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Review of Aeronautical Fatigue Investigations in Poland (2013-2014)

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This review was presented on the 34 Conference of the International Committee on Aeronautical Fatigue and Structural Integrity, Helsinki, Finland, June 1-2, 2015. It contains description of main works and investigations in fatigue of aircraft structures performed in Poland during the years 2013 and 2014.
Słowa kluczowe
Rocznik
Tom
Strony
5--48
Opis fizyczny
Bibliogr. 19 poz., fot., rys., tab., wykr., wzory
Twórcy
  • Institute of Aviation, Al. Krakowska 110/114, Warsaw, Poland
autor
  • Air Force Institute of Technology, ul. Księcia Bolesława 6, 01-494 Warsaw, Poland
autor
  • Air Force Institute of Technology, ul. Księcia Bolesława 6, 01-494 Warsaw, Poland
Bibliografia
  • [1] Brzęczek J, Gruszecki H, Pieróg L, Pietruszka J. Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe. Fatigue of Aircraft Structures. Issue 2014. Institute of Aviation Scientific Publications, Warsaw, Poland.
  • [2] Brzęczek J, Gruszecki H, Pieróg L, Pietruszka J. Selected Aspects Related to Preparation of Fatigue Tests of a Metallic Airframe. Fatigue of Aircraft Structures. Issue 2014. Institute of Aviation Scientific Publications, Warsaw, Poland.
  • [3] Brzęczek J, Chodur J, Pietruszka J. Selected Aspects Related to the Applied Loads Control during fatigue Tests of a Metallic Airframe. Fatigue of Aircraft Structures. Issue 2014. Institute of Aviation Scientific Publications, Warsaw, Poland.
  • [4] Brzęczek J, Gruszecki H, Pieróg L, Deszcz F, Pietruszka J. Stress Analysis of the PZL M28’s Airframe Subjected to Repairs during Fatigue Tests. Fatigue of Aircraft Structures. Issue 2014. Institute of Aviation Scientific Publications, Warsaw, Poland.
  • [5] Rodzewicz M, Głowacki D. Investigation into Load Spectra of UAVS Aircraft. Fatigue of Aircraft Structures. Issue 2013. Institute of Aviation Scientific Publications, Warsaw, Poland.
  • [6] Gadalińska E, Baczmański A. Micromechanical Properties and Stress Measurements with Diffraction Methods. Fatigue of Aircraft Structures. Issue 2013. Institute of Aviation Scientific Publications, Warsaw, Poland.
  • [7] Kurdelski M, Leski A., Klimaszewski S., Stefaniuk M. Structural load monitoring systems for military aircraft in the Polish armed forces with examples of selected activities. ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives: Proceedings of the 26th Symposium of the International Committee on Aeronautical Fatigue (edited by J. Komorowski), Montreal, Canada, 1-3 June 2011.
  • [8] Leski A, Reymer P, Kurdelski M. Development of load spectrum for full scale fatigue test of a trainer aircraft. ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives: Proceedings of the 26th Symposium of the International Committee on Aeronautical Fatigue (edited by J. Komorowski), Montreal, Canada, 1-3 June 2011.
  • [9] Sałaciński M., Leski A., Synaszko P., Stefaniuk M., Dragan K.: Determination of Composite Patch Thickness on the Accuracy of Nondestructive Testing of The Repaired Structure of PZL-130 ORLIK Aircraft. Proceedings of the AIAC16 Sixteenth Australian International Aerospace Congress. 23-26.02.2015 Melbourne, Australia.
  • [10] Reymer P., Leski A., Kurdelski M. Introduction of a Structure Integrity Program for a Military Trainer Aircraft. 28th International Congress of the Aeronautical Sciences. 23-28 Sept. 2012, Brisbane Australia. Proceedings of ICAS2012-12.6.2.
  • [11] Reymer P., Leski A. Flight Loads Acquisition for PZL-130 TC-II Full-Scale Fatigue Test. Fatigue of Aircraft Structures. Issue 2011. Institute of Aviation Scientific Publications, Warsaw Poland.
  • [12] Dragan, K., Klimaszewski, S. “Holistic Approach for Structural Integrity Evaluation of Composite Main Rotor Blades” WCNDT 2008, Shanghai, China
  • [13] Dragan K. NDE activities connected with Service Life Extension of Main Rotor Blades of Helicopters used in Polish Armed Forces. 7th Australian Pacific Vertiflite Conference on Helicopter Technology, 9-12 March, 2009, Melbourne.
  • [14] Dragan, K., Klimaszewski, S. “Holistic Approach for Structural Integrity Evaluation of Composite Main Rotor Blades”, WCNDT 2008, Shanghai, China.
  • [15] Dragan K., Klimaszewski S. „In-service Flaw Detection and Quantification on the MiG-29 Composite Vertical Tail Skin”, 9th ECNDT Berlin, (Germany) 25.09.2006 - 29.09.2006.
  • [16] Dragan K., Klimaszewski S., Salacinski M., Synaszko P., Latoszek A., „DAMAGE DETECTION AND FAILURE MODE DISTRIBUTION FOR THE MiG-29 VERTICAL STABILIZER”, 2010 Aircraft Airworthiness and Sustainment Conference, 11-13 May, Austin Convention Center.
  • [17] Sałaciński M., Synaszko P., Stefaniuk M., Dragan K., Monitoring of Crack Growth in a Structure Under a Composite Patch, Journal of Fatigue of Aircraft Structures, Volume 1, Number 3 / August 2011, Pages, 103-111, ISSN 2081-7738.
  • [18] Dragan K., Leski A., Dziendzikowski M., „Health Monitoring of the aircraft structure based on the embedded piezosensor network on the example of PZL-130 Orlik”, Proceedings of the 27th ICAF Symposium, Jerusalem ISRAEL, 5-7 June 2013, pp.835-844 Volume 2.
  • [19] Leski A., Dragan K., Reymer P., „Full Scale Fatigue Test of PZL-130 Orlik structure”, Proceedings of the 27th ICAF Symposium, Jerusalem ISRAEL, 5-7 June 2013, pp.199-208 Volume 1.
Uwagi
PL
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-c838eb48-31a8-44da-9b60-d103a07e3225
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