Internal combustion engine with common rail pilot and main injection

Patent metadata

Field	Value
Publication number	US-9957885-B2
Application number	US-201715707000-A
Country	US
Kind code	B2
Filing date	Sep 18, 2017
Priority date	Mar 12, 2013
Publication date	May 1, 2018
Grant date	May 1, 2018

Abstract

An internal combustion engine includes first and second common rails each having a metering or pressure regulating valve, with the valves settable at different pressure values from one another. Rotors are each sealingly and rotationally received within a respective cavity to define at least one combustion chamber of variable volume. The engine includes for each of the rotors a pilot subchamber in communication with the respective cavity, a pilot fuel injector in communication with the pilot subchamber, an ignition element positioned to ignite fuel within the pilot subchamber, and a main fuel injector in communication with the respective cavity at a location spaced apart from the pilot subchamber. Each main fuel injector is in fluid communication with the first common rail and each pilot fuel injector is in fluid communication with the second common rail. A method of combusting fuel in an internal combustion engine is also provided.

First claim

The invention claimed is:

1. A rotary internal combustion engine comprising:
a first common rail having a first metering or pressure regulating valve in fluid communication therewith;
a second common rail having a second metering or pressure regulating valve in fluid communication therewith, the first and second metering or pressure regulating valves being settable at different pressure values from one another; and
at least two rotors each sealingly and rotationally received within a respective cavity to define at least one combustion chamber of variable volume, the engine including, for each of the rotors:
a pilot subchamber in communication with the respective cavity,
a pilot fuel injector in communication with the pilot subchamber,
an ignition element positioned to ignite fuel within the pilot subchamber, and
a main fuel injector in communication with the respective cavity at a location spaced apart from the pilot subchamber;

wherein each main fuel injector is in fluid communication with the first common rail and each pilot fuel injector is in fluid communication with the second common rail.

2. The engine as defined in claim 1 , further comprising a first pump in fluid communication with a fuel source and with an inlet of the first common rail and a second pump in fluid communication with the fuel source and with an inlet of the second common rail.

3. The engine as defined in claim 2 , wherein the first metering or pressure regulating valve is provided at an outlet of the first common rail, the second metering or pressure regulating valve is provided at an outlet of the second common rail, and the outlets of the first and second metering or pressure regulating valves are in fluid communication with the fuel source.

4. The engine as defined in claim 2 , wherein the first and second pumps and the first and second metering or pressure regulating valves are actuable by an engine control unit.

5. The engine as defined in claim 1 , wherein the main and pilot fuel injectors have a size and configuration similar to each other.

6. The engine as defined in claim 1 , wherein the main and pilot fuel injectors have tip openings through which the fuel is injected, and an open area defined by the tip openings of the pilot fuel injector is smaller than that defined by the tip openings of the main fuel injector.

7. The engine as defined in claim 1 , wherein the first metering or pressure regulating valve is provided at an outlet of the first common rail and the second metering or pressure regulating valve is provided at an outlet of the second common rail.

8. The engine as defined in claim 1 , wherein each respective cavity is defined by two axially spaced apart end walls and a peripheral wall extending between the end walls, and each of the at least two rotors is rotatable within the respective cavity in sealing engagement with the peripheral and end walls.

9. The engine as defined in claim 8 , wherein each of the at least two rotors has three circumferentially spaced apex portions and the respective cavity defines an epitrochoid shape with two lobes, the at least one combustion chamber include three rotating chambers of variable volume, the at least two rotors being engaged to an eccentric portion of a shaft to rotate and perform orbital revolutions within the respective cavity with each of the apex portions remaining in sealing engagement with the peripheral wall and separating the chambers.

10. A rotary internal combustion engine comprising:
a first common rail having a first metering or pressure regulating valve in fluid communication therewith;
a second common rail having a second metering or pressure regulating valve in fluid communication therewith, the first and second metering or pressure regulating valves being settable at different pressure values from one another;
an outer body having at least two rotor cavities each defined by two axially spaced apart end walls and a peripheral wall extending between the end walls;
a rotor received in each of the at least two rotor cavities, each rotor being rotatable within the rotor cavity in sealing engagement with the peripheral and end walls and defining at least one chamber of variable volume in the rotor cavity; and
for each of the rotor cavities:
a pilot subchamber defined in the outer body in fluid communication with the rotor cavity,
a pilot fuel injector in communication with the pilot subchamber,
an ignition element positioned to ignite fuel within the pilot subchamber, and
a main fuel injector in communication with the rotor cavity at a location spaced apart from the pilot subchamber;

wherein each main fuel injector is in fluid communication with the first common rail and each pilot fuel injector is in fluid communication with the second common rail.

11. The engine as defined in claim 10 , wherein each rotor cavity defines an epitrochoid shape with two lobes, and each rotor has three circumferentially spaced apex portions, and the at least one combustion chamber include three rotating chambers of variable volume, the rotor being engaged to an eccentric portion of a shaft to rotate and perform orbital revolutions within the rotor cavity with each of the apex portions remaining in sealing engagement with the peripheral wall and separating the chambers.

12. The engine as defined in claim 10 , further comprising a first pump in fluid communication with a fuel source and with an inlet of the first common rail and a second pump in fluid communication with the fuel source and with an inlet of the second common rail.

13. The engine as defined in claim 12 , wherein the first metering or pressure regulating valve is provided at an outlet of the first common rail, the second metering or pressure regulating valve is provided at an outlet of the second common rail, and the outlets of the first and second metering or pressure regulating valves are in fluid communication with the fuel source.

14. The engine as defined in claim 10 , wherein the main and pilot fuel injectors have a size and configuration similar to each other.

15. The engine as defined in claim 10 , wherein the pilot fuel injector and the main fuel injector have tip openings through which the fuel is injected, and an open area defined by the tip openings of the pilot fuel injector is smaller than that defined by the tip openings of the main fuel injector.

16. The engine as defined in claim 10 , wherein the first metering or pressure regulating valve is provided at an outlet of the first common rail.

17. The engine as defined in claim 10 , wherein the second metering or pressure regulating valve is provided at an outlet of the second common rail.

18. A method of combusting fuel in an internal combustion engine having at least two rotors each defining at least one combustion chamber, the method comprising:
pressurizing the fuel in a first common rail at a first pressure;
pressurizing the fuel in a second common rail separate from the first common rail at a second pressure different from the first pressure; and
for each of the rotors of the engine:
feeding a respective pilot injector with fuel at the second pressure from the second common rail to inject fuel in a respective pilot subchamber,
igniting the fuel within the respective pilot subchamber,
circulating the ignited fuel out of the respective pilot subchamber and into the one of the combustion chambers, and
feeding a respective main injector with fuel at the first pressure from the first common rail to inject fuel into the one of the combustion chambers spaced apart from the respective

Assignees

• Pratt & Whitney Canada

Inventors

• Thomassin Jean
• Schulz Edwin

Classifications

• Y02T10/142

  Cross-Sectional Technologies · mapped topic

• Y02T10/17

  Cross-Sectional Technologies · mapped topic

• F02B2275/32

  Miller cycle · CPC title

• F02D41/3836

  Controlling the fuel pressure · CPC title

• F01C1/22

  of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth- equivalents than the outer member · CPC title