Service Life Assessment Program of PZL-130 Orlik TCII Structure

• Autorzy: Leski A.

Identyfikatory

DOI

10.2478/v10164-010-0040-8

• Języki publikacji: EN

Abstrakty

EN

The following paper concerns the structural integrity program (SEWST) for the PZL-130 Orlik TCII trainer aircraft. The origin of the program is defined as well as the most important tasks necessary to fulfill the assumed goal.

Słowa kluczowe

EN

SEWST; full scale fatigue test; flight loads; teardown inspection

• Wydawca: Wydawnictwa Naukowe Sieci Badawczej Łukasiewicz - Instytutu Lotnictwa
• Czasopismo: Fatigue of Aircraft Structures
• Rocznik: 2011
• Tom: Iss. 3
• Strony: 74--77
• Opis fizyczny: Bibliogr. 11 poz., fot., rys., wykr.

Twórcy

autor

Leski A.

• Air Force Institute of Technology, Warsaw, Poland

Bibliografia

• [1] Anderson, I.A. & Parker, R.G. (1999). Full Scale Fatigue Test of the Pilatus PC9/A trainer aircraft. In 20th ICAF Symposium: Structural Integrity for the next Millennium, 14-16 July 1999. Bellevue, Washington, USA.
• [2] Molent, L., Barter, S.A., White, P., Dixon, B. (2008). Damage tolerance demonstration testing for the Australian F/A-18. International Journal of Fatigue. Vol. 31(2009), 1031-1038.
• [3] Rutledge, R.S., Backman D.S. & Hiscocks, R.J. Evaluation, Modification And Damage Tolerance of an In-Service Aircraft Critical Area, In 25th ICAF Symposium: Bridging the Gap Between Theory and Operational Practice, 27-29 May 2009. Rotterdam, The Netherlands.
• [4] Klimaszewski, S., Leski, A. & Zurek, J. The Role of AFIT in the Polish Aging Military Aircraft Programs. Proceedings of 7th Joint FAA/DoD/NASA Conference on Aging Aircraft, 9-11 September 2003. New Orleans.
• [5] Klimaszewski, S., Leski, A., Dragan, K. & Kurdelski, M. Aircraft Structural Integrity Program of Polish Su-22 Fitter. Proceedings from the ASIP Conference, 30.11-06.12.2006. San Antonio, USA.
• [6] Klimaszewski, S., Kurdelski, M. & Leski, A. Program zapewnienia integralności struktury samolotu jako praktyczne zastosowanie mechaniki pękania. Materiały konferencyjne CD z XI Krajowej Konferencji Naukowo-Szkoleniowej Mechaniki Pękania, 9-12 wrzesień 2007. Kielce/Cedzyna.
• [7] Leski, A, Klimaszewski, S. & Kurdelski, M. The Assessment of Fatigue-Life Resources of the PZL-130 Orlik’s Structure. Proceedings from Sixth DSTO International Conference of Health & Usage Monitoring, 6-9 March 2009. Melbourne, Australia.
• [8] Klimaszewski, S., Leski, A., Dragan, K., Kurdelski, M. & Wrona, M. (2009). Helicopter Structural Integrity Program of Polish Mi-24 Helicopters. In 25th ICAF Symposium: Bridging the Gap Between Theory and Operational Practice, 27-29 May 2009, Rotterdam, The Nederlands. Part 4, 263-277.
• [9] Leski, A., Klimaszewski, S. & Kurdelski, M. (2009). The Fatigue Life Assessment of PZL-130 Orlik Structures Based on Historical Usage Data. In Antoni Niepokólczycki (Editor), Fatigue of aircraft Structures (pp. 131-139). Warsaw, Poland: Institute of Aviation Scientific Publications.
• [10] Leski, A. An Algorithm of Selecting a Representative Load Sequence for a Trainer. In 2nd International Conference on Engineering Optimization. 6-9 September 2010. Lisbon, Portugal.
• [11] Leski, A., Obrycki, L. (2010). Representative Load Sequence for the PZL-130 ORLIK. In Antoni Niepokólczycki (Editor), Fatigue of aircraft Structures (pp. 69-77). Warsaw, Poland: Institute of Aviation Scientific Publications