IP Library Granted Patent US 10,180,115
Granted Patent B2
US 10,180,115 · App. 13/843,686 · Granted Jan 15, 2019

Piston crown bowls defining combustion chamber constructions in opposed-piston engines

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,180,115
App. No.
13/843,686
Granted
Jan 15, 2019
Kind
B2
Abstract

A combustion chamber for an opposed-piston engine is defined between a pair of pistons disposed for opposing reciprocal movement in a cylinder. The combustion chamber is formed between crowns of the pistons and has a radius that decreases from the longitudinal axis of the cylinder. Each crown includes a periphery, a bowl within the periphery defining a concave surface with a first portion curving inwardly toward the interior of the piston and a second portion curving outwardly from the interior, and a convex surface within the periphery curving outwardly and meeting the second portion of the concave surface to form a ridge. Each ridge has a height that decreases with the distance from a longitudinal axis.

Claims (11)

1. A piston having a crown for defining a combustion chamber with the crown of an opposing piston, in which the crown has a periphery centered on the longitudinal axis of the piston, the piston comprising:

a flat circumferential area extending from the periphery toward the longitudinal axis;

a bowl within the periphery, the bowl defining a concave surface with a first portion curving inwardly toward the interior of the piston from a first plane that is orthogonal to the longitudinal axis of the piston and that contacts the periphery, and a second portion curving outwardly from the interior of the piston through the first plane; and,

a convex surface within the periphery curving outwardly from the first plane and meeting the second portion of the concave surface to form a ridge; wherein,

the flat circumferential area lies in the first plane; and

the ridge has a height H that decreases from a maximum at a midpoint of a major axis of the combustion chamber in a direction along the major axis toward the periphery.

2. The piston of claim 1 , in which opposing notches are provided in the periphery at respective positions on the major axis of the combustion chamber.

3. The piston of claim 2 , in which the ridge has a rounded configuration having a radius RL in a second plane that orthogonally intersects the major axis of the combustion chamber.

4. The piston of claim 2 , wherein the flat circumferential area has a generally annular shape except where the notches are positioned.

5. The piston of claim 4 , in which a radius R changes in value from a central combustion region of the bowl along an axis extending between the notches to reduce volume of the bowl near the notches and a piston cooling gallery extends into an interior portion of the crown between an end surface of the crown and a top land on the crown.

6. The piston of claim 1 , in which the ridge has a rounded configuration having a radius RL in a second plane that orthogonally intersects the major axis of the combustion chamber.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 23, 2025
From: ACHATES POWER, INC.
To: GENERAL ATOMICS AERONAUTICAL SYSTEMS, INC.
Reel/Frame 072956/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 20, 2013
From: BURTON, TRISTAN M.
To: ACHATES POWER, INC.
Reel/Frame 030049/0967 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 20, 2013
From: REDON, FABIEN G.
To: ACHATES POWER, INC.
Reel/Frame 030050/0092 →