Air-fuel-ratio dithering using a dual fuel path source
An apparatus for dithering fuel into an internal combustion engine includes a turbine that is powered by the internal combustion engine and a first fuel injector that injects a first fuel into an air stream to create a fuel/air stream. The apparatus also includes an air/fuel compressor that provides a compressed fuel/air stream to the internal combustion engine. The air/fuel compressor is powered by the turbine, and the air/fuel compressor compresses the fuel/air stream to create the compressed fuel/air stream. Additionally, the apparatus includes a second fuel injector that injects a second fuel into the compressed fuel/air stream prior to the compressed fuel/air stream entering the engine and after the compressed fuel/air stream exits the air/fuel compressor.
1. An apparatus for dithering fuel into an internal combustion engine, the apparatus comprising:
a turbine powered by the internal combustion engine;
a first fuel injector that injects a first fuel into an air stream to create a fuel/air stream;
an air/fuel compressor that provides a compressed fuel/air stream to the internal combustion engine, the air/fuel compressor being powered by the turbine, the air/fuel compressor compressing the fuel/air stream to create the compressed fuel/air stream; and
a second fuel injector that injects a second fuel into the compressed fuel/air stream prior to the compressed fuel/air stream entering the engine and after the compressed fuel/air stream exits the air/fuel compressor.
2. The apparatus of claim 1 , further comprising a catalyst in exhaust receiving communication with the engine.
3. The apparatus of claim 1 , further comprising a charge air cooler that cools the compressed fuel/air stream, the charge air cooler being positioned in the compressed fuel/air stream between the fuel/air compressor and the engine, the second fuel injector injecting the second fuel into the compressed fuel/air stream after the compressed fuel/air stream leaves the charge air cooler.
4. The apparatus of claim 1 , wherein the second fuel injector injects a compressed second fuel into the compressed fuel/air stream.
5. The apparatus of claim 4 , further comprising a fuel compressor separate from the fuel/air compressor, the fuel compressor being configured to compress the second fuel injected by the second fuel injector.
6. The apparatus of claim 5 , wherein the fuel compressor is powered by a power source other than the turbine.
7. The apparatus of claim 1 , wherein the second fuel injector injects the second fuel into the compressed fuel/air stream only in response to a transient loading condition of the engine.
8. The apparatus of claim 1 , wherein the second fuel injector injects the second fuel into the compressed fuel/air stream during steady-state and transient loading conditions of the engine.
9. The apparatus of claim 8 , wherein the second fuel injector injects more of the second fuel into the compressed fuel/air stream during increased transient loading conditions on the engine, and injects less of the second fuel into the compressed fuel/air stream during decreased transient loading conditions of the engine.
10. The apparatus of claim 1 , wherein at least one of the first and second fuels is a gaseous fuel.
11. The apparatus of claim 1 , wherein the first and second fuels are the same.
12. The apparatus of claim 1 , wherein the first and second fuels are different.
13. An apparatus for dithering fuel into an internal combustion engine, the apparatus comprising:
a turbine powered by exhaust from the internal combustion engine;
a first fuel injector that injects a portion of fuel into an air stream to create a fuel/air stream;
an air/fuel compressor that provides a compressed fuel/air stream, the air/fuel compressor powered by the turbine, the air/fuel compressor compressing the fuel/air stream to create the compressed fuel/air stream;
a charge air cooler that cools the compressed fuel/air stream, the charge air cooler receiving the compressed fuel/air stream from the compressor and providing the compressed fuel/air stream to the engine;
a fuel compressor that compresses another portion of the fuel to form a compressed fuel; and
a second fuel injector that injects the compressed fuel from the fuel compressor into the compressed fuel/air stream prior to the compressed fuel/air stream entering the engine and after the compressed fuel/air stream exits the charge air cooler.
14. The apparatus of claim 12 , wherein the fuel compressor is powered by a source other than the turbine.
15. The apparatus of claim 13 , further comprising an alternator, and wherein the fuel compressor is powered by the alternator.
16. The apparatus of claim 12 , wherein the second fuel injector injects the compressed fuel into the compressed fuel/air stream in response to a transient loading condition on the engine.
17. The apparatus of claim 16 , further comprising a fuel flow module that adjusts flow volume of the compressed fuel/air stream into the engine to adjust engine output, and a dithering module that adjusts an amount of fuel injected by the second fuel injector into the compressed fuel/air stream in response to a transient loading condition of the engine.
18. A method for dithering fuel into an internal combustion engine, the method comprising:
injecting fuel into an air stream to create a fuel/air stream;
compressing the fuel/air stream to create a compressed fuel/air stream;
combusting the compressed fuel/air stream; and
dithering fuel into the compressed fuel/air stream before the fuel/air stream is combusted.
19. The method of claim 18 , wherein fuel is dithered into the compressed fuel/air stream only in response to a transient loading condition of the engine.
20. The method of claim 18 , wherein dithering fuel into the compressed fuel/air stream comprises adjusting the quantity of the dithered fuel in response to a transient loading condition of the engine.