Abstract:
It is widely known in the aviation community that the use of Halon1301 as fire
suppression agent has been banned as it presents high ozone depleting
potential. This fact dictates that there is a necessity for fire suppression systems
replacement on all existing aircraft within a limited timeframe. So far, Nitrogen
(IG-100) was proven to be the most promising replacement agent for future
aviation. The present research project attempts to assess the handling,
performance and installation of a Nitrogen (IG-100) fire suppression system on
aircraft cargo in order to accelerate the transition to Halon-free systems. The
research has been conducted under the umbrella of the EU Clean Sky 2 (CS2)
“Environmentally Friendly Fire Suppression System for Cargo using Innovative
Green Technology” (EFFICIENT) project.
The methods used to achieve the project targets are based on analytical and
numerical 3D-CFD modelling as well as both in-house and public domain
experimental information of respective cargo fire suppression systems.
Additionally, they are aligned with FAA requirements and follow the Minimum
Performance Standard (MPS) required for testing and certification. The Nitrogen
(IG-100) system design space exploration focused on the examination of
exchange rates between parameters such as the number and location of
discharge nozzles and ventilation ports with the system effectiveness, operability
and safety. The resulted fire suppression system design was also used for the
development of the detailed design and operation strategy of the Cranfield in-
house test rig as well as the experimental testing and procedures, the risk
assessment and installation cost estimation.
The outcomes of CFD simulations presented satisfactory agreement with the
theoretically expected analytical calculations. Additionally, they were validated
against the experimental data coming from the above mentioned Cranfield based
test rig. The data regarded No-Fire and Open Surface Liquid Fire tests using Jet-
A fuel. Both CFD and experiments showed that system achieved the desired
average Oxygen concentration within 60 seconds discharge, while maintaining it
below 16% for more than 45 minutes, satisfying the FAA MPS. Additionally, the
average overpressure level inside the compartment remains within limits both
during and after agent discharge. Finally, based on their comparison, numerical
model adaptations and calibration are suggested in order to improve modelling
fidelity and simulation accuracy.
The proposed Nitrogen based design suggests minimum modifications to the
already existing Halon1301 based systems in order to accelerate the
replacement process. Furthermore, the system provides ease in handling and
operation with capabilities of minimising Nitrogen wastage by varying the agent
mass used based on the level of the cargo load and the nature of its content.
Finally, recommendations for future improvements regarding the system
response time, the fire protection time, the weight and complexity are included.