Aerodynamic trip for a combustion system

Details Aerodynamic trip for a combustion system Aerodynamic trip for a combustion system

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/04 (2006.01) F23R 3/00 (2006.01)

Patent

CA 2542307

A apparatus and method for improving combustion by improving at least one of temperature distribution in the combustor, pressure distribution around the combustor and combustion noise level in the combustor, by redistributing air around the combustor to modify the structure of the air flow prior to entry into the combustor.

La présente invention se rapporte à un appareil et à un procédé permettant d'améliorer la combustion, et ce par l'amélioration d'au moins la répartition de la température dans la chambre de combustion, la répartition de la pression autour de la chambre de combustion, ou le niveau de bruit de la combustion dans la chambre de combustion, et par une nouvelle répartition de l'air autour de la chambre de combustion, cette dernière permettant de modifier la structure de l'écoulement d'air avant son entrée dans la chambre de combustion.

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