Combustion chamber configurations for two cycle engines

• US 4,872,433 A
• Filed: 12/07/1987
• Issued: 10/10/1989
• Est. Priority Date: 12/07/1987
• Status: Expired due to Term

• Current Assignee: Ana Paul, Marius A. Paul
• Original Assignee: Ana Paul, Marius A. Paul
• Inventors: Paul, Marius A., Paul, Ana
• Primary Examiner(s): Dolinar, Andrew M.
• Application Number:
  US07/129,453
• Time in Patent Office: 673 Days
• Field of Search: 123/299, 123/300, 123/307, 123/290, 123/257, 123/65 VC, 123/261, 123/262, 123/263, 123/270, 123/271, 123/275, 123/289, 123/301, 123/663, 123/661
• US Class Current: 123/257
• CPC Class Codes: F02B 2075/025 two
• CPC Class Codes: F02B 2275/40 Squish effect
• CPC Class Codes: F02B 23/02 with compression ignition
• CPC Class Codes: F02B 23/04 the combustion space being subdivided into two or more chambers with pre-combustion chambers F02B19/00
• CPC Class Codes: F02B 23/0624 Swirl flow
• CPC Class Codes: F02B 23/0663 having multiple injectors per combustion chamber
• CPC Class Codes: F02B 23/0672 Omega-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder center axis the surrounding wall being exactly vertical F02B23/0696
• CPC Class Codes: F02B 25/04 Engines having ports both in cylinder head and in cylinder wall near bottom of piston stroke
• CPC Class Codes: F02B 3/06 with compression ignition compression ignition engines using air or gas for blowing fuel into compressed air in cylinder F02B13/02
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

Improved combustion chamber configurations for two-cycle engines with high pressure fuel injected systems having reciprocal pistons, cylinders with multiple injectors for each cylinder and a cylinder head liner with a chamber having a discoidal configuration that cooperates with a piston head structure to generate a toroidal, swirling, compressed air flow during compression strokes of the reciprocating piston.

Claims

1. A combustion chamber assembly in a two-cycle, internal combustion engine for improving combustion of injected fuel, the engine having a cylinder and at least one piston reciprocatable in the cylinder with the piston and cylinder defining in part a toroidal combustion chamber, the assembly including a plurality of fuel injector nozzles spaced around the cylinder with fuel passages directed tangentially toward the chamber in an arrangement that enhances the toroidal, swirling, compressed air flow during fuel injection, the injector having means for selectively controlling the fuel delivery and fuel timing to each injector nozzle.

2. An improved combustion chamber assembly in a two-cycle internal combustion, engine have a cylinder with a cylinder axis and a top end and a piston with a piston head reciprocatable in the cylinder, the assembly comprising:

a cylinder head capping the cylinder having a centrally positioned, single exhaust valve with a valve face, the valve being aligned with the cylinder axis,

a cylinder head liner forming a combustion chamber over the top end of the cylinder, the chamber having a discoidal configuration and a concentric communication passage with the cylinder dimensioned smaller than the cylinder and chamber, and means for generating a toroidal, swirling, compressed air flow during compression strokes of the reciprocating piston said air flow being directed away from the face of the exhaust valve, wherein the means for generating a toroidal air flow includes a central projection on the piston head that projects into the central area of the discoidal chamber wherein the discoidal chamber becomes toroidal, the projection terminating proximate the face of the valve when the piston is at top dead center of a compression stroke, and includes a flat underside on the cylinder head liner and a flat shoulder portion of the piston head that is positioned opposite and proximate the flat underside of the cylinder head liner when the piston is at the top dead center of a compression stroke such that compressed air is squished both from between the central projection and valve face and the flat underside of the cylinder head liner and the flat shoulder portion of the piston head.

3. The assembly of claim 2 wherein the central projection is substantially cylindrical in configuration.

4. The assembly of claim 3 wherein the central projection has a flared base at the junction of the projection and piston.

5. The assembly of claim 4 wherein the central projection has a flared end proximate the face of the valve.

6. The assembly of claim 2 wherein the means for generating a toroidal air flow includes a plurality of angularly directed, spaced fuel injection nozzles, wherein the liner has angularly directed fuel injection passages communicating between the injection nozzles and the chamber for generating a swirl on injection of fuel.

7. The assembly of claim 6 wherein the nozzles have central means for selectively regulating quantity and timing of fuel to the injection nozzles.