Opposed piston, homogeneous charge pilot ignition engine
First Claim
1. A method of operating an opposed piston compression ignition engine including a cylinder, a pair of opposed pistons in the bore of the cylinder and spaced-apart inlet and exhaust ports controlled by the pistons, comprising:
- introducing air into the cylinder between the pistons;
moving the pistons toward each other;
injecting a lean main charge of liquid fuel into the cylinder between the pistons through at least one main injection site on the cylinder between the inlet port and the exhaust port;
in response to movement of the pistons, the main charge fully evaporating before an autoignition temperature is reached; and
then injecting a pilot charge of liquid fuel through at least one pilot injection site;
the pilot charge igniting the evaporated main charge.
2 Assignments
0 Petitions
Accused Products
Abstract
An engine of the opposed piston, two-stroke, compression ignition type includes provision for injection of a main charge of liquid fuel into the bore of a cylinder between opposed pistons early in a compression stroke to permit the fuel to evaporate and mix with air during the remainder of the compression stroke to the point where the stoichiometric components of the mixture are insufficient for autoignition. Further provision is made for injection of a pilot charge of liquid fuel into the compressed air/fuel mixture later in the compression stroke. The pilot charge provides a stoichiometric component which autoignites, thereby activating ignition of the compressed air/fuel mixture.
41 Citations
41 Claims
-
1. A method of operating an opposed piston compression ignition engine including a cylinder, a pair of opposed pistons in the bore of the cylinder and spaced-apart inlet and exhaust ports controlled by the pistons, comprising:
-
introducing air into the cylinder between the pistons;
moving the pistons toward each other;
injecting a lean main charge of liquid fuel into the cylinder between the pistons through at least one main injection site on the cylinder between the inlet port and the exhaust port;
in response to movement of the pistons, the main charge fully evaporating before an autoignition temperature is reached; and
theninjecting a pilot charge of liquid fuel through at least one pilot injection site;
the pilot charge igniting the evaporated main charge. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12)
-
-
13. A method of operating an opposed piston compression ignition engine including a cylinder with opposing pistons disposed in the cylinder and spaced apart inlet and exhaust ports, comprising:
-
introducing air into the cylinder between the pistons;
moving the pistons toward each other;
injecting a lean main charge of liquid fuel into the cylinder between the pistons through at least one main injection site on the cylinder between the inlet port and the exhaust port;
in response to movement of the pistons, the main charge fully evaporating before an autoignition temperature is reached; and
theninjecting a pilot charge of liquid fuel through at least one pilot injection site near the longitudinal midpoint of the cylinder;
the pilot charge igniting the evaporated main charge. - View Dependent Claims (14, 15, 16, 17, 18, 19, 20)
-
-
21. A compression ignition engine, comprising:
-
a cylinder;
a pair of opposing pistons slidably disposed in the cylinder;
spaced-apart inlet and exhaust ports near respective ends of the cylinder;
at least one main fuel injector communicating with the bore of the cylinder through an injector site in the cylinder between the inlet port and the exhaust port;
at least one pilot fuel injector communicating with the bore through an injector site in the cylinder near a longitudinal midpoint of the cylinder; and
a fuel injection system coupled to the at least one main fuel injector and to the at least one pilot fuel injector for operating the at least one main fuel injector when the pistons are near bottom dead center positions and then operating the at least one pilot fuel injector when the pistons are near top dead center positions. - View Dependent Claims (22, 23, 24, 25)
-
-
26. An internal combustion engine, comprising:
-
a cylinder with spaced-apart inlet and exhaust ports;
opposing pistons disposed in a central bore of the cylinder;
a first main fuel injector positioned at an injection site on the cylinder near the inlet port;
a second main fuel injector positioned at an injection site on the cylinder near the exhaust port;
a main fuel injection system connected to the main fuel injectors;
a pilot fuel injector positioned at an injection site between respective top dead center positions of the pistons; and
a pilot fuel injection system connected to the pilot fuel injector. - View Dependent Claims (27, 28, 29)
-
-
30. An internal combustion engine, comprising:
-
a cylinder with spaced-apart inlet and exhaust ports;
opposing pistons disposed in the bore of the cylinder;
at least one main fuel injector communicating with the bore through at least one injection site on the cylinder between the inlet port and the exhaust port;
a main fuel injection system connected to the at least one main fuel injector for operating the at least one main fuel injector when the pistons are near bottom dead center positions;
a pilot fuel injector communicating with the bore through at least one injection site near a longitudinal midpoint of the cylinder;
a pilot fuel injection system connected to the pilot fuel injector for operating the pilot fuel injector when the pistons are near top dead center positions; and
an electrical ignition element mounted to the cylinder. - View Dependent Claims (31)
-
-
32. A fuel injection combination for an opposed piston compression ignition engine, comprising:
-
a cylinder with spaced-apart inlet and exhaust ports;
opposing pistons disposed in a bore of the cylinder for moving between bottom dead center and top dead center positions;
at least one main fuel injector communicating with the bore through at least one injection site on the cylinder between the inlet port and the exhaust port;
at least one pilot fuel injector communicating with the bore through at least one injection site near a longitudinal midpoint of the cylinder; and
control means for operating the least one main fuel injector when the pistons are near their bottom dead center positions and operating the at least one pilot fuel injector when the pistons are near their top dead center positions.
-
-
33-35. -35. (canceled)
-
36. A fuel injection combination for an opposed piston compression ignition engine, comprising:
-
a cylinder with spaced-apart inlet and exhaust ports;
opposing pistons disposed in a bore of the cylinder;
a first main fuel injector communicating with the bore through a first main injection site on the cylinder near the inlet port, the first main fuel injector for injecting a first portion of a main charge of liquid fuel through the first main injection site in a direction toward the longitudinal midpoint; and
a second main fuel injector communicating with the bore through a second main injection site on the cylinder near the exhaust port, the second main fuel injector for injecting a second portion of the main charge of liquid fuel through the second main injection site in a direction toward the longitudinal midpoint.
-
-
37. (canceled)
-
38. An opposed piston compression ignition engine, comprising:
-
at least one cylinder with spaced-apart inlet and exhaust ports, a bore and a longitudinal midpoint;
opposed pistons disposed in the bore for moving between top dead center and bottom dead center positions;
at least one main fuel injector communicating with the bore through at least one main injection site on the cylinder between the inlet and exhaust ports;
at least one pilot fuel injector communicating with the bore through a pilot injection site on the cylinder near the longitudinal midpoint; and
control means for operating the at least one main fuel injector when the pistons are near their bottom dead center positions and operating the at least one pilot fuel injector when the pistons are near their top dead center positions. - View Dependent Claims (39, 40, 41)
-
Specification