Gaseous fuel combustion apparatus for an internal combustion engine
Diesel-cycle engines are known to have greater power, torque and efficiency compared to Otto-cycle engines of like displacement. When the fuel is a gaseous fuel, such as natural gas, a pilot fuel (such as diesel) is normally required to assist with ignition in a gaseous fuelled Diesel-cycle engine. It would be advantageous to reduce the power, torque and efficiency gap between a Diesel-cycle engine and a gaseous fuelled Otto-cycle engine. A combustion apparatus for a gaseous fuelled internal combustion engine comprises a combustion chamber defined by a cylinder bore, a cylinder head and a piston reciprocating within the cylinder bore. A diameter of the cylinder bore is at least 90 mm and a ratio between the diameter and a stroke length of the piston is at most 0.95. There is at least one intake passage for delivering a charge to the combustion chamber, and at least one intake valve is configured in the cylinder head and cooperates with the intake passage to create a predominant tumble flow motion in the combustion chamber.
1. A combustion apparatus for a gaseous fuelled internal combustion engine comprising:
a combustion chamber defined by a cylinder bore, a cylinder head and a piston reciprocating within said cylinder bore, said piston comprising a concave piston bowl, a diameter of said cylinder bore is at least 90 mm and a ratio between said diameter to a stroke length of said piston is at most 0.95;
at least one intake passage for delivering a charge to said combustion chamber; and
at least one intake valve configured in said cylinder head and cooperating with said intake passage to create a predominant tumble flow motion in said combustion chamber.
2. The combustion apparatus of claim 1 , wherein said ratio is at least 0.75.
3. The combustion apparatus of claim 1 , wherein said diameter is less than or equal to 120 mm.
4. The combustion apparatus of claim 1 , further comprising an injection valve that introduces gaseous fuel upstream from said at least one intake valve.
5. The combustion apparatus of claim 1 , further comprising an ignition device disposed in said combustion chamber to assist with ignition of gaseous fuel and said charge.
6. The combustion apparatus of claim 5 , wherein said ignition device is a spark plug.
7. The combustion apparatus of claim 1 , wherein said tumble flow motion comprises an average tumble ratio between a range of 2 and 5.
8. The combustion apparatus of claim 1 , wherein a maximum engine speed of said internal combustion engine is 2700 revolutions per minute.
9. The combustion apparatus of claim 1 , wherein said cylinder bore and said piston define a swept volume between 0.8 liters and 2.5 liters.
10. The combustion apparatus of claim 1 , wherein each intake valve comprises a valve member and a valve seat, said valve seat comprising a valve seat angle between 25° and 35°.
11. The combustion apparatus of claim 10 , wherein
a difference between said valve seat angle and a port angle is between a range of −5° and 5°.
12. The combustion apparatus of claim 1 , wherein at least one of:
a compression ratio of said internal combustion engine is at least 11 to 1; and
said compression ratio is at most 15 to 1.
13. The combustion apparatus of claim 1 , further comprising an intake manifold, said intake manifold comprising:
a first distribution chamber in fluid communication with an air intake of said internal combustion engine;
a second distribution chamber in fluid communication with said at least one intake passage; and
a diffuser fluidly connecting said first and second distribution chambers.
14. The combustion apparatus of claim 4 , wherein said at least one intake passage is a first intake passage and a second intake passage and said at least one intake valve is a first intake valve and a second intake valve; further comprising a flow divider in fluid communication with said injection valve to receive gaseous fuel and with said first and second intake passages to deliver gaseous fuel received from said injection valve.
15. The combustion apparatus of claim 14 , wherein said flow divider comprises a body having a bore and a pair of conduits, said bore in fluid communication with said injection valve and each conduit in fluid communication with said bore and with a respective one of said first and second intake passages.
16. The combustion apparatus of claim 1 , wherein said internal combustion engine comprises an engine block and an intake manifold, and said at least one intake passage is a first intake passage and a second intake passage, further comprising six bolts arranged around said cylinder bore for retaining said cylinder head to said engine block, said first and second intake passages extending from said intake manifold along respective sides of one of said bolts towards said combustion chamber.
17. The combustion apparatus of claim 16 , further comprising an EGR valve for selectively supplying exhaust gases to said intake manifold.
18. The combustion apparatus of claim 17 , where said exhaust gases are cooled.
19. The combustion apparatus of claim 16 , further comprising a throttle valve for variably supplying air to said intake manifold.
20. The combustion apparatus of claim 19 , wherein said throttle valve is commanded to maintain a stoichiometric gaseous fuel-air mixture within a predetermined tolerance when said gaseous fueled internal combustion operates.