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The effect of the coating process thermal cycle on mechanical properties of AA6061-T6 used for load-carrying elements of a space instrument: a case study

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EN
Abstrakty
EN
Components used for the structure of the GLObal Solar Wind Structure experiment in the NASA Interstellar Mapping and Acceleration Probe space mission, made of AA6061-T6 alloy, are subjected to the coating process, where the temperature affects its mechanical properties. This paper aims to examine the impact of the coating thermal cycle on the mechanical properties of AA6061-T6 alloy, which is the load-carrying material in a spaceborne instrument. As a part of the manufacturing process, the parts made of AA6061-T6 are subjected to a coating process at a temperature of about 220◦C for a time longer than 1 hour. This treatment modifies the mechanical properties of the alloy. To evaluate the consequences of this change for spaceborne components, mechanical testing, and numerical simulation were conducted. It was found that as a result of the coating process, the reduction in AA6061-T6 yield strength is about 16%, which entails a decrease in the margins of safety by 25% at its maximum.
Rocznik
Strony
art. no. e150338
Opis fizyczny
Bibliogr. 20 poz., rys., tab.
Twórcy
  • Space Research Center, Polish Academy of Sciences (CBK PAN), Warsaw, Poland
  • Department of Fatigue and Machine Design, Faculty of Mechanical Engineering, Military University of Technology, Warsaw, Poland
  • Space Research Center, Polish Academy of Sciences (CBK PAN), Warsaw, Poland
  • Space Research Center, Polish Academy of Sciences (CBK PAN), Warsaw, Poland
  • Space Research Center, Polish Academy of Sciences (CBK PAN), Warsaw, Poland
  • Space Research Center, Polish Academy of Sciences (CBK PAN), Warsaw, Poland
  • Space Research Center, Polish Academy of Sciences (CBK PAN), Warsaw, Poland
  • Space Research Center, Polish Academy of Sciences (CBK PAN), Warsaw, Poland
Bibliografia
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  • [6] K. Farrell, “Materials Selection for the HFIR Cold Neutron Source; TOPICAL,” Oak Ridge National Lab. (ORNL), Oak Ridge, United States, Aug. 2001.
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  • [12] F. Ozturk, A. Sisman, S. Toros, S. Kilic, and R.C. Picu, “Influence of aging treatment on mechanical properties of 6061 aluminum alloy,” Mater. Des., vol. 31, no. 2, pp. 972–975, Feb. 2010, doi: 10.1016/j.matdes.2009.08.017.
  • [13] G.D. Jiang, Y.H. Cai, C. Qiu, W.W. Zhang, and D.T. Zhang, “Effect of overaging on the microstructure, mechanical properties and crashing performance of thin-walled Al–Mg–Si–Cu alloy profiles,” J. Mater. Res. Technol., vol. 21, pp. 3074–3085, Nov. 2022, doi: 10.1016/j.jmrt.2022.10.137.
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  • [17] S. Hussein, M. Al-Shammari, A. Takhakh, and M. Al-Waily, “Effect of Heat Treatment on Mechanical and Vibration Properties for 6061 and 2024 Aluminum Alloys,” J. Mech. Eng. Res. Develop., vol. 43, pp. 48–66, Jan. 2020.
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Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-b735117e-1fd3-456f-b8d1-0c6de9952313
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