Apparatus and method for controlling pilot injection

F - Mech Eng,Light,Heat,Weapons – 02 – D

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F02D 41/40 (2006.01)

Patent

CA 2618514

In certain embodiments, there is provided a method of operating a turbocharged system including injecting a first quantity of fuel into an engine cylinder at a first predetermined time during a second half of a compression stroke before a piston of the engine cylinder reaches top dead center of the compression stroke. The method further includes injecting a second quantity of fuel into the engine cylinder at a second predetermined time after the first predetermined time when the piston is advanced by a predetermined advance value before the piston reaches the top dead center of the compression stroke.

L'invention porte dans certaines exécutions sur une méthode d'utilisation d'un système à turbocompresseur consistant: à injecter une première quantité de carburant dans un cylindre à un premier instant prédéterminé pendant la deuxième moitié de la course de compression et avant que le piston n'atteigne le point mort haut;puis à injecter une deuxième quantité de carburant dans le cylindre à un deuxième instant prédéterminé suivant le premier instant prédéterminé lorsque le piston a avancé d'une valeur prédéterminée et avant que le piston n'atteigne le point mort haut.

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