Dual compressor turbocharger
View Patent ↗A dual compressor turbocharger includes two compressors. One compressor supplies fuel pressure, and one compressor supplies air pressure. The dual compressor turbocharger includes a turbine driven by exhaust of an engine and a shaft coupled to the turbine. The first compressor is mounted on the shaft and includes a first inlet coupled to an air supply and a first outlet coupled to an air intake of the engine. The second compressor is mounted on the shaft and includes a second inlet coupled to a fuel supply and a second outlet coupled to a fuel supply rail of the engine.
1. An engine system comprising:
a turbine driven by exhaust of an engine;
a shaft coupled to the turbine;
a first compressor mounted on the shaft and having a first inlet coupled to an air supply and a first outlet coupled to an air intake of the engine;
a second compressor mounted on the shaft having a second inlet coupled to a fuel supply and a second outlet coupled to a fuel supply rail of the engine;
the engine having a plurality of cylinders, each of the plurality of cylinders having a venturi passage; and
a controller configured to generate a plurality of digital fuel injection drive signals including pulse trains, the digital fuel injection drive signals configured to release fuel from the fuel supply rail of the engine to plurality cylinders, each of the plurality of digital fuel injection drive signals corresponding to an individual one of the plurality of cylinders,
wherein the digital fuel injection drive signals are selected according to a type of gaseous fuel used by the engine.
2. The engine system of claim 1 , wherein the first compressor compresses air to a first pressure lower than a second pressure that the second compressor compresses fuel.
3. The engine system of claim 1 , wherein air from the first compressor and fuel from the second compressor are mixed downstream of the turbocharger and upstream of the engine.
4. The engine system of claim 1 , wherein air from the first compressor and fuel from the second compressor are not mixed within the turbocharger.
5. The engine system of claim 1 , wherein pressures of fuel and air are regulated by a common wastegate by controlling exhaust air flow associated with the turbine.
6. The engine system of claim 5 , wherein the common wastegate is controlled electronically.
7. The engine system of claim 1 , wherein the turbine for the first compressor and the second compressor has a variable geometry controlled electronically.
8. The engine system of claim 1 , wherein a capacity of the first compressor is greater than a capacity of the second compressor.
9. The engine system of claim 8 , wherein a capacity of the first compressor and the capacity of the second compressor define an air to fuel ratio.
10. The engine system of claim 1 , wherein air from the first compressor and fuel from the second compressor are mixed downstream of the turbocharger.
11. The engine system of claim 1 , wherein fuel is selectively injected from the fuel supply rail of the engine into the air intake of the engine.
12. An internal combustion engine comprising:
a fuel supply rail configured to deliver fuel to the internal combustion engine;
an air intake configured to deliver air to the internal combustion engine;
a turbine driven by exhaust of the internal combustion engine; a shaft coupled to the turbine;
a first compressor mounted on the shaft and having a first inlet coupled to an air supply and a first outlet coupled to the air intake of the engine;
a second compressor mounted on the shaft having a second inlet coupled to a fuel supply and a second outlet coupled to the fuel supply rail of the engine;
a manifold pressure sensor configured to measure a venturi pressure; and
a controller configured to generate a pulse train as a digital fuel injection drive signal based on the venturi pressure, the digital fuel injection drive signal selected to release fuel from the fuel supply rail of the internal combustion engine to at least one of a plurality of cylinders according to the venturi pressure.
13. The internal combustion engine of claim 12 , wherein the air intake includes a venturi, wherein an air and fuel mixture is only downstream of the venturi.
14. The internal combustion engine of claim 13 , wherein the venturi creates a pressure that draws fuel from the fuel supply rail.
15. The internal combustion engine of claim 12 , wherein air from the first compressor and fuel from the second compressor are mixed downstream of the turbocharger.
16. The internal combustion engine of claim 12 , further comprising:
a wastegate for controlling exhaust air flow associated with the turbine.
17. The internal combustion engine of claim 12 , wherein the turbine has a variable geometry controlled electronically.
18. The internal combustion engine of claim 12 , wherein a capacity of the first compressor is greater than a capacity of the second compressor, and the capacity of the first compressor and the capacity of the second compressor define an air to fuel ratio.
19. A method comprising: driving a turbine from exhaust of an engine; rotating a shaft coupled to the turbine;
generating air pressure by a first compressor mounted on the shaft and having a first inlet coupled to an air supply and a first outlet coupled to an air intake of the engine;
generating fuel pressure by a second compressor mounted on the shaft having a second inlet coupled to a fuel supply and a second outlet coupled to a fuel supply rail of the engine;
drawing fuel from the fuel supply rail via suction pressure generated by the air traveling through a venturi;
determining a type of gaseous fuel used by the engine; and
generating, based on the type of gaseous fuel, a digital pulse train for a fuel injection drive signal to release fuel from the fuel supply rail of the engine to at least one of a plurality of cylinders.
20. The method of claim 19 , wherein air from the first compressor and fuel from the second compressor are mixed downstream of the turbocharger.