GB2079871A - Oil supply system - Google Patents

Oil supply system Download PDF

Info

Publication number
GB2079871A
GB2079871A GB8121965A GB8121965A GB2079871A GB 2079871 A GB2079871 A GB 2079871A GB 8121965 A GB8121965 A GB 8121965A GB 8121965 A GB8121965 A GB 8121965A GB 2079871 A GB2079871 A GB 2079871A
Authority
GB
United Kingdom
Prior art keywords
oil
supply system
oil supply
pumping means
relief valve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB8121965A
Other versions
GB2079871B (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hobourn Eaton Ltd
Original Assignee
Hobourn Eaton Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hobourn Eaton Ltd filed Critical Hobourn Eaton Ltd
Priority to GB8121965A priority Critical patent/GB2079871B/en
Publication of GB2079871A publication Critical patent/GB2079871A/en
Application granted granted Critical
Publication of GB2079871B publication Critical patent/GB2079871B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01MLUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
    • F01M1/00Pressure lubrication
    • F01M1/16Controlling lubricant pressure or quantity
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01MLUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
    • F01M5/00Heating, cooling, or controlling temperature of lubricant; Lubrication means facilitating engine starting
    • F01M5/005Controlling temperature of lubricant

Abstract

A pumped oil supply system, for example for lubricating an internal combustion engine incorporates a relief valve 4 whose control element or piston 5 is responsive to pressure in chamber 2 and which has superimposed thereon an opening force derived from an element 14 responsive to the temperature of the oil delivered via chamber 3 by the pumping means. The pumping means has separate first and second outlets 2a, 3a feeding chambers 2, 3, the second chamber 3 communicating with the oil gallery of the engine and the first chamber 2 communicating with the second chamber 3 through a variable restrictor 9, 10. The loaded piston 5 is acted on by the delivery pressure in the first outlet, and the piston is connected to a centre body 10 constituting the adjustable member of the variable restrictor. The temperature responsive element 14 is disposed in the second chamber and imposes a resilient force on the piston which, with increase of the oil temperature, augments the action thereon of the delivery pressure in the first outlet. Oil passing through the relief valve flows to the inlet side of the pumping means. <IMAGE>

Description

SPECIFICATION Oil supply system The invention relates to an oil supply system and has a particularly useful but not exclusive application in lubricating systems of petrol and diesel engines.
Under normal operating conditions an internal combustion engine runs at different speeds and different temperatures. The lubrication requirement of the engine change with speed and the characteristics of the oil change with temperature. Therefore, the pressure and flow rate characteristics required of the oil pump vary over the operating range. Naturally, it is necessary to arrange that the oil pump is capabie of delivering the maximum required flow rate at the appropriate engine speed and it should also have the ability to deliver oil at the maximum required pressure.
Accordingly, a pump is provided which has more than adequate capacity for all practical conditions.
Generally, a pressure relief valve is provided at the pump outlet to limit the output pressure to a preset maximum. Nevertheless, under most operating conditions the excess capacity of the oil pump means that power is wasted in driving the pump.
According to this invention there is provided an oil supply system comprising pumping means having an inlet and an outlet which leads to a point of utilisation whence the oil is returned to a reservoir, the inlet communicating with the reservoir, and a spring-loaded relief valve which opens progressively with increase of a delivery pressure of the pumping means above a predetermined value to by-pass a proportion of the delivery of the pumping means to the inlet side of the pumping means, and a temperature responsive element responsive to a temperature of the oil delivered by the pumping means and connected to superimpose a loading on the relief valve in a sense to increase the opening of the relief valve with increase of said temperature.
The pumping means in one preferred construction provides separate first and second outlets for the pumped oil, said outlets being interconnected through a variable restrictor controlled in accordance with the control of the relief valve. In other arrangements, separate pumps, e.g. gear-type pumps or other positive displacement pumps may be employed. However, the invention can be employed in conjunction with a pump or pump system providing effectively a single outlet.
Said relief valve may comprise a piston member slidably mounted to uncover the valve aperture to a variable extent, said piston member having the delivery pressure of the first pump applied to it to urge it in a sense to open the valve against the force of a spring urging the piston in the opposite direction.
The piston member may be connected to the control element of the variable restrictor. This control element may comprise a centre body slidably mounted within an annular passage such that axial movement of the centre body alters the effective area of the restrictor.
The temperature responsive element may comprise a bi-metal strip, which is intrinsically resilient. Alternatively, however, the temperature responsive element may comprise a wax thermostat type which has an output member whose movement depends upon the degree of expansion of a wax sleeve. With such an arrangement a spring is preferably used to couple the output member to the relief valve piston.
The invention will further be described with reference to the accompanying drawings, in which: Figure 1 is a cross-sectional view of an oil supply system embodying the invention; Figure 2 is a plan view illustrating the porting of the pump of Figure 1; Figure 3 is a cross-sectional elevation of the coupling passage of the system of Figure 1; and Figure 4 is a schematic block diagram of the system of Figure 1.
Referring to Figures 1 to 3 the pump system comprises a double pump constituted by a rotortype pump arrangement with two sets of ports. A rotor type pump is the kind described, for example in Patent Specification No. 596379. It comprises a lobed rotor which moves eccentrically within a lobed stator, the rotor and stator making permanent rubbing contact at points spaced around their periphery and defining a rotor-stator gap which decreases in volume between fixed inlet and outlet ports. In the arrangement of Figure 1 there are effectively two pumps having a common inlet port 1. The first pump has an outlet port 2a which is coupled to a chamber 2 and the second pump has an outlet port 3a which communicates with a chamber 3.
A relief valve 4 is provided comprising a piston 5 spring-loaded by a spring 6 towards a position in which the piston obstructs a by-pass channel 8 through which oil from chamber 2 can be returned to the inlet 1. The face 7 of the piston is subjected to the pressure of the oil in chamber 2 and when this pressure exceeds a predetermined level the piston is depressed sufficiently to open by-pass channel 8 to a degree dependent upon the said pressure.
A passage 9 interconnects chambers 2 and 3 and a restrictor core 10 disposed in the passage is shaped to have a shoulder 1 A step 12 in the wall of the passage defines with shoulder 11 an annular restriction 1 3, the effective area of which depends upon the axial position of the core. The core 10 is fixed to piston 5.
Chamber 3 houses a temperature-sensitive element 1 4 which comprises a rigid casing 15, a wax sleeve 16, a rubber insert 17 within the sleeve and an actuating member 1 8 bonded in the insert 1 7. At high temperatures the wax softens and expands and tends to expel the member 18.
Member 1 8 is axially coupled to the stem of core 10 through a compression spring 1 9. The effect of the temperature-sensitive element 14 is to apply to piston 5, through spring 19, an axial force which augments the force exerted by the oil pressure and which increases with temperature.
Thus, at high temperatures the pressure setting of the relief valve 4 is reduced.
Figure 4 shows the arrangement of Figures 1 to 3 in schematic form. The first pump is designated A and the second pump B. The pumps draw oil from the sump S and feed the oil supply gallery G which supplies oil to the moving parts of the engine E, from whence the oil is returned to the sump. The pressure relief valve 4 by-passes pump A, depending on the pressure in chamber 2. The pressure setting of valve 4 is determined by the temperature sensitive element 14.
Movement of the piston 5 of valve 4 actuates movement of the restrictor core 10 (Figure 1 ) and thus controls the restriction 1 3 in the passage 9 coupling the outlets 2 and 3 of the pumps A and B.
The operation of the system can be described with reference to four basic conditions: (a) high temperature and low speed requiring relatively low oil pressure; (b) high temperature and high speed requiring higher oil pressure than (a) to give adequate flow; (c) low temperature and low speed -- requiring higher oil pressure from the pump than (b) to overcome the high pressure drop in the gallery; and (d) low temperature and high speed - also requiring higher oil pressure at the pump than (b).
Thus, in operation, in condition (a) - high temperature and low speed - the flow from pump A is relatively small and the pressure drop across restriction 1 3 is small. Pump A is effectively connected to pump B and augments the flow. Thus, even though the pumps are being driven slowly because of the low engine speed, adequate pressure and flow is developed.
As engine speed increases the pressure rises until the relief valve 4 opens at the predetermined pressure. This pressure may be typically of 2 bars or so, which is significantly less than the setting of 6 bars typically employed to cater for the cold oil condition in pumps not embodying the invention.
When the relief valve opens, the flow from pump A is split, part going to the engine and part being by-passed. Continuing increases in speed open the relief valve further until the valve is fully open and causes the total flow from pump A to be returned to the suction side of the pump. At this time the pressure from pump B is adequate to supply the needs of the engine and the power lost in driving pump A is kept to a minimum. As there is now no flow across restriction 1 3 there is no pressure differential between chambers 2 and 3.
Further rise in speed (condition (b) above) causes the pressure in chamber 3 to rise above that in chamber 2 and oil flows in the reverse direction through the restriction 1 3 and is returned to sump S via the relief valve 4. At maximum speed the pressure at the output of pump B is greater than the relief pressure because of the effect of the flow through restriction 13.
Restriction 13 is made variable by the contour of shoulder 11 to optimise the flow characteristics.
For condition (c), when the oil is cold and the speed is low, pump B is able to deliver all the required oil because even at low speed it develops sufficient pressure by virtue of the fact that the oil is cold. Pump A also produces a high pressure oR flow and this opens the relief valve 4. Thus, excess flow from pump B can pass through the restriction 13 to the by-pass channel. Because of this restriction, however, the pressure in chamber 3 can rise above the low relief setting of the valve 4 and adequate pressure can be provided. Therefore, 6 bars of pressure may be raised, for example, even though the pressure setting of valve 4 is only 2 bars.
In condition (d), the flow and hence the available pressure is greater and the excess flow from pump A and any excess flow from pump B is effectively by-passed as in condition (c).
The effect of the temperature compensation of the relief valve setting by element 14 has been explained above and further helps optimisation of the pump characteristics.

Claims (9)

1. An oil supply system comprising pumping means having an inlet and an outlet which leads to a point of utilisation whence the oil is returned to a reservoir, the inlet communicating with the reservoir, and a spring-loaded relief valve which opens progressively with increase of a delivery pressure of the pumping means above a predetermined value to by-pass a proportion of the delivery of the pumping means to the inlet side of the pumping means, and a temperature responsive element responsive to a temperature of the oil delivered by the pumping means and connected to superimpose a loading on the relief valve in a sense to increase the opening of the relief valve with increase of said temperature.
2. An oil supply system as claimed in claim 1, wherein the pumping means provides separate first and second outlets for the pumped oil, said outlets being interconnected through a variable restrictor controlled in accordance with the control of the relief valve.
3. An oil supply system as claimed in claim 1 wherein the relief valve comprises a piston member slidably mounted to uncover the valve aperture to a variable extent, said piston member having the delivery pressure of the first pump applied to it to urge it in a sense to open the valye against the force of a spring urging the piston in the opposite direction.
4. An oil supply system as claimed in claim 2 and claim 3 taken in combination, wherein the piston member is connected to the control element of the variable restrictor.
5. An oil supply system as claimed in claim 4, wherein the control element of the variable restrictor comprises a centre body slidabiy mounted within an annular passage such that axial movement of the centre body alters the effective area of the restrictor.
6. An oil supply system as claimed in claim 5, wherein the temperature responsive element is connected to apply an axial loading to the centre body through a spring acting against an extension of the centre body.
7. An oil supply system as claimed in claim 5, wherein the temperature responsive element comprises a quantity of wax disposed in a housing disposed in the outlet passage of the second pump, a rod being slidably mounted in the housing so as to be caused to project from the housing to a greater or lesser extent with expansion or contraction of the wax with variation of temperature of the oil flowing about the casing, said rod constituting the output member of the element.
8. An oil supply system as claimed in claim 5, wherein the temperature responsive element comprises a bimetallic element acting on an extension of said centre body.
9. An oil supply system substantially as hereinbefore described with reference to and as illustrated in Figures 1 to 3 or Figure 4 of the accompanying drawings.
GB8121965A 1980-07-17 1981-07-16 Oil supply system Expired GB2079871B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8121965A GB2079871B (en) 1980-07-17 1981-07-16 Oil supply system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8023451 1980-07-17
GB8121965A GB2079871B (en) 1980-07-17 1981-07-16 Oil supply system

Publications (2)

Publication Number Publication Date
GB2079871A true GB2079871A (en) 1982-01-27
GB2079871B GB2079871B (en) 1984-08-08

Family

ID=26276257

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8121965A Expired GB2079871B (en) 1980-07-17 1981-07-16 Oil supply system

Country Status (1)

Country Link
GB (1) GB2079871B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0376150A2 (en) * 1988-12-24 1990-07-04 Klöckner-Humboldt-Deutz Aktiengesellschaft Internal-combustion engine having two hydraulic liquid loops

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0376150A2 (en) * 1988-12-24 1990-07-04 Klöckner-Humboldt-Deutz Aktiengesellschaft Internal-combustion engine having two hydraulic liquid loops
EP0376150A3 (en) * 1988-12-24 1990-11-07 Klockner-Humboldt-Deutz Aktiengesellschaft Internal-combustion engine having two hydraulic liquid loops

Also Published As

Publication number Publication date
GB2079871B (en) 1984-08-08

Similar Documents

Publication Publication Date Title
US5800131A (en) Process for regulating the capacity of lubricant pumps and lubricant pump therefor
US6086337A (en) Variable capacity pump
US2768585A (en) Pump control mechanism
US4336903A (en) Control valve
US4390322A (en) Lubrication and sealing of a free floating piston of hydraulically driven gas compressor
US3394688A (en) Fuel pump timing means
US2403371A (en) Variable output pump
US2429005A (en) Liquid fuel pump governor
EP0274408B1 (en) Automatic thermal and speed controls for viscous fluid clutches
EP0049838A1 (en) Variable-displacement sliding-vane pump
US4368008A (en) Reciprocating controls of a gas compressor using free floating hydraulically driven piston
US4671232A (en) Fuel injection system for self-igniting internal combustion engines
US2296876A (en) Aircraft fuel system
GB1295647A (en)
US4426196A (en) Oil supply system
US2433220A (en) Pressure control for pumps
US4401082A (en) Fuel injection pump for internal combustion engines
US4170438A (en) Fluid pump with a continuously variable speed converter
US9206800B2 (en) Multiple stage passive variable displacement vane pump
US3238884A (en) Variable positive displacement pump with rising pressure curve
US3983693A (en) Device for starting one of a plurality of airplane engines
US3063245A (en) Torque converters
US4738596A (en) Fuel pumping apparatus
US2771066A (en) Fuel injection pump
GB2079871A (en) Oil supply system

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee