[미국특허]
System and method for controlling a dual fuel engine
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F02D-019/10
F02D-019/06
F02D-019/08
F02D-041/02
F02D-041/14
F02D-041/18
F02D-041/00
F02B-003/06
F02D-035/02
출원번호
US-0138200
(2013-12-23)
등록번호
US-10190509
(2019-01-29)
발명자
/ 주소
Lavertu, Thomas Michael
Primus, Roy James
Klingbeil, Adam Edgar
Mischler, James Robert
출원인 / 주소
GE Global Sourcing LLC
대리인 / 주소
McCoy Russell LLP
인용정보
피인용 횟수 :
0인용 특허 :
23
초록▼
A method includes receiving a plurality of signals from a plurality of sensors coupled to a dual fuel engine. The method further includes altering an actual speed of the dual fuel engine to obtain a predetermined air-fuel ratio in response to a changed operating condition of the dual fuel engine det
A method includes receiving a plurality of signals from a plurality of sensors coupled to a dual fuel engine. The method further includes altering an actual speed of the dual fuel engine to obtain a predetermined air-fuel ratio in response to a changed operating condition of the dual fuel engine determined based on the plurality of signals, so as to maintain operation of the dual fuel engine between knock and misfire conditions.
대표청구항▼
1. A method comprising: receiving a plurality of signals from a plurality of sensors coupled to a dual fuel engine; andaltering an actual speed of the dual fuel engine to obtain a predetermined air-fuel ratio in response to a changed operating condition of the dual fuel engine determined based on th
1. A method comprising: receiving a plurality of signals from a plurality of sensors coupled to a dual fuel engine; andaltering an actual speed of the dual fuel engine to obtain a predetermined air-fuel ratio in response to a changed operating condition of the dual fuel engine determined based on the plurality of signals, so as to maintain operation of the dual fuel engine between knock and misfire conditions. 2. The method of claim 1, further comprising determining a base operating condition of the dual fuel engine. 3. The method of claim 2, wherein the base operating condition comprises a base airflow, a base air-fuel ratio, a base substitution ratio, a base engine speed, base engine power, and a base fuel injection timing. 4. The method of claim 3, further comprising determining the changed operating condition from the base operating condition of the dual fuel engine operating at same power level, based on the plurality of signals. 5. The method of claim 4, wherein the plurality of signals is representative of a plurality of actual emissions, an intake manifold temperature, an exhaust manifold temperature, an actual engine speed, an actual fuel injection timing, and an actual airflow. 6. The method of claim 5, further comprising determining an estimated airflow based on at least one signal from the plurality of signals. 7. The method of claim 6, wherein the altering comprises altering the actual speed of the dual fuel engine from the base engine speed in response to the changed operating condition. 8. The method of claim 7, further comprising altering the actual airflow from the base airflow, based on the estimated airflow, to obtain the predetermined air-fuel ratio equal to or different from the base air-fuel ratio. 9. The method of claim 4, wherein the base operating condition corresponds to a sea-level operating condition of the dual fuel engine. 10. The method of claim 9, wherein the changed operating condition comprises at least one of an actual altitude different from the sea-level, an actual ambient temperature different from a sea-level temperature, and an actual ambient pressure different from a sea-level pressure. 11. The method of claim 2, wherein the base operating condition corresponds to a reference ambient temperature and a reference ambient pressure of the dual fuel engine. 12. The method of claim 11, wherein the changed operating condition comprises at least one of an actual ambient temperature different from a reference ambient temperature and an actual ambient pressure different from a reference ambient pressure. 13. The method of claim 1, further comprising maintaining a plurality of actual emissions from the dual fuel engine within a predetermined emission limit, an actual specific fuel consumption of the dual fuel engine within a predetermined specific fuel consumption limit, an actual in-cylinder peak pressure within a predetermined pressure limit, and an exhaust manifold temperature within a predetermined temperature limit. 14. A system comprising: a signal acquisition system configured to receive a plurality of signals from a plurality of sensors coupled to a dual fuel engine; andat least one processor coupled to the signal acquisition system, the at least one processor encoded with instructions to perform processing of the plurality of signals, the instructions including: a speed control module for altering an actual speed of the dual fuel engine to obtain a predetermined air-fuel ratio in response to a changed operating condition of the dual fuel engine determined based on the plurality of signals, so as to maintain operation of the dual fuel engine between knock and misfire conditions. 15. The system of claim 14, wherein the instructions further include a base condition module for determining a base operating condition comprising a base airflow, a base air-fuel ratio, a base substitution ratio, a base engine speed of the dual fuel engine, base engine power, and a base fuel injection timing. 16. The system of claim 15, wherein the instructions further include a changed condition module for determining the changed operating condition from the base operating condition of the dual fuel engine operating at same power level, based on the plurality of signals. 17. The system of claim 16, wherein the instructions further include an airflow module for determining an estimated airflow based on at least one signal from the plurality of signals. 18. The system of claim 17, wherein the speed control module alters the actual speed of the dual fuel engine from the base engine speed in response to the changed operating condition. 19. The system of claim 18, wherein the speed control module alters the actual speed of the dual fuel engine so as to alter an actual airflow from the base airflow, based on the estimated airflow, to obtain the predetermined air-fuel ratio equal to or different from the base air-fuel ratio. 20. The system of claim 14, wherein the plurality of sensors comprises at least one of an altitude sensor, an ambient pressure sensor, and an ambient temperature sensor. 21. The system of claim 14, wherein the plurality of sensors comprises an emission sensor, an intake manifold temperature sensor, an exhaust manifold temperature sensor, an engine speed sensor, a fuel injection timing sensor, and an airflow sensor. 22. The system of claim 14, wherein the instructions further include the speed control module for altering the actual speed of the dual fuel engine so as to obtain the predetermined air-fuel ratio in response to the changed operating condition of the dual fuel engine determined based on the plurality of signals, so as to maintain a plurality of actual emissions from the dual fuel engine within a predetermined emission limit, an actual specific fuel consumption of the dual fuel engine within a predetermined specific fuel consumption limit, an actual in-cylinder peak pressure within a predetermined pressure limit, and an exhaust manifold temperature within a predetermined temperature limit. 23. A vehicle comprising: a dual fuel engine;a plurality of sensors coupled to the dual fuel engine;a control unit coupled to the dual fuel engine and the plurality of sensors; the control unit comprising: a signal acquisition system coupled to the plurality of sensors and configured to receive a plurality of signals from a plurality of sensors; andat least one processor coupled to the signal acquisition system, the at least one processor encoded with instructions to perform processing of the plurality of signals, the instructions including: a speed control module for altering an actual speed of the dual fuel engine to obtain a predetermined air-fuel ratio in response to the changed operating condition of the dual fuel engine determined based on the plurality of signals, so as to maintain operation of the dual fuel engine between knock and misfire conditions. 24. The system of claim 23, wherein the instructions further include a base condition module for determining a base operating condition comprising a base airflow, a base air-fuel ratio, a base substitution ratio, a base engine speed of the dual fuel engine operating, base engine power, and a base fuel injection timing. 25. The system of claim 24, wherein the instructions further include a changed condition module for determining the changed operating condition from the base operating condition of the dual fuel engine operating at same power level, based on the plurality of signals. 26. The system of claim 25, wherein the instructions further include an airflow module for determining an estimated airflow based on at least one signal from the plurality of signals. 27. The system of claim 26, wherein the speed control module alters the actual speed of the dual fuel engine from the base engine speed in response to the changed operating condition. 28. The system of claim 27, wherein the speed control module alters the actual speed of the dual fuel engine so as to alter an actual airflow from the base airflow, based on the estimated airflow, to obtain the predetermined air-fuel ratio equal to or different from the base air-fuel ratio. 29. The system of claim 23, wherein the instructions further include the speed control module for altering the actual speed of the dual fuel engine so as to obtain the predetermined air-fuel ratio in response to the changed operating condition of the dual fuel engine determined based on the plurality of signals, so as to maintain a plurality of actual emissions from the dual fuel engine within a predetermined emission limit, an actual specific fuel consumption of the dual fuel engine within a predetermined specific fuel consumption limit, an actual in-cylinder peak pressure within a predetermined pressure limit, and an exhaust manifold temperature within a predetermined temperature limit.
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