Ducted combustion systems utilizing duct-exit tabs
A ducted combustion system is disclosed. The ducted combustion system includes a combustion chamber bound by a flame deck surface of a cylinder head of an internal combustion engine and by a piston top surface of a piston disposed within the internal combustion engine. The system includes a fuel injector including one or more orifices, the one or more orifices injecting fuel into the combustion chamber as at least one fuel jet. The system includes at least one duct disposed within the combustion chamber between the flame deck surface and the piston top surface, the at least one duct including one or more structural tabs proximate to an outlet of the at least one duct and being disposed such that the at least one fuel jet, at least partially, enters one of the at least one duct upon being injected into the combustion chamber.
1. A ducted combustion system, comprising:
a combustion chamber defined as an enclosure bound at a first end by a flame deck surface of a cylinder head of an internal combustion engine, and bound at a second end by a piston top surface of a piston disposed within the internal combustion engine;
a fuel injector in fluid connection with the combustion chamber and including one or more orifices opening from an injector tip of the fuel injector, the one or more orifices injecting fuel into the combustion chamber as at least one fuel jet; and
at least one duct disposed within the combustion chamber between the flame deck surface and the piston top surface, the at least one duct including one or more structural tabs proximate to an outlet of the at least one duct and being disposed such that the at least one fuel jet, at least partially, enters the at least one duct upon being injected into the combustion chamber.
2. The ducted combustion system of claim 1 , wherein the outlet of the at least one duct includes a tapered portion, which is tapered by converging towards a center line of the at least one duct.
3. The ducted combustion system of claim 2 , wherein at least one of the one or more structural tabs are, at least partially, defined by the tapered portion, tapered with the outlet of the at least one duct and, at least partially, tapered by converging an outer wall of the at least one duct towards a center line of the at least one duct.
4. The ducted combustion system of claim 2 , wherein an outer wall of the at least one duct converges in a fuel flow direction of the at least one fuel jet.
5. The ducted combustion system of claim 2 , wherein the tapered portion includes one or more of tapered tabs and tapered voids, proximate to the outlet of the at least one duct.
6. The ducted combustion system of claim 1 , wherein the one or more structural tabs are configured to inhibit ignition of the at least one fuel jet, upstream of the one or more structural tabs.
7. The ducted combustion system of claim 1 , wherein the one or more structural tabs are arranged circumferentially about a circumference of the outlet of the at least one duct.
8. The ducted combustion system of claim 1 , further comprising a plurality of valves located in the cylinder head, the plurality of valves including at least one air intake valve and at least one exhaust valve, and
wherein each of the at least one ducts is circumferentially disposed between two members of the plurality of valves.
9. An internal combustion engine, comprising:
an engine block having at least one cylinder bore;
a cylinder head having a flame deck surface disposed at one end of the cylinder bore;
a piston connected to a crankshaft and configured to reciprocate within the cylinder bore, the piston having a piston top surface facing the flame deck surface such that a combustion chamber is defined within the cylinder bore bound at a first end by the flame deck surface and at a second end by the piston top surface;
a fuel injector in fluid connection with the combustion chamber and including one or more orifices opening from an injector tip of the fuel injector, the one or more orifices injecting fuel into the combustion chamber as at least one fuel jet; and
at least one duct disposed within the combustion chamber between the flame deck and the piston top surface, the one or more including one or more structural tabs proximate to an outlet of the at least one duct and being disposed such that the at least one fuel jet at least partially enters the at least one duct upon being injected into the combustion chamber.
10. The internal combustion engine of claim 9 , wherein the outlet of the at least one duct includes a tapered portion, which is tapered by converging towards a center line of the at least one duct.
11. The internal combustion engine of claim 10 , wherein at least one of the one or more structural tabs are, at least partially, defined by the tapered portion, tapered with the outlet of the at least one duct and, at least partially, tapered by converging an outer wall of the at least one duct towards a center line of the at least one duct.
12. The internal combustion engine of claim 10 , wherein an outer wall of the at least one duct converges in a fuel flow direction of the at least one fuel jet.
13. The internal combustion engine of claim 9 , wherein the tapered portion includes one or both of a tapered tab and a tapered void, proximate to the outlet of the at least one duct.
14. The internal combustion engine of claim 9 , wherein the one or more structural tabs are configured to inhibit ignition of the at least one fuel jet, upstream of the one or more structural tabs.
15. The internal combustion engine of claim 9 , wherein the one or more structural tabs are arranged circumferentially about a circumference of the outlet of the at least one duct.
16. The internal combustion engine of claim 9 , further comprising a plurality of valves located in the cylinder head, the plurality of valves including at least one air intake valve and at least one exhaust valve, and
wherein each of the at least one ducts is circumferentially disposed between two members of the plurality of valves.