Internal combustion engine with direct fuel injection
In an internal combustion engine with at least one cylinder in which a combustion space is delimited between a piston and a cylinder head, with a fuel injector having an outwardly opening injection nozzle arranged in the combustion space for injecting fuel in the form of a hollow cone into the combustion space, and a spark plug mounted in the cylinder head and having electrodes arranged outside the hollow fuel cone generated by the injection nozzle, into which the electrodes of the spark plug project, the cylinder has a bore diameter (D) dimensioned such that, at an ignition time point of the internal combustion engine, a ratio dmR/D of the mean diameter (dmR) of the fuel boundary vortex ( 10 ) to the cylinder bore diameter (D) is in a range of 0.08 to 0.2, in particular of 0.1 to 0.12.
1. An internal combustion engine ( 1 ), comprising
at least one cylinder ( 2 ) including a piston ( 3 ) and a cylinder head ( 5 ), defining therebetween a combustion space ( 4 ),
a spark plug ( 7 ) arranged in the cylinder bead so as to extend into the combustion space ( 4 ),
an outwardly opening injection nozzle ( 11 ) arranged in the cylinder head ( 5 ) and having nozzle opening projecting into the combustion space ( 4 ) for the injection of a fuel jet in the form of a hollow cone ( 8 ) into the combustion space ( 4 ),
the spark plug ( 7 ) being arranged outside the surface area ( 9 ) of the hollow fuel cone ( 8 ) generated by the injection nozzle, and having electrodes ( 12 ) projecting into a fuel boundary vortex ( 10 ), formed at the surface area ( 9 ) of the injected fuel jet,
said cylinder ( 2 ) having a cylinder bore ( 2 a ) with a diameter (D) dimensioned such that
at an ignition time point of the internal combustion engine ( 1 ) a ratio (dmR/D) of a mean diameter (dmR) of the fuel boundary vortex ( 10 ) to the bore diameter (D) is in a range of 0.08 to 0.2.
2. The internal combustion engine as claimed in claim 1 , wherein the ratio dmR/d is between 0.1 and 0.12.
3. The internal combustion engine as claimed in claim 1 , wherein, at the ignition time point, a ratio (dmR/aR) of the mean diameter (dmR) of the boundary vortex ( 10 ) to the boundary vortex center (aR) lies in a range of between 0.25 and 1.5.
4. The internal combustion engine as claimed in claim 3 , wherein the ratio dmR/aR is between 0.5 and 1.1.
5. The internal combustion engine as claimed in claim 1 , wherein the hollow fuel cone ( 8 ) has at the ignition time point a toroidal vortex diameter (dR), a ratio (dR/C) of the toroidal vortex diameter (dR) La the bore diameter (D) lying in a range of between 0.2 and 0.4.
6. The internal combustion engine as claimed in claim 5 , wherein the ratio dR/D is between 0.25 and 0.35.
7. The internal combustion engine as claimed in claim 1 , wherein the hollow fuel cone ( 8 ) has a maximum diameter (dS) of the fuel cloud and, at the ignition time point a ratio (dS/D) of the maximum diameter (dS) to the bore diameter (D) is in the range of 0.33 to 0.65.
8. The internal combustion engine as claimed in claim 7 , wherein the ratio dS/D is 0.45 to 0.55.
9. The internal combustion engine as claimed in claim 1 , wherein the piston ( 3 ) has a recess ( 3 a ) with a recess diameter (dm), at the ignition time point a ratio (dS/dm) of the maximum diameter (dS) of the fuel cloud to the recess diameter (dm) lying between 0.5 and 1.5.
10. The internal combustion engine as claimed in claim 9 , wherein the ratio dS/dm is between 0.8 and 1.2.
11. The internal combustion engine as claimed in claim 1 , wherein at the ignition time point, a ratio (ES/D) of the maximum, depth of penetration (ES) of the hollow fuel cone ( 8 ) to the bore diameter (D) amounts to 0.1 to 0.5.
12. The internal combustion engine as claimed in claim 11 , wherein the ratio ES/D is 0.2 to 0.3.