US20120325823A1 - Surge Tank - Google Patents
Surge Tank Download PDFInfo
- Publication number
- US20120325823A1 US20120325823A1 US13/583,075 US201013583075A US2012325823A1 US 20120325823 A1 US20120325823 A1 US 20120325823A1 US 201013583075 A US201013583075 A US 201013583075A US 2012325823 A1 US2012325823 A1 US 2012325823A1
- Authority
- US
- United States
- Prior art keywords
- coolant
- reservoir
- surge tank
- objects
- engine
- 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.)
- Abandoned
Links
- 239000002826 coolant Substances 0.000 claims abstract description 85
- 230000008878 coupling Effects 0.000 claims abstract description 5
- 238000010168 coupling process Methods 0.000 claims abstract description 5
- 238000005859 coupling reaction Methods 0.000 claims abstract description 5
- 239000007787 solid Substances 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 4
- 239000000498 cooling water Substances 0.000 description 11
- 239000012530 fluid Substances 0.000 description 11
- 238000001816 cooling Methods 0.000 description 10
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 238000005273 aeration Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000006260 foam Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000005187 foaming Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 230000003134 recirculating effect Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P11/00—Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
- F01P11/02—Liquid-coolant filling, overflow, venting, or draining devices
- F01P11/029—Expansion reservoirs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P2060/00—Cooling circuits using auxiliaries
- F01P2060/04—Lubricant cooler
- F01P2060/045—Lubricant cooler for transmissions
Definitions
- the present disclosure relates generally to surge tanks for use in vehicles, including surge tanks that receive coolant, deaerates the coolant, and returns the deaerated coolant to the system.
- a cooling water reservoir tank is provided and is used not only for storing an overflow of cooling water but also for ensuring a recirculation of a part of the cooling water to the reservoir tank, to thereby separate and remove air and vapor from the cooling water in the reservoir tank, to thereby separate and remove air and vapor from the cooling water in the reservoir tank, whereby the cooling efficiency of the cooling system is increased.
- an independent cooling water passageway connects the reservoir tank to an engine body and a radiator
- the reservoir tank is provided with a cap equipped with a relief valve which allows air or vapor held in an upper portion of the reservoir tank to be discharged to the atmosphere, when the pressure inside the reservoir tank exceeds a predetermined value, and thus prevents an excessive increase of the pressure in the cooling system.
- This operation also allows air to be quickly separated from the cooling water: this air is entrained in the cooling system when the cooling water is supplemented, and remains in the cooling system. The separated air is discharged by the relief valve in the reservoir tank, and thus, the cooling efficiency of the system is enhanced.
- FIG. 1 a schematic diagram of a simplified example of a vehicle (not shown) having a surge tank 110 for de-aerating coolant is illustrated.
- the vehicle comprises an engine 112 and a radiator 114 through which coolant is circulated, at least at selected times, to cool the coolant for use in removing heat from the engine 112 .
- Other components may also be cooled by the coolant such as a transmission 116 and an exhaust gas recirculation cooler (e.g. EGR cooler) not shown in this figure.
- the coolant may also be used to provide energy to or remove energy from an HVAC—heating ventilation and air conditioning—system (not shown) of the vehicle.
- a vehicle is a truck, such as a heavy duty or medium duty truck (not shown) used in long hauling operations or a truck tractor used for such purposes. Land vehicles are particularly desirable applications in which surge tanks would be used.
- segments of the coolant recirculation conduits are indicated by the numbers 118 , 120 , 122 .
- aerated coolant from the engine 112 passes via a conduit 118 to an inlet 124 to a surge tank 110 .
- aerated coolant passes through a conduit 120 from radiator 114 to an inlet 126 to the surge tank 110 , which may separate from or in common with the inlet 126 that receive aerated fluid from conduit 24 .
- Air is removed from the coolant as it passes through the surge tank 26 .
- the deaerated coolant is returned to the engine 112 via a conduit 122 in FIG. 1 .
- a surge tank is provided according to the embodiment(s) disclosed herein.
- the surge tank includes a reservoir wherein the reservoir defines a coolant receiving inlet for coupling to the engine.
- the reservoir also defines a reservoir outlet.
- the coolant receiving inlet receives a flow of coolant from the engine.
- the reservoir outlet is the outlet through which the flow of coolant is returned to the engine.
- the surge tank further includes a plurality of objects disposed within the coolant reservoir. The plurality of objects are operatively configured to float at an upper surface of the coolant in the reservoir and to dampen the momentum of the coolant flowing from the engine.
- FIG. 1 is a simplified diagram of one example of a vehicle system incorporating a surge tank.
- FIG. 2A is a perspective, partial view of a prior art surge tank.
- FIG. 2B is a perspective, partial view of a prior art surge tank where the baffles are shown disposed within the tank.
- FIG. 2C is a perspective view of one embodiment of a surge tank of the present disclosure.
- FIG. 3 is a perspective view of one embodiment of a surge tank of the present disclosure.
- FIG. 4A is a cross-sectional view of an embodiment of a surge tank of the present disclosure.
- FIG. 4B is an enlarged view of a perforated object.
- FIG. 4C is an enlarged schematic view of the coolant interacting with the perforations in an object where an increased surface area of the fluid is exposed to air (i.e. straining effect for water).
- FIG. 4D is an enlarged schematic view of the coolant flowing through a hole in the object.
- FIG. 5A is a cross sectional view of a second embodiment of a surge tank of the present disclosure where a baffle maintains the plurality of objects in area of the surge tank.
- FIG. 5B is a cross sectional view of the second embodiment of a surge tank when the tank is in an inclined position.
- FIG. 5C is a cross sectional view of the second embodiment of a surge tank when the tank is agitated.
- FIG. 6 is an enlarged, cross-sectional view of the second embodiment of a surge tank when the incoming flow of coolant is dampened by the plurality of objects.
- a surge tank 10 of the present disclosure provides improved dampening to an incoming flow of coolant 12 .
- one embodiment of the present disclosure includes a reservoir wherein the reservoir 14 defines a coolant receiving inlet 16 for coupling to the engine.
- the coolant receiving inlet 16 receives a flow of coolant 12 from the engine (shown as 112 in FIG. 1 ) and a reservoir outlet 19 through which the flow of coolant 12 is returned to the engine.
- the surge tank 10 further includes a plurality of objects 18 disposed within the coolant reservoir 14 .
- the plurality of objects 18 are operatively configured to float at an upper surface 20 of the coolant 22 in the reservoir 14 and to dampen the momentum of the coolant flowing from the engine.
- the plurality of objects 18 may cover a portion (not shown) of the entire upper surface 20 of the coolant 22 disposed within the reservoir 14 or it may cover the entire upper surface 20 of the coolant 22 disposed within the reservoir 14 as shown in FIG. 3 .
- the plurality of objects 18 may come in a variety of shapes such as, but not limited to spheres, octagons, squares, rectangles, pyramids, and the like.
- the plurality of objects 18 are formed from polymeric materials.
- the plurality of objects 18 (which may be spheres, octagons, squares) may be hollow or solid. It is to be understood that it may be more cost effective and lighter weight to have hollow instead of solid objects 18 .
- FIG. 4A a cross sectional view of the first embodiment of the present disclosure is shown where the plurality of objects 18 form multiple layers 24 , 26 , 28 near the surface 20 of the coolant 22 which is disposed within the reservoir 14 . It is to be understood that a first layer 24 of the plurality of objects 18 may be disposed below the surface 20 of the coolant 22 . A second layer 26 may be disposed at the surface 20 of the coolant 22 and a third layer 28 of objects 18 may be disposed above the surface 20 of the coolant 22 as shown.
- Each of the objects 18 may be solid, or perforated or both solid and perforated. Referring to FIGS. 4B and 4C , the perforations 30 in the objects 18 increase the surface area of the fluid 32 which would be exposed to air. The exposure of the surface area of the fluid to air causes a straining effect for the water. It is also to be understood that the flow of coolant 12 may pass through the perforations as well as shown in FIG. 4D .
- the surge tank 10 includes a reservoir 14 wherein the reservoir 14 defines a coolant receiving inlet 16 which is coupled to an engine (not shown).
- the coolant receiving inlet 16 receives a flow of coolant 12 from the engine.
- the surge tank 10 further includes a reservoir outlet 19 through which the flow of coolant 12 is returned to the engine.
- the surge tank 10 further includes a baffle (or grating) 32 and a plurality of objects 18 .
- the baffle (or grating) 32 may be affixed to the internal surface of the reservoir 14 or may be integral to the reservoir 14 .
- the baffle (or grating) 32 forces the plurality of objects 18 to remain in the upper portion 34 of the surge tank 10 even when the surge tank 10 is inclined or agitated as shown in FIGS. 5B and 5C respectively. Therefore, as fluid flows from the coolant receiving inlet 16 , there will always be a plurality of objects 18 to dampen the flow of coolant 12 before or as it comes into contact with the coolant 22 that is disposed within the reservoir 14 .
- FIG. 5B shows the second embodiment of the present disclosure in an inclined position. As shown, the surface 20 of the coolant remains horizontal. The plurality of objects 18 remains in the upper portion 34 of the reservoir 14 due to the baffle (or grating) 32 .
- FIG. 5C shows the second embodiment of the present disclosure where the reservoir is agitated. Again, the plurality of objects 18 remains in the upper portion 34 of the reservoir 14 due to the baffle (or grating) 32 despite the movement of the reservoir 14 and the flow of coolant 12 will always be dampened under this condition.
- the plurality of objects 18 are disposed within the coolant reservoir 14 in an upper portion 34 of the surge tank 10 and are operatively configured to float at an upper surface 20 of the coolant 22 in the reservoir 14 .
- the plurality of objects 18 in conjunction with the baffle 32 are operatively configured to dampen the momentum of the flow of coolant 12 from the engine. Accordingly, air in the form of air bubbles is minimized within the coolant due to the dampened momentum in the flow of coolant 12 from the engine and the dispersing of the air bubbles that are in the coolant.
- the plurality of objects 18 may be either hollow or solid or semi-sold (perforated) as described above.
- the plurality of objects 18 may also be formed from a polymeric material or the like.
- Each object 18 may have a diameter of about 0.5 inches. However, it is to be understood that the diameter may vary depending on the configuration of the surge tank 10 . It is also to be understood that the plurality of objects 18 cover at least a substantial amount of the upper surface 20 of the coolant 22 in the reservoir 14 . The entire upper surface 20 of the coolant 22 in the reservoir 14 may be covered by the plurality of objects 18 or a substantial portion of the coolant 22 in the reservoir 14 may be covered.
- air bubbles are dispersed due to the plurality of objects.
- the incoming flow of coolant 12 which enters the reservoir 14 merely needs to be dampened by engaging with the plurality of objects 18 .
- the air bubbles 36 are dispersed and move up to the surface of the coolant as the air bubbles engage with the plurality of objects 18 .
- a thin liquid film ( 38 in FIG. 6 ) forms over and around the objects 18 which makes a shorter travel distance for air bubbles 36 to rise up to be exposed to air and to break up.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Air-Conditioning For Vehicles (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Body Structure For Vehicles (AREA)
Abstract
A surge tank includes a reservoir wherein the reservoir defines a coolant receiving inlet for coupling to the engine. The reservoir further defines a reservoir outlet through which the flow of coolant is returned to the engine. The coolant receiving inlet receives a flow of coolant from the engine. The surge tank further includes a plurality of objects disposed within the coolant reservoir. The plurality of objects are operatively configured to float at an upper surface of the coolant in the reservoir and to dampen the momentum of the coolant flowing from the engine.
Description
- The present disclosure relates generally to surge tanks for use in vehicles, including surge tanks that receive coolant, deaerates the coolant, and returns the deaerated coolant to the system.
- In a known cooling system for an internal combustion engine, a cooling water reservoir tank is provided and is used not only for storing an overflow of cooling water but also for ensuring a recirculation of a part of the cooling water to the reservoir tank, to thereby separate and remove air and vapor from the cooling water in the reservoir tank, to thereby separate and remove air and vapor from the cooling water in the reservoir tank, whereby the cooling efficiency of the cooling system is increased.
- In this type of cooling system, in general, an independent cooling water passageway connects the reservoir tank to an engine body and a radiator, and the reservoir tank is provided with a cap equipped with a relief valve which allows air or vapor held in an upper portion of the reservoir tank to be discharged to the atmosphere, when the pressure inside the reservoir tank exceeds a predetermined value, and thus prevents an excessive increase of the pressure in the cooling system. This operation also allows air to be quickly separated from the cooling water: this air is entrained in the cooling system when the cooling water is supplemented, and remains in the cooling system. The separated air is discharged by the relief valve in the reservoir tank, and thus, the cooling efficiency of the system is enhanced.
- When the engine is stopped just after a high load operation, the circulation of the cooling water is stopped, and accordingly, the temperature of the cooling water becomes very high, which causes a large amount of the cooling water to be vaporized and this vapor collects in the upper portion of the cooling system (i.e. a hot soak).
- Referring now to
FIG. 1 , a schematic diagram of a simplified example of a vehicle (not shown) having asurge tank 110 for de-aerating coolant is illustrated. InFIG. 1 , the vehicle comprises anengine 112 and aradiator 114 through which coolant is circulated, at least at selected times, to cool the coolant for use in removing heat from theengine 112. Other components may also be cooled by the coolant such as atransmission 116 and an exhaust gas recirculation cooler (e.g. EGR cooler) not shown in this figure. The coolant may also be used to provide energy to or remove energy from an HVAC—heating ventilation and air conditioning—system (not shown) of the vehicle. - One specific example of a vehicle is a truck, such as a heavy duty or medium duty truck (not shown) used in long hauling operations or a truck tractor used for such purposes. Land vehicles are particularly desirable applications in which surge tanks would be used. In
FIG. 1 , segments of the coolant recirculation conduits are indicated by the 118, 120, 122. In the example ofnumbers FIG. 1 , aerated coolant from theengine 112 passes via aconduit 118 to aninlet 124 to asurge tank 110. In addition, aerated coolant passes through aconduit 120 fromradiator 114 to aninlet 126 to thesurge tank 110, which may separate from or in common with theinlet 126 that receive aerated fluid fromconduit 24. Air is removed from the coolant as it passes through thesurge tank 26. The deaerated coolant is returned to theengine 112 via aconduit 122 inFIG. 1 . - There are a number of reasons for de-aerating coolant. For example, poor de-aeration of coolant can result in cavitation of an engine water pump, pitting of engine liners, engine overheating, cab HVAC system failures, EGR cooler erosion, and other drawbacks. For example, modern truck engines have relatively high fluid flow rates to a surge tank, such as in excess of four gallons per minute. As a result, it becomes more difficult to de-aerate the coolant. In addition, high fluid flow rates into a surge tank can result in fracturing air bubbles into microbubbles (e.g., pin sized bubbles) which are even more difficult to remove from the coolant.
- It is known to make surge tanks out of plastic for weight and cost saving purposes. However, because of the high temperatures often reached by coolant, plastic can tend to soften when used. As a result, plastic surge tanks are typically provided with reinforcing
baffles 128 as shown inFIGS. 2A , 2B, and 2C. However, high coolant flow rates into surge tanks withbaffles 128 increases the foaming (formation of small bubbles) when the entering liquid impacts thebaffles 128. Also, because extremely small bubbles entrained in fluid are difficult to separate, bubbles formed from fracturing larger bubbles are more easily carried through asurge tank 110, resulting in poorer de-aeration of the coolant. To reduce the possibility of small foam formed bubbles entering the fluid and being carried through asurge tank 110, some engine manufacturers have issued specifications for 124, 126 of afluid inlets surge tank 110 so that foam can escape into an air gap above the fluid level. - A need exists for an improved surge tank which is operatively configured to reduce or minimize air bubbles from recirculating through the engine cooling system.
- A surge tank is provided according to the embodiment(s) disclosed herein. The surge tank includes a reservoir wherein the reservoir defines a coolant receiving inlet for coupling to the engine. The reservoir also defines a reservoir outlet. The coolant receiving inlet receives a flow of coolant from the engine. The reservoir outlet is the outlet through which the flow of coolant is returned to the engine. The surge tank further includes a plurality of objects disposed within the coolant reservoir. The plurality of objects are operatively configured to float at an upper surface of the coolant in the reservoir and to dampen the momentum of the coolant flowing from the engine.
- Features and advantages of embodiments of the present disclosure will become apparent by reference to the following detailed description and drawings, in which like reference numerals correspond to similar, though perhaps not identical, components. For the sake of brevity, reference numerals or features having a previously described function may or may not be described in connection with other drawings in which they appear.
-
FIG. 1 is a simplified diagram of one example of a vehicle system incorporating a surge tank. -
FIG. 2A is a perspective, partial view of a prior art surge tank. -
FIG. 2B is a perspective, partial view of a prior art surge tank where the baffles are shown disposed within the tank. -
FIG. 2C is a perspective view of one embodiment of a surge tank of the present disclosure. -
FIG. 3 is a perspective view of one embodiment of a surge tank of the present disclosure. -
FIG. 4A is a cross-sectional view of an embodiment of a surge tank of the present disclosure. -
FIG. 4B is an enlarged view of a perforated object. -
FIG. 4C is an enlarged schematic view of the coolant interacting with the perforations in an object where an increased surface area of the fluid is exposed to air (i.e. straining effect for water). -
FIG. 4D is an enlarged schematic view of the coolant flowing through a hole in the object. -
FIG. 5A is a cross sectional view of a second embodiment of a surge tank of the present disclosure where a baffle maintains the plurality of objects in area of the surge tank. -
FIG. 5B is a cross sectional view of the second embodiment of a surge tank when the tank is in an inclined position. -
FIG. 5C is a cross sectional view of the second embodiment of a surge tank when the tank is agitated. -
FIG. 6 is an enlarged, cross-sectional view of the second embodiment of a surge tank when the incoming flow of coolant is dampened by the plurality of objects. - A surge tank 10 of the present disclosure provides improved dampening to an incoming flow of
coolant 12. Referring now toFIG. 3 , one embodiment of the present disclosure includes a reservoir wherein thereservoir 14 defines acoolant receiving inlet 16 for coupling to the engine. Thecoolant receiving inlet 16 receives a flow ofcoolant 12 from the engine (shown as 112 inFIG. 1 ) and areservoir outlet 19 through which the flow ofcoolant 12 is returned to the engine. - The surge tank 10 further includes a plurality of
objects 18 disposed within thecoolant reservoir 14. The plurality ofobjects 18 are operatively configured to float at anupper surface 20 of thecoolant 22 in thereservoir 14 and to dampen the momentum of the coolant flowing from the engine. The plurality ofobjects 18 may cover a portion (not shown) of the entireupper surface 20 of thecoolant 22 disposed within thereservoir 14 or it may cover the entireupper surface 20 of thecoolant 22 disposed within thereservoir 14 as shown inFIG. 3 . - The plurality of
objects 18 may come in a variety of shapes such as, but not limited to spheres, octagons, squares, rectangles, pyramids, and the like. The plurality ofobjects 18 are formed from polymeric materials. The plurality of objects 18 (which may be spheres, octagons, squares) may be hollow or solid. It is to be understood that it may be more cost effective and lighter weight to have hollow instead ofsolid objects 18. - Referring now to
FIG. 4A , a cross sectional view of the first embodiment of the present disclosure is shown where the plurality ofobjects 18 form 24, 26, 28 near themultiple layers surface 20 of thecoolant 22 which is disposed within thereservoir 14. It is to be understood that afirst layer 24 of the plurality ofobjects 18 may be disposed below thesurface 20 of thecoolant 22. Asecond layer 26 may be disposed at thesurface 20 of thecoolant 22 and athird layer 28 ofobjects 18 may be disposed above thesurface 20 of thecoolant 22 as shown. - Each of the
objects 18 may be solid, or perforated or both solid and perforated. Referring toFIGS. 4B and 4C , theperforations 30 in theobjects 18 increase the surface area of the fluid 32 which would be exposed to air. The exposure of the surface area of the fluid to air causes a straining effect for the water. It is also to be understood that the flow ofcoolant 12 may pass through the perforations as well as shown inFIG. 4D . - Referring now to
FIG. 5A-5C , another embodiment of a surge tank 10 of the present disclosure is shown. The surge tank 10 includes areservoir 14 wherein thereservoir 14 defines acoolant receiving inlet 16 which is coupled to an engine (not shown). Thecoolant receiving inlet 16 receives a flow ofcoolant 12 from the engine. The surge tank 10 further includes areservoir outlet 19 through which the flow ofcoolant 12 is returned to the engine. The surge tank 10 further includes a baffle (or grating) 32 and a plurality ofobjects 18. The baffle (or grating) 32 may be affixed to the internal surface of thereservoir 14 or may be integral to thereservoir 14. The baffle (or grating) 32 forces the plurality ofobjects 18 to remain in theupper portion 34 of the surge tank 10 even when the surge tank 10 is inclined or agitated as shown inFIGS. 5B and 5C respectively. Therefore, as fluid flows from thecoolant receiving inlet 16, there will always be a plurality ofobjects 18 to dampen the flow ofcoolant 12 before or as it comes into contact with thecoolant 22 that is disposed within thereservoir 14. -
FIG. 5B shows the second embodiment of the present disclosure in an inclined position. As shown, thesurface 20 of the coolant remains horizontal. The plurality ofobjects 18 remains in theupper portion 34 of thereservoir 14 due to the baffle (or grating) 32.FIG. 5C shows the second embodiment of the present disclosure where the reservoir is agitated. Again, the plurality ofobjects 18 remains in theupper portion 34 of thereservoir 14 due to the baffle (or grating) 32 despite the movement of thereservoir 14 and the flow ofcoolant 12 will always be dampened under this condition. - As indicated, the plurality of
objects 18 are disposed within thecoolant reservoir 14 in anupper portion 34 of the surge tank 10 and are operatively configured to float at anupper surface 20 of thecoolant 22 in thereservoir 14. The plurality ofobjects 18 in conjunction with thebaffle 32 are operatively configured to dampen the momentum of the flow ofcoolant 12 from the engine. Accordingly, air in the form of air bubbles is minimized within the coolant due to the dampened momentum in the flow ofcoolant 12 from the engine and the dispersing of the air bubbles that are in the coolant. - Similar to the first embodiment, it is to be understood that the plurality of
objects 18 may be either hollow or solid or semi-sold (perforated) as described above. The plurality ofobjects 18 may also be formed from a polymeric material or the like. - Each
object 18 may have a diameter of about 0.5 inches. However, it is to be understood that the diameter may vary depending on the configuration of the surge tank 10. It is also to be understood that the plurality ofobjects 18 cover at least a substantial amount of theupper surface 20 of thecoolant 22 in thereservoir 14. The entireupper surface 20 of thecoolant 22 in thereservoir 14 may be covered by the plurality ofobjects 18 or a substantial portion of thecoolant 22 in thereservoir 14 may be covered. - Referring now to
FIG. 6 , air bubbles are dispersed due to the plurality of objects. The incoming flow ofcoolant 12 which enters thereservoir 14 merely needs to be dampened by engaging with the plurality ofobjects 18. As shown, the air bubbles 36 are dispersed and move up to the surface of the coolant as the air bubbles engage with the plurality ofobjects 18. A thin liquid film (38 inFIG. 6 ) forms over and around theobjects 18 which makes a shorter travel distance for air bubbles 36 to rise up to be exposed to air and to break up.
Claims (12)
1. A surge tank comprising:
a reservoir including a coolant receiving inlet for coupling to the engine to receive a flow of coolant from the engine and a reservoir outlet through which the flow of coolant is returned to the engine; and
a plurality of objects disposed within the coolant reservoir, the plurality of objects operatively configured to float at an upper surface of the coolant in the reservoir and to dampen the momentum of the coolant flowing from the engine.
2. The surge tank, as defined in claim 1 , wherein the plurality of objects are balls.
3. The surge tank, as defined in claim 1 , wherein the plurality of objects are formed from a polymeric material.
4. The surge tank, as defined in claim 2 , wherein the balls are hollow.
5. The surge tank, as defined in claim 1 , wherein the plurality of objects are solid.
6. A surge tank comprising:
a reservoir including a coolant receiving inlet for coupling to the engine to receive a flow of coolant from the engine and a reservoir outlet through which the flow of coolant is returned to the engine;
a baffle; and
a plurality of objects disposed within the coolant reservoir, the plurality of objects operatively configured to float at an upper surface of the coolant in the reservoir and to dampen the momentum of the coolant flowing from the engine.
7. The surge tank, as defined in claim 6 , wherein the plurality of objects are hollow.
8. The surge tank, as defined in claim 6 , wherein the plurality of objects are formed from a polymeric material.
9. The surge tank, as defined in claim 7 , wherein the plurality of objects have a diameter of about 0.5 inches.
10. The surge tank, as defined in claim 6 , wherein the plurality of objects form multiple layers near the upper surface of the coolant in the reservoir.
11. The surge tank, as defined in claim 6 wherein the baffle spans the internal width of the reservoir.
12. The surge tank, as defined in claim 6 , wherein the baffle is a grate.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/US2010/026518 WO2011112175A1 (en) | 2010-03-08 | 2010-03-08 | Surge tank |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20120325823A1 true US20120325823A1 (en) | 2012-12-27 |
Family
ID=44563748
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US13/583,075 Abandoned US20120325823A1 (en) | 2010-03-08 | 2010-03-08 | Surge Tank |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US20120325823A1 (en) |
| CN (1) | CN102791984A (en) |
| AU (1) | AU2010347751A1 (en) |
| BR (1) | BR112012022635A2 (en) |
| DE (1) | DE112010005371T5 (en) |
| MX (1) | MX2012009999A (en) |
| SE (1) | SE1251139A1 (en) |
| WO (1) | WO2011112175A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2022149428A (en) * | 2021-03-25 | 2022-10-06 | 株式会社Subaru | Reserve tank |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102013019494A1 (en) | 2013-11-19 | 2015-05-21 | Daimler Ag | Cooling device for cooling a drive unit, in particular an internal combustion engine, a motor vehicle |
| EP4459111A1 (en) * | 2023-05-03 | 2024-11-06 | Volvo Car Corporation | Thermal management system for a vehicle, vehicle comprising a thermal management system, use of a thermal management system, method for controlling a thermal management system and computer program element |
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| US5111776A (en) * | 1989-09-26 | 1992-05-12 | Nippon Soken, Inc. | Cooling system for an internal combustion engine |
| US20090078705A1 (en) * | 2007-09-21 | 2009-03-26 | Ramsay Thomas N | Floating Absorber Assembly for Reduced Fuel Slosh Noise |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2273505A (en) * | 1942-02-17 | Container | ||
| US2809656A (en) * | 1955-12-07 | 1957-10-15 | Dan Kamphausen | Toilet flush tank assembly |
| US5052224A (en) * | 1990-10-15 | 1991-10-01 | Betz Laboratories, Inc. | Shielded sight gauge for storage tanks |
| US5067561A (en) * | 1990-11-30 | 1991-11-26 | General Motors Corporation | Radiator tank oil cooler |
| US5970928A (en) * | 1998-10-28 | 1999-10-26 | Navistar International Transportation Corp | Self restricting engine cooling system deaeration line |
| JP2001276506A (en) * | 2000-03-30 | 2001-10-09 | Ishikawajima Harima Heavy Ind Co Ltd | Method for suppressing bubble generation in gas absorption tower and device therefor |
| KR100571223B1 (en) * | 2003-09-26 | 2006-04-13 | 현대자동차주식회사 | Coolant Surge Tank Structure for Commercial Vehicle |
| JP2007277610A (en) * | 2006-04-04 | 2007-10-25 | Nippon Paint Co Ltd | Cleaning method and cleaning system for workpieces in electrodeposition coating |
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2010
- 2010-03-08 WO PCT/US2010/026518 patent/WO2011112175A1/en not_active Ceased
- 2010-03-08 SE SE1251139A patent/SE1251139A1/en not_active Application Discontinuation
- 2010-03-08 US US13/583,075 patent/US20120325823A1/en not_active Abandoned
- 2010-03-08 AU AU2010347751A patent/AU2010347751A1/en not_active Abandoned
- 2010-03-08 MX MX2012009999A patent/MX2012009999A/en not_active Application Discontinuation
- 2010-03-08 BR BR112012022635A patent/BR112012022635A2/en not_active IP Right Cessation
- 2010-03-08 DE DE112010005371T patent/DE112010005371T5/en not_active Withdrawn
- 2010-03-08 CN CN2010800652240A patent/CN102791984A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5111776A (en) * | 1989-09-26 | 1992-05-12 | Nippon Soken, Inc. | Cooling system for an internal combustion engine |
| US20090078705A1 (en) * | 2007-09-21 | 2009-03-26 | Ramsay Thomas N | Floating Absorber Assembly for Reduced Fuel Slosh Noise |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2022149428A (en) * | 2021-03-25 | 2022-10-06 | 株式会社Subaru | Reserve tank |
| JP7633059B2 (en) | 2021-03-25 | 2025-02-19 | 株式会社Subaru | Reserve tank |
Also Published As
| Publication number | Publication date |
|---|---|
| BR112012022635A2 (en) | 2017-10-17 |
| DE112010005371T5 (en) | 2012-12-27 |
| CN102791984A (en) | 2012-11-21 |
| AU2010347751A1 (en) | 2012-09-13 |
| SE1251139A1 (en) | 2012-10-15 |
| MX2012009999A (en) | 2012-10-01 |
| WO2011112175A1 (en) | 2011-09-15 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:JUAN, TAIUNG;REEL/FRAME:028906/0945 Effective date: 20091223 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |