[0001] The present invention relates to cooling systems and in particular to cooling systems
for internal combustion engines.
[0002] In conventional internal combustion engine cooling systems an engine driven pump
circulates coolant from the cooling jacket of the engine, through a radiator and back
to the cooling jacket. A thermostatically controlled bypass is provided so that all
or part of the flow of coolant may be circulated through the cooling jacket without
passing through the radiator. Consequently, from start-up while the engine is still
cold, the thermostat will prevent coolant flowing through the radiator and as the
engine gradually warms up, flow of coolant through the thermostat from the radiator
will increase.
[0003] A fan is provided to cause air to flow through the radiator to assist heat exchange.
This fan may be driven directly from the engine and may be driven continuously or
may be arranged to cut-in at some temperature, under for example the control of a
viscous clutch or similar means. Alternatively, the fan may be driven electrically
under suitable control. Whether driven directly by the engine or electrically, the
fan imposes a significant power loss on the engine output. Controlling the fan so
that it only operates at higher temperatures requires sophisticated control means
which adds significantly to the cost of the system.
[0004] According to one aspect of the present invention, a cooling system for an internal
combustion engine having an engine driven pump for circulating coolant around a circuit
including a cooling jacket and a radiator, a bypass in parallel with the radiator
and thermostatic means for controlling flow through the bypass and radiator; and a
fan for forcing air through the radiator, characterised in that said fan is driven
by means of a turbine, said turbine being disposed in the return between the radiator
and cooling jacket.
[0005] In this manner, the flow of coolant in the cooling system is used to drive the fan.
This may be achieved with minimal additional power consumption and the thermostat
which controls the rate of flow of coolant through the radiator will also control
the speed of the fan.
[0006] An embodiment of the invention is now described, by way of example only, with reference
to the accompanying drawing which illustrates schematically a cooling system in accordance
with the present invention.
[0007] In the system illustrated, an engine driven pump 10 circulates coolant from a water
jacket 11 via outlet 12, to the inlet 13 of a radiator 14 via line 15. The outlet
16 from the radiator 14 is connected to the inlet 17 of water jacket 11 by return
line 18. A bypass 19 interconnects lines 15 and 18, a thermostatic valve 20 being
provided at the junction between return line 18 and bypass 19 to control the relative
rates of flow of coolant from return line 18 and bypass 19 to the inlet 17.
[0008] A turbine 21 is located in a housing 22 which forms part of the return line 18. The
turbine 21 is mounted on a shaft 23 which is located in suitable bearings and extends
through the wall of housing 22, sealing means being provided to prevent leakage of
coolant. A fan 25 is attached to the end of shaft 23 which extends from the housing
22, said fan 25 upon rotation of the shaft 23 due to flow of coolant over the turbine
21 from the outlet 16 of radiator 14 to the inlet 17 of cooling jacket 11, being arranged
to draw air through the radiator 14.
[0009] In operation, when the engine and coolant are cold, the thermostatic valve 20 will
close connection between the return line 18 and inlet 17 and will fully open the connection
between bypass 19 and inlet 17. The engine driven pump 10 will consequently recirculate
coolant from the water jacket 11, via line 15 and bypass 19 back into the coolant
jacket via inlet 17. Under these conditions, there will be no flow of coolant through
the radiator 14 or past the turbine 21 and consequently the fan 25 will remain stationary.
[0010] As the temperature of the coolant increases, the connection between return line 18
and inlet 17 is gradually opened so that coolant will begin to flow through the radiator
14. As this coolant flows past the turbine 21, it will rotate the fan 25. The speed
of the fan 25 and hence the amount of air drawn through the radiator 14 will depend
upon the rate of flow of coolant through the radiator 14 which in turn is controlled
by the thermostatic valve 20 as a function of the temperature of the coolant.
[0011] The system described above thus provides a cooling system in which the speed of the
fan 25 will be automatically adjusted so that it will be stationary or slow when the
coolant temperature is low and the radiator is only required to remove a small amount
of heat and will be fast when the coolant temperature is high and the radiator is
required to remove large amounts of heat.
[0012] Various modifications may be made without departing from the invention. For example,
while in the above embodiment the fan is driven directly by the turbine, the turbine
may alternatively be arranged to drive the fan through suitable drive means, for example
a belt and pulley system. Such drive means may also include means for increasing or
reducing the drive ratio. Also the thermostatic valve may be located in any suitable
position in which it will control the rate of flow through the radiator and the bypass.
[0013] If required, a low powered electric motor may be provided to assist the turbine at
low engine speeds. This motor may be mounted directly on the turbine shaft. Switching
means responsive to engine speed and coolant temperature will energise the motor when
the speed of the engine is below a predetermined value and the coolant is at or above
its normal operating temperature.
1. A cooling system for an internal combustion engine having an engine driven pump
(10) for circulating coolant around a circuit including a cooling jacket (11) and
a radiator (14), a bypass (19) in parallel with the radiator (14) and thermostatic
means (20) for controlling flow through the bypass (19) and radiator (14); and a fan
(25) for forcing air through the radiator (14), characterised in that said fan (25)
is driven by means of a turbine (21, 22, 23), said turbine (21, 22, 23) being disposed
in the return (18) between the radiator (14) and cooling jacket (11).
2. A cooling system according to Claim 1 characterised in that the thermostat (20)
will prevent flow of coolant through the turbine (21, 22, 23), when the coolant is
below a predetermined temperature.
3. A cooling system according to Claim 1 or 2 characterised in that a thermostatic
valve (20) is situated between the outlet (16) from the radiator (14) and inlet (17)
to the water jacket (11), and between the bypass (19) and the inlet (17) to the water
jacket (11).
4. A cooling system according to Claim 3 characterised in that the turbine (21, 22,
23) is disposed between the outlet (16) from the radiator (14) and the thermostatic
valve (20).
5. A cooling system according to any one of Claims 1 to 4 characterised in that the
fan (25) is driven directly by the turbine (21, 22, 23).
6. A cooling system according to any one of Claims 1 to 4 characterised in that the
fan (25) is driven by the turbine (21, 22, 23) via means which will increase or reduce
the drive ratio.