Analysis of Landing Buffer Characteristics of Unmanned Airdrop Rescue Vehicle

Xin Zhang

doi:10.54097/rxvm3q06

Authors

Xin Zhang

DOI:

https://doi.org/10.54097/rxvm3q06

Keywords:

Aerial vehicle; Airbag buffer; The finite element method.

Abstract

Taking an unmanned airdrop rescue vehicle as the research object, in order to reduce the impact overload of the airdrop landing, the exhaust type airbag buffer mode suitable for the airdrop vehicle is determined. Firstly, the scheme of the airdrop system is designed. According to the basic assumption of the airdrop process, the thermodynamic analysis model of the buffer bag is derived and the parameters are designed. Secondly, the finite element model of airdrop system with airbag buffer is established based on the airbag finite element algorithm (CV method). Finally, the buffering effect is evaluated by analyzing the change of tire force. The calculation results show that the system overload is reduced from 35g to 22g by using airbag buffer, and the buffer effect is obvious.

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