Toroidal combustion chamber with side injection

• US 8,783,218 B2
• Filed: 07/06/2012
• Issued: 07/22/2014
• Est. Priority Date: 07/15/2011
• Status: Expired due to Fees

• Current Assignee: Achates Power, Inc.
• Original Assignee: EcoMotors, Inc
• Inventors: Shen, Huixian, Hofbauer, Peter
• Primary Examiner(s): Low, Lindsay
• Assistant Examiner(s): BRAUCH, CHARLES JOSEPH
• Application Number:
  US13/542,706
• Publication Number:
  US 20130014718A1
• Time in Patent Office: 746 Days
• Field of Search: 123/51.R, 123/53.3, 123/53.6, 123/55.2, 123/58.1
• US Class Current: 123/51.R
• CPC Class Codes: F01B 7/08 with side rods
• CPC Class Codes: F02B 23/0663 having multiple injectors per combustion chamber
• CPC Class Codes: F02B 23/0675 the combustion space being substantially spherical, hemispherical, ellipsoid or parabolic
• CPC Class Codes: F02B 75/282 the pistons having equal strokes
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A toroidal combustion chamber shape with a side injector is disclosed for an opposed-piston engine. Fuel is injected into the toroidal volume from a fuel injector in the cylinder wall. In one embodiment, fuel is injected from each injector a plurality of times with the timing between the injections such that fuel clouds from each injection remain substantially isolated from each other.

Claims

1. An internal combustion engine, comprising:

a cylinder wall;

a first piston disposed in the cylinder;

a second piston disposed in the cylinder in an opposed relationship with respect to the first piston;

a crankshaft having first and second eccentric journals;

a first connecting rod coupling the first piston to the first eccentric journal; and

a second connecting rod coupling the second piston to the second eccentric journal, wherein;

the pistons reciprocate within the cylinder upon rotation of the crankshaft;

there is a particular angle of rotation of the crankshaft at which the pistons are closest to each other;

the piston top of the first piston has three regions;

a center, an outer ring near the periphery of the piston, and an inner ring, all of which have a center that is substantially coincident with a central axis of the cylinder;

the piston top of the second piston has three regions;

a center, an outer ring near the periphery of the piston, and an inner ring, all of which have a center that is substantially coincident with the central axis of the cylinder;

a face of the first piston and a face of the second piston are a predetermined distance apart in their respective center regions and the same predetermined distance apart in their respective outer rings when the crankshaft is at the particular angle, the predetermined distance is taken in a direction parallel to the central axis of the cylinder; and

a volume between the first and second pistons proximate the inner ring substantially forms a toroidal volume when the crankshaft is at the particular angle.

2. The engine of claim 1, further comprising:

a fuel injector mounted in the cylinder wall with a longitudinal axis of the fuel injector roughly normal to the cylinder wall wherein a channel is defined in the outer ring of second piston to provide an opening for line-of-sight access from a tip of the injector to the toroidal volume formed between the pistons.

3. The engine of claim 2 wherein the fuel injector has at least one orifice and the orifice is arranged so that a spray exiting the orifice is largely directed into the toroidal volume.

4. The engine of claim 3 wherein fuel jets which exit from the injector are directed into the toroidal volume;

the center region of the top of the second piston is oval; and

the spray is directed substantially tangent to the oval near a shorter of the axes of symmetry of the oval.

5. The engine of claim 1 wherein the center region of the top of the first piston is oval in a direction taken perpendicular with respect to the central axis of the cylinder.

6. The engine of claim 1 wherein a cross sectional area of the substantially toroidal volume varies around the circumference of the toroidal volume.

7. The engine of claim 1, further comprising:

first and second fuel injectors disposed in the cylinder wall; and

first and second channels defined in the outer ring of at least one of the first and second pistons and evenly spaced around the cylinder, the first channel providing line-of sight access between a tip of the first injector and the toroidal volume and the second channel providing line-of-sight access between a tip of the second injector and the toroidal volume wherein a cross-sectional area of the toroidal volume is less proximate the channels than at a position away from the channels.

8. The engine of claim 1 wherein surfaces of the first and second pistons in the center regions are substantially flat.

9. The engine of claim 1 wherein a surface of the first piston is concave in the central region and the second piston is convex in the central region.

10. The piston of claim 9 wherein the engine is an opposed-piston engine;

the first piston is an intake piston; and

the second piston is an exhaust piston.

11. The engine of claim 2 in which a swirl flow is induced in the toroidal volume during operation and fuel from the fuel injector is injected in the same general direction as the induced swirl flow.

12. A combustion chamber in an opposed-piston engine, comprising:

a cylinder wall;

an intake piston disposed within the cylinder wall;

an exhaust piston disposed within the cylinder wall with a top of the intake piston opposite a top of the exhaust piston wherein;

the piston top of the intake piston has three regions;

a center, an outer ring near the periphery of the piston, and an inner ring, all of which are substantially symmetrically arranged with respect to a plane through a central axis of the cylinder;

the piston top of the exhaust piston has three regions;

a center, an outer ring near the periphery of the piston, and an inner ring, all of which have a center substantially coincident with the central axis of the cylinder;

a channel is defined in the outer ring region of the exhaust piston; and

wherein the center of the intake piston and the center of exhaust piston are a predetermined distance apart; and

the outer ring of the intake piston and the outer ring of the exhaust piston are the same predetermined distance apart.

13. The combustion chamber of claim 12, further comprising:

a fuel injector mounted in the cylinder wall wherein a volume between the first and second pistons proximate the inner ring substantially forms a toroidal volume and fuel jets which exit from the injector are directed into the toroidal volume.

14. The combustion chamber of claim 12 wherein the center region of the top of the exhaust piston is oval.

15. The combustion chamber of claim 13, further comprising:

a fuel injector disposed in the cylinder wall wherein fuel jets which exit from the injector are directed into the toroidal volume and the center region of the top of the exhaust piston is oval and the jets are substantially tangent to the oval near a shorter of the axes of symmetry.

16. The combustion chamber of claim 12 wherein surfaces of the intake and exhaust pistons in the center regions are substantially flat.

17. The combustion chamber of claim 12 wherein a surface of the first piston is concave in the central region and the second piston is convex in the central region.

18. The combustion chamber of claim 14 wherein a volume between the first and second pistons proximate the inner ring substantially forms a toroidal volume;

a swirl flow is induced in the toroidal volume;

, and fuel from the fuel injector is injected in the same general direction as the induced swirl flow.

19. A method to provide fuel to an opposed-piston, internal-combustion engine, the method comprising:

injecting fuel multiple times into a combustion chamber of the engine, the combustion chamber comprising;

a cylinder wall;

an intake piston disposed within the cylinder wall;

an exhaust piston disposed within the cylinder wall with a top of the intake piston opposite a top of the exhaust piston wherein;

the piston top of the intake piston has three regions;

a center, an outer ring near the periphery of the piston, and an inner ring, all of which are have a center substantially coincident with a central axis of the cylinder;

the piston top of the exhaust piston has three regions;

a center, an outer ring near the periphery of the piston, and an inner ring, all of which have a center substantially coincident with the central axis of the cylinder wherein the center of the intake piston and the center of exhaust piston are a predetermined distance apart; and

the outer ring of the intake piston and the outer ring of the exhaust piston are the same predetermined distance apart;

two channels are defined in the outer ring region of the intake piston with the two channels diametrically opposed; and

a volume between the intake and exhaust pistons proximate the inner ring substantially forms a toroidal volume.

20. The method of claim 19 wherein the combustion chamber further includes first and second fuel injectors disposed in the cylinder wall.

21. The method of claim 19 wherein the multiple injections are separated in time such that a fuel cloud from a second injection is substantially separate from a fuel cloud from the first injection.