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  • The paper deals with computational tools used for a development of a new aircraft diesel engine for possible military use. The engine utilized potentials are discussed at the beginning of the paper. The cranktrain dynamics and fatigue of main components are solved by computational approaches. The presented methods are based on commercial tools like ANSYS or ADAMS, and also based on new software tools developed by authors during the development process. The computational models incorporate flexible bodies (based on FEM) and highly specialized software tools written in Fortran and Matlab. The developed computational dynamic models incorporates slide bearing, piston-liner and piston ring-liner models. The results include vibrations of the cranktrain and also fatigue analyses of cranktrain key parts like crankshafts or a propeller shaft. There are also presented design modifications enabling a reduction of vibrations and a fatigue increase of main parts.
  • The paper deals with computational tools used for a development of a new aircraft diesel engine for possible military use. The engine utilized potentials are discussed at the beginning of the paper. The cranktrain dynamics and fatigue of main components are solved by computational approaches. The presented methods are based on commercial tools like ANSYS or ADAMS, and also based on new software tools developed by authors during the development process. The computational models incorporate flexible bodies (based on FEM) and highly specialized software tools written in Fortran and Matlab. The developed computational dynamic models incorporates slide bearing, piston-liner and piston ring-liner models. The results include vibrations of the cranktrain and also fatigue analyses of cranktrain key parts like crankshafts or a propeller shaft. There are also presented design modifications enabling a reduction of vibrations and a fatigue increase of main parts. (en)
Title
  • Computational Tools Used For Aircraft Diesel Engine Development
  • Computational Tools Used For Aircraft Diesel Engine Development (en)
skos:prefLabel
  • Computational Tools Used For Aircraft Diesel Engine Development
  • Computational Tools Used For Aircraft Diesel Engine Development (en)
skos:notation
  • RIV/00216305:26210/11:PU94198!RIV12-MSM-26210___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • S
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 191522
http://linked.open...ai/riv/idVysledku
  • RIV/00216305:26210/11:PU94198
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Aircraft engine, crankshaft, fatigue, vibration, hydrodynamics, slide bearing (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [088EDDE7E90E]
http://linked.open...v/mistoKonaniAkce
  • Brno
http://linked.open...i/riv/mistoVydani
  • Brno
http://linked.open...i/riv/nazevZdroje
  • International Conference on Military Technologies 2011
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Ambróz, Richard
  • Drápal, Lubomír
  • Novotný, Pavel
  • Píštěk, Václav
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
number of pages
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  • Univerzita obrany
https://schema.org/isbn
  • 978-80-7231-787-5
http://localhost/t...ganizacniJednotka
  • 26210
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