A fuel tank inert air preparation system for UAV

The fuel tank inert air preparation system (APS) for unmanned aerial vehicles (UAVs) is a relatively novel field. APS is essentially an air refrigeration cycle. APS can cool engine bleed air to a suitable temperature before being used by the on board inert gas generation system (OBIGGS). According to the characteristics of UAVs, an inert APS for fuel tank without ram air and pre-cooling system is proposed in this paper. The matching calculation process of APS is introduced in detail in this paper. Based on AMESim software, the performance simulation model of APS is built. The simulation results show that the APS can meet the performance demand of cooling air under the full flight envelope. The research results of this paper have certain guiding significance for the design work of the tank inert APS applicable to UAVs.

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Publication Details

Journal
IET conference proceedings.
Published
2025-01-01
DOI
https://doi.org/10.1049/icp.2024.2835
Citations
1
Primary Topic
Rocket and propulsion systems research
Type
article
Field-Weighted Citation Impact
4.99
Controls
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article

A fuel tank inert air preparation system for UAV

Shi‐Zhang Qiao, Chengyan Liu, Yueliang Lu, Ruirui Gou
1 citations
IET conference proceedings.
Rocket and propulsion systems research
4.99
article

A fuel tank inert air preparation system for UAV

Shi‐Zhang Qiao, Chengyan Liu, Yueliang Lu, Ruirui Gou
article en
1 citations

Abstract

The fuel tank inert air preparation system (APS) for unmanned aerial vehicles (UAVs) is a relatively novel field. APS is essentially an air refrigeration cycle. APS can cool engine bleed air to a suitable temperature before being used by the on board inert gas generation system (OBIGGS). According to the characteristics of UAVs, an inert APS for fuel tank without ram air and pre-cooling system is proposed in this paper. The matching calculation process of APS is introduced in detail in this paper. Based on AMESim software, the performance simulation model of APS is built. The simulation results show that the APS can meet the performance demand of cooling air under the full flight envelope. The research results of this paper have certain guiding significance for the design work of the tank inert APS applicable to UAVs.

IET conference proceedings.Vol. 2024(13)
Chinese People's Liberation Army (CN)
Affordable and clean energy
Openalex Percentile: Top 8%
Rocket and propulsion systems research
4.99
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