scholarly journals Numerical assessment for aircraft cargo compartment fire suppression system safety

2021 ◽  
pp. 073490412110032
Author(s):  
Yifang Xiong ◽  
Michail Diakostefanis ◽  
Akhil Dinesh ◽  
Suresh Sampath ◽  
Theoklis Nikolaidis

Fire on board an aircraft cargo compartment can lead to catastrophic consequences. Therefore, fire safety is one of the most important considerations during aircraft design and certification. Conventionally, Halon-based agents were used for fire suppression in such cases. However, an international agreement under the Montreal Protocol of 1994 banned further production of Halon and several other halocarbons considered harmful to the environment. There is therefore a requirement for new suppression agents, along with suitable system design and certification. This article aims to describe the creation of a mechanism to validate a preliminary design for fire suppression systems using Computational Fluid Dynamics and provide further guidance for fire suppression experiments in aircraft cargo compartments. Investigations were performed for the surface burning fire, one of the fire testing scenarios specified in the Minimum Performance Standard, using the numerical code Fire Dynamics Simulator. This study investigated the use and performance of nitrogen, a potential replacement for Halon 1301, as an environmentally friendly agent for cargo fire suppression. Benchmark fires using the pyrolysis model and fire design model were built for the surface-burning fire scenario. Compared with experiment results, the two Computational Fluid Dynamics models captured the suppression process with high accuracy and displayed similar temperature and gas concentration profiles. Fire consequences in response to system uncertainties were studied using fire curves with various fire growth rates. The results suggested that using nitrogen as a fire suppression agent could achieve a lower post-suppression temperature compared to a Halon 1301-based system. It can therefore be considered as a potential candidate for aircraft cargo fire suppression. Such work will feed directly into system safety assessments during the early design stages, where analyses must precede testing. Future work proposed for the application of this model can be extended to other fire scenarios such as buildings, shipping, and surface transport vehicles.

2021 ◽  
pp. 073490412110344
Author(s):  
Michail Diakostefanis ◽  
Suresh Sampath ◽  
Akhil Dinesh ◽  
Rainer Beuermann ◽  
Areti Malkogianni

Fire suppression systems in cargo compartments are a certification requirement for commercial aircraft safety. Halon production was banned and usage ends in 2040 according to Montreal Protocol for environmental reasons. This necessitates an alternative environmentally friendly agent. Quantitative analysis of nitrogen as agent established suitability of the suppression system. The Minimum Performance Standards specifies the qualification procedure of an agent through four scenarios – bulk load; containerised load; surface burning; and aerosol can explosion. Empirical sources from Airbus, independent computational fluid dynamics studies and small-scale cup-burner tests indicate suitability of nitrogen specific to aircraft cargo fire suppression. The nitrogen delivery system and the experimental apparatus are presented. Extensive commissioning tests verified instrumentation reliability. All the four scenarios were conducted at Cranfield University, in a replica of a wide-body aircraft cargo compartment. In a reduced oxygen environment (11%) obtained with nitrogen discharge, the aerosol can explosion tests were performed without any evidence of explosion or pressure increase beyond the expected baseline value. The surface burning scenario was completed successfully and passed the Minimum Performance Standard criteria. The maximum average temperature was found to be 220°C (limit – 293°C). All the scenarios passed the Minimum Performance Standard criteria for indicating successful prevention of Class B fire re-ignition. Similarly, the containerised and bulk-load scenarios obtained results that passed the Minimum Performance Standard criteria for successfully maintaining continued fire suppression for a specified period of time. The maximum average temperature in containerised-load fire scenario was found to be 210°C (limit – 343°C) and in bulk-load scenario was 255°C (limit – 377°C). Additional qualification criteria and system design are presented in this article according to the Minimum Performance Standard format. This work can be extended to introduce standard testing for safety critical systems, such as engine bay and lithium-ion fires.


Author(s):  
Sławomir Dykas ◽  
Mirosław Majkut ◽  
Krystian Smołka ◽  
Michał Strozik

This study presents experimental and numerical testing of the steam condensing flow through a linear blade cascade made of blades of a 200 MW steam turbine last stage stator. The tests were carried out on an in-house laboratory stand and using an in-house numerical code modelling the water vapour flow with homo- and heterogeneous condensation. Additionally, this paper presents a comparison of calculations of a flow field modelled by means of a single-fluid model using both an in-house computational fluid dynamics code and the commercial Ansys CFX v16.2 software package. The aim of the research was to identify difficulties involved by comparing the numerical modelling results with the experimental data for a linear blade cascade. The experimental results, which are very well supplemented by those obtained from numerical computations, may be used to validate computational fluid dynamics codes.


Author(s):  
Francisco Lamas ◽  
Antonio Carlos Fernandes

The main objective of the present work is to propose a methodology to evaluate the Directional Stability index of a displacement ship using Computational Fluid Dynamics to evaluate its linear hydrodynamic derivatives. The first step is the review of the ship’s equations of motion, followed by the formulation of the straight-line stability problem, which depends basically on the evaluation of the ship’s linear hydrodynamic derivatives. After this, the experimental methods that are normally used to evaluate these characteristics during ship design are presented, since they will be simulated in a numerical environment. Having reviewed the common experimental methods applied to determine the straight-line stability of a ship, the numerical code used to evaluate it in this work is presented, in order to show how the physical constitution of the experimental apparatus is adapted to a computational environment. Together with this will be presented the KVLCC2 model used or the computations, together with the numerical mesh where the computations were carried out. With this, it becomes possible to show the numerical results obtained in this work. The last part of this paper consists in comparing the numerical results obtained in the step before with the Clarke statistical correlations in order to assess or not the accuracy of the methodology proposed.


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