Detail aplikovaného výsledku

VTOL/Aircraft/Drone airbag

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

Originální název

VTOL/Aircraft/Drone airbag

Anglický název

VTOL/Aircraft/Drone airbag

Druh

Funkční vzorek

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.

Abstrakt anglicky

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

Airbag system; Impact mitigation

Klíčová slova anglicky

Airbag system; Impact mitigation

Licenční poplatek

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