IP Library Granted Patent US 9,464,592
Granted Patent B2
US 9,464,592 · App. 13/891,523 · Granted Oct 11, 2016

Piston thermal management in an opposed-piston engine

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Quick Facts
Patent No.
US 9,464,592
App. No.
13/891,523
Granted
Oct 11, 2016
Kind
B2
Abstract

An opposed-piston engine includes pistons, each piston having an annular cavity in the piston's sidewall and positioned between its crown and ring grooves to block transfer of heat from the crown to the piston body.

Claims (16)

1. An internal combustion engine including at least one cylinder with longitudinally-separated exhaust and intake ports and a pair of pistons disposed in opposition to one another in a bore of the cylinder, each piston including a piston body with a crown at one end, an end surface on the crown, in which an end surface of a first piston has a bowl that cooperates with the end surface of an opposing piston to define a combustion chamber, at least one ring groove in the piston sidewall near the crown, an annular thermally-resistant cavity formed in the piston sidewall along a circumference of the piston body and positioned between the end surface and the at least one ring groove, and one of a band, a flange, and a pair of opposing flanges covering the cavity to form a chamber that contains a near-vacuum.

2. The piston of claim 1 , wherein the pair of opposing flanges comprises an upper flange that extends in a radial direction of the piston and a lower flange that extends downwardly in an axial direction of the piston, further wherein:

a sleeve comprises the upper flange and lower flange, and

the sleeve is seated on an outer circumferential surface of the crown with the upper flange held against a shoulder of the crown and the lower flange covering the cavity.

3. The piston of claim 1 , further including one or more cooling galleries within the piston body under the crown.

4. A piston for a two-stroke internal combustion engine, comprising:

a piston body with a crown at one end;

an end surface formed on the crown;

the end surface including an elongated bowl that cooperates with an opposing piston end surface to define a combustion chamber;

at least one ring groove in the piston sidewall near the crown;

an annular thermally-resistant cavity formed in the piston sidewall, extending along a circumference of the piston body, and positioned between the end surface and the at least one ring groove; and,

one of a band, a flange, and a pair of opposing flanges covering the cavity to form a chamber that contains a near-vacuum.

5. The piston of claim 4 , wherein the pair of opposing flanges comprises an upper flange that extends in a radial direction of the piston and a lower flange that extends downwardly in an axial direction of the piston, further wherein:

a sleeve comprises the upper flange and lower flange, and

the sleeve is seated on an outer circumferential surface of the crown with the upper flange held against a shoulder of the crown and the lower flange covering the cavity.

6. The piston of claim 4 , further including one or more cooling galleries within the piston body under the crown.

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 May 14, 2013
From: DION, ERIC P.
To: ACHATES POWER, INC.
Reel/Frame 030414/0893 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 14, 2013
From: MACKENZIE, RYAN G.
To: ACHATES POWER, INC.
Reel/Frame 030414/0977 →