During this first period of work, 2 designs of injectors were defined by GDTech in order to reach the objectives of swirls and cross sections given by Safran. These objectives are directly related to NOx and particulate emissions. To validate the two designs of injector, GDTech performed aerodynamic simulations of the injection systems in the test bed configuration at the test operating points. At least, reactive calculations were carried out by GDTech to check the stability of the flame and to anticipate the temperatures to which the bench will be exposed to during the tests.
As the designs of the injectors were validated by the results of the simulations, those were produced by additive manufacturing.
Concerning the experimental part, INSA Rouen has mainly fitted out the HERON test bench to integrate the injectors, to cool the combustion chamber. Moreover, INSA Rouen has set up on another bench the methodology of optical measurements which will be applied for the LOOPS project. The first tests will take place in January 2022.
CERFACS started to prepare numerical models but the main work will occur once the test results will be available in 2022.
During the second period of work, the experimental investigations of the injectors were carried out. At first, INSA Rouen performed the analysis of the global performances of the 2 injections systems to get the flame structure and first emission index of NO. Then INSA Rouen performed the detailed experimental investigations with laser diagnostics and get measurements of OH, soot, NO, kerosen, mean velocity for different operating points. In parallel to the tests, the CERFACS has started the development of numerical models for prediction of NOw and soot. For that purpose, Large Eddy simulations (LES) were carried out while new numerical tools were implemented and validated against the experimental results. The non reactive simulations for different operating conditions fit well with the experimental results so the fisrt reactive simulations could be performed.
During the 3rd period, INSA Rouen carried out measurements characterising the spray from the 2 injectors for several operational points and finalized the analyses of the laser measurements to determine the concentration of the various. Cerfacs continued to develop NOx and soot emission models and performed the LES simulations of the injector in the test combustion chamber to compare the numerical and the experimental results. This allowed to validate the flow simulation in the non-reacting case and obtain first results on NOx and soot emissions. GDTech demonstrated the CFD tools capabilities and the new injector performances on a full scale spinning combustor of Safran Helicopter Engines. The simulations carried out include : modification of the combustor drilling map , combustion behavior and the wall temperature distribution, Lean Blow-Off (LBO) simulations , NOx and soot emissions.
The LOOPS project enabled to design two injectors, one low soot injector dedicated to the turboshaft market and one low NOx and Low soot injector commercialy dedicated to the turbo propeller market. The decrease of Nox and soot emissions has been demonstrated by tests and simulation results. The key combustion characteristics and the pollutant concentration as NOX and soot have been measured inside the combustion chamber at high pressure level and the LES models and simulations have been improved.
All this work resulting from the LOOPS project will enable the Topic Manager Safran Helicopter Engine to ensure the exploitation for its future engine developments:
• The elaboration of an unprecedented experimental database regrouping the key combustion characteristics (position of the flame front, flame structure, velocity field, fuel/air distribution, fuel droplet distribution, temperature, size droplet distribution, temperature NO and soot concentration) inside innovative spinning combustion system.
• the development of a LES numerical tool that will help to develop low-emission spinning combustion technologies.
• The transfer of experimental data and numerical tools to SAFRAN Helicopter Engines. This action will actively participate to the further improvement and to the up or downscale of the spinning combustion technology.
• The extension in the next future of the low-emission spinning combustion technology to a wide range of SAFRAN engines
