IP Library Granted Patent US 8,015,963
Granted Patent B2
US 8,015,963 · App. 12/407,190 · Granted Sep 13, 2011

Fuel pressure control strategy at engine shutdown

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Quick Facts
Patent No.
US 8,015,963
App. No.
12/407,190
Granted
Sep 13, 2011
Kind
B2
Abstract

A fuel system control method may include determining when an engine transitions from an engine on condition to an engine off condition. The method further includes determining a first fuel pressure in a fuel system of the engine a predetermined time after the determined engine off condition. A fuel injector of the fuel system may be actuated during the engine off condition when the first determined fuel pressure is above a first predetermined pressure limit to bleed fuel from the fuel system and reduce pressure within the fuel system.

Claims (31)

1. A method comprising:

determining when an engine transitions from an engine on condition to an engine off condition;

determining a first fuel pressure in a direct injection fuel system of the engine a predetermined time after the determined engine off condition; and

actuating a fuel injector of the direct injection fuel system during the engine off condition when the first determined fuel pressure is above a first predetermined pressure limit to bleed fuel from the direct injection fuel system and reduce pressure within the direct injection fuel system to a pressure below the first predetermined pressure limit.

2. The method of claim 1 , wherein the first fuel pressure is determined in a fuel rail of the direct injection fuel system.

3. The method of claim 2 , wherein the direct injection fuel system operates at a fuel pressure of at least 30 megapascal (MPa) within the fuel rail during the engine on condition.

4. The method of claim 3 , wherein the first predetermined pressure limit is less than or equal to 5 MPa.

5. The method of claim 1 , wherein the actuating includes actuating the fuel injector for at least 100 microseconds.

6. The method of claim 1 , further comprising determining a second fuel pressure in the direct injection fuel system after the actuating and indicating a system fault when the second fuel pressure is above a second predetermined pressure limit.

7. The method of claim 6 , wherein the system fault indicates a faulty pressure sensor.

8. The method of claim 6 , wherein the second predetermined pressure limit is equal to the first predetermined pressure limit.

9. The method of claim 1 , wherein the predetermined time and the first predetermined pressure limit are empirically determined based on a fuel leak rate through the fuel injector when the fuel injector is in a non-actuated state.

10. A method comprising:

determining when an engine transitions from an engine on condition to an engine off condition;

determining a first fuel pressure in a direct injection fuel system of the engine a predetermined time after the determined engine off condition;

actuating a fuel injector of the direct injection fuel system during the engine off condition when the first determined fuel pressure is above a first predetermined pressure limit to bleed fuel from the direct injection fuel system and reduce pressure within the direct injection fuel system to a pressure below the first predetermined pressure limit;

determining a second fuel pressure in the direct injection fuel system after the actuating; and

indicating a system fault when the second fuel pressure is above a second predetermined pressure limit.

11. The method of claim 10 , wherein the predetermined time and the first and second predetermined pressure limits are empirically determined based on a fuel leak rate through the fuel injector when the fuel injector is in a non-actuated state.

12. A control module comprising:

an engine operating condition evaluation module that determines when an engine transitions from an on condition to an off condition;

a fuel pressure determination module in communication with the engine operating condition evaluation module that determines a first fuel pressure in a direct injection fuel system of the engine a predetermined time after the determined engine off condition; and

a fuel injector actuation module in communication with the fuel pressure determination module that actuates a fuel injector of the direct injection fuel system during the engine off condition when the first determined fuel pressure is above a first predetermined pressure limit to bleed fuel from the direct injection fuel system and reduce pressure within the direct injection fuel system to a pressure below the first predetermined pressure limit.

13. The control module of claim 12 , wherein the fuel pressure determination module determines the fuel pressure within a fuel rail of the direct injection fuel system.

14. The control module of claim 13 , wherein the direct injection fuel system operates at a fuel pressure of at least 30 megapascal (MPa) within the fuel rail during the engine on condition.

15. The control module of claim 14 , wherein the first predetermined pressure limit is less than or equal to 5 MPa.

16. The control module of claim 12 , wherein the fuel injector actuation module actuates the fuel injector for at least 100 microseconds.

17. The control module of claim 12 , further comprising a fuel system fault determination module in communication with the fuel pressure determination module, the fuel pressure determination module determining a second fuel pressure in the direct injection fuel system after the actuating and the direct injection fuel system fault determination module indicating a system fault when the second fuel pressure is above a second predetermined pressure limit.

18. The control module of claim 17 , wherein the system fault indicates a faulty pressure sensor.

19. The control module of claim 18 , wherein the second predetermined pressure limit is equal to the first predetermined pressure limit.

20. The control module of claim 12 , wherein the predetermined time and the first predetermined pressure limit are empirically determined based on a fuel leak rate through the fuel injector when the fuel injector is in a non-actuated state.

Assignments (8)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034185/0789 →
CHANGE OF NAME Recorded Feb 10, 2011
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 025781/0245 →
SECURITY AGREEMENT Recorded Nov 8, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: WILMINGTON TRUST COMPANY
Reel/Frame 025324/0515 →
RELEASE OF SECURITY INTEREST Recorded Nov 5, 2010
From: UAW RETIREE MEDICAL BENEFITS TRUST
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025315/0091 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025246/0056 →
SECURITY AGREEMENT Recorded Aug 28, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UAW RETIREE MEDICAL BENEFITS TRUST
Reel/Frame 023162/0048 →
SECURITY AGREEMENT Recorded Aug 27, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 023201/0118 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 19, 2009
From: ELKOLALY, OMAR
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 022420/0169 →