Abstract
This paper examines the architecture and component characteristics of the fuel tank inerting system in civil aircraft, as well as the loads it experiences. The study further investigates the strength of the system through a finite element model analysis by using CAEPIPE and explores the design of the bracket supporting the inerting system. The paper aims to contribute to the field by providing a detailed analysis of the fuel tank inerting system and its components, as well as offering insights into the system’s strength and design considerations.
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