Combustion chamber geometry
Diesel engines modified to be fueled with gaseous fuels experience problems with knocking and pre-ignition, limiting the compression ratio and efficiency of the engine. A new combustion chamber for a gaseous fueled internal combustion engine, in which the combustion chamber is defined by a cylinder head, a bore in a cylinder block and a piston reciprocating in the bore, comprises a piston portion of the combustion chamber defined by a recessed shape in a piston crown; and a head portion of the combustion chamber defined by a recessed surface in the cylinder head. A ratio between the piston portion of combustion chamber volume and the head portion of combustion chamber volume is in a range of 0.7 to 1.3.
1. A combustion chamber of a gaseous fueled internal combustion engine, the combustion chamber defined by a cylinder head, a bore in a cylinder block and a piston reciprocating in the bore, the combustion chamber comprising:
a piston portion of the combustion chamber of said gaseous fueled internal combustion engine defined by a recessed shape in a piston crown;
a head portion of the combustion chamber of said gaseous fueled internal combustion engine defined by a recessed surface in the cylinder head; and
a positive ignition device for igniting a gaseous fuel;
wherein the gaseous fueled internal combustion engine operates at a stoichiometric air-fuel ratio and a ratio between the piston portion of combustion chamber volume and the head portion of combustion chamber volume is in a range of 0.7 to 1.3; and wherein the recessed shape in said piston crown is bounded by a piston top land, and an annular upper surface of said piston top land cooperatively faces an annular outer periphery of said head portion along a plane substantially perpendicular to said longitudinal cylinder axis at top dead center whereby said piston portion remains substantially below said plane at top dead center and said head portion remains substantially above said plane at top dead center.
2. The combustion chamber of claim 1 , wherein the head portion of the combustion chamber is shaped as a hip roof.
3. The combustion chamber of claim 2 , wherein the hip roof is rectangular and comprises hip ends each having a curved concave contour.
4. The combustion chamber of claim 2 , wherein the hip roof comprises sloping faces that form an angle with a plane perpendicular to a longitudinal cylinder axis between a range of 8° and 12°.
5. The combustion chamber of claim 1 , wherein the recessed shape in the piston crown is a bowl having a curved concave contour.
6. The combustion chamber of claim 1 , wherein the ratio is in a range of 0.765 to 0.945.
7. The combustion chamber of claim 1 , wherein the positive ignition device is centrally located in the combustion chamber.
8. The combustion chamber of claim 1 , wherein the combustion chamber cooperates with an air intake passage to form a tumble flow of an intake charge.
9. The combustion chamber of claim 1 , wherein a bore to stroke ratio between a diameter of the cylinder bore and a stroke of the piston is in a range of 0.75 and 0.95.
10. The combustion chamber of claim 1 , wherein the piston portion of combustion chamber volume is in a range of 40 cc to 53 cc.
11. The combustion chamber of claim 1 , wherein the head portion of combustion chamber volume is in a range of 53 cc to 56 cc.
12. The combustion chamber of claim 1 , wherein a compression ratio is in a range of 11 to 1 (11:1) and 15 to 1 (15:1).
13. The combustion chamber of claim 1 , wherein the internal combustion engine is modified from a Diesel internal combustion engine.
14. A combustion chamber of a spark ignited, gaseous fueled internal combustion engine, the combustion chamber defined by a cylinder head, a bore in a cylinder block and a piston reciprocating in the bore, the combustion chamber fluidly communicating with an air intake passage and an exhaust passage, the combustion chamber comprising:
a concave bowl in a crown of the piston;
a rectangular hip roof in the cylinder head; and
a positive ignition device for igniting a gaseous fuel;
wherein the combustion chamber of said gaseous fueled internal combustion engine cooperates with the air intake passage to form a tumble flow in the combustion chamber;
wherein a compression ratio is in a range of 11 to 1 (11:1) and 15 to 1 (15:1); a ratio between a first portion of combustion chamber volume in the piston and a second portion of the combustion chamber volume in the cylinder head is in a range of 0.7 to 1.3; and wherein the concave bowl in said piston crown is bounded by a piston top land, and an annular upper surface of said piston top land cooperatively faces an annular outer periphery of said head portion along a plane substantially perpendicular to said longitudinal cylinder axis at top dead center whereby said piston portion remains substantially below said plane at top dead center and said head portion remains substantially above said plane at top dead center.
15. The combustion chamber of claim 14 , wherein the rectangular hip roof comprises hip ends having a curved concave contour.
16. The combustion chamber of claim 14 , wherein the concave bowl is spherical.
17. A combustion chamber of a gaseous fueled internal combustion engine, the combustion chamber defined by a cylinder head, a bore in a cylinder block and a piston reciprocating in the bore, the combustion chamber comprising:
a piston portion of the combustion chamber of said gaseous fueled internal combustion engine defined by a recessed shape in a piston crown; and
a head portion of the combustion chamber of said gaseous fueled internal combustion engine defined by a recessed surface in the cylinder head shaped as a hip roof having sloping faces that form an angle with a plane perpendicular to a longitudinal cylinder axis between a range of 8° and 12°;
wherein a ratio between the piston portion of combustion chamber volume and the head portion of combustion chamber volume is in a range of 0.7 to 1.3; and
wherein the recessed shape in said piston crown is bounded by a piston top land, and an annular upper surface of said piston top land cooperatively faces an annular outer periphery of said head portion along a plane substantially perpendicular to said longitudinal cylinder axis at top dead center whereby said piston portion remains substantially below said plane at top dead center and said head portion remains substantially above said plane at top dead center.
18. The combustion chamber of claim 17 , wherein a combustion chamber facing surface of an intake or exhaust valve is parallel to one of the sloping faces such that the combustion chamber facing surface of the intake or the exhaust valve forms an angle with the plane perpendicular to the longitudinal cylinder axis between a range of 8° and 12°.
19. The combustion chamber of claim 17 , wherein the combustion chamber cooperates with an air intake passage to form a tumble flow of an intake charge.
20. The combustion chamber of claim 17 , wherein the piston portion of combustion chamber volume is in a range of 40 cc to 53 cc.
21. The combustion chamber of claim 17 , wherein the head portion of combustion chamber volume is in a range of 53 cc to 56 cc.
22. The combustion chamber of claim 17 , wherein a compression ratio is in a range of 11 to 1 (11:1) and 15 to 1 (15:1).