EP2065584A1 - Coolant pump cavitation guarding system - Google Patents

Coolant pump cavitation guarding system Download PDF

Info

Publication number
EP2065584A1
EP2065584A1 EP07122038A EP07122038A EP2065584A1 EP 2065584 A1 EP2065584 A1 EP 2065584A1 EP 07122038 A EP07122038 A EP 07122038A EP 07122038 A EP07122038 A EP 07122038A EP 2065584 A1 EP2065584 A1 EP 2065584A1
Authority
EP
European Patent Office
Prior art keywords
coolant
cavitation
sensor
power source
inlet
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
EP07122038A
Other languages
German (de)
French (fr)
Other versions
EP2065584B1 (en
Inventor
Christopher John Holt
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.)
Perkins Engines Co Ltd
Original Assignee
Perkins Engines Co 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 Perkins Engines Co Ltd filed Critical Perkins Engines Co Ltd
Priority to EP07122038A priority Critical patent/EP2065584B1/en
Priority to AT07122038T priority patent/ATE522710T1/en
Publication of EP2065584A1 publication Critical patent/EP2065584A1/en
Application granted granted Critical
Publication of EP2065584B1 publication Critical patent/EP2065584B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P11/00Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
    • F01P11/14Indicating devices; Other safety devices
    • F01P11/18Indicating devices; Other safety devices concerning coolant pressure, coolant flow, or liquid-coolant level
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P5/00Pumping cooling-air or liquid coolants
    • F01P5/14Safety means against, or active at, failure of coolant-pumps drives, e.g. shutting engine down; Means for indicating functioning of coolant pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P2025/00Measuring
    • F01P2025/08Temperature
    • F01P2025/30Engine incoming fluid temperature

Definitions

  • the present disclosure is directed to a coolant pump system, and, more particularly to a coolant pump cavitation guarding system.
  • Coolant pump systems may include a power source and a coolant pump associated therewith.
  • the coolant pump is driven by the power source, for example an internal combustion engine, and circulates coolant through the power source.
  • the coolant pump commonly includes a housing having a liquid inlet, a liquid outlet and a liquid pressurizing mechanism arranged between the liquid inlet and the liquid outlet of the pump.
  • the pressurizing mechanism of the coolant pump is commonly embodied as a fixed displacement impeller.
  • Coolant pump systems for power sources may currently be exposed to water pump failures caused by cavitation. Cavitation is localized generation of vapor phase of the coolant in the pump, which may occur at the liquid inlet if coolant temperature is relatively high, and coolant pressure is relatively low. Upon subsequent pressurizing of the coolant, vapor bubbles may implode onto the pump mechanism, and may cause severe damage to the pump mechanism. Such damage often goes undetected initially, but may lead to loss of efficiency of the pressurizing mechanism and ultimately to failure of the pump mechanism.
  • the coolant pump system may include a cooling arrangement, for example a radiator, so that a cooling system is formed.
  • the cooling arrangement matches the power source such that generation of cavitation in the coolant pump is prevented.
  • the cooling arrangement is provided by another party than the supplier of the coolant pump system, it has been found that the issue of pump cavitation is sometimes overlooked. This may occur particularly when a cooling arrangement is designed to save space and weight, and the power source thus runs with a relatively high coolant inlet temperature.
  • Japanese patent publication 57191413 discloses a water pump controller system for an engine that is provided with a cavitation sensor to reduce the generation of cavitation and to prevent overheating of the engine.
  • the cavitation sensor is a unit separate from the water pump having a housing with a coolant chamber that is fluidly connected to the coolant system.
  • the coolant chamber has a diaphragm that is mechanically linked to a potentiometer.
  • a signal from the potentiometer is sent to a comparison circuit. If the signal is smaller than a reference signal, an output of the comparison circuit reduces rotational speed of the engine driving the water pump in accordance with the output of a temperature sensor. By reducing the engine speed, the pump speed is reduced, and generation of cavitation is prevented.
  • a disadvantage associated with the water pump controller system of Japanese patent publication 57191413 is that it is mechanically complex, and thus may be prone to failure. Further it is relatively costly to install. In addition, the accuracy of the system leaves much to be desired.
  • the disclosed coolant pump cavitation guarding system is directed at alleviating one or more of the disadvantages set forth above.
  • the system comprises a power source and a coolant pump.
  • the coolant pump includes a housing having a liquid inlet and a liquid outlet, and a liquid pressurizing mechanism.
  • the liquid pressurizing mechanism is arranged between the liquid inlet and the liquid outlet, and is driven to circulate coolant through the power source.
  • the system further includes a sensor associated with the liquid inlet that is configured to generate a signal indicative of cavitation in the coolant.
  • the system includes a controller arranged to take precautionary action upon receipt of a signal indicative of cavitation from the sensor.
  • Another aspect of the present disclosure is directed to a method of guarding against cavitation.
  • the method comprises circulating coolant to flow through a power source, and pressurizing the coolant.
  • the method further includes sensing at least one parameter characteristic of cavitation in the coolant just prior to or while being pressurized, and taking precautionary action upon said sensed parameter being indicative of cavitation.
  • Fig. 1 is a diagrammatic illustration of an exemplary disclosed coolant cavitation guarding system
  • Fig. 2 is a cross sectional illustration of an exemplary disclosed coolant pump for use with the system of Fig. 1 ;
  • Fig. 3 is a flow chart illustrating an exemplary disclosed method of guarding against cavitation
  • Fig. 4 is a flow chart illustrating an exemplary method of control of the system of Fig. 1 .
  • Fig. 1 shows an exemplary disclosed cavitation guarding system 1.
  • the system 1 comprises a power source 2.
  • the power source 2 may be a power generating apparatus of any type that requires cooling.
  • the power source 2 may be an internal combustion engine, for example a diesel or gasoline engine.
  • the power source 2 may also be of another type, for example an external combustion engine, such as a gas turbine.
  • the cavitation guarding system 1 may further comprise a coolant pump 3 to pump liquid coolant.
  • the coolant may be of any type, for example a water based coolant with optionally anti-corrosion and anti freeze additives. In one embodiment, such water based coolant may include ethylene glycol and a so called corrosion prevention package.
  • such water based coolant may be propylene glycol.
  • the coolant may be a so called extended life coolant without water.
  • the coolant may be a mixture including about 50% water and about 50% ethylene glycol, and optionally a so called corrosion prevention package.
  • the cavitation guarding system 1 may include an engine cooling arrangement including one or more radiators 4 and/or expansion tanks 5, so that a cooling system is formed. The configuration of such cooling arrangements is well known to the skilled person, and hence shall not be discussed further.
  • the coolant pump 3 may include a pump housing 6, which may be provided with a liquid inlet 7 and a liquid outlet 8.
  • the liquid inlet 7 may comprise an inlet chamber 9 defined by the wall 10 of the pump housing 6.
  • the liquid outlet 8 may comprise an outlet chamber 11 defined by the wall 10.
  • a liquid pressurizing mechanism 12 may be arranged between the liquid inlet 7 and the liquid outlet 8.
  • the pressurizing mechanism 12 may be of any type that is capable of pressurizing a coolant, and susceptible to cavitation damage.
  • the pressurizing mechanism 12 may be a fixed displacement impeller 21 of the radial type carried on a central shaft 20, as is common for internal combustion engines.
  • the pressurizing mechanism 12 may be for example that of a gerotor type coolant pump 3.
  • the pressurizing mechanism 12 may be that of a vane type pump 3.
  • the pressurizing mechanism 12 may be driven by the power source 2 to circulate coolant through the power source 2.
  • the pressurizing mechanism 12 may be driven by the power source 2 directly or indirectly.
  • the pressurizing mechanism may be driven directly via a mechanical transmission, for example a gear drive of drive belt.
  • the pressurizing mechanism may be driven indirectly, for example via a hydraulic motor driven by a hydraulic pump actuated by the power source.
  • the pressurizing mechanism may be driven indirectly, for example using an electric motor powered by an alternator driven by the power source.
  • the pressurizing mechanism may be driven by another device than the power source 2, for example by a motor that is powered separately.
  • the impeller 21 of the pressurizing mechanism 12 may have a central shaft 20 that is directly driven to rotate by the power source via a gear drive having a fixed ratio mechanical transmission that branches off the crankshaft of the engine forming the power source 2.
  • the coolant may be circulated to and from the power source 2 using conduits 13, for example hoses, pipes or channels.
  • the coolant may likewise be circulated through the power source 2 using conduits 13, for example hoses, pipes or channels.
  • coolant flows to and from the engine via flexible hoses, and circulates through the engine via channels that define a water jacket surrounding the cylinders (not shown).
  • a sensor 14 may be associated with the liquid inlet 7, and shall hereafter for ease of reference also be referred to as inlet sensor 14.
  • the inlet sensor 14 may be in close proximity to the liquid inlet 7. It should be noted that within this context the expression that the inlet sensor 14 in close proximity to the liquid inlet 7 is meant to also encompass that the inlet sensor 7 extends into the introductory flow passage to the pressurizing mechanism or in the pressurizing zone of the coolant pump 3 itself.
  • the inlet sensor 14 may be arranged in the liquid inlet 7. In another embodiment, the inlet sensor 14 may be arranged at the liquid inlet 7. In yet another embodiment, the inlet sensor 14 may be placed just before the liquid inlet. In still another embodiment the inlet sensor 14 may be located at the pressurizing mechanism or near the stream upward side of the pressurizing mechanism. The inlet sensor 14 may be configured to generate a signal indicative of cavitation in the coolant.
  • the inlet sensor 14 in the liquid inlet 7 may be of any type capable of sensing one or more characteristics of the coolant that are indicative of cavitation, and may for example sense pressure and/or temperature of the coolant. In the exemplary disclosed embodiment, the inlet sensor 14 may sense both pressure and temperature of the coolant.
  • the inlet sensor 14 may extend through the wall 10 of the coolant pump housing 6 into the liquid inlet 7. The inlet sensor 14 may then be in direct contact with the coolant, and may be subject to operating conditions of the coolant. Such operating conditions may include a temperature range of for example about -40 °C to about 130 °C, and a pressure range of for example about -50 kPa to about 150 kPa.
  • a suitable inlet sensor 14 is for example an integrated pressure and temperature sensor of the 112CP series that is commercially available from Sensata Technologies.
  • the system 1 may comprise a plurality of inlet sensors 14, for example separate temperature and pressure sensors.
  • the system 1 may also include a sensor 15 associated with the liquid outlet 8, which sensor 15 shall hereafter for ease of reference also be referred to as outlet sensor 15.
  • the outlet sensor 15 may be in close proximity to the liquid outlet 8. It should be noted that within this context, the expression that the outlet sensor is in close proximity to the liquid outlet 8 is meant to also encompass that the outlet sensor 15 extends into the exit flow passage from the pressurizing mechanism.
  • the outlet sensor 15 may be arranged in the liquid outlet 8.
  • the outlet sensor 15 may be arranged at the liquid outlet 7.
  • the outlet sensor 15 may be placed just before the liquid outlet 8.
  • the outlet sensor 15 may be arranged at or near the downstream side of the pressurizing mechanism.
  • the outlet sensor 15 may be configured to generate a signal indicative of cavitation in the coolant.
  • the outlet sensor 15 may be of any type capable of sensing one or more characteristics of the coolant that are indicative of cavitation, and may for example sense pressure and/or temperature of the coolant. In the exemplary disclosed embodiment, the outlet sensor 15 may sense both pressure and temperature of the coolant.
  • the outlet sensor 15 may extend through the wall 10 of the pump housing 6 into the liquid outlet 8. The outlet sensor 15 may then be in direct contact with the coolant, and may be subject to operating conditions of the coolant. Such operating conditions may include a temperature range of for example about -40 °C to about 130 °C, and a pressure range of for example about -50 kPa to about 150 kPa.
  • a suitable outlet sensor 15 is for example an integrated pressure and temperature sensor of the 112CP series that is commercially available from Sensata Technologies.
  • the system 1 may comprise a plurality of outlet sensors 15, for example separate temperature and pressure sensors. By providing sensors capable of sensing the same characteristic of the coolant in both the liquid inlet 7 and the liquid outlet 8, an actual differential value of that characteristic across the coolant pump 3 may be determined.
  • the system 1 may include a further sensor 17 downstream of the liquid outlet 8.
  • the system 1 may instead of the outlet sensor 15 include further sensor 17 in the engine 2.
  • the further sensor 17 is shown in Fig. 1 in dotted lines.
  • the system 1 may further include a controller 16.
  • the controller 16 may have one or more sensor data inputs, for example to receive data from inlet sensor 14, outlet sensor 15 and/or further sensor 17.
  • the controller 16 may be arranged to take precautionary action on receipt of a signal indicative of cavitation from one of the sensors.
  • the precautionary action may include activating an operator alarm 18, for example a visible and/or audible alarm, upon receipt of a signal indicative of cavitation from one of the sensors.
  • the precautionary action may include reducing an output of the power source 2, for example crankshaft power, upon receipt of a signal indicative of cavitation.
  • the controller 16 may be arranged to reduce fuelling of an engine upon receipt of a signal indicative of cavitation.
  • the precautionary action may include first activating one or more operator alarms 18, and, if the control system 1 continues to receive a signal indicative of cavitation for a predetermined time span, subsequently reducing output of the power source 2.
  • the predetermined time span may for example be several tens of seconds, and may be a fixed or a variable time span, for example based on operating conditions.
  • the controller 16 may further be associated with an input for coolant pump speed data, for example actual rpm of the coolant pump 3 or, for example engine rpm in case there is a fixed relation between engine rpm and coolant pump rpm.
  • the controller 16 may be associated with a reference value, for example an electronic map 19 with threshold values for coolant parameters indicative of cavitaton.
  • the electronic map 19 may include threshold inlet pressure and inlet temperature values for various speeds of the coolant pump 3.
  • the controller 16 may further be configured to regulate engine operation during normal operation of the coolant pump 3.
  • the controller 16 may be for example part of the engine management system 1.
  • Fig. 3 is a flow chart illustrating an exemplary disclosed method of guarding against cavitation.
  • Fig. 4 illustrates an exemplary disclosed method of control of the cavitation guarding system 1. Fig. 3 and Fig. 4 shall be discussed in the next section.
  • the disclosed coolant pump 3 cavitation guarding system 1 may be used to guard against cavitation in any coolant pump system 1 for pumping coolant through a power source 2, for example a power source 2 of a mobile machine.
  • the cavitation guarding system 1 may function as follows.
  • coolant may be circulated through the power source 2, for example to remove excess heat generated by a combustion process in the power source 2.
  • the coolant may flow from the coolant pump 3 to the power source 2 via conduits 13 formed by flexible hoses, and may subsequently flow through the power source 2 via internal conduits 13 formed by channels that form the water jacket around the cylinders (not shown).
  • the coolant may absorb excess heat from the internal combustion process of the engine by flowing around the cylinders.
  • the coolant may flow away from the engine via conduits 13 formed by flexible hoses, and may pass through a radiator 4 to exchange the absorbed heat with an air stream passing through the radiator 4.
  • the coolant may flow through an expansion tank 5, to arrive back at the coolant pump 3.
  • the coolant may flow into the coolant pump 3 via the liquid inlet 7.
  • the coolant may be pressurized by the pressurizing mechanism 12, and may exit the coolant pump 3 via the liquid outlet 8.
  • the coolant may enter the coolant pump 3 via the liquid inlet chamber 9 just before being pressurized, and may be subsequently pressurized by the fixed displacement impeller 21 as pressurizing mechanism 12.
  • the pressurized coolant may leave the coolant pump 3 via the liquid outlet chamber 11.
  • the portion of conduit 13 extending from the liquid outlet 8 of coolant pump 3 to the power source 2 may be a relatively high pressure portion 22, while the portion of the conduit 13 extending from the power source 2 to the liquid inlet 7 of the coolant pump 3 may be a relatively low pressure portion 23.
  • the power source 2 may be used to pressurize the coolant by driving the pressurizing mechanism 12 of the coolant pump 3.
  • the central shaft 20 of the impeller 21 of the pressurizing mechanism 12 may be driven to rotate through a fixed ratio mechanical transmission that branches off the crankshaft of the engine forming the power source 2.
  • the operation of such a system 1 is well known to the skilled person, and shall not be discussed in further detail.
  • At least one parameter characteristic of cavitation in the coolant may be sensed just before or while the coolant is pressurized, and precautionary action may be taken upon the sensed parameter being indicative of cavitation.
  • Such a parameter may include a pressure of the coolant flow just before or while being pressurized, and may further include a pressure of the coolant flow after it has been pressurized. Alternatively or in addition, such a parameter may further include a temperature of the coolant flow just before or while being pressurized, and optionally a temperature of the coolant after it has been pressurized.
  • Such parameters may be sensed by one or more sensors 14 in the liquid inlet 7 of the coolant pump 3, and/or one or more sensors 15 in the liquid outlet 8 of the coolant pump 3.
  • pressure and temperature may be sensed of the coolant flowing through the inlet chamber 9 using an integrated pressure and temperature sensor 14.
  • pressure and temperature may be sensed of the coolant flowing through the outlet chamber 11 using an integrated pressure and temperature sensor 15. Using these data, an accurate pressure and temperature differential across the coolant pump 3 may be obtained.
  • the controller 16 may further be provided with coolant pump speed data, for example actual rpm of the coolant pump 3 or engine rpm.
  • the one or more sensors may generate a signal that may be indicative of cavitation when the sensed parameter is indicative of cavitation.
  • the controller 16 may take precautionary action, for example activating an operator alarm 18 and/or reducing an output of the power source 2, for example crankshaft power.
  • the controller 16 may for example reduce fuelling of the power source 2 upon receipt of a signal indicative of cavitation.
  • the controller 16 may compare the received signal with reference value to determine whether the signal is indicative of cavitation.
  • a reference value may be an electronic map 19 with threshold values for signal values corresponding to sensed coolant parameters that are indicative of cavitaton for certain coolant pump speeds or engine speeds.
  • parameters of the coolant may be mapped that are indicative of the possible generation of cavitation in the coolant.
  • the actual generation of cavitation in a specific cooling liquid may be mapped for a specific type of coolant pump 3 for one or more of pump speed, inlet pressure, inlet temperature, outlet pressure and outlet temperature, and subsequently threshold values for those parameters may be mapped and stored in an electronic map 19.
  • the mapped data may form threshold value curves that are offset from actual cavitation curves for a specific pump design and a specific type of coolant. In the cavitation guarding system 1, sensing inlet pressure may suffice.
  • other parameters characteristic of cavitation may be determined intrinsically, for example an assumed inlet temperature of the coolant, and an assumed pressure and temperature differential across the coolant pump 3.
  • the accuracy of the system 1 may be enhanced when both temperature and pressure are sensed in the coolant flow in the liquid inlet 7, and when they are sensed at the same location.
  • the accuracy of the system 1 may be enhanced still further, when in addition pressure and/or temperature are sensed in the coolant flow downstream of the liquid inlet 7, for example in the liquid outlet 8 using an outlet sensor 15 or a further sensor 17 or in the engine 2.
  • Accuracy of the system 1 may be most important when a coolant pump 3 is to run at a relatively high inlet temperature in view of design constraints on the cooling system 1.
  • the controller 16 may also regulate engine operation during normal operation of the coolant pump 3.
  • the controller 16 may be for example part of the engine management system, for example an Engine Control Unit. It may be recorded, for example in an Engine Control Unit, when the sensed parameter has been indicative of cavitation. For purposes of diagnosis and, for example, warranty, also other operational characteristics may be recorded, such as operator response to a cavitation alarm
  • the method for guarding against cavitation may include the following steps. Referring to Fig. 3 , a flow chart with an exemplary disclosed method of guarding against cavitation is shown.
  • the method for guarding against cavitation may include circulating coolant to flow through a power source (step 100) and pressurizing the coolant (step 600). At least one parameter indicative of cavitation may be sensed in the coolant just before being pressurized (Step 200). The sensed parameter may be evaluated for being indicative of cavitation (Step 300). If the sensed parameter is found to be indicative of cavitation, precautionary action may be taken (Step 400). If the sensed parameter is not found to be indicative of cavitation, the coolant may be pressurized without taking preventive action (Step 500).
  • the controller 16 may read coolant pressure and temperature from the inlet sensor 14 (step 1000). Next, it may read coolant pressure and temperature from the outlet sensor 15 (step 2000). Subsequently, it may read speed or rpm value of the engine driving the coolant pump 3 (step 3000). The data read may be entered in an electronic map 19, and a cavitation value may be read from the map (step 4000).
  • the steps 1000 through 4000 may be performed in another order, for example taking step 3000 first.
  • some of the steps 1000 through 4000 may be combined, for example combining step 1000 with step 2000 and combining step 4000 with step 5000.
  • At least one of the steps 1000 through step 4000 may be omitted, for example omitting steps 4000 and 5000.
  • it may be assessed if the cavitation value exceeds a threshold value (step 5000). If the cavitation value is equal to or lower then a threshold value, the controller 16 may not take precautionary action, and may start a new cycle (step 6000). If the cavitation value exceeds the threshold value, the controller 16 may take precautionary action for example by activating visible and audible operator alarms 18 (step 7000). Next, it may be evaluated whether the cavitation value exceeds the threshold value for a predetermined time or not (step 8000).
  • a new cycle may be started (step 9000). If the cavitation value exceeds the threshold value for a predetermined time, for example 30 seconds or more, then the controller 16 may reduce fuelling (step 10000), and may start a new cycle (step 11000).
  • the coolant pump 3 may at least substantially be prevented from being subjected to cavitation.
  • coolant pump cavitation guarding system of the present disclosure without departing from the scope of the disclosure.
  • Other embodiments will be apparent to those skilled in the art from consideration of the specification and practice of the coolant pump cavitation guarding system disclosed herein.
  • coolant is considered to also encompass a lubricant such as engine oil
  • a coolant pump is also considered to encompass an oil pump for an engine. It is intended that the specification and examples be considered as exemplary only, with a true scope of invention being indicated by the following claims and their equivalents.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Positive-Displacement Pumps (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

A coolant pump cavitation guarding system is disclosed that has a power source and a coolant pump. The coolant pump has a housing having a liquid inlet and a liquid outlet. The housing further has a liquid pressurizing mechanism that is arranged between the liquid inlet and the liquid outlet and that is driven to circulate coolant through the power source. The system further has a sensor that is associated with the liquid inlet and that configured to generate a signal indicative of cavitation in the coolant. In addition, the system has a controller that is arranged to take precautionary action upon receipt of a signal indicative of cavitation from the sensor.

Description

    Technical Field
  • The present disclosure is directed to a coolant pump system, and, more particularly to a coolant pump cavitation guarding system.
  • Background
  • Coolant pump systems may include a power source and a coolant pump associated therewith. Commonly the coolant pump is driven by the power source, for example an internal combustion engine, and circulates coolant through the power source. The coolant pump commonly includes a housing having a liquid inlet, a liquid outlet and a liquid pressurizing mechanism arranged between the liquid inlet and the liquid outlet of the pump. The pressurizing mechanism of the coolant pump is commonly embodied as a fixed displacement impeller.
  • Coolant pump systems for power sources may currently be exposed to water pump failures caused by cavitation. Cavitation is localized generation of vapor phase of the coolant in the pump, which may occur at the liquid inlet if coolant temperature is relatively high, and coolant pressure is relatively low. Upon subsequent pressurizing of the coolant, vapor bubbles may implode onto the pump mechanism, and may cause severe damage to the pump mechanism. Such damage often goes undetected initially, but may lead to loss of efficiency of the pressurizing mechanism and ultimately to failure of the pump mechanism. In an end product, for example a vehicle, the coolant pump system may include a cooling arrangement, for example a radiator, so that a cooling system is formed. In normal manufacture of an end product, the cooling arrangement matches the power source such that generation of cavitation in the coolant pump is prevented. However, in case the cooling arrangement is provided by another party than the supplier of the coolant pump system, it has been found that the issue of pump cavitation is sometimes overlooked. This may occur particularly when a cooling arrangement is designed to save space and weight, and the power source thus runs with a relatively high coolant inlet temperature.
  • Japanese patent publication 57191413 discloses a water pump controller system for an engine that is provided with a cavitation sensor to reduce the generation of cavitation and to prevent overheating of the engine. The cavitation sensor is a unit separate from the water pump having a housing with a coolant chamber that is fluidly connected to the coolant system. The coolant chamber has a diaphragm that is mechanically linked to a potentiometer. A signal from the potentiometer is sent to a comparison circuit. If the signal is smaller than a reference signal, an output of the comparison circuit reduces rotational speed of the engine driving the water pump in accordance with the output of a temperature sensor. By reducing the engine speed, the pump speed is reduced, and generation of cavitation is prevented.
  • A disadvantage associated with the water pump controller system of Japanese patent publication 57191413 is that it is mechanically complex, and thus may be prone to failure. Further it is relatively costly to install. In addition, the accuracy of the system leaves much to be desired.
  • The disclosed coolant pump cavitation guarding system is directed at alleviating one or more of the disadvantages set forth above.
  • Summary of the Invention
  • One aspect of the present disclosure is directed to a coolant pump cavitation guarding system. The system comprises a power source and a coolant pump. The coolant pump includes a housing having a liquid inlet and a liquid outlet, and a liquid pressurizing mechanism. The liquid pressurizing mechanism is arranged between the liquid inlet and the liquid outlet, and is driven to circulate coolant through the power source. The system further includes a sensor associated with the liquid inlet that is configured to generate a signal indicative of cavitation in the coolant. In addition, the system includes a controller arranged to take precautionary action upon receipt of a signal indicative of cavitation from the sensor.
  • Another aspect of the present disclosure is directed to a method of guarding against cavitation. The method comprises circulating coolant to flow through a power source, and pressurizing the coolant. The method further includes sensing at least one parameter characteristic of cavitation in the coolant just prior to or while being pressurized, and taking precautionary action upon said sensed parameter being indicative of cavitation.
  • Brief Description of the Drawings
  • Fig. 1 is a diagrammatic illustration of an exemplary disclosed coolant cavitation guarding system;
  • Fig. 2 is a cross sectional illustration of an exemplary disclosed coolant pump for use with the system of Fig. 1;
  • Fig. 3 is a flow chart illustrating an exemplary disclosed method of guarding against cavitation, and
  • Fig. 4 is a flow chart illustrating an exemplary method of control of the system of Fig. 1.
  • Detailed Description
  • Fig. 1 shows an exemplary disclosed cavitation guarding system 1. The system 1 comprises a power source 2. The power source 2 may be a power generating apparatus of any type that requires cooling. In the exemplary disclosed system 1, the power source 2 may be an internal combustion engine, for example a diesel or gasoline engine. The power source 2 may also be of another type, for example an external combustion engine, such as a gas turbine. The cavitation guarding system 1 may further comprise a coolant pump 3 to pump liquid coolant. The coolant may be of any type, for example a water based coolant with optionally anti-corrosion and anti freeze additives. In one embodiment, such water based coolant may include ethylene glycol and a so called corrosion prevention package. In another embodiment, such water based coolant may be propylene glycol. In yet another embodiment, the coolant may be a so called extended life coolant without water. In the exemplary disclosed system 1, the coolant may be a mixture including about 50% water and about 50% ethylene glycol, and optionally a so called corrosion prevention package. The cavitation guarding system 1 may include an engine cooling arrangement including one or more radiators 4 and/or expansion tanks 5, so that a cooling system is formed. The configuration of such cooling arrangements is well known to the skilled person, and hence shall not be discussed further.
  • The coolant pump 3 may include a pump housing 6, which may be provided with a liquid inlet 7 and a liquid outlet 8. The liquid inlet 7 may comprise an inlet chamber 9 defined by the wall 10 of the pump housing 6. Likewise, the liquid outlet 8 may comprise an outlet chamber 11 defined by the wall 10. A liquid pressurizing mechanism 12 may be arranged between the liquid inlet 7 and the liquid outlet 8. The pressurizing mechanism 12 may be of any type that is capable of pressurizing a coolant, and susceptible to cavitation damage. In the exemplary disclosed system 1, the pressurizing mechanism 12 may be a fixed displacement impeller 21 of the radial type carried on a central shaft 20, as is common for internal combustion engines. In another embodiment, the pressurizing mechanism 12 may be for example that of a gerotor type coolant pump 3. In yet another embodiment, the pressurizing mechanism 12 may be that of a vane type pump 3. The pressurizing mechanism 12 may be driven by the power source 2 to circulate coolant through the power source 2. The pressurizing mechanism 12 may be driven by the power source 2 directly or indirectly. In one embodiment, the pressurizing mechanism may be driven directly via a mechanical transmission, for example a gear drive of drive belt. In another embodiment, the pressurizing mechanism may be driven indirectly, for example via a hydraulic motor driven by a hydraulic pump actuated by the power source. In yet another embodiment, the pressurizing mechanism may be driven indirectly, for example using an electric motor powered by an alternator driven by the power source. In yet another embodiment, the pressurizing mechanism may be driven by another device than the power source 2, for example by a motor that is powered separately. In the exemplary disclosed embodiment, the impeller 21 of the pressurizing mechanism 12 may have a central shaft 20 that is directly driven to rotate by the power source via a gear drive having a fixed ratio mechanical transmission that branches off the crankshaft of the engine forming the power source 2. The coolant may be circulated to and from the power source 2 using conduits 13, for example hoses, pipes or channels. The coolant may likewise be circulated through the power source 2 using conduits 13, for example hoses, pipes or channels. In the exemplary disclosed embodiment, coolant flows to and from the engine via flexible hoses, and circulates through the engine via channels that define a water jacket surrounding the cylinders (not shown).
  • In accordance with the disclosure, a sensor 14 may be associated with the liquid inlet 7, and shall hereafter for ease of reference also be referred to as inlet sensor 14. The inlet sensor 14 may be in close proximity to the liquid inlet 7. It should be noted that within this context the expression that the inlet sensor 14 in close proximity to the liquid inlet 7 is meant to also encompass that the inlet sensor 7 extends into the introductory flow passage to the pressurizing mechanism or in the pressurizing zone of the coolant pump 3 itself.
  • In one embodiment, the inlet sensor 14 may be arranged in the liquid inlet 7. In another embodiment, the inlet sensor 14 may be arranged at the liquid inlet 7. In yet another embodiment, the inlet sensor 14 may be placed just before the liquid inlet. In still another embodiment the inlet sensor 14 may be located at the pressurizing mechanism or near the stream upward side of the pressurizing mechanism. The inlet sensor 14 may be configured to generate a signal indicative of cavitation in the coolant. The inlet sensor 14 in the liquid inlet 7 may be of any type capable of sensing one or more characteristics of the coolant that are indicative of cavitation, and may for example sense pressure and/or temperature of the coolant. In the exemplary disclosed embodiment, the inlet sensor 14 may sense both pressure and temperature of the coolant. The inlet sensor 14 may extend through the wall 10 of the coolant pump housing 6 into the liquid inlet 7. The inlet sensor 14 may then be in direct contact with the coolant, and may be subject to operating conditions of the coolant. Such operating conditions may include a temperature range of for example about -40 °C to about 130 °C, and a pressure range of for example about -50 kPa to about 150 kPa. A suitable inlet sensor 14 is for example an integrated pressure and temperature sensor of the 112CP series that is commercially available from Sensata Technologies. As an alternative, in another embodiment, the system 1 may comprise a plurality of inlet sensors 14, for example separate temperature and pressure sensors.
  • The system 1 may also include a sensor 15 associated with the liquid outlet 8, which sensor 15 shall hereafter for ease of reference also be referred to as outlet sensor 15. The outlet sensor 15 may be in close proximity to the liquid outlet 8. It should be noted that within this context, the expression that the outlet sensor is in close proximity to the liquid outlet 8 is meant to also encompass that the outlet sensor 15 extends into the exit flow passage from the pressurizing mechanism. In one embodiment, the outlet sensor 15 may be arranged in the liquid outlet 8. In another embodiment, the outlet sensor 15 may be arranged at the liquid outlet 7. In yet another embodiment, the outlet sensor 15 may be placed just before the liquid outlet 8. In still another embodiment, the outlet sensor 15 may be arranged at or near the downstream side of the pressurizing mechanism. The outlet sensor 15 may be configured to generate a signal indicative of cavitation in the coolant. The outlet sensor 15 may be of any type capable of sensing one or more characteristics of the coolant that are indicative of cavitation, and may for example sense pressure and/or temperature of the coolant. In the exemplary disclosed embodiment, the outlet sensor 15 may sense both pressure and temperature of the coolant. The outlet sensor 15 may extend through the wall 10 of the pump housing 6 into the liquid outlet 8. The outlet sensor 15 may then be in direct contact with the coolant, and may be subject to operating conditions of the coolant. Such operating conditions may include a temperature range of for example about -40 °C to about 130 °C, and a pressure range of for example about -50 kPa to about 150 kPa. A suitable outlet sensor 15 is for example an integrated pressure and temperature sensor of the 112CP series that is commercially available from Sensata Technologies. As an alternative, in another embodiment, the system 1 may comprise a plurality of outlet sensors 15, for example separate temperature and pressure sensors. By providing sensors capable of sensing the same characteristic of the coolant in both the liquid inlet 7 and the liquid outlet 8, an actual differential value of that characteristic across the coolant pump 3 may be determined. In yet another embodiment, the system 1 may include a further sensor 17 downstream of the liquid outlet 8. For example, the system 1 may instead of the outlet sensor 15 include further sensor 17 in the engine 2. The further sensor 17 is shown in Fig. 1 in dotted lines.
  • The system 1 may further include a controller 16. The controller 16 may have one or more sensor data inputs, for example to receive data from inlet sensor 14, outlet sensor 15 and/or further sensor 17. The controller 16 may be arranged to take precautionary action on receipt of a signal indicative of cavitation from one of the sensors. In one embodiment, the precautionary action may include activating an operator alarm 18, for example a visible and/or audible alarm, upon receipt of a signal indicative of cavitation from one of the sensors. In another embodiment, the precautionary action may include reducing an output of the power source 2, for example crankshaft power, upon receipt of a signal indicative of cavitation. For example, the controller 16 may be arranged to reduce fuelling of an engine upon receipt of a signal indicative of cavitation. In another embodiment, the precautionary action may include first activating one or more operator alarms 18, and, if the control system 1 continues to receive a signal indicative of cavitation for a predetermined time span, subsequently reducing output of the power source 2. The predetermined time span may for example be several tens of seconds, and may be a fixed or a variable time span, for example based on operating conditions. The controller 16 may further be associated with an input for coolant pump speed data, for example actual rpm of the coolant pump 3 or, for example engine rpm in case there is a fixed relation between engine rpm and coolant pump rpm. The controller 16 may be associated with a reference value, for example an electronic map 19 with threshold values for coolant parameters indicative of cavitaton. For example, the electronic map 19 may include threshold inlet pressure and inlet temperature values for various speeds of the coolant pump 3. The controller 16 may further be configured to regulate engine operation during normal operation of the coolant pump 3. In the exemplary disclosed embodiment, the controller 16 may be for example part of the engine management system 1.
  • Fig. 3 is a flow chart illustrating an exemplary disclosed method of guarding against cavitation. Fig. 4 illustrates an exemplary disclosed method of control of the cavitation guarding system 1. Fig. 3 and Fig. 4 shall be discussed in the next section.
  • Industrial Applicability
  • The disclosed coolant pump 3 cavitation guarding system 1 may be used to guard against cavitation in any coolant pump system 1 for pumping coolant through a power source 2, for example a power source 2 of a mobile machine. The cavitation guarding system 1 may function as follows. During operation, coolant may be circulated through the power source 2, for example to remove excess heat generated by a combustion process in the power source 2. Referring to Fig. 1 it is shown that in the exemplary disclosed embodiment, the coolant may flow from the coolant pump 3 to the power source 2 via conduits 13 formed by flexible hoses, and may subsequently flow through the power source 2 via internal conduits 13 formed by channels that form the water jacket around the cylinders (not shown). In an embodiment in which the power source 2 is configured as a combustion engine, the coolant may absorb excess heat from the internal combustion process of the engine by flowing around the cylinders. Next, the coolant may flow away from the engine via conduits 13 formed by flexible hoses, and may pass through a radiator 4 to exchange the absorbed heat with an air stream passing through the radiator 4. Subsequently, the coolant may flow through an expansion tank 5, to arrive back at the coolant pump 3. The coolant may flow into the coolant pump 3 via the liquid inlet 7. Next, the coolant may be pressurized by the pressurizing mechanism 12, and may exit the coolant pump 3 via the liquid outlet 8. In the exemplary disclosed embodiment of Fig. 2, it is shown that the coolant may enter the coolant pump 3 via the liquid inlet chamber 9 just before being pressurized, and may be subsequently pressurized by the fixed displacement impeller 21 as pressurizing mechanism 12. The pressurized coolant may leave the coolant pump 3 via the liquid outlet chamber 11. The portion of conduit 13 extending from the liquid outlet 8 of coolant pump 3 to the power source 2 may be a relatively high pressure portion 22, while the portion of the conduit 13 extending from the power source 2 to the liquid inlet 7 of the coolant pump 3 may be a relatively low pressure portion 23.
  • The power source 2 may be used to pressurize the coolant by driving the pressurizing mechanism 12 of the coolant pump 3. In the exemplary disclosed embodiment of Fig. 1 and Fig. 2, the central shaft 20 of the impeller 21 of the pressurizing mechanism 12 may be driven to rotate through a fixed ratio mechanical transmission that branches off the crankshaft of the engine forming the power source 2. The operation of such a system 1 is well known to the skilled person, and shall not be discussed in further detail.
  • In accordance with the disclosure, to guard against subjecting the coolant pump 3 to cavitation, at least one parameter characteristic of cavitation in the coolant may be sensed just before or while the coolant is pressurized, and precautionary action may be taken upon the sensed parameter being indicative of cavitation.
  • Such a parameter may include a pressure of the coolant flow just before or while being pressurized, and may further include a pressure of the coolant flow after it has been pressurized. Alternatively or in addition, such a parameter may further include a temperature of the coolant flow just before or while being pressurized, and optionally a temperature of the coolant after it has been pressurized. Such parameters may be sensed by one or more sensors 14 in the liquid inlet 7 of the coolant pump 3, and/or one or more sensors 15 in the liquid outlet 8 of the coolant pump 3. In the exemplary disclosed embodiment in Fig. 1 and Fig. 2, pressure and temperature may be sensed of the coolant flowing through the inlet chamber 9 using an integrated pressure and temperature sensor 14. Optionally, pressure and temperature may be sensed of the coolant flowing through the outlet chamber 11 using an integrated pressure and temperature sensor 15. Using these data, an accurate pressure and temperature differential across the coolant pump 3 may be obtained. The controller 16 may further be provided with coolant pump speed data, for example actual rpm of the coolant pump 3 or engine rpm.
  • The one or more sensors may generate a signal that may be indicative of cavitation when the sensed parameter is indicative of cavitation. Upon receipt of a signal indicative of cavitation from the inlet sensor 14 in one of the data inputs, the controller 16 may take precautionary action, for example activating an operator alarm 18 and/or reducing an output of the power source 2, for example crankshaft power. In the exemplary disclosed embodiment of Fig. 1 and Fig. 2, the controller 16 may for example reduce fuelling of the power source 2 upon receipt of a signal indicative of cavitation. The controller 16 may compare the received signal with reference value to determine whether the signal is indicative of cavitation. In one embodiment, such a reference value may be an electronic map 19 with threshold values for signal values corresponding to sensed coolant parameters that are indicative of cavitaton for certain coolant pump speeds or engine speeds.
  • Based on experimental data for a specific type of coolant pump 3 or physical calculations, parameters of the coolant may be mapped that are indicative of the possible generation of cavitation in the coolant. For example, the actual generation of cavitation in a specific cooling liquid may be mapped for a specific type of coolant pump 3 for one or more of pump speed, inlet pressure, inlet temperature, outlet pressure and outlet temperature, and subsequently threshold values for those parameters may be mapped and stored in an electronic map 19. The mapped data may form threshold value curves that are offset from actual cavitation curves for a specific pump design and a specific type of coolant. In the cavitation guarding system 1, sensing inlet pressure may suffice. In one embodiment, other parameters characteristic of cavitation may be determined intrinsically, for example an assumed inlet temperature of the coolant, and an assumed pressure and temperature differential across the coolant pump 3. However, the accuracy of the system 1 may be enhanced when both temperature and pressure are sensed in the coolant flow in the liquid inlet 7, and when they are sensed at the same location. The accuracy of the system 1 may be enhanced still further, when in addition pressure and/or temperature are sensed in the coolant flow downstream of the liquid inlet 7, for example in the liquid outlet 8 using an outlet sensor 15 or a further sensor 17 or in the engine 2. Accuracy of the system 1 may be most important when a coolant pump 3 is to run at a relatively high inlet temperature in view of design constraints on the cooling system 1.
    The controller 16 may also regulate engine operation during normal operation of the coolant pump 3. In the exemplary disclosed embodiment, the controller 16 may be for example part of the engine management system, for example an Engine Control Unit. It may be recorded, for example in an Engine Control Unit, when the sensed parameter has been indicative of cavitation. For purposes of diagnosis and, for example, warranty, also other operational characteristics may be recorded, such as operator response to a cavitation alarm
  • In general, the method for guarding against cavitation may include the following steps. Referring to Fig. 3, a flow chart with an exemplary disclosed method of guarding against cavitation is shown. In accordance with the disclosure, the method for guarding against cavitation may include circulating coolant to flow through a power source (step 100) and pressurizing the coolant (step 600). At least one parameter indicative of cavitation may be sensed in the coolant just before being pressurized (Step 200). The sensed parameter may be evaluated for being indicative of cavitation (Step 300). If the sensed parameter is found to be indicative of cavitation, precautionary action may be taken (Step 400). If the sensed parameter is not found to be indicative of cavitation, the coolant may be pressurized without taking preventive action (Step 500).
  • Referring to Fig. 4, an exemplary method of controlling the dislosed cavitation guarding system 1 is provided. First, the controller 16 may read coolant pressure and temperature from the inlet sensor 14 (step 1000). Next, it may read coolant pressure and temperature from the outlet sensor 15 (step 2000). Subsequently, it may read speed or rpm value of the engine driving the coolant pump 3 (step 3000). The data read may be entered in an electronic map 19, and a cavitation value may be read from the map (step 4000). In another embodiment, the steps 1000 through 4000 may be performed in another order, for example taking step 3000 first. In yet another embodiment, some of the steps 1000 through 4000 may be combined, for example combining step 1000 with step 2000 and combining step 4000 with step 5000. In still another embodiment, at least one of the steps 1000 through step 4000 may be omitted, for example omitting steps 4000 and 5000. Next, it may be assessed if the cavitation value exceeds a threshold value (step 5000). If the cavitation value is equal to or lower then a threshold value, the controller 16 may not take precautionary action, and may start a new cycle (step 6000). If the cavitation value exceeds the threshold value, the controller 16 may take precautionary action for example by activating visible and audible operator alarms 18 (step 7000). Next, it may be evaluated whether the cavitation value exceeds the threshold value for a predetermined time or not (step 8000). If the cavitation value does not exceed the threshold value for a predetermined time, for example less than 30 seconds, a new cycle may be started (step 9000). If the cavitation value exceeds the threshold value for a predetermined time, for example 30 seconds or more, then the controller 16 may reduce fuelling (step 10000), and may start a new cycle (step 11000).
  • With the disclosed cavitation guarding system 1, even when a cooling arrangement including a radiator 4 that is designed to save space and weight is supplied by another party than the engine manufacturer, and even when the power source 2 runs the coolant pump 3 with a relatively high coolant inlet temperature, the coolant pump 3 may at least substantially be prevented from being subjected to cavitation.
  • It will be apparent to those skilled in the art that various modifications and variations can be made to the coolant pump cavitation guarding system of the present disclosure without departing from the scope of the disclosure. Other embodiments will be apparent to those skilled in the art from consideration of the specification and practice of the coolant pump cavitation guarding system disclosed herein. It should be noted that within the context of this description, the term coolant is considered to also encompass a lubricant such as engine oil, and the term a coolant pump is also considered to encompass an oil pump for an engine. It is intended that the specification and examples be considered as exemplary only, with a true scope of invention being indicated by the following claims and their equivalents.

Claims (23)

  1. A coolant pump cavitation guarding system, comprising:
    a power source;
    a coolant pump including:
    a housing having a liquid inlet and a liquid outlet; and
    a liquid pressurizing mechanism that is arranged between the liquid inlet and
    the liquid outlet and that is driven to circulate coolantthrough the power
    source; and
    a sensor associated with the liquid inlet configured to generate a signal indicative of cavitation in the coolant; and
    a controller arranged to take precautionary action based upon said signal.
  2. The system of claim 1, wherein the pressurizing mechanism is driven by the power source.
  3. The system of claim 1 or 2, wherein the sensor in the inlet senses a pressure of the coolant.
  4. The system of any of claims 1-3, wherein the sensor in the inlet senses a temperature of the coolant.
  5. The system of any of claims 1-4, wherein the sensor in the inlet extends through the wall of the housing into the liquid inlet.
  6. The system of any of the preceding claims, further including a further sensor that generates a signal indicative of cavitation in the coolant arranged downstream of the coolant pump.
  7. The system of claim 5, wherein the further sensor senses a pressure and/or a temperature of the coolant.
  8. The system of any of the preceding claims wherein the precautionary action includes activating an operator alarm.
  9. The system of any of the preceding claims, wherein the precautionary action includes reducing an output of the power source.
  10. The system of any of the preceding claims, wherein the power source is an engine.
  11. The system of claim 10, wherein the precautionary action includes reducing fueling of the engine upon receipt of a signal indicative of cavitation.
  12. The system of claim 11, wherein the system is further configured to regulate engine operation during normal pump operation.
  13. A method of guarding against cavitation, comprising:
    circulating coolant to flow through a power source;
    pressurizing the coolant;
    sensing at least one characteristic indicative of cavitation in the coolant just before or while being pressurized; and
    taking precautionary action upon said sensed parameter being indicative of cavitation.
  14. The method of claim 13, wherein the power source is used to pressurize the coolant.
  15. The method of claim 13 or 14, wherein the precautionary action includes activating an operator alarm.
  16. The method of any of claims 13-15, wherein the precautionary action includes reducing an output of the power source.
  17. The method of claim 16, wherein reducing the output includes reducing fueling of the power source.
  18. The method of any of claims 13-17, wherein the at least one parameter includes a pressure of the coolant flow just before being pressurized.
  19. The method of claim 18, wherein the at least one parameter further includes a temperature of the coolant flow just before being pressurized.
  20. The method of any of claims 18-20, wherein the parameter further includes pump speed or engine speed
  21. A coolant pump, comprising:
    a housing having a liquid inlet and a liquid outlet;
    a liquid pressurizing mechanism arranged between the liquid inlet and the liquid outlet; and
    an pressure sensor arranged in the liquid inlet to generate a signal indicative of cavitation.
  22. The coolant pump of claim 21, wherein the sensor in the inlet comprises an integrated pressure and temperature sensor.
  23. The coolant pump of claim 21 or 22, wherein the sensor in the inlet extends through the housing into an inlet chamber.
EP07122038A 2007-11-30 2007-11-30 Coolant pump cavitation guarding system Not-in-force EP2065584B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP07122038A EP2065584B1 (en) 2007-11-30 2007-11-30 Coolant pump cavitation guarding system
AT07122038T ATE522710T1 (en) 2007-11-30 2007-11-30 COOLING PUMP CAVITATION PROTECTION SYSTEM

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP07122038A EP2065584B1 (en) 2007-11-30 2007-11-30 Coolant pump cavitation guarding system

Publications (2)

Publication Number Publication Date
EP2065584A1 true EP2065584A1 (en) 2009-06-03
EP2065584B1 EP2065584B1 (en) 2011-08-31

Family

ID=39494552

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07122038A Not-in-force EP2065584B1 (en) 2007-11-30 2007-11-30 Coolant pump cavitation guarding system

Country Status (2)

Country Link
EP (1) EP2065584B1 (en)
AT (1) ATE522710T1 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015520819A (en) * 2012-03-28 2015-07-23 アイエムオー・インダストリーズ・インコーポレーテッド System and method for cavitation monitoring and control in positive displacement pumps
CN105736116A (en) * 2016-04-18 2016-07-06 江苏大学 Anti-cavitation intelligent controllable water pump
US9546652B2 (en) 2012-03-28 2017-01-17 Imo Industries, Inc. System and method for monitoring and control of cavitation in positive displacement pumps
CN109989947A (en) * 2019-03-19 2019-07-09 上海航天动力科技工程有限公司 A kind of cavitation arrester
CN111075553A (en) * 2018-10-22 2020-04-28 现代自动车株式会社 Method for determining coolant condition of vehicle
CN112177752A (en) * 2020-08-21 2021-01-05 东风汽车集团有限公司 Control method and control system of engine thermal management module
CN115298422A (en) * 2020-03-23 2022-11-04 五十铃自动车株式会社 Detection device and detection method
DE102013224398B4 (en) 2013-04-08 2023-04-20 Hyundai Motor Company Method for controlling a vehicle water pump and system therefor

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10134257B2 (en) 2016-08-05 2018-11-20 Caterpillar Inc. Cavitation limiting strategies for pumping system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3958548A (en) 1974-12-23 1976-05-25 General Motors Corporation Engine with differential pressure responsive protective device
JPS57191413A (en) 1981-05-21 1982-11-25 Mazda Motor Corp Water pump controller of engine
JPS57193716A (en) * 1981-05-22 1982-11-29 Mazda Motor Corp Cooler for engine
JPS6181517A (en) * 1984-09-28 1986-04-25 Nissan Motor Co Ltd Evaporative cooling device for internal-combustion engine
US5094192A (en) * 1990-05-30 1992-03-10 Volkswagen Ag Safety arrangement for an internal combustion engine
EP0893582A2 (en) * 1997-07-23 1999-01-27 UNITECH Aktiengesellschsft Method for controlling a coolant pump of an internal combustion engine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3958548A (en) 1974-12-23 1976-05-25 General Motors Corporation Engine with differential pressure responsive protective device
JPS57191413A (en) 1981-05-21 1982-11-25 Mazda Motor Corp Water pump controller of engine
JPS57193716A (en) * 1981-05-22 1982-11-29 Mazda Motor Corp Cooler for engine
JPS6181517A (en) * 1984-09-28 1986-04-25 Nissan Motor Co Ltd Evaporative cooling device for internal-combustion engine
US5094192A (en) * 1990-05-30 1992-03-10 Volkswagen Ag Safety arrangement for an internal combustion engine
EP0893582A2 (en) * 1997-07-23 1999-01-27 UNITECH Aktiengesellschsft Method for controlling a coolant pump of an internal combustion engine

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015520819A (en) * 2012-03-28 2015-07-23 アイエムオー・インダストリーズ・インコーポレーテッド System and method for cavitation monitoring and control in positive displacement pumps
US9546652B2 (en) 2012-03-28 2017-01-17 Imo Industries, Inc. System and method for monitoring and control of cavitation in positive displacement pumps
DE102013224398B4 (en) 2013-04-08 2023-04-20 Hyundai Motor Company Method for controlling a vehicle water pump and system therefor
CN105736116A (en) * 2016-04-18 2016-07-06 江苏大学 Anti-cavitation intelligent controllable water pump
CN111075553A (en) * 2018-10-22 2020-04-28 现代自动车株式会社 Method for determining coolant condition of vehicle
CN109989947A (en) * 2019-03-19 2019-07-09 上海航天动力科技工程有限公司 A kind of cavitation arrester
CN115298422A (en) * 2020-03-23 2022-11-04 五十铃自动车株式会社 Detection device and detection method
CN115298422B (en) * 2020-03-23 2023-09-29 五十铃自动车株式会社 Detection device and detection method
CN112177752A (en) * 2020-08-21 2021-01-05 东风汽车集团有限公司 Control method and control system of engine thermal management module

Also Published As

Publication number Publication date
EP2065584B1 (en) 2011-08-31
ATE522710T1 (en) 2011-09-15

Similar Documents

Publication Publication Date Title
EP2065584B1 (en) Coolant pump cavitation guarding system
US9394832B2 (en) Aeronautical engine with cooling of an electric starting device
US9863294B2 (en) Hydraulic control system for vehicle
CN102482982B (en) Control device for variable water pump
US7258083B2 (en) Integrated cooling system
US9650925B2 (en) System and method of augmenting low oil pressure in an internal combustion engine
KR20110014233A (en) Method and device for the diagnosis of a coolant pump for an internal combustion engine
EP1701014A1 (en) Rotational speed control method of fan
US6414399B1 (en) Multifunctional operating unit for nautical use
CN111878212B (en) Efficient hybrid engine cooling system and engine cooling method
US20220154600A1 (en) Pneumatic starter supplemental lubrication system
JP2008223626A (en) Lubricating liquid supply system to turbo supercharger
CN111817503A (en) Hybrid gearbox driving motor cooling system and control method
SE541765C2 (en) An oil system for lubrication and cooling in a vehicle driven at least partly by an electrical machine
KR101224965B1 (en) Water Pump including a Temperature sensor For vehicle and Engine Cooling System including the same
JP2010156314A (en) Waste heat recovery device and engine
EP2521852B1 (en) Vapor separator with integral low pressure lift pump
JP4983777B2 (en) Engine waste heat recovery system
CN104005829B (en) Waste heat utilization system with supply pump, particularly for motor vehicle
JP5879940B2 (en) Cooling device for internal combustion engine and cooling method for internal combustion engine
JP2017078347A (en) Liquid-cooled cooling device
EP3306095B1 (en) Oil supply device and method of controlling electric oil pump
WO2021193431A1 (en) Detection device and detection method
US11975721B2 (en) Work machine having a hydro-mechanical drive unit
US11691707B1 (en) Cooling system for a power generation system on a marine vessel

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK RS

17P Request for examination filed

Effective date: 20091126

17Q First examination report despatched

Effective date: 20091223

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

RBV Designated contracting states (corrected)

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602007016711

Country of ref document: DE

Effective date: 20111103

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20110831

LTIE Lt: invalidation of european patent or patent extension

Effective date: 20110831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111231

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 522710

Country of ref document: AT

Kind code of ref document: T

Effective date: 20110831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111201

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120102

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111130

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20111130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111130

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111130

26N No opposition filed

Effective date: 20120601

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20120731

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602007016711

Country of ref document: DE

Effective date: 20120601

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111130

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111211

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110831

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20141201

Year of fee payment: 8

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602007016711

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20160601