Method and system for non-functional combustion chamber detection

Patent metadata

Field	Value
Publication number	US-10823097-B2
Application number	US-201815980724-A
Country	US
Kind code	B2
Filing date	May 15, 2018
Priority date	May 15, 2018
Publication date	Nov 3, 2020
Grant date	Nov 3, 2020

Abstract

Systems and methods for detecting at least one non-functional combustion chamber of an engine comprising a plurality of combustion chambers are described herein. In response to detecting a partial output power loss of the engine, one of the plurality of combustion chambers is assessed by monitoring an engine parameter indicative of an output power of the engine, determining whether a change in the engine parameter has occurred, when the change has occurred, determining that the combustion chamber is functional, and when no change has occurred, determining that the combustion chamber is non-functional and discontinuing fuel injection to the non-functional combustion chamber.

First claim

What is claimed is:

1. A method for operating a rotary engine including detecting at least one non-functional combustion chamber of the rotary engine comprising a plurality of combustion chambers and having an apex seal for sealing the plurality of combustion chambers, each combustion chamber for receiving a fuel-air mixture that when ignited causes the rotary engine to generate output power, the method comprising:
in response to detecting a partial output power loss of the rotary engine, assessing one of the plurality of combustion chambers by:
reducing fuel injection to the combustion chamber;
monitoring an engine parameter indicative of the output power of the rotary engine;
determining whether a decrease in the engine parameter has occurred when fuel injection is reduced to the combustion chamber;
if the decrease in the engine parameter has occurred, restoring fuel injection to the combustion chamber and assessing another one of the plurality of combustion chambers;
if no decrease in the engine parameter has occurred, determining that the combustion chamber is non-functional and discontinuing fuel injection to the combustion chamber; and
detecting failure of the apex seal when two adjacent combustion chambers are determined as non-functional.

2. The method of claim 1 , wherein reducing fuel injection to the combustion chamber comprises decreasing an amount of fuel injected into the combustion chamber to substantially zero, thereby shutting off fuel injection to the combustion chamber.

3. The method of claim 2 , wherein discontinuing fuel injection to the combustion chamber comprises maintaining the shut-off of the fuel injection to the combustion chamber.

4. The method of claim 1 , further comprising assessing another one of the plurality of combustion chambers subsequent to discontinuing fuel injection to the combustion chamber.

5. The method of claim 4 , wherein the method is repeated until all combustion chambers have been assessed.

6. The method of claim 1 , wherein monitoring the engine parameter comprises monitoring the output power of the rotary engine.

7. The method of claim 1 , wherein monitoring the engine parameter comprises monitoring at least one of an output torque of the rotary engine and a rotational speed of an output shaft of the rotary engine.

8. The method of claim 1 , further comprising adjusting at least one of a timing of fuel injection to the engine and a rail pressure of the engine, in response to detecting that the combustion chamber is non-functional.

9. A system for operating a rotary engine including detecting at least one non-functional combustion chamber of the rotary engine comprising a plurality of combustion chambers and having an apex seal for sealing the plurality of combustion chambers, each combustion chamber for receiving a fuel-air mixture that when ignited causes the rotary engine to generate output power, the system comprising:
at least one processing unit; and
a non-transitory computer-readable memory having stored thereon program instructions executable by the at least one processing unit for:
in response to detecting a partial output power loss of the rotary engine, assessing one of the plurality of combustion chambers by:
reducing fuel injection to the combustion chamber;
monitoring an engine parameter indicative of the output power of the rotary engine;
determining whether a decrease in the engine parameter has occurred when fuel injection is reduced to the combustion chamber;
if the decrease in the engine parameter has occurred, restoring fuel injection to the combustion chamber and assessing another one of the plurality of combustion chambers;

if no decrease in the engine parameter has occurred, determining that the combustion chamber is non-functional and discontinuing fuel injection to the combustion chamber; and
detecting failure of the apex seal when two adjacent combustion chambers are determined as non-functional.

10. The system of claim 9 , wherein the program instructions are executable by the at least one processing unit for reducing fuel injection to the at least one combustion chamber comprising decreasing an amount of fuel injected into the at least one combustion chamber to substantially zero, thereby shutting off fuel injection to the at least one combustion chamber.

11. The system of claim 10 , wherein the program instructions are executable by the at least one processing unit for discontinuing fuel injection to the at least one combustion chamber comprising maintaining the shut-off of the fuel injection to the at least one combustion chamber.

12. The system of claim 9 , wherein the program instructions are further executable by the at least one processing unit for assessing another one of the plurality of combustion chambers subsequent to discontinuing fuel injection to the combustion chamber.

13. The system of claim 12 , wherein the program instructions are further executable by the at least one processing unit for repeating the assessing until all combustion chambers have been evaluated.

14. The system of claim 9 , wherein the program instructions are executable by the at least one processing unit for monitoring the output power of the rotary engine.

15. The system of claim 9 , wherein the program instructions are executable by the at least one processing unit for monitoring at least one of an output torque of the rotary engine and a rotational speed of an output shaft of the rotary engine.

16. The system of claim 9 , wherein the program instructions are further executable by the at least one processing unit for adjusting at least one of a timing of fuel injection to the rotary engine and a rail pressure of the rotary engine, in response to detecting that the combustion chamber is non-functional.

17. A method for operating a rotary engine including detecting at least one non-functional combustion chamber of the rotary engine comprising a plurality of combustion chambers and having an apex seal for sealing the plurality of combustion chambers, each combustion chamber for receiving a fuel-air mixture that when ignited causes the rotary engine to generate output power, the method comprising:
in response to detecting a partial output power loss of the engine, assessing one of the plurality of combustion chambers by:
monitoring an engine parameter indicative of the output power of the combustion chamber;
determining whether a change in the engine parameter has occurred;
if no change in the engine parameter has occurred, determining that the combustion chamber is non-functional and discontinuing fuel injection to the combustion chamber; and
detecting failure of the apex seal when two adjacent combustion chambers are determined as non-functional.

18. The method of claim 17 , wherein the engine parameter is a metal temperature of the combustion chamber.

Assignees

• Pratt & Whitney Canada

Inventors

• Lanktree Michael
• Gagnon-Martin David
• Villeneuve Bruno

Classifications

• F02B53/02 Primary

  Methods of operating · CPC title

• Y02T10/40

  Engine management systems · CPC title

• F02D2200/1002

  Output torque · CPC title

• F02B2053/005

  Wankel engines · CPC title

• F02D41/22 Primary

  Safety or indicating devices for abnormal conditions {(in air/fuel ratio feedback systems F02D41/1495, in electric control linkage F02D11/107, in purge control systems F02M25/0809)} · CPC title