Detail publikace

Crashworthiness of Aircraft Seat

PLHAL, M. ŠPLÍCHAL, J.

Originální název

Crashworthiness of Aircraft Seat

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

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.First 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 recommendations of regulations for max. accelerations imposed on the human body.

Klíčová slova

Crashworthiness, Aircraft, Dummy, FEM

Autoři

PLHAL, M.; ŠPLÍCHAL, J.

Rok RIV

2006

Vydáno

4. 9. 2006

Nakladatel

Optimage Ltd., Edinburgh, UK

Místo

HAMBURG, GERMANY

ISBN

0-9533991-7-6

Kniha

CD PROCEEDINGS

Strany od

1

Strany do

4

Strany počet

4

BibTex

@inproceedings{BUT19577,
  author="Martin {Plhal} and Jan {Šplíchal}",
  title="Crashworthiness of Aircraft Seat",
  booktitle="CD PROCEEDINGS",
  year="2006",
  pages="1--4",
  publisher="Optimage Ltd., Edinburgh, UK",
  address="HAMBURG, GERMANY",
  isbn="0-9533991-7-6"
}