Líneas de Investigación
finsiguiente

MICRO-GAS TURBINE
COMBUSTION CHAMBERS

Small gas turbines find their application in several fields of interest: as auxiliary energy units for planes, in hybrid vehicles, in the internal combustion engine turbocharging system, as a power source in the distributed energy market, etc. An essential part of the gas turbine is the combustion chamber. LAM has developed a research line related to the micro-gas turbines combustion chamber experimental design and overhaul.


Micro-combustion chamber
Micro-combustion chamber
Highslide JS
Micro-combustion chamber and flame tube
Highslide JS
Primary pressure loss during combustion
Highslide JS
Secondary pressure loss during combustion

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