Abstract

The fire-extinguishing system is an indispensable fire-protection facility on the aircraft. In order to guide weight reduction of the aircraft’s fixed gas fire-extinguishing system by improving its release efficiency, so as to improve fuel economy and reduce carbon emissions, the influence of filling pressures and filling amounts on the release efficiency of gas extinguishing agent along pipelines were studied based on numerical simulations. The release process of the fire-extinguishing system was analyzed. The effects of the filling pressure and filling amount of Halon 1301 agent on the release characteristics, such as release time, mass flow rate, and gasification ratio, were studied. Results show that the release process can be divided into three major phases, which are firstly the initial rapid filling of the pipeline, secondly the concentrated release of the liquid extinguishing agent, and thirdly the gas ejection along the pipeline. The second phase can also be subdivided into two stages: the outflow of the liquid extinguishing agent from the bottle, and the release of the residual liquid extinguishing agent along the pipeline. The release characteristics of the fire-extinguishing agent were obviously affected by the filling pressures and filling amounts. When the filling pressure was relatively low (2.832 MPa), increasing the filling pressure can significantly increase the mass flow rate, shorten the release time, and reduce the gasification ratio of the extinguishing agent during the release processes. Under the same filling pressure, with the increase of the filling amount of the extinguishing agent, the release times and the gasification ratio showed a linear increase trend, while the average mass flow rates showed a linear decrease trend.

Highlights

  • Fire is one of the main factors that threaten aircraft safety

  • The typical curves of the volume fraction and mass flow rate of each constituent at the pipe outlet of the fire-extinguishing system are presented in Figure 5a,b, respectively

  • It can be clearly seen from these two figures that the release process of the extinguishing agent presents three obvious stages

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Summary

Introduction

Fire is one of the main factors that threaten aircraft safety. Since passengers cannot escape from the aircraft during flight, the fire-extinguishing system has become an indispensable fixed firefighting facility [1], and its fire-extinguishing performance is extremely demanding. In the context of global energy conservation and emission reduction, in order to promote the healthy and sustainable development of the aviation industry, many countries in the world have made various energy-conservation and emission-reduction plans for the aviation industry to save costs and improve operational efficiency and profitability [3,4]. This means that energy saving has become an important factor in aircraft design, and reducing the weight of the aircraft itself is one of the most effective means [5]. Studying the influence of filling conditions on the flow and release characteristics in the pipeline, which can provide a theoretical basis for the optimization design of aircraft fire-extinguishing system and aircraft weight reduction, has important practical value

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