15th CONFERENCE „FATIGUE OF AIRCRAFT STRUCTURES”
13-14 January 2022
13 January 2022 (Thursday) |
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10:00 – 11:40 | Session 1
WELCOME AND CONFERENCE OPENINGINFLUENCE OF HOT ISOSTATIC PRESSING ON THE FATIGUE BEHAVIOR OF ADDITIVELY MANUFACTURED TITANIUM ALUMINIDES AT APPLICATION-RELEVANT TEMPERATURESMirko Teschke 1, Juliane Moritz 2,3, Axel Marquardt 2,3, Christoph Leyens 2,3 and Frank Walther 1 1 Chair of Materials Test Engineering (WPT), TU Dortmund University, Dortmund, Germany STRUCTURAL INTEGRITY, FATIGUE BEHAVIOUR AND CYCLIC DEFORMATION OF TITANIUM TI-6AL-4V ADDITIVELY MANUFACTURED BY W-DEDR. Plaskitt 1, M. Hill 1, A. K. Syed 2, X. Zhang 2, S. Williams 3 1 Prenscia (HBK) ADVANCED DIGITAL DATA PROCESSING AND INTEGRATION INTO STRUCTURAL INTEGRITY MONITORING OF THE AIRCRAFTS STRUCTUREKrzysztof Dragan; Piotr Synaszko; Jarosław Ziemkiewicz; Andrzej Żyluk |
11:40 – 12:00 | Break |
12:00 – 14:00 | Session 2
OPERATIONAL DEFLECTION SHAPE ANALYSIS – GAIN MORE INFORMATION FROM A VIBRATION TESTEmanuel Malek ACHIEVING SAFETY IN FATIGUE TESTS OF AIRCRAFT STRUCTURESJasper Knool, Mike van Dijk, Michał Jabłoński COMPOSITE MATERIALS TESTING USING ELECTRIC ACTUATORSMarco Salvador, Michał Jabłoński, Andrea Dengo |
14:00 – 14:30 | Break |
14:30 – 15:40 | Session 3
EFFICIENCY AND FATIGUE/ENDURANCE LABORATORY TESTS OF AVIATION FRICTION BRAKESZbigniew Skorupka THE INFLUENCE OF MATERIAL CONFIGURATION OF FIBER-METAL LAMINATES WITH ALUMINA CORE ON FLEXURAL STRENGTHFrankiewicz M. 1, Karoluk M.1, Osiecki T.2, Scholz P.3 1 Faculty of Mechanical Engineering, Wroclaw University of Science and Technology FATIGUE DETERMINATION OF MAIN LANDING GEAR ATTACHMENT FRAME OF AN AIRCRAFT BASED ON LOAD MONITORING SYSTEM INDICATIONSMichal Dziendzikowski 1, Artur Kurnyta 1, Piotr Reymer 1,2, Marcin Kurdelski 1, Sylwester Klysz 1,3, Andrzej Leski 2,4 and Krzysztof Dragan 1 1 Airworthiness Division, Air Force Institute of Technology, Warsaw, Poland |
15:40 – 16:00 | Break |
16:00 – 17:15 | Session 4
FATIGUE CRACK MONITORING TECHNOLOGY FOR METAL AIRCRAFT STRUCTURES WITH THE USE OF THE FLEXIBLE INTEGRATED EDDY CURRENT SENSORSKamil Kowalczyk, Michał Dziendzikowski, Patryk Niedbała, Krzysztof Dragan, STUDY OF INTERLAMINAR FRACTURE TOUGHNESS IN AIRCRAFT COMPOSITE MATERIALSNowakowski Dominik 1, Baran Marta 1, Lisiecki Janusz 1, Kłysz Sylwester 1,2 1 Airworthiness Division, Air Force Institute of Technology, Warsaw, Poland DETERMINATION OF LIFE AND DEGRADATION MECHANISMS OF MATERIAL OPERATING UNDER FATIGUE-CREEP CONDITIONSAnna Polnik 2, Hubert Matysiak 2, Zbigniew Pakieła 1 1 Warsaw University of Technology, Warsaw, Poland |
14 January 2022 (Friday) |
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10:00 – 11:15 | Session 5
IMPROVING STRENGTH AND STIFFNESS PERFORMANCE OF A GYROCOPTER COMPOSITE LANDING GEARPaweł Borkowski, Adam Dacko, Mirosław Rodzewicz COATING BASED ON ALUMINUM OXIDE MODIFIED BY POLYMER EVALUATED IN TERMS OF SUPERHYDROPHOBIC, ANTI-FOULING AND ANTI-ICING PROPERTIESKlaudia Olkowicz 1, Zofia Buczko 2, Kamil Kowalczyk 1, Barbara Nasiłowska 3 1 Air Force Institute of Technology, Warsaw, Poland SENSITIVITY ANALYSIS OF THE NASGRO EQUATION BASED ON THE PZL-130 TC-II ORLIK TRAINER AIRCRAFT FULL SCALE FATIGUE TEST RESULTSPiotr Reymer 1,2, Andrzej Leski 1,3, Marcin Kurdelski 2 1 Military University of Technology, Warsaw, Poland |
11:15 – 11:45 | Break | |
11:45 – 13:15 | Session 6
INVESTIGATIONS OF A DAMPER PROTOTYPE WITH A MAGNETORHEOLOGICAL ELASTOMERPaweł Skalski, Paweł Grygorcewicz, Ryszard Harla, Jakub Piłczyński, Zbigniew Skorupka, Jacek Majewski, Arkadiusz Naumiuk DAMPING PERFORMANCE IMPROVEMENT OF TURBINE BLADING THROUGH ADVANTAGES OF ADDITIVE MANUFACTURING TECHNOLOGYGrzegorz Moneta, Michal Fedasz, Michal Szmidt, Slawomir Cieslak, Wieslaw Krzymien DETERMINATION OF STRENGTH PARAMETERS OF THE COMPOSITE LAYER BASED ON REVERSE ENGINEERING AND FEM CALCULATIONSPiotr Samoraj |
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13:15 – 13:45 | Break |
13:45 – 15:15 | Session 7
MULTI-CRITERIA APPROACH TO NON-DESTRUCTIVE TESTING OF POLYMER COMPOSITESPiotr Synaszko; Krzysztof Dragan; Norbert Pałka; Jarosław Ziemkiewicz DIFFRACTION METHODS IN ADDITIVE MANUFACTURINGŁukasz Pawliszak and Elżbieta Gadalińska VALIDATION OF FATIGUE ANALYSIS RESULTS AND SHORTENING TIME OF LANDING GEAR CERTIFICATION TEST BY KSTF METHODAlex Oudovikine |