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Statements

Subject Item
n2:RIV%2F00216305%3A26210%2F11%3APU94198%21RIV12-MSM-26210___
rdf:type
skos:Concept n19:Vysledek
dcterms:description
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.
dcterms:title
Computational Tools Used For Aircraft Diesel Engine Development Computational Tools Used For Aircraft Diesel Engine Development
skos:prefLabel
Computational Tools Used For Aircraft Diesel Engine Development Computational Tools Used For Aircraft Diesel Engine Development
skos:notation
RIV/00216305:26210/11:PU94198!RIV12-MSM-26210___
n19:predkladatel
n20:orjk%3A26210
n3:aktivita
n12:S
n3:aktivity
S
n3:dodaniDat
n14:2012
n3:domaciTvurceVysledku
n5:8272263 n5:2355221 n5:4714431 Ambróz, Richard
n3:druhVysledku
n9:D
n3:duvernostUdaju
n17:S
n3:entitaPredkladatele
n18:predkladatel
n3:idSjednocenehoVysledku
191522
n3:idVysledku
RIV/00216305:26210/11:PU94198
n3:jazykVysledku
n6:eng
n3:klicovaSlova
Aircraft engine, crankshaft, fatigue, vibration, hydrodynamics, slide bearing
n3:klicoveSlovo
n4:Aircraft%20engine n4:slide%20bearing n4:vibration n4:hydrodynamics n4:crankshaft n4:fatigue
n3:kontrolniKodProRIV
[088EDDE7E90E]
n3:mistoKonaniAkce
Brno
n3:mistoVydani
Brno
n3:nazevZdroje
International Conference on Military Technologies 2011
n3:obor
n11:JT
n3:pocetDomacichTvurcuVysledku
4
n3:pocetTvurcuVysledku
4
n3:rokUplatneniVysledku
n14:2011
n3:tvurceVysledku
Novotný, Pavel Drápal, Lubomír Píštěk, Václav Ambróz, Richard
n3:typAkce
n15:WRD
n3:zahajeniAkce
2011-05-10+02:00
s:numberOfPages
250
n7:hasPublisher
Univerzita obrany
n13:isbn
978-80-7231-787-5
n16:organizacniJednotka
26210