초록 ▼

An engine control system determines a desired temperature range of air flowing into an intake manifold of the engine as a function of an operating characteristic, such as the load on the engine or the operating speed of the engine. A bypass conduit is provided in parallel with a heat exchanger, wher

An engine control system determines a desired temperature range of air flowing into an intake manifold of the engine as a function of an operating characteristic, such as the load on the engine or the operating speed of the engine. A bypass conduit is provided in parallel with a heat exchanger, wherein both the bypass conduit and the heat exchanger are connected to an outlet of a compressor to direct air from the compressor to an intake manifold along the parallel paths. By manipulating an air valve in the bypass conduit, an engine control unit can regulate the temperature at an inlet of the intake manifold. A desired temperature is selected from a matrix of stored values as a function of the load on the engine and the engine operating speed.

대표청구항 ▼

We claim: 1. A method for controlling a marine engine control system for an outboard motor comprising: an intake manifold directing combustion air to cylinders of an internal combustion engine; a compressor having an inlet and an outlet and compressing air flowing to said intake manifold; a charge

We claim: 1. A method for controlling a marine engine control system for an outboard motor comprising: an intake manifold directing combustion air to cylinders of an internal combustion engine; a compressor having an inlet and an outlet and compressing air flowing to said intake manifold; a charge air cooler having an inlet and an outlet and cooling compressed air flowing to said intake manifold; a first bypass conduit having an inlet and an outlet; a second bypass conduit having an inlet and an outlet; a first junction having an inlet from said outlet of said compressor, and having first and second outlets, said first outlet of said first junction being connected to said inlet of said charge air cooler, said second outlet of said first junction being connected to said inlet of said first bypass conduit; a second junction having first and second inlets, and having first and second outlets, said first inlet of said second junction being connected to said outlet of said charge air cooler, said second inlet of said second junction being connected to said outlet of said first bypass conduit, said first outlet of said second junction being connected to said intake manifold, said second outlet of said second junction being connected to said inlet of said second bypass conduit, said method comprising controllably changing the temperature of compressed air flowing to said intake manifold as a function of at least one operating characteristic of said engine. 2. The method according to claim 1 comprising controllably changing said temperature of said compressed air flowing to said intake manifold by controlling cooling thereof by said charge air cooler. 3. The method according to claim 2 comprising providing said charge air cooler as a heat exchanger, and pumping water through said heat exchanger, and comprising controllably changing said temperature of said compressed air flowing to said intake manifold by variably changing at least one of the amount of air flowing through said heat exchanger and the amount of water flowing through said heat exchanger. 4. The method according to claim 3 comprising: providing an air valve controlling the amount of air flow through said first bypass conduit; controllably changing the temperature of compressed air flowing to said intake manifold by variably changing the amount of air flowing through said heat exchanger by varying the amount of air flow through said first bypass conduit by operating said air valve. 5. The method according to claim 3 comprising: providing a water valve controlling the amount of water flow through said heat exchanger; controllably changing the temperature of compressed air flowing to said intake manifold by variably changing the amount of water flowing through said heat exchanger by varying the amount of water flow therethrough by operating said water valve. 6. The method according to claim 3 comprising providing a first valve, and providing at least one of a second and third valve, said first valve being an air valve controlling the amount of air flow through said second bypass conduit, said second valve being a water valve controlling the amount of water flow through said heat exchanger, said third valve being an air valve controlling the amount of air flow through said first bypass conduit, and comprising controlling the amount of compressed air flowing to said intake manifold by operating said first valve, and controllably changing the temperature of compressed air flowing to said intake manifold by operating at least one of said second and third valves. 7. The method according to claim 1 wherein said at least one operating characteristic of said engine comprises a load on said engine. 8. The method according to claim 1 wherein said at least one operating characteristic of said engine comprises an operating speed of said engine. 9. A marine engine control system for an outboard motor comprising: an intake manifold directing combustion air to cylinders of an internal combustion engine; a compressor having an inlet and an outlet and compressing air flowing to said intake manifold; a charge air cooler having an inlet and an outlet and cooling compressed air flowing to said intake manifold; a first bypass conduit having an inlet and an outlet; a second bypass conduit having an inlet and an outlet; a first junction having an inlet from said outlet of said compressor, and having first and second outlets, said first outlet of said first junction being connected to said inlet of said charge air cooler, said second outlet of said first junction being connected to said inlet of said first bypass conduit; a second junction having first and second inlets, and having first and second outlets, said first inlet of said second junction being connected to said outlet of said charge air cooler, said second inlet of said second junction being connected to said outlet of said first bypass conduit, said first outlet of said second junction being connected to said intake manifold, said second outlet of said second junction being connected to said inlet of said second bypass conduit. 10. The marine engine control system according to claim 9 wherein said first and second bypass conduits are connected in series between said first junction and said inlet of said compressor. 11. The marine engine control system according to claim 10 wherein said second junction is connected in series between said first and second bypass conduits. 12. The marine engine control system according to claim 9 wherein: said first bypass conduit is connected in parallel with said charge air cooler; said second bypass conduit is connected in parallel with said compressor and said charge air cooler. 13. The marine engine control system according to claim 9, wherein: said compressor and said charge air cooler are connected in series, with said first junction being connected in series therebetween; said compressor and said first bypass conduit are connected in series, with said first junction being connected in series therebetween; said second bypass conduit is connected in parallel with the series connection of said compressor and said charge air cooler; said second bypass conduit is connected in parallel with the series connection of said compressor and said first bypass conduit. 14. The marine engine control system according to claim 9 comprising three air flow path portions comprising: a first air flow path portion from said first junction through said charge air cooler to said second junction; a second air flow path portion from said first junction through said first bypass conduit to said second junction; a third air flow path portion from said second junction through said second bypass conduit to said inlet of said compressor. 15. The marine engine control system according to claim 14 comprising a pair of valves comprising: a first valve in said second air flow path and controlling the amount of air flowing through said first air flow path; a second valve in said third air flow path and controlling the amount of air flowing to said intake manifold. 16. The marine engine control system according to claim 15 wherein: said first and second valves are connected in series between said outlet of said compressor and said inlet of said compressor; said second junction is connected in series between said first and second valves; said second junction is connected in series between said outlet of said charge air cooler and said intake manifold.