodzewicz M., Rzymkowski C. and Kedzior K., (2009) Experimental Study of Impact Phenomena in the case of a Composite Glider, Technical Soaring, vol. 33, no. 2, pp. 54-62.
  • [8] Lindstedt L., (2011) Numerical simulation of glider crash against a nondeformable barrier, The Archive of Mechanical Engineering, vol. 58, no. 2, pp. 245-265.
  • [9] Roger, W, N. Ludwig and M. Conradi, (1999) Glider ground impact tests, Technical Soaring, 23(4), pp. 120-128.
  • [10] Soaring Safety Foundation, Soaring Safety Foundation Annual Report 1999, Post Office Box 2100, Hobbs, New Mexico 88241.
  • [11] SAE International, SAE J 211-1.Revised MAR95.
  • [12] Sperber, M, Crashworthiness of glider cockpits, TUV Rheinland, 51105 Köln, Germany.
  • [13] TNO Automotive MADYMO Theory Manual ver. 6.4, Delft, The Netherlands, 2007.
  • [14] Yamada, H., (1970) Strength of biological materials, Published by F.G. Evans Williams and Wilkins, Baltimore, Ohio, USA.
Uwagi
PL
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-6538e6e7-8b05-4ce8-a58f-fc19fb6b9d57
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