Detail produktu

VTOL/Aircraft/Drone airbag

Popela R. Grim R. Bábovka M. Dorotka M. Moser M.

Anglický název

VTOL/Aircraft/Drone airbag

Typ

Funkční vzorek

Jazyk

en

Originální abstrakt

The functional prototype of an under-fuselage airbag impact-attenuation system was developed to reduce landing impact loads through a multi-chamber airbag structure ensuring pressure distribution and structural stability during compression. The system consists of two main subsystems: an inflation system providing controlled airbag deployment, and a multi-chamber airbag structural assembly designed for efficient impact energy absorption.

Klíčová slova anglicky

Airbag system; Impact mitigation

Datum vzniku

2025-12-18

BIBTEX


@misc{BUT201012,
  author="Robert {Popela} and Robert {Grim} and  {} and  {} and  {}",
  title="VTOL/Aircraft/Drone airbag",
  year="2025",
  note="Functioning sample"
}