ОЦІНКА ВПЛИВУ ПАРЕМЕТРІВ ПРУЖНОГО ПІЛОННОГО ПІДВІСУ ДВИГУНА НА ДИНАМІЧНІ НАВАНТАЖЕННЯ

Authors

  • В. В. Сухов National Technical University of Ukraine «Kyiv Polytechnic Institute», Kyiv, Ukraine
  • А. Р. Мєсьянінов National Technical University of Ukraine «Kyiv Polytechnic Institute», Kyiv, Ukraine

DOI:

https://doi.org/10.20535/2305-9001.2011.62.70655

Keywords:

The article examines the impact of the layout of the wing and engine pylon suspension on dynamic loading transport aircraft

Abstract

To simulate the elastic vibration aircraft structuret in flight using girder schematization. Placing the engine under the wing on pylons suspension puts additional demands on the control of the adequacy of schematization girder construction. The article examines the impact of the layout of the wing and engine pylon suspension on dynamic loading transport aircraft. As a method of analysis used a method of constructing the transfer functions of congestion in the center of gravity of the engine.

Author Biographies

В. В. Сухов, National Technical University of Ukraine «Kyiv Polytechnic Institute», Kyiv

д-р.техн.наук

А. Р. Мєсьянінов, National Technical University of Ukraine «Kyiv Polytechnic Institute», Kyiv

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Published

2016-06-06

Issue

No. 62 (2011)

Section

Original study

License

The authors reserve the right to authorship of the work and pass the journal right of first publication of this work is licensed under a Creative Commons Attribution License, which allows others to freely distribute the work published with reference to the authors of the original work and the first publication of this magazine.