IP Library Granted Patent US 10,066,545
Granted Patent B2
US 10,066,545 · App. 15/472,002 · Granted Sep 4, 2018

Fuel injection strategies in opposed-piston engines with multiple fuel injectors

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Quick Facts
Patent No.
US 10,066,545
App. No.
15/472,002
Granted
Sep 4, 2018
Kind
B2
Abstract

In an opposed-piston engine, two or more fuel injectors are mounted to a cylinder for direct side injection into the cylinder. The injectors are controlled so as to inject either a single fuel pulse or a plurality of fuel pulses per cycle of engine operation in order to initiate combustion during varying engine speeds and operating conditions.

Claims (15)

1. A method of operating an opposed-piston engine with fuel injectors located for direct side injection of fuel into a cylinder of the opposed-piston engine, in which a pair of pistons is disposed crown to crown in the cylinder, the method comprising:

causing the pair of opposed pistons to move in the cylinder;

compressing charge air between end surfaces of the pair of opposed pistons as they move toward top dead center positions in the cylinder;

injecting fuel from a first fuel injector and a second fuel injector in response to successive drive signal pulses;

the fuel being injected into a combustion chamber defined in the cylinder between the end surfaces of the pair of opposed pistons as the pair of opposed pistons approach top dead center locations, such that fuel injected by the first fuel injector includes at least a pilot injection followed by a main injection, and fuel injected by the second fuel injector includes at least a pilot injection followed by a main injection;

maintaining an inter-pulse gap between successive edges of the drive signal pulses that causes each pilot injection to be separated from its following main injection by at least a minimum time interval; and,

causing the fuel to ignite in response to heat produced by compression of the charge air.

2. The method of claim 1 , wherein the pilot injections injected by the first and second fuel injectors are offset by an amount of time less than the inter-pulse gap.

3. The method of claim 2 , wherein the main injections injected by the first and second fuel injectors are substantially simultaneous.

4. The method of claim 1 , wherein the fuel injected by the first fuel injector includes a second pilot injection delayed from the pilot injection by at least the inter-pulse gap, and the main injection is delayed from the second pilot injection.

5. The method of claim 4 , wherein the pilot injection injected by the second fuel injector occurs in time between the pilot injection and the second pilot injection of the first fuel injector.

6. The method of claim 5 , wherein the main injections of the first and second fuel injectors occur substantially simultaneously in time.

7. The method of claim 5 , wherein the main injections of the first and second fuel injectors overlap in time.

8. The method of claim 1 , wherein the fuel injected by the first fuel injector further includes at least one post injection following the main injection.

9. The method of claim 1 , wherein the fuel injected by the second fuel injector further includes at least one post injection following the main injection.

Assignments (2)
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 29, 2017
From: KLYZA, CLARK A.; REDON, FABIEN G.
To: ACHATES POWER, INC.
Reel/Frame 041781/0696 →