Detail publikace

IMPLEMENTATION STUDY OF A PASSIVE SAFETY FEATURE IN THE RESCUE SYSTEMS OF SMALL AIRCRAFTS

HÁJEK, T. GRIM, R. POPELA, R.

Originální název

IMPLEMENTATION STUDY OF A PASSIVE SAFETY FEATURE IN THE RESCUE SYSTEMS OF SMALL AIRCRAFTS

Typ

článek v časopise ve Web of Science, Jimp

Jazyk

angličtina

Originální abstrakt

Article History: Abstract. The aim of this paper is to evaluate the feasibility of implementation of a passive safety feature in the form of an under-fuselage airbag in the rescue systems of small aircraft. The paper presents a multidisciplinary approach for the viability of the implementation. It presents the development of mathematical model for airbag performance analysis. The model is validated against the experimental data to account for various simplifications. Validated mathematical model is used to design a full-scale airbag for the chosen airplane to perform in the designed range. Weight penalty for increased safety is determined.

Klíčová slova

parachute rescue; passive safety; airbag; impact attenuation; experimental validation; ultralight aircraft.

Autoři

HÁJEK, T.; GRIM, R.; POPELA, R.

Vydáno

13. 10. 2023

Nakladatel

VILNIUS GEDIMINAS TECH UNIV

Místo

VILNIUS

ISSN

1648-7788

Periodikum

AVIATION

Ročník

27

Číslo

3

Stát

Litevská republika

Strany od

187

Strany do

196

Strany počet

10

URL

Plný text v Digitální knihovně

BibTex

@article{BUT187871,
  author="Tomáš {Hájek} and Robert {Grim} and Robert {Popela}",
  title="IMPLEMENTATION STUDY OF A PASSIVE SAFETY FEATURE IN THE RESCUE SYSTEMS OF SMALL AIRCRAFTS",
  journal="AVIATION",
  year="2023",
  volume="27",
  number="3",
  pages="187--196",
  doi="10.3846/aviation.2023.19966",
  issn="1648-7788",
  url="https://journals.vilniustech.lt/index.php/Aviation/article/view/19966#"
}