Internal combustion engine turbosystem and method

• US 4,885,911 A
• Filed: 02/24/1988
• Issued: 12/12/1989
• Est. Priority Date: 02/24/1988
• Status: Expired due to Fees

• Current Assignee: Niels J. Beck, William E. Woollenweber
• Original Assignee: Niels J. Beck, William E. Woollenweber
• Inventors: Woollenweber, William E., Beck, Niels J.
• Primary Examiner(s): Koczo, Michael
• Application Number:
  US07/159,840
• Time in Patent Office: 657 Days
• Field of Search: 60/597, 60/599, 60/605.1, 60/605.3, 60/614, 60/607, 60/608, 60/316, 123/41.11, 123/41.12, 123/41.42, 123/41.65, 123/41.49, 123/196 AB, 123/563
• US Class Current: 60/597
• CPC Class Codes: F01N 13/082 of tailpipe, e.g. with means for mixing air with exhaust for exhaust cooling, dilution or evacuation F01N13/20 takes precedence
• CPC Class Codes: F01P 11/08 Arrangements of lubricant coolers in lubrication apparatus F01M
• CPC Class Codes: F01P 5/08 Use of engine exhaust gases for pumping cooling-air
• CPC Class Codes: F01P 9/00 Cooling having pertinent characteristics not provided for in, or of interest apart from, groups F01P1/00 - F01P7/00 profiting from waste heat of combustion-engine cooling F02G5/00
• CPC Class Codes: F02B 29/0412 Multiple heat exchangers arranged in parallel or in series
• CPC Class Codes: F02B 29/0425 Air cooled heat exchangers
• CPC Class Codes: F02B 29/0431 Details or means to guide the ambient air to the heat exchanger, e.g. having a fan, flaps, a bypass or a special location in the engine compartment
• CPC Class Codes: F02B 37/005 Exhaust driven pumps being combined with an exhaust driven auxiliary apparatus, e.g. a ventilator
• CPC Class Codes: F02B 37/007 with exhaust-driven pumps arranged in parallel , e.g. at least one pump supplying alternatively
• CPC Class Codes: F02B 37/18 by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

An exhaust-driven cooling system for an internal combustion engine includes a turbocooler having an exhaust-driven turbine and fan means to generate a flow of cooling air for use in an internal combustion engine heat exchanger to dissipate heat losses of the engine. The system can provide internal combustion engines with substantially reduced temperatures and pressures for its exhaust gas and exhaust system components and substantially improved reliability and efficiency.

Claims

1. An oil-only, internal combustion engine system with an exhaust-driven, cooling system, comprising:

a multi-cylinder, internal, combustion-engine assembly;

means for providing a mixture of fuel and air to the internal combustion engine assembly;

means for carrying the product of the combusted fuel-air mixture from the internal combustion engine assembly;

means for providing a flow of lubricant to and from the internal combustion engine assembly for lubricating the internal combustion engine assembly and for carrying heat generated by operation of the internal combustion engine assembly away from the internal combustion engine assembly;

an oil cooler, connected with said means for providing a flow of lubricant, to dissipate the heat carried by said lubricant from the internal combustion engine assembly prior to its return to the internal combustion engine assembly;

a turbocooler having a turbine connected with the means to carry the product of the combusted fuel-air mixture from the internal combustion engine assembly so that the exhaust gas carried from the internal combustion engine assembly by said exhaust means drives the turbine of the turbocooler, said turbocooler also having a ducted fan means driven by the turbine of the turbocooler, said ducted fan means communicating with atmosphere and generating a ducted flow of cooling air;

means for directing the flow of cooling air generated by the fan means of said turbocooler through the oil cooler to cool the lubricant and dissipate the heat generated in operation of the internal combustion engine assembly; and

means for directing the cooling air generated by said turbocooler from said oil cooler to said means for carrying the product of the combusted fuel-air mixture from said internal combustion engine assembly, said means for directing the cooling air including a portion forming a cooling air inlet surrounding said means for carrying the combusted fuel-air product prior to its leaving the exhaust-carrying means, thereby substantially reducing both the temperature and the pressure of the internal combustion engine exhaust.

2. A method of providing cooling for an internal combustion engine using the exhaust gas of the engine, comprising:

directing the exhaust gas from said engine to a turbocooling device having a turbine and a ducted fan means;

driving the turbine and ducted fan means of the turbocooling device with the exhaust gas of the internal combustion engine;

directing ambient air to the turbine-driven ducted fan means of the turbocooling device;

generating a ducted flow of cooling air with said ducted turbine-driven fan means;

directing the ducted flow of cooling air from said ducted fan means of the turbocooler to a heat exchanger connected with said internal combustion engine to receive heated coolant from the internal combustion engine;

cooling said heated coolant with the ducted cooling air from said turbocooler;

directing the ducted cooling air to an exhaust from the turbocooler device;

surrounding the exhaust from the turbocooler device with the ducted cooling air; and

reducing the temperature and pressure in the exhaust system with said ducted cooling air prior to its release to atmosphere.

3. The method of claim 2 wherein the exhaust gas temperature is lowered to a temperature below about 500°

F. (260°

C.).

4. The method of claim 2 further including the step of driving a gear-reduction device by mechanically linking it to said turbocooling device and thereby providing a driving means for engine accessories.

5. A method of turbocompounding an internal combustion engine, comprising:

directing a flow of exhaust from the internal combustion engine to a turbocooling device having a turbine portion and a fan portion;

driving the turbine portion of the turbocooling device with the exhaust gas, thereby driving the fan portion of the turbocooling device;

generating a flow of cooling air with the fan portion of the turbocooling device;

driving the turbine portion of a turbocharger with the exhaust gas, thereby driving the compressor portion of the turbocharger;

compressing ambient air with the compressor of said turbocharger, thereby generating a flow of charge-air for introduction into said engine;

directing said compressed charge-air through a first charge-air cooling means;

directing a flow of cooling air through said first charge-air cooling means, thereby lowering the temperature of said charge air;

compressing said charge-air further with a compressor of a compressor-expander device;

directing said further compressed charge-air through a second charge-air cooling means;

directing a flow of cooling air through said second charge-air cooling means, thereby lowering the temperature of said further compressed charge-air;

directing said cooled, further compressed charge-air from said second charge-air cooling means to an expander of the compressor-expander device;

expanding the cooled, further compressed charge-air with the expander of said compressor-expander device to further cool said cooled, further compressed charge-air;

introducing said further cooled, compressed charge-air into said internal combustion engine; and

cooling coolant from said engine with said cooling air.

6. The method of claim 5 wherein the first and second charge-air cooling means comprise air-to-air heat exchangers.

7. The method of claim 5 wherein the cooling air flow produced by said turbocooler is directed initially to the first and second charge-air cooling means and is directed secondly from said first and second charge-air cooling means to a heat exchanger for cooling the coolant employed by said engine.

8. The method of claim 5 including the further step of lastly directing the exhaust gas to an exhaust system located adjacent said turbocooler device and mixing the coolant air and exhaust gas to reduce the final exhaust gas temperature.

9. The method of claim 5 wherein the engine is both cooled and lubricated by a common fluid.

10. The method of claim 9 wherein said common fluid employed by said lubricating and cooling systems of said engine is a synthetic oil.

11. An internal combustion engine system with an exhaust-driven, cooling system, comprising:

a multi-cylinder internal combustion engine assembly;

means for carrying the product of the combusted fuel-air mixture from the internal combustion engine assembly;

means for providing a flow of coolant to and from the internal combustion engine assembly for carrying heat generated by operation of the internal combustion engine assembly away from the internal combustion engine assembly;

a heat exchanger connected with said means for providing a flow of coolant to dissipate the heat carried by said coolant from the internal combustion engine assembly prior to its return to the internal combustion engine assembly;

a turbocooler having an exhaust-driven turbine and ducted fan means for generating a ducted flow of cooling air;

means to direct the ducted flow of cooling air generated by the exhaust-driven ducted fan means of said turbocooler through the heat exchanger to cool the coolant and dissipate the heat losses generated by the internal combustion engine assembly; and

means for directing the ducted flow of cooling air generated by said turbocooler from said heat exchanger to an engine exhaust system portion adapted to use the cooling air to surround and cool the engine exhaust gas prior to its leaving the exhaust system.

12. The internal combustion engine system of claim 11 further comprising means for providing a mixture of fuel and air to the internal combustion engine assembly, including a turbocharger having a turbine connected with the means to carry the product of the combusted fuel-air mixture from the internal combustion engine assembly so that the exhaust gas drives the turbine of the turbocharger, said turbocharger also having a compressor driven by the turbine of the turbocharger to deliver a flow of pressurized charge-air to the cylinders of the internal combustion engine assembly;

and

a first charge-air cooler connected between the charge-air compressor of the turbocharger and the cylinders of the internal combustion engine assembly,

said system further comprising means for directing the ducted flow of cooling air generated by the ducted fan means of the turbocooler through the charge-air cooler.

13. The internal combustion engine system of claim 11 wherein the engine exhaust system portion includes an exhaust outlet and a cooling air inlet, said cooling air inlet surrounding said exhaust outlet and directing the cooling air to lower the pressure of the engine exhaust and to mix the cooling air and engine exhaust prior to their leaving the system.

14. An oil-only, internal combustion engine system with an exhaust-driven, cooling system, comprising:

a multi-cylinder, internal, combustion-engine assembly;

means for providing a mixture of fuel and air to the internal combustion engine assembly;

means for carrying exhaust gas from the internal combustion engine assembly;

means for providing a flow of lubricant to and from the internal combustion engine assembly for lubricating the internal combustion engine assembly and for carrying heat generated by operation of the internal combustion engine assembly away from the internal combustion engine assembly;

an oil cooler, connected with said means for providing a flow of lubricant, to dissipate the heat carried by said lubricant from the internal combustion engine assembly prior to its return to the internal combustion engine assembly;

a turbocooler having a turbine connected with the means to carry exhaust gas from the internal combustion engine assembly so that the exhaust gas carried from the internal combustion engine assembly by said exhaust-carrying means drives the turbine of the turbocooler, said turbocooler also having a fan means driven by the turbine of the turbocooler, said fan means communicating with atmosphere and generating a flow of cooling air; and

means for directing the flow of cooling air generated by the fan means of said turbocooler through the oil cooler to cool the lubricant and dissipate the heat generated in operation of the internal combustion engine assembly,

said means for providing a mixture of fuel and air to the internal combustion engine assembly comprising;

a turbocharger having a turbine connected with the means to carry the exhaust gas from the internal combustion engine assembly so that the exhaust gas carried from the internal combustion engine assembly by said exhaust-carrying means drives the turbine of the turbocharger, said turbocharger also having a charge-air compressor driven by the turbine of the turbocharger to deliver a flow of pressurized charge-air to the cylinders of the internal combustion engine assembly;

a charge-air cooler connected between the charge-air compressor of the turbocharger and the cylinders of the internal combustion engine assembly; and

means for directing the cooling air generated by the fan means of the turbocooler through the charge-air cooler.

15. The oil-only internal combustion engine system of claim 14 wherein said means for directing the cooling air generated by the fan means of the turbocooler through the oil cooler includes said means for directing cooling air generated by the fan means of the turbocooler through the first charge-air cooler.

16. The oil-only internal combustion engine system of claim 15 wherein the cooling air is directed from the fan means of the turbocooler first through the charge-air cooler and secondly through the oil cooler.

17. The oil-only internal combustion engine system of claim 16 further comprising means for directing the cooling air generated by said turbocooler from said oil cooler to an engine exhaust system, said engine exhaust system being adapted to use the cooling air from the oil cooler to mix with and cool the engine exhaust gas prior to its leaving the exhaust system, thereby substantially reducing the temperature and pressure of the internal combustion engine exhaust gas.

18. The oil-only, internal combustion engine system of claim 14 wherein the multi-cylinder, internal combustion engine assembly is a V engine with one set of cylinders in each side of the V engine, and said means for carrying exhaust gas from the internal combustion engine assembly includes a first exhaust system for the cylinders in one side of the V engine and a second exhaust system for the cylinders in the other side of the V engine.

19. The oil-only, internal combustion engine system of claim 14 wherein said means for directing the cooling air generated by the fan means of the turbocooler through the charge-air cooler has an input connected with atmosphere and an output connected with the fan means of the turbocooler whereby cooling air flows from atmosphere through the charge-air cooler prior to compression by the fan means of the turbocooler.

20. The oil-only, internal combustion engine system of claim 14 further comprising:

a compressor-expander device having a second charge-air compressor and a charge-air-driven expander;

a second charge-air cooler;

means for directing charge-air from said first charge-air cooler through the second charge-air compressor, the second charge-air cooler, and the charge-air-driven expander and then to the cylinders of the internal combustion engine assembly,

said second charge-air compressor further compressing the charge-air for direction to the second charge air cooler, said second charge-air cooler cooling the further compressed charge-air for direction to the charge-air-driven expander of the compressor-expander device, and said the charge-air-driven expander of the compressor-expander device expanding the cooled further compressed charge-air to provide a flow of cold, compressed charge-air to the cylinders of the internal combustion engine assembly and to drive the second charge-air compressor; and

means for directing the cooling air generated by the fan means of the turbocooler through the second charge-air cooler.

21. The oil-only, internal combustion engine of claim 20 wherein said means for directing the cooling air generated by the fan means of the turbocooler through the oil cooler includes both said means for directing cooling air generated by the fan means of the turbocooler through said first charge-air cooler and said means for directing cooling air generated by the fan means of the turbocooler through said second charge air cooler.

22. The oil-only internal combustion engine system of claim 14 wherein said turbocooler drives a high-speed gear-reduction system, and the output of the high-speed gear-reduction system drives one or more internal combustion engine accessory devices.

23. A method of providing cooling for an internal combustion engine using the exhaust gas of the engine, comprising:

directing the exhaust gas from said engine to a turbocooling device having a turbine and a fan means;

driving the turbine and fan means of the turbocooling device with the exhaust gas of the internal combustion engine;

directing ambient air to the turbine-driven fan means of the turbocooling device;

generating a flow of cooling air with said turbine-driven fan means;

directing the cooling air from said fan means of the turbocooler to a heat exchanger connected with said internal combustion engine to receive heated coolant from the internal combustion engine;

cooling said heated coolant with the cooling air from said turbocooler;

directing the exhaust gas from said engine to a turbocharger device having a turbine and a compressor;

driving the turbine and compressor of the turbocharger with the exhaust gas of the internal combustion engine;

directing ambient air to the compressor of the turbocharger;

compressing the ambient air with the compressor of the turbocharger to create compressed charge-air for said engine;

directing the compressed charge-air from the compressor of the turbocharger to a first charge-air cooler;

generating a flow of cooling air through the first charge-air cooler with the fan means of the turbocooler; and

cooling the compressed charge-air with the flow of cooling air prior to directing the compressed ambient air to the internal combustion engine.

24. The method of claim 23 wherein said cooling means includes ambient air directed initially to the first charge-air cooler and subsequently to the fan means of the turbocooling device, and said cooling air leaving the fan means of the turbocooler is directed to the heat exchanger for engine coolant.

25. The method of claim 23 wherein said cooling air from the fan means of the turbocooler is directed initially to the first charge-air cooler and subsequently from the first charge-air cooler to the heat exchanger for engine coolant.

26. The method of claim 23 wherein the internal combustion engine is a V-type engine with cylinders divided between each side of the V-type engine and with separate exhaust systems for the cylinders on each side of the V-type engine, and exhaust gas from one side of the V-type engine drives one turbocharger and exhaust gas from the other side of the V-type engine drives another turbocharger.

27. The method of claim 23 further comprising the steps of:

directing the compressed charge-air from said first charge-air cooler to a compressor of a compressor-expander device to further compress the charge-air;

directing the further compressed charge-air to a second charge-air cooler to further cool the further compressed charge-air;

directing the cooled further compressed charge-air to the expander of the compressor-expander device;

expanding the cooled further compressed charge-air with said expander of the compressor-expander device;

further cooling said charge-air and driving said expander and compressor of the compressor-expander device; and

directing said further cooled charge-air to said engine.

28. An internal combustion engine assembly with an exhaust-driven, cooling system, comprising:

a multi-cylinder internal combustion engine assembly;

means for carrying exhaust gas from the internal combustion engine assembly;

means for providing a flow of coolant to and from the internal combustion engine assembly for carrying heat generated by operation of the internal combustion engine assembly away from the internal combustion engine assembly;

a heat exchanger connected with said means for providing a flow of coolant to dissipate the heat carried by said coolant from the internal combustion engine assembly prior to its return to the internal combustion engine assembly;

a turbocooler having an exhaust-driven fan means for generating a flow of cooling air;

means to direct the flow of cooling air generated by the exhaust-driven fan means of said turbocooler through the heat exchanger to cool the coolant and dissipate the heat losses generated by the internal combustion engine assembly;

means for directing the cooling air generated by said turbocooler from said heat exchanger to an engine exhaust system portion adapted to use the cooling air to cool the engine exhaust gas prior to its leaving the exhaust system;

means for providing a mixture of fuel and air to the internal combustion engine assembly, including a turbocharger having a turbine connected with the means to carry the exhaust gas from the internal combustion engine assembly so that the exhaust gas drives the turbine of the turbocharger, said turbocharger also having a compressor driven by the turbine of the turbocharger to deliver a flow of pressurized charge-air to the cylinders of the internal combustion engine assembly; and

a first charge-air cooler connected between the charge-air compressor of the turbocharger and the cylinders of the internal combustion engine assembly,

said system further comprising means for directing the cooling air generated by the fan means of the turbocooler through the charge-air cooler.

29. The internal combustion engine system of claim 28 wherein said means for directing the cooling air generated by the fan means of the turbocooler through the first charge-air cooler includes said means to direct the flow of cooling air generated by the exhaust-driven fan means of said turbocooler through the heat exchanger.

30. The internal combustion engine system of claim 29 wherein the cooling air is directed from the fan means of the turbocooler first through the first charge-air cooler and secondly through the heat exchanger.

31. The internal combustion engine system of claim 28 wherein said means for directing the cooling air generated by the fan means of the turbocooler through the first charge-air cooler has an input connected with atmosphere and an output connected with the fan means of the turbocooler whereby cooling air flows from atmosphere through the charge-air cooler prior to compression by the fan means of the turbocooler.

32. An internal combustion engine assembly, comprising:

a multi-cylinder internal combustion engine producing exhaust gas;

means for providing flows of a plurality of fluids in operation of the internal combustion engine assembly;

means for carrying the exhaust gas from the internal combustion engine;

a turbocooler communicating with said means for carrying the exhaust gas and including ducted fan means driven by said exhaust gas for generating a flow of cooling air;

a plurality of heat exchangers connected with said means for providing flows of a plurality of fluids, with a separate heat exchanger for each of said plurality of fluids;

conduit means to direct the cooling air from said ducted fan means of said turbocooler through each of the plurality of heat exchangers to cool each of the plurality of fluids provided in operation of the internal combustion engine assembly.

33. The internal combustion engine assembly of claim 32 wherein said means for providing flows of a plurality of fluids comprise means providing a flow of coolant for the internal combustion engine and means providing a flow of charge-air for the cylinders of the internal combustion engine.