Method of operating an internal combustion engine with a dual fuel injection system
View Patent ↗In a method of operating an internal combustion engine by supplying a gaseous fuel from a gaseous fuel tank to a combustion air feed line in which a compressor is arranged to the engine, part of the gaseous fuel is added to the combustion air feed line upstream of the compressor so as to form an intense pre-mixture with the air in the compressor and additional fuel is added to the gas/air pre-mixture downstream of the compressor.
1. A method of operating a gaseous fuel internal combustion engine ( 1 ) having a cylinder bank ( 10 ) with at least one cylinder ( 8 ) a manifold ( 6 ) connected to each cylinder bank for conducting combustion air to each cylinder ( 8 ), a combustion air feed line ( 2 ) connected to the manifold ( 6 ) and a compressor ( 3 ) disposed in the combustion air feed line ( 2 ) for compressing the combustion air supplied to the engine ( 1 ), the method comprising the steps of introducing gaseous fuel from a gaseous fuel tank in an amount smaller than required for combustion with the combustion air in the internal combustion engine to the combustion air in the feed line ( 2 ) upstream of the compressor ( 3 ) for a thorough mixture in the compressor with the combustion air, and introducing an additional amount of fuel to the combustion air-gaseous fuel mixture downstream of the compressor ( 3 ) and upstream of the cylinders ( 8 ) of the internal combustion engine ( 1 ) the relative fuel amounts being determined as a function of the rotational speed of the compressor ( 3 ).
2. The method according to claim 1 , wherein liquid fuel can be injected into the combustion air downstream of the compressor 3 at least in addition to the gaseous fuel supplied to the feed line ( 2 ) upstream of the compressor ( 3 ) so that engine operation can optionally at least be supported by liquid fuel taken from a liquid fuel tank which is separate from the gaseous fuel tank.
3. The method according to claim 2 , wherein engine operation is switched between a gaseous fuel operating mode and a liquid fuel operating mode as a function of a fuel amount left in the gaseous fuel tank.
4. The method according to claim 3 , wherein at least one liquid fuel injector ( 7 ) is provided in the feed pipe ( 2 ) upstream of the manifold branches and the liquid fuel is injected into the combustion air when switching to a liquid fuel operating mode.
5. The method as claimed in claim 1 , wherein the cylinder bank includes a plurality of cylinders and the manifold includes branches leading to the individual cylinders ( 8 ) and the additional amount of fuel is injected into the branches leading to the individual cylinders ( 8 ) so that a specific individual gas/air ratio is set for each cylinder ( 8 ).
6. The method according to claim 5 , wherein a specific desired gas/air ratio is determined as a function of the engine load and the amount of additional fuel introduced into the manifold branches is controlled so as to obtain the desired gas/air ratio.
7. The method as claimed in claim 1 , wherein the additional amount of fuel is introduced into the feed line ( 2 ) upstream of any branch ducts of the manifold ( 6 ).
8. The method according to claim 1 , wherein the quantity of gaseous fuel introduced into the feed line ( 2 ) upstream of the compressor ( 3 ) is determined also as a function of engine load.