Agenda

13 January 2022 (Thursday)

WELCOME AND CONFERENCE OPENING

INFLUENCE OF HOT ISOSTATIC PRESSING ON THE FATIGUE BEHAVIOR OF ADDITIVELY MANUFACTURED TITANIUM ALUMINIDES AT APPLICATION-RELEVANT TEMPERATURES

Mirko 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
² Technische Universität Dresden, Institute of Materials Science (IfWW), Dresden, Germany
³ Fraunhofer Institute for Material and Beam Technology IWS, Dresden, Germany

STRUCTURAL INTEGRITY, FATIGUE BEHAVIOUR AND CYCLIC DEFORMATION OF TITANIUM TI-6AL-4V ADDITIVELY MANUFACTURED BY W-DED

R. Plaskitt ¹, M. Hill ¹, A. K. Syed ², X. Zhang ², S. Williams ³

¹ Prenscia (HBK)
² Centre for Manufacturing and Materials, Coventry University, UK
³ Welding Engineering and Laser Processing Centre, Cranfield University, UK

ADVANCED DIGITAL DATA PROCESSING AND INTEGRATION INTO STRUCTURAL INTEGRITY MONITORING OF THE AIRCRAFTS STRUCTURE

Krzysztof Dragan; Piotr Synaszko; Jarosław Ziemkiewicz; Andrzej Żyluk
Airworthiness Division, Air Force Institute of Technology,
Warsaw, Poland

OPERATIONAL DEFLECTION SHAPE ANALYSIS – GAIN MORE INFORMATION FROM A VIBRATION TEST

Emanuel Malek
m+p international Mess- und Rechnertechnik GmbH, Hannover, Germany

ACHIEVING SAFETY IN FATIGUE TESTS OF AIRCRAFT STRUCTURES

Jasper Knool, Mike van Dijk, Michał Jabłoński
MOOG, Amsterdam, The Netherlands

COMPOSITE MATERIALS TESTING USING ELECTRIC ACTUATORS

Marco Salvador, Michał Jabłoński, Andrea Dengo
STEPLAB, Resana, Italy

EFFICIENCY AND FATIGUE/ENDURANCE LABORATORY TESTS OF AVIATION FRICTION BRAKES

Zbigniew Skorupka
Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

THE INFLUENCE OF MATERIAL CONFIGURATION OF FIBER-METAL LAMINATES WITH ALUMINA CORE ON FLEXURAL STRENGTH

Frankiewicz M. ¹, Karoluk M.¹, Osiecki T.², Scholz P.³

¹ Faculty of Mechanical Engineering, Wroclaw University of Science and Technology
² Institute of Lightweight Structures and Polymer Technology, Technische Universität Chemnitz
³ Fraunhofer Institute for Machine Tools and Forming Technology IWU

FATIGUE DETERMINATION OF MAIN LANDING GEAR ATTACHMENT FRAME OF AN AIRCRAFT BASED ON LOAD MONITORING SYSTEM INDICATIONS

Michal 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
² Faculty of Mechanical Engineering, Military University of Technology, Warsaw, Poland
³ Faculty of Technical Sciences, University of Warmia and Mazury in Olsztyn, Olsztyn, Poland
⁴ Institute of Aviation, Lukasiewicz Research Network, Warsaw, Poland

FATIGUE CRACK MONITORING TECHNOLOGY FOR METAL AIRCRAFT STRUCTURES WITH THE USE OF THE FLEXIBLE INTEGRATED EDDY CURRENT SENSORS

Kamil Kowalczyk, Michał Dziendzikowski, Patryk Niedbała, Krzysztof Dragan,
Air Force Institute of Technology, Warsaw, Poland

STUDY OF INTERLAMINAR FRACTURE TOUGHNESS IN AIRCRAFT COMPOSITE MATERIALS

Nowakowski Dominik ¹, Baran Marta ¹, Lisiecki Janusz ¹, Kłysz Sylwester ^1,2

¹ Airworthiness Division, Air Force Institute of Technology, Warsaw, Poland
² Faculty of Technical Sciences, University of Warmia and Mazury in Olsztyn, Poland

DETERMINATION OF LIFE AND DEGRADATION MECHANISMS OF MATERIAL OPERATING UNDER FATIGUE-CREEP CONDITIONS

Anna Polnik ², Hubert Matysiak ², Zbigniew Pakieła ¹

¹ Warsaw University of Technology, Warsaw, Poland
² BH Poland Sp. z o.o., Warsaw, Poland

14 January 2022 (Friday)

IMPROVING STRENGTH AND STIFFNESS PERFORMANCE OF A GYROCOPTER COMPOSITE LANDING GEAR

Paweł Borkowski, Adam Dacko, Mirosław Rodzewicz
Faculty of Power and Aeronautical Engineering, Warsaw University of Technology,
Warsaw, Poland

COATING BASED ON ALUMINUM OXIDE MODIFIED BY POLYMER EVALUATED IN TERMS OF SUPERHYDROPHOBIC, ANTI-FOULING AND ANTI-ICING PROPERTIES

Klaudia Olkowicz ¹, Zofia Buczko ², Kamil Kowalczyk ¹, Barbara Nasiłowska ³

¹ Air Force Institute of Technology, Warsaw, Poland
² Łukasiewicz – Institute of Precision Mechanics, Warsaw, Poland
³ Institute of Optoelectronics, Military University of Technology, Warsaw, Poland

SENSITIVITY ANALYSIS OF THE NASGRO EQUATION BASED ON THE PZL-130 TC-II ORLIK TRAINER AIRCRAFT FULL SCALE FATIGUE TEST RESULTS

Piotr Reymer ^1,2, Andrzej Leski ^1,3, Marcin Kurdelski ²

¹ Military University of Technology, Warsaw, Poland
² Air Force Institute of Technology, Warsaw, Poland
³ Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

INVESTIGATIONS OF A DAMPER PROTOTYPE WITH A MAGNETORHEOLOGICAL ELASTOMER

Paweł Skalski, Paweł Grygorcewicz, Ryszard Harla, Jakub Piłczyński, Zbigniew Skorupka, Jacek Majewski, Arkadiusz Naumiuk
Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

DAMPING PERFORMANCE IMPROVEMENT OF TURBINE BLADING THROUGH ADVANTAGES OF ADDITIVE MANUFACTURING TECHNOLOGY

Grzegorz Moneta, Michal Fedasz, Michal Szmidt, Slawomir Cieslak, Wieslaw Krzymien
Lukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

DETERMINATION OF STRENGTH PARAMETERS OF THE COMPOSITE LAYER BASED ON REVERSE ENGINEERING AND FEM CALCULATIONS

Piotr Samoraj
Air Force Institute of Technology, Warsaw, Poland

MULTI-CRITERIA APPROACH TO NON-DESTRUCTIVE TESTING OF POLYMER COMPOSITES

Piotr Synaszko; Krzysztof Dragan; Norbert Pałka; Jarosław Ziemkiewicz
Airworthiness Division, Air Force Institute of Technology, Warsaw, Poland

DIFFRACTION METHODS IN ADDITIVE MANUFACTURING

Łukasz Pawliszak and Elżbieta Gadalińska
Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

VALIDATION OF FATIGUE ANALYSIS RESULTS AND SHORTENING TIME OF LANDING GEAR CERTIFICATION TEST BY KSTF METHOD

Alex Oudovikine
STEDAX Inc., Maple, Ontario CANADA