IP Library › Granted Patent US 11,773,792
Granted Patent B1
US 11,773,792 · App. 18/073,430 · Granted Oct 3, 2023

Multi-fuel injection system and injector

Inventors: Dana R. Coldren (Secor, IL); Eric L. Schroeder (Germantown Hills, IL); Robert Graumueller (Kiel, DE); Andrew O. Marrack (Peoria, IL)
Assignee: Caterpillar Inc.
F02D19/0694F02D41/38
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Quick Facts
Patent No.
US 11,773,792
App. No.
18/073,430
Granted
Oct 3, 2023
Kind
B1
Abstract

A multi-fuel injector includes a primary fuel inlet configured to receive a liquid primary fuel, a pilot fuel inlet configured to receive a liquid pilot fuel that is a different fuel than the primary fuel, and a spill valve in fluid communication with the primary fuel inlet. The fuel injector also includes a control valve configured to control a pressure of fluid within a hydraulic control chamber, and an injection valve abutting the hydraulic control chamber, the injection valve being configured to move to an injection position to inject both the primary fuel and the pilot fuel.

Claims (37)

1. A multi-fuel injector, comprising:

a primary fuel inlet configured to receive a liquid primary fuel;

a pilot fuel inlet configured to receive a liquid pilot fuel that is a different fuel than the primary fuel;

a spill valve in fluid communication with the primary fuel inlet;

a control valve configured to control a pressure of fluid within a hydraulic control chamber; and

an injection valve abutting the hydraulic control chamber, the injection valve being configured to move to an injection position to inject both the primary fuel and the pilot fuel.

2. The multi-fuel injector of claim 1 , wherein the injection valve includes an injection valve member having a hollow interior configured to receive the pilot fuel.

3. The multi-fuel injector of claim 2 , wherein the hydraulic control chamber is in fluid communication with the hollow interior of the injection valve.

4. The multi-fuel injector of claim 3 , wherein the injection valve includes at least one opening at a distal end portion of the hollow interior of the injection valve.

5. The multi-fuel injector of claim 1 , wherein the hydraulic control chamber is in fluid communication with the pilot fuel inlet.

6. The multi-fuel injector of claim 5 , wherein the control valve is configured to block a flow of pilot fuel from the pilot fuel inlet to the hydraulic control chamber when in a first position.

7. The multi-fuel injector of claim 6 , wherein the control valve is configured to permit the flow of pilot fuel from the pilot fuel inlet to the hydraulic control chamber when in a second position.

8. A fuel injection system, comprising:

a fuel injector configured to inject multiple liquid fuels from a single injection nozzle;

a fuel supply system configured to supply a first fuel at a first pressure and a second fuel at a second pressure; and

an electronic control module configured to:

set the first pressure,

set the second pressure, and

adjust at least one of the first pressure or the second pressure to change a quantity of the first fuel injected by the injection nozzle.

9. The fuel injection system of claim 8 , wherein the first fuel is a pilot fuel injected prior to the second fuel in the same injection event.

10. The fuel injection system of claim 9 , wherein the pilot fuel has a higher cetane number as compared to the second fuel .

11. The fuel injection system of claim 8 , wherein the electronic control module is further configured to increase the first pressure and/or decrease the second pressure to increase an amount of the first fuel present within the injection nozzle prior to injection of the first fuel.

12. The fuel injection system of claim 8 , wherein the fuel supply system includes a primary fuel fitting connected to a body of the fuel injector and a pilot fuel connection formed on the body of the fuel injector.

13. A fuel injection method, comprising:

setting a first pressure for a first liquid fuel;

setting a second pressure for a second liquid fuel, the first liquid fuel being different than the second liquid fuel;

supplying the first liquid fuel to a fuel injector at the first pressure;

supplying the second liquid fuel to the fuel injector at the second pressure;

injecting the first liquid fuel and the second liquid fuel in a first injection; and

adjusting at least one of the first pressure and the second pressure to modify a quantity of first liquid fuel injected in a second injection.

14. The fuel injection method of claim 13 , wherein the first liquid fuel and the second liquid fuel are injected from at least one shared orifice in a nozzle of the fuel injector.

15. The fuel injection method of claim 14 , wherein the first liquid fuel is injected via a hollow injection valve member that supplies the first liquid fuel to an interior of the nozzle.

16. The fuel injection method of claim 13 , wherein adjusting at least one of the first pressure and the second pressure includes increasing a difference between the first pressure and the second pressure based on at least one of a cold start condition or a low intake air temperature condition.

17. The fuel injection method of claim 16 , wherein the second liquid fuel includes an alcohol.

18. The fuel injection method of claim 13 , wherein injection occurs when an injection valve member moves away from an orifice in a nozzle of the fuel injector, a movement of the injection valve member being permitted or blocked with a control chamber.

19. The fuel injection method of claim 18 , wherein the control chamber is in fluid communication with a hollow interior of the injection valve member.

20. The fuel injection method of claim 19 , wherein the fuel injector includes a first fluid path for the first liquid fuel and a second fluid path for the second liquid fuel, the first fluid path and the second fluid path being isolated from each other until the first fluid path and the second fluid path connect to each other within the nozzle.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 20, 2023
From: COLDREN, DANA R.; SCHROEDER, ERIC L.; GRAUMUELLER, ROBERT; MARRACK, ANDREW O.
To: CATERPILLAR INC.
Reel/Frame 062431/0176 →
Cited By (2)
US 12,486,809 US 12,486,810