초록 ▼

A power cylinder system for a reciprocating engine includes a piston with a top-most groove extending circumferentially about the piston. The top-most groove includes one or more channels spaced apart circumferentially about the top-most groove and extending inward from an outer perimeter of the pis

A power cylinder system for a reciprocating engine includes a piston with a top-most groove extending circumferentially about the piston. The top-most groove includes one or more channels spaced apart circumferentially about the top-most groove and extending inward from an outer perimeter of the piston assembly. The system also includes a ring positioned in the top-most groove, the ring including a top face, a bottom face, an inner circumferential face, and an outer circumferential face that tapers between the top face and the bottom face. A space is defined between a portion of the top-most groove and the inner circumferential face of the ring, and the space is in fluid communication with the one or more radial channels.

대표청구항 ▼

1. A power cylinder system for a reciprocating engine, comprising: a piston configured to be disposed within a cylinder having an inner wall and defining a cavity and configured to move in a reciprocating manner within the cylinder;a top-most groove extending circumferentially about the piston benea

1. A power cylinder system for a reciprocating engine, comprising: a piston configured to be disposed within a cylinder having an inner wall and defining a cavity and configured to move in a reciprocating manner within the cylinder;a top-most groove extending circumferentially about the piston beneath a top land of the piston, wherein the top-most groove is defined by a top surface, a bottom surface, and an inner surface extending between the top surface and the bottom surface;a ring disposed within the top-most groove, wherein the ring comprises an inner face disposed proximate to the inner surface of the top-most groove and an outer face opposite the inner face, wherein the outer face comprises a tapered profile and is configured to contact the inner wall of the cylinder as the piston moves within the cylinder; andone or more channels formed in the top land or an upper face of the ring, wherein the one or more channels are configured to enable combustion gases to flow from the cavity to a space defined by the inner surface of the top-most groove and the inner face of the ring and to enable the combustion gases flowing through the one or more channels to contact the inner face of the ring. 2. The system of claim 1, wherein at least some of the one or more channels extend radially in the top surface of the top-most groove to the space, and the one or more channels are positioned at one or more discrete locations about the circumference of the top-most groove. 3. The system of claim 1, wherein at least some of the one or more channels extend axially through the top land of the piston to the space. 4. The system of claim 1, wherein a radius of the ring increases from a top axially-facing surface to a bottom axially-facing surface of the ring such that a smallest radius of the ring coincides with the top axially-facing surface and a largest radius of the ring coincides with the bottom axially-facing surface, the bottom axially-facing surface is flat and is configured to contact the bottom surface of the top-most groove, and the bottom axially-facing surface and the outer face of the ring form a sealing point that is configured to contact the inner wall of the cylinder. 5. The system of claim 1, wherein the outer face of the ring is positioned at an angle greater than approximately 1.5 degrees relative to the inner wall of the cylinder. 6. The system of claim 1, wherein a sealing point at which the outer face of the top ring contacts the inner wall of the cylinder is positioned between a top face and a bottom face of the ring, the ring comprises a notch between the sealing point and the bottom face of the ring, the bottom face is configured to contact the bottom surface of the top-most groove, the sealing point is located a first axial distance from the top face of the ring, and the first axial distance is approximately 75 to 99 percent of a height of the ring. 7. The system of claim 1, wherein the cavity defined by the cylinder comprises a diameter of between approximately 13.5 and 34 centimeters. 8. The system of claim 1, wherein one or more channels and the ring are configured to enable the combustion gases that flow through the one or more channels to the space to exert a radially-outward force on the inner face of the ring that substantially balances a radially-inward force exerted by another flow of combustion gases against the outer face of the ring. 9. The system of claim 1, comprising the cylinder. 10. The system of claim 1, wherein a radius of the ring increases linearly from the upper face of the ring to an intermediate portion of the ring located a first axial distance from the upper face of the ring, and wherein the radius of the ring decreases from the intermediate portion to a bottom face of the ring. 11. The system of claim 10, wherein the first axial distance is between approximately 75 to 99 percent of a height of the ring. 12. The system of claim 1, wherein at least some of the one or more channels are formed in the upper face of the ring. 13. The system of claim 1, wherein the one or more channels comprises at least two channels. 14. The system of claim 1, wherein the piston comprises steel. 15. The system of claim 1, wherein the piston comprises aluminum.