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Description
  • Tento článek se zabývá dynamickým výpočtem letecké sedačky dle požadavků předpisu FAR/JAR 23.562 (b) s využitím figuríny pro stanovení zatížení působící na osobu sedící na sedadle během to toho zatížení .Model byl vytvořen v systému systému MSC.Patran a jako řešič byl použit systém MSC.Dytran v kterém je figurína integrována. V průběhu výpočtu byly sledovány zrychlení a rychlosti v místech potřebných k vyhodnocení tohoto výpočtu. (cs)
  • The dynamic analysis will be demonstrated on the example of a seat for a small 4-seater GA airplane. The airplane is designed according to JAR/FAR-23 regulations. The geometry was subsequently transferred to the MSC.PATRAN preprocessor. This allowed creation of the finite element (FEM) model of the seat. FEM model of the dummy (simulating a pilot) is integrated in MSC.PATRAN/DYTRAN package and the dummy is generated by GEBOD application. The dummy is composed of 2 main parts - ellipsoids and skin.Firstt part is made from RIGID ellipsoids. Ellipsoids are connected together using linkages that simulate articulations. This part of the dummy is responsible for the behavior of the dummy. Second part is the dummy's skin, using 2D elements. Velocities and accelerations in chosen points on the dummy were monitored during computation. Points were chosen where necessary with respect to monitoring of max. accelerations. Such points are in the CG of occupant's head, chest and pelvis. Results were compared with r
  • The dynamic analysis will be demonstrated on the example of a seat for a small 4-seater GA airplane. The airplane is designed according to JAR/FAR-23 regulations. The geometry was subsequently transferred to the MSC.PATRAN preprocessor. This allowed creation of the finite element (FEM) model of the seat. FEM model of the dummy (simulating a pilot) is integrated in MSC.PATRAN/DYTRAN package and the dummy is generated by GEBOD application. The dummy is composed of 2 main parts - ellipsoids and skin.Firstt part is made from RIGID ellipsoids. Ellipsoids are connected together using linkages that simulate articulations. This part of the dummy is responsible for the behavior of the dummy. Second part is the dummy's skin, using 2D elements. Velocities and accelerations in chosen points on the dummy were monitored during computation. Points were chosen where necessary with respect to monitoring of max. accelerations. Such points are in the CG of occupant's head, chest and pelvis. Results were compared with r (en)
Title
  • Crashworthiness of Aircraft Seat
  • Crashworthiness of Aircraft Seat (en)
  • Dynamický výpočet pilotní sedačky (cs)
skos:prefLabel
  • Crashworthiness of Aircraft Seat
  • Crashworthiness of Aircraft Seat (en)
  • Dynamický výpočet pilotní sedačky (cs)
skos:notation
  • RIV/00216305:26210/06:PU62719!RIV06-MSM-26210___
http://linked.open.../vavai/riv/strany
  • 1-4
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(1M0501)
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
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http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
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  • 469972
http://linked.open...ai/riv/idVysledku
  • RIV/00216305:26210/06:PU62719
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Crashworthiness, Aircraft, Dummy, FEM (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [56F4D5DB31D3]
http://linked.open...v/mistoKonaniAkce
  • Hamburg
http://linked.open...i/riv/mistoVydani
  • HAMBURG, GERMANY
http://linked.open...i/riv/nazevZdroje
  • CD PROCEEDINGS
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http://linked.open...vavai/riv/projekt
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Šplíchal, Jan
  • Plhal, Martin
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
number of pages
http://purl.org/ne...btex#hasPublisher
  • Optimage Ltd., Edinburgh, UK
https://schema.org/isbn
  • 0-9533991-7-6
http://localhost/t...ganizacniJednotka
  • 26210
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