Engine cooling system

Information

  • Patent Grant
  • 6532910
  • Patent Number
    6,532,910
  • Date Filed
    Tuesday, February 20, 2001
    23 years ago
  • Date Issued
    Tuesday, March 18, 2003
    21 years ago
Abstract
An improved cooling system for a turbo charged internal combustion engine is disclosed. A conduit connects a pressurizing engine air intake to the cooling system to raise the pressure in the cooling system thereby enabling an increase of the maximum temperature which coolant in the cooling system can reach.
Description




TECHNICAL FIELD




This invention relates to engine cooling systems and more particularly to a novel and improved cooling system in a turbo charged internal combustion engine.




BACKGROUND ART




The development of internal combustion engines for reduced exhaust emissions has resulted in significant increases in the amount of heat dissipation into engine cooling systems. Traditionally, increases in the required amount of heat dissipation has been accomplished by improving the radiator cooling capacity through increasing the core size of the radiator. In addition, increased coolant and cooling air flow has been used to deal with the increase in required heat dissipation.




Packaging space for larger radiator cores and high energy consumption due to increased coolant and cooling air flow limit the amount of heat dissipation capacity increase that can be accomplished with these traditional approaches.




It is possible to improve cooling capacity by elevating the maximum permissible coolant temperature above traditional levels. The adoption of pressurized cooling systems which permitted operation with coolants at 100° C./212° F. was a step in this direction. The addition of expansion tanks assisted in maintaining such temperature levels. However, it has become desirable to elevate coolant temperatures to even higher levels.




Utilization of elevated coolant temperatures requires proper pressurization under all operating, stand-still and ambient conditions in order to control cooling characteristics, secure coolant flow, prevent cavitation and cavitation erosion and to prevent unwanted boiling and overflow.




Temperature and pressure increase becomes more critical as the heat dissipation from the engine approaches the cooling capacity of the cooling system. A now traditional approach for pressurizing cooling systems is to rely on closed expansion or pressure tanks which depend on temperature increases of coolant and air to create and maintain desired pressures. Such a system communicates with ambient air by opening two way pressure valves to thereby communicating the system with ambient air to entrain new air into the pressure tank when entrapped air and the coolant cool to create a vacuum in the system. Such systems are passive and vulnerable to leaks. Moreover, if such a system is depressurized for any reason, such as maintenance or top-off, pressure is reduced to ambient and operating time and cycles are needed to increase the pressure in the system.




SUMMARY OF THE INVENTION




According to the present invention, an internal combustion engine cooling system is pressurized by introducing air under pressure from an external pressurized source. More specifically, in the preferred and disclosed embodiment, air under pressure from an engine intake manifold is communicated into the cooling system thereby to pressurize the system and elevate the maximum available coolant temperature. In its simplest form, a conduit connects an engine intake manifold with a cooling system expansion tank via a flow control check valve. The flow control valve is in the form of a spring loaded non-return valve connected in the conduit for enabling unidirectional flow from the intake manifold to the expansion tank.




In an alternate embodiment, a flow control valve in the form of a spring loaded non-return valve is also used. A second spring loaded non-return valve allows decompression of the expansion tank to a threshold pressure level corresponding to the spring pressure of the second valve plus the pressure in the engine air inlet system. In order to dampen decay of pressure in the coolant system, a restrictor is interposed in series with the second non-return valve.




A further alternative includes an electric or pneumatic switch between the restrictor and the second non-return valve. A control algorithm for this switch is based on coolant pressure, temperature, engine load parameters and duty cycles for optimizing the expansion tank pressure.




In a still further alternative, a two directional two way control valve is used together with pressure sensors respectively located on opposite sides of the control valve. A control algorithm for pressure control is based on selected parameters such as coolant pressure, engine load, charge air pressure, coolant temperature, ambient temperature and pressure, cooling system capacity, cooling fan speed and duty cycles.




The alternate embodiments using electronic control units enable diagnosis of the systems actual functioning condition. The system compares actual pressure levels, time temperatures and valve positions with expected critical pressures under given conditions in the setting and design parameters for the system and components used in it. Diagnostic information is available for drivers and service information. It also can be used for actively changing the functioning of the system to enable continued use of the engine vehicle in a so-called limp home mode in case of system malfunction.




Accordingly, the objects of this invention are to provide a novel and improved engine coolant system and a method of engine cooling.











BRIEF DESCRIPTION OF DRAWINGS





FIG. 1

is a schematic view of an over the highway heavy duty truck or tractor equipped with a turbo charged engine and cooling system made in accordance with the present invention;





FIG. 2

is a schematic view of one embodiment of the novel portions of the cooling system of the present invention;





FIG. 3

is a schematic showing of an alternate flow control valve arrangement for the system of

FIG. 2

;





FIG. 4

is a further alternate arrangement of the flow control valving for the system of

FIG. 2

; and





FIG. 5

is a schematic view of yet another alternate flow control valving arrangement for the system of FIG.


2


.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




Referring to the drawings and

FIG. 1

in particular, an over the highway truck or tractor is shown generally at


10


. The truck is equipped with a turbo charged engine


12


. As shown somewhat schematically in

FIG. 2

the engine


12


is equipped with a cylinder head


14


having an air intake manifold


15


. The engine


12


is equipped with a turbo charger pressurizing the intake manifold


15


as shown schematically at


16


in FIG.


2


.




The engine


12


is equipped with a cooling system which includes an expansion tank


18


, FIG.


2


. The expansion tank


18


is a now standard tank including an outlet


20


connected to an inlet of a water or coolant pump. The tank


18


includes a fill opening equipped with a pressure cap


22


. In the disclosed embodiment, the cap


22


includes a tank pressure relief and coolant overflow valve


24


and a vacuum relief valve


25


as is now conventional in coolant systems.




A conduit


26


connects the intake manifold


15


to the expansion tank


18


. The conduit


26


communicates with the expansion tank


18


through an inlet


28


. A floating check valve


30


functions to control unidirectional fluid flow through the inlet


28


when a level of coolant


32


in the tank


18


rises to a higher level than that depicted in FIG.


2


. Thus, the check valve


28


functions to prevent coolant


32


from entering the conduit


26


.




A flow control valve


34


is interposed in the conduit


26


. In its simplest form, the flow control valve is a simple spring loaded non-return valve which allows pressurized flow from the manifold


15


to the tank


18


, but prevents reverse flow of pressurized fluid from the tank


18


to the manifold


15


.




With the embodiment of

FIG. 2

, the tank pressure relief valve


24


will control the pressure in the cooling system. So long as the pressure level at which the tank pressure relief valve operates is higher than the pressure in the system, the operating pressure in the system will always be above the opening pressure of the flow control valve and below the tank pressure relief valve's opening pressure due to the one way functioning of the flow control valve


34


.




In the embodiment of

FIG. 3

, a second valve in the form of another spring loaded non-return valve


35


is provided. The valve


35


allows decompression of the expansion tank pressure down to a threshold pressure level corresponding to the spring pressure of the valve


35


plus the pressure of the engine air inlet system. In order to dampen the pressure decay in the cooling system, a restrictor


36


is in series with the second flow control valve


35


. In

FIG. 3

, the restrictor is shown on the coolant side of the valve but it could be on the engine side.




With the embodiment of

FIG. 4

, a directional control flow valve


38


is added to the system in series with the restrictor


36


and the second or decompression control valve


35


. The directional control valve


38


functions to prevent automatic pressure decay in the expansion tank by maintaining a higher pressure when the engine load and the pressure in the engine intake system is reduced.




An electronic control unit


40


controls the positioning of the directional control valve. The control algorithm for this function is based on coolant pressure, temperature, engine load parameters, and duty cycles relevant for optimizing the expansion tank pressure. Alternatively, a pneumatic switch may be substituted for the electrically control directional control valve that has been described.





FIG. 5

discloses an alternative which offers full flexibility in building up and maintaining pressure in the expansion tank


18


and therefore in the coolant system. The alternate of

FIG. 5

includes control of pressure variations and amplitudes. The system of

FIG. 5

utilizes a two directional, two way control valve


42


. Pressure sensors


44


,


45


are respectively positioned between the one way valve


42


and the expansion tank


18


and between the one way valve and the engine intake manifold


15


. A restrictor


46


is interposed in series with the direction control valve


42


and the pressure sensor


45


.




The direction control valve


42


is controlled by an electronic control unit


48


. A control algorithm for the control unit


48


is based on selected parameters such as coolant pressure, engine load, charge pressure, coolant temperature, ambient temperature, ambient pressure, cooling system capacity, cooling fan speed, and duty cycles. The pressure in the expansion tank is optimized by actively pressurizing to satisfy coolant system function. While the pressure is optimized, it is only to necessary pressure levels and with pressure variations and amplitudes which match the properties of materials used in the coolant system.




A passive pressure build-up in the expansion tank will take place naturally and in parallel with the active pressure control systems that have been described. How the passive pressure build-up will interact depends on which of the embodiments is employed.




The embodiments of

FIGS. 4 and 5

make it possible to diagnose a system's actual functioning condition and to identify problems. Such a system compares actual pressure levels, time, temperatures and valve positions with expected critical pressures under given conditions and the setting of design parameters for the system as well as components used in it.




Diagnostic information derived when either the embodiment of

FIGS. 4

or


5


is in use, can be used for driver and service information. It can also be used for actively changing the functioning of the system to enable continued use of the vehicle in a so-called limp home mode in case of an identified system malfunction. Examples of changing functions are modifying valve functions, shutting off the active system pressurizing by the turbo charger, reduction of available engine power and heat dissipation, and altered cooling fan, speed and fan-clutch engagement.




OPERATION




In operation from cold engine start up, operation of the turbo charger will transmit air under pressure through the conduit


26


to the expansion tank


18


. Assuming the pressure relief setting of the cap pressure relief valve


24


is high enough, air under pressure will flow through the flow control valve


34


until pressure in the expansion tank


18


is approaching the relief valve opening pressure (but not higher). Should the pressure of air from the turbo charger


16


drop, the one way flow control valve


34


will prevent a pressure drop in the expansion tank


18


.




With the embodiment of

FIG. 3

, the second non-return flow valve


35


functions to reduce the pressure in the coolant system when outlet pressure from the turbo charger is reduced, but not lower than the pre-set opening pressure of the second flow control valve


35


.




With the embodiment of

FIG. 4

, the directional control valve


38


functions to prevent automatic pressure decay in the expansion tank to maintain higher pressure when the engine load and the pressure of the engine intake system is reduced. The electronic control unit


40


of the

FIG. 4

embodiment, will function based on the parameters that have been selected to control pressure decay in the coolant system.




With the embodiment of

FIG. 4

, pressure in the coolant system in relation to pressure in the engine air inlet


15


is totally controlled by the one way directional control valve


42


which in turn is controlled by the electronic control unit


46


. This functioning is in accordance with the parameters that have been described.




The embodiment of

FIG. 5

is effective to control coolant system pressure appropriate for operating parameters and as such to maximize performance benefits of a pressurized cooling system.




Although the invention has been described in its preferred form with a certain degree of particularity, it is understood that the present disclosure of the preferred form has been made only by way of example and that numerous changes in the details of construction, operation and the combination and arrangement of parts may be resorted to without departing from the spirit and scope of the invention as hereinafter claimed.



Claims
  • 1. In a turbo charged engine, an improved cooling system comprising at least one conduit connecting a pressurized engine air intake to an inlet to an expansion tank of the cooling system whereby to raise the pressure in the cooling system and thereby enable an increase of the maximum temperature which coolant in the cooling system can reach and a floating check valve in said tank that prevents said coolant from entering said at least one conduit when a level of said coolant exceeds a predetermined level.
  • 2. The system of claim 1, wherein there is a flow control valve in the conduit.
  • 3. The system of claim 2, wherein the flow control valve is an electronically controlled two directional, two way control valve.
  • 4. The system of claim 2, wherein the conduit is connected to the expansion tank check valve.
  • 5. The system of claim 2, wherein the flow control valve is a spring loaded non-return valve permitting flow of air under pressure to the coolant system.
  • 6. The system of claim 5, wherein a second spring loaded non-return valve is in parallel with the flow control valve to allow decompression of the expansion tank whereby to maintain the pressure in the expansion tank between said maximum and a threshold pressure.
  • 7. The system of claim 6, wherein a directional control valve is connected in series with the second non-return valve.
  • 8. The system of claim 7, wherein there are a pair of pressure sensors connected to said conduit on opposite sides of the flow control valve.
  • 9. In a vehicle having a turbo charged engine equipped with a cooling system, a system for elevating the maximum temperature of coolant in the system, the system comprising:a) an expansion tank forming a part of the system; b) the tank having a pressure relief and coolant overflow valve and a vacuum relief valve; c) the tank also having a floating check valve; d) a conduit connecting a pressurized air intake manifold of the engine to the check valve, said check valve prevents coolant from entering said at least one conduit when a level of said coolant exceeds a predetermined level; and, e) a flow control valve in the conduit.
  • 10. The system of claim 9, wherein the flow control valve is a spring loaded non-return valve permitting flow of air under pressure to the coolant system.
  • 11. The system of claim 10, wherein a second spring loaded non-return valve is in parallel with the flow control valve to allow decompression of the expansion tank whereby to maintain the pressure in the expansion tank between said maximum and a threshold pressure.
  • 12. The system of claim 11, wherein a directional control valve is connected in series with the second non-return valve.
  • 13. The system of claim 12, wherein there are a pair of pressure sensors connected to said conduit on opposite sides of the flow control valve.
  • 14. The system of claim 9 wherein the engine is a vehicle engine.
  • 15. The system of claim 14 wherein the vehicle is an over the highway heavy duty vehicle.
  • 16. In a powered mechanism including a combustion engine having a liquid cooling system, an arrangement for elevating the available operating temperature of the engine comprising:a) a source of air under pressure; b) a conduit connecting the source to an inlet to an expansion tank of the system; c) a floating check valve in said tank that prevents coolant from entering said conduit when a level of said coolant exceeds a predetermined level.
  • 17. The arrangement of claim 16, wherein the engine includes a turbocharger and the source is an engine air intake.
  • 18. The arrangement of claim 16, wherein the engine is in an over the highway heavy duty vehicle.
  • 19. The arrangement of claim 16, wherein there is a flow control valve in the conduit.
  • 20. The arrangement of claim 19, wherein the flow control valve is a spring loaded non-return valve.
  • 21. The arrangement of claim 19, wherein a second spring loaded non-return valve is in parallel with the flow control valve to allow decompression of the expansion tank whereby to maintain the pressure in the expansion tank between said maximum and a threshold pressure.
  • 22. The arrangement of claim 21, wherein a directional control valve is connected in series with the second non-return valve.
  • 23. A process of improving engine performances with elevated operating temperatures comprising:a) delivering air under pressure in excess of ambient pressures from a pressurizing source to an engine cooling system; b) controlling the pressure in the system by delivering the pressurized air via a valve; and, c) preventing coolant from entering said pressurizing source when a level of coolant in the cooling system exceeds a predetermined level.
  • 24. The process of claim 23, wherein the engine is turbo charged and the source is an engine intake manifold.
  • 25. The process of claim 24, wherein the valve is a spring biased one way valve.
  • 26. The process of claim 24, wherein the engine is in a heavy duty over the highway vehicle.
  • 27. The process of claim 23, wherein the valve is a spring biased one way valve.
  • 28. The process of claim 23, wherein the engine is in a heavy duty over the highway vehicle.
US Referenced Citations (31)
Number Name Date Kind
2191611 Eshbaugh et al. Feb 1940 A
3162182 Gratzmuller Dec 1964 A
3256868 Gratzmuller Jun 1966 A
3576181 Neal et al. Apr 1971 A
4478178 Pernet Oct 1984 A
4565162 Seki et al. Jan 1986 A
4608827 Hasegawa et al. Sep 1986 A
4640235 Martin Feb 1987 A
4649869 Hayashi et al. Mar 1987 A
4669426 Hirano et al. Jun 1987 A
4722305 Haskell Feb 1988 A
4782689 DeRome Nov 1988 A
4913107 Schweiger Apr 1990 A
4928637 Naitoh et al. May 1990 A
4930455 Creed et al. Jun 1990 A
4958600 Janthur Sep 1990 A
5036888 Scharrer et al. Aug 1991 A
5044430 Avrea Sep 1991 A
5111777 Steinberg et al. May 1992 A
5186242 Adachi et al. Feb 1993 A
5241926 Sato et al. Sep 1993 A
5289803 Matsushiro et al. Mar 1994 A
5666911 Gohl et al. Sep 1997 A
5809944 Aoki et al. Sep 1998 A
5836269 Schneider Nov 1998 A
5899266 Szucs May 1999 A
6016774 Bokkers et al. Jan 2000 A
6053132 Evans Apr 2000 A
6135067 Klamm et al. Oct 2000 A
6213062 Kawase Apr 2001 B1
6244294 Hollis Jun 2001 B1
Foreign Referenced Citations (9)
Number Date Country
2222919 Nov 1972 DE
360252 Sep 1989 EP
520135 Feb 1992 EP
2175997 May 1986 GB
63-85215 Apr 1988 JP
2-294515 Dec 1990 JP
1211-422 Jul 1984 SU
1218-160 Sep 1984 SU
1204757 Jan 1986 SU