GB2504470A - Separator - Google Patents

Separator Download PDF

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Publication number
GB2504470A
GB2504470A GB201213377A GB201213377A GB2504470A GB 2504470 A GB2504470 A GB 2504470A GB 201213377 A GB201213377 A GB 201213377A GB 201213377 A GB201213377 A GB 201213377A GB 2504470 A GB2504470 A GB 2504470A
Authority
GB
United Kingdom
Prior art keywords
separator
hollow body
gas
coolant
conduit
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
GB201213377A
Other versions
GB201213377D0 (en
GB2504470B (en
Inventor
Vivian Page
Ian Nolan
Stuart Wagstaff
Jean-Yves Tillier
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 GB1420563.7A priority Critical patent/GB2517103B/en
Priority to GB201213377A priority patent/GB2504470B/en
Publication of GB201213377D0 publication Critical patent/GB201213377D0/en
Priority to PCT/GB2013/051704 priority patent/WO2014016554A1/en
Priority to CN201390000606.4U priority patent/CN204436567U/en
Publication of GB2504470A publication Critical patent/GB2504470A/en
Application granted granted Critical
Publication of GB2504470B publication Critical patent/GB2504470B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D19/00Degasification of liquids
    • B01D19/0042Degasification of liquids modifying the liquid flow
    • B01D19/0052Degasification of liquids modifying the liquid flow in rotating vessels, vessels containing movable parts or in which centrifugal movement is caused
    • B01D19/0057Degasification of liquids modifying the liquid flow in rotating vessels, vessels containing movable parts or in which centrifugal movement is caused the centrifugal movement being caused by a vortex, e.g. using a cyclone, or by a tangential inlet
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D19/00Degasification of liquids
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D19/00Degasification of liquids
    • B01D19/0042Degasification of liquids modifying the liquid flow
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D19/00Degasification of liquids
    • B01D19/0042Degasification of liquids modifying the liquid flow
    • B01D19/0052Degasification of liquids modifying the liquid flow in rotating vessels, vessels containing movable parts or in which centrifugal movement is caused
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D19/00Degasification of liquids
    • B01D19/0073Degasification of liquids by a method not covered by groups B01D19/0005 - B01D19/0042
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D19/00Degasification of liquids
    • B01D19/0073Degasification of liquids by a method not covered by groups B01D19/0005 - B01D19/0042
    • B01D19/0094Degasification of liquids by a method not covered by groups B01D19/0005 - B01D19/0042 by using a vortex, cavitation
    • 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
    • F01P11/02Liquid-coolant filling, overflow, venting, or draining devices
    • F01P11/028Deaeration devices

Abstract

A separator 122 for separating gas and liquid in a coolant, the separator comprises a hollow body 124 having a first end 302 and a second end 304. An inlet 126 is arranged towards the first end and a liquid outlet 130 arranged towards the second end. The separator includes a gas outlet 128 and a conduit 402 mounted in the hollow body and defining a gas flow path at least partway between the first end and the second end. In use a coolant such as distilled water or mixtures of water, antifreeze and additives may enter the inlet and adopt cyclonic flow from the first end to the second end and any gas such as air present in the fluid is separated and may enter the conduit before exiting the separator via the gas outlet. The gas free liquid may exit the separator via the liquid outlet. The separator may be included in a cooling system for an engine such as diesel or gasoline fuelled engines.

Description

Description
COOLANT SEPARATOR
Technical Field
10001] The present disclosure relates to a cooling system for an engine, and more particularly to a separator for separating gas and liquid in a coolant used in the cooling system.
Background
100021 Coolant flowing in a cooling systcm for an enginc can become aerated. The aerated coolant may cause a reduction in the efficiency of a pump, contributing to an overall reduction in the coolant flow in the cooling system.
The reduced coolant flow may in turn result in inadequate cooling of various components present in the system. If unchecked, deterioration in performance of the pump may lead to thermal issues especially in an engine head or other heat exchanger elements present in the system.
100031 Typically, high performance engines make use of swirl pots to separate air bubbles present in the coolant. Commercial engincs use shunt tanks or radiator hcadcr tanks to provide an arca of low coolant flow for thc dc-aeration of the coolant. However, these solutions are generally ineffective at separating relatively small air bubbles, which have a tendency to be easily re-entrained into the coolant. Also, these solutions take up considerable space, which may not be available on some machines.
10004] For example, U.S. Published Application No. 2009/0134175 relates to a fuel tank that is made of a plastic material. The fuel tank includes, but is not limited to, an outer tank and a swirl pot arranged in the interior thereof. The edge of the swirl pot and the opcning of the fuel tank are connected positively.
Summary of the Disclosure
10005] The present disclosure provides a separator for separating gas and liquid in a coolant, the separator comprising a hollow body having a first end and a second end; an inlet arranged towards the first end; a gas outlet; a liquid outlet arranged towards the second end; and a conduit mounted in the hollow body and defining a gas flow path at least partway between the first end and the second end.
100061 Other features and aspects of this disclosure will be apparent from the following description and the accompanying figures.
Brief Description of the FiEzures
10007] Figure 1 is a schematic view of a cooling system for an engine, including a separator, according to one embodiment of the present disclosure; 100081 Figure 2 is a schematic view of another cooling system including the separator; 10009] Figure 3 is a perspective view of the separator; 10010] Figure 4 is a cross-sectional view of the separator shown in Figure 3; and 10011] Figure 5 is another cross-sectional view of the separator shown in Figure 3.
Detailed Description
10012] Wherever possible, the same reference numbers will be used throughout the figures to refer to the same or like parts. Figures 1 and 2 illustrate exemplary cooling systems 100, 200 respectively for an engine 102 according to various embodiments of the present disclosure. In one embodiment, the engine 102 may include for example, a diesel engine, a gasoline engine, a gaseous fuel powered engine such as a natural gas engine, a combination of known sources of power or any other type of power source apparent to one of skill in the art. Further, as shown in those figures, the engine 102 may include an engine head 104 and an engine block 106.
10013] A heat exchanger or a radiator 108 may be fluidly connected to the engine 102, in order to dissipate heat from a coolant leaving the engine 102. A person of ordinary skill in the art will appreciate that any suitable coolant known in the art may be used, for example the coolant may include distilled water or a mixture of water, antifreeze and other additives. A first passageway 110 may supply a coolant flow from the engine head 104 to an inlet of the radiator 108.
Further, a second passageway 112 may be connected to an outlet of the radiator 108 to permit flow of the coolant away from the radiator 108.
100141 A thermostat controlled valve 114 may be disposed in the first passageway 110. The thermostat controlled valve 114 may control thc coolant flow into the radiator 108. One of ordinary skill in the art will appreciate that the thermostat controlled valve 114 may be configured to re-circulate the coolant flow through a bypass circuit until a temperature of thc coolant reaches a pre-determined threshold. On reaching the pre-determined threshold, the coolant flow may be routed towards the radiator 108. It should be noted that the placement of the thermostat controlled valve 114 depicted in the accompanying figures illustrates an outlet controlled cooling system. An inlet controlled cooling system, wherein the thermostat controlled valve 114 may be placed within the second passageway 112 also lies within the scope of this disclosure.
100151 As shown in Figures 1 and 2, a pump 116 may be disposed in the second passageway 112. The pump 116 is fluidly connected to the engine block 106 in order to circulate the coolant within the engine 102. The pump 116 may include a fixed displacement or variable displacement pump known in the art.
Further, an expansion tank 118 may be fluidly connectcd to the radiator 108 via a third passageway 120. The expansion tank 118 may providc volume for the thermal expansion of the coolant. The expansion tank 118 may also serve as a coolant reservoir to ensure the presence of coolant despite evaporative losses over time.
100161 The coolant flowing in the cooling system 100, 200 may contain gas in the form of air bubbles. In the present disclosure, as shown in Figures 1 and 2, a separator 122 may be provided in the cooling systems 100, 200, for separating the gas and liquid in the coolant. Figures 1 and 2 illustrate different locations in the cooling systems 100, 200 where the separator 122 may be disposed. The separator 122 may include a hollow body 124. The separator 122 may also include an inlet 126, a gas outlet 128 and a liquid outlet 130 to connect the separator 122 to various components in the cooling systems 100, 200. In one embodiment, the separator 122 may be made of metal or any other suitable material. The detailed structure of the separator 122 will be explained in connection with Figure 3.
100171 Referring to Figure 1, in one embodiment, the separator 122 may be disposed in the first passageway 110, more specifically between the radiator 108 and the thermostat controlled valve 114. It should be noted that in this arrangement, the separator 122 is disposed in series with respect to the radiator 108 of the cooling system 100. As shown, the inlet 126 of the separator 122 may be fluidly connected to the thermostat controlled valve 114. Further, the liquid outlet 130 of the separator 122 may be fluidly connected to the inlet of the radiator 108. In this case, the gas outlet 128 of the separator 122 may be connected to the expansion tank 118 via a communication line 132.
10018] In another embodiment, as shown in Figure 2, the separator 122 may be positioned in parallel with respect to the radiator 108. In this case, the separator 122 may be disposed in the bypass branch 202, more specifically between the thermostat controlled valve 114 and the pump 116. The inlet 126 of the separator 122 may be connected to a fluid junction downstream of the thermostat controlled valve 114 and the liquid outlet 130 of the separator 122 may be connected to a fluid junction upstream of the thermostat controlled valve 114. Further, the gas outlet 128 of the separator 122 may be connected to the expansion tank 118 via the communication line 132. In yet another embodiment, the separator 122 may be disposed in both the first passageway 110 as well as in the bypass branch 202.
100191 Moreover, it should be understood that parameters related to the separator 122 such as size of the inlet 126, the liquid outlet 130 and the gas outlet 128, length of the hollow body 124, material used, and the like, may vary depending on the application. For example, the separator 122 used in the cooling system 200 may have a relatively shorter hollow body 124 than that used in the cooling system 100. This may be because a smaller portion of the coolant flows through the separator 122 located in the bypass branch 202 as against a full flow arrangement provided in the cooling system 100. A person of ordinary skill in the art will appreciate that the positioning of the separator 122 depicted in the accompanying figures is merely exemplary and may vary without any limitation.
100201 Figure 3 illustrates an exploded view of the separator 122. The separator 122 may include the hollow body 124 having a first end 302 and a second end 304. The hollow body 124 may be generally cylindrical so as to define a longitudinal axis AA. Further, the inlet 126 of the separator 122 maybe arranged towards the first end 302 of the hollow body 124. In one embodiment, the inlet 126 may have a substantially rectangular cross section. The inlet 126 may be configured to receive at least a portion of the coolant flowing through the cooling systems 100, 200. As shown in the accompanying figures, the inlet 126 may be located substantially tangentially to the hollow body 124. Also, the gas outlet 128 may be located towards the first end 302 of the hollow body 124. It should be noted that the gas outlet 128 may alternatively be located towards a rear middle portion of the hollow body 124. In one embodiment, the gas outlet 128 may include an opening 306 provided at the first end 302 of the separator 122.
100211 The gas outlet 128 may be provided substantially coaxially to the hollow body 124, along the longitudinal axis AA. Further, the liquid outlet 130 of the separator 122 may be arranged towards the second end 304 of the hollow body 124. As shown in the accompanying figures, the liquid outlet 130 may be arranged laterally with respect to the longitudinal axis AA of the hollow body 124. In an embodiment, based on the application, the liquid outlet 130 may be arranged substantially axially or parallel to the longitudinal axis AA of the hollow body 124. Moreover, the hollow body 124 may define an hour glass chamber such that there is a reduction in throat diameter partway along the length of the hollow body 124.
100221 Figures 4 and S depict different cross sectional views of the separator 122, according to an embodiment of the present disclosure. As shown, the separator 122 may include a conduit 402 mounted in the hollow body 124. The conduit 402 may define a gas flow path at least partway between the first end 302 and the second end 304 of the hollow body 124. In one embodiment, the conduit 402 may include an outlet end 404 proximal to the gas outlet 128 and an inlet end 406 distal to the gas outlet 128. Moreover, the conduit 402 may have a hollow cylindrical shape or a hollow conical shape. Figures 4 and 5 depict two different variations of mounting the conduit 402 in the hollow body 124.
100231 Referring to Figure 4, a plurality of ribs 408 extending radially from an inner surface of the hollow body 124 may be used to mount the conduit 402 in the hollow body 124. The plurality of ribs 408 may be provided proximal to the first end 302 of the hollow body 124, such that the conduit 402 extends into the gas outlet 128. Alternatively, as shown in Figure 5, the outlet end 404 of the conduit 402 may be integral with the first end 302 of the hollow body 124. In this arrangement, the conduit 402 may be integral with the gas outlet 128 of the hollow body 124. A person of ordinary skill in the art will appreciate that the variations of mounting the conduit 402 described herein are merely exemplary and do not limit the scope of this disclosure. Moreover, in one embodiment, a plurality of perforations in the form of holes or slots (not shown in figures) may be provided on the conduit 402.
100241 The present disclosure relates to providing an effective design for the separation of the relatively small air bubbles, having a diameter of approximately microns and above, from the coolant flowing through the separator 122. The conduit 402 is configured to provide the gas flow path for the separated air bubbles to rise under the influence of the buoyancy forces and pass out of the separator 122 via the gas outlet 128. A person of ordinary skill in the art will appreciate that the separator 122 may be easily installed into standard cooling systems 100, 200. In some cases, the separator 122 may be used as a replacement for the shunt tank in the system.
md ustrial App lie ability 100251 The working of the separator 122 will now be described in detail.
During operation, at least a portion of the coolant may be received by the inlet 126. Due to the substantially tangential positioning of the inlet 126 with respect to the hollow body 124, the coolant flow may adopt a cyelonic or swirl flow from the first end 302 towards the second end 304 of the hollow body 124. It should be understood that typically, the velocity of the swirl flow of the coolant within the hollow body 124 may be relatively high in the core of the separator 122.
100261 The conduit 402 mounted within the hollow body 124 may be configured to generate a low yelocity region in the core of the separator 122 to facilitate the separation of thc gas and liquid in the coolant. It should be notcd that the liquid present in the coolant flow is comparatively heavier and may be urged outwardly in the swirl flow. Also, the liquid may fall downwardly towards the second end 304, due to the effect of gravity and the centrifugal force generated within the hollow body 124. Whereas, the gas may be present inwardly of the swirl flow and may collect in the form of air bubbles at the inlet cnd 406 of the conduit 402. This may result in the separation of thc gas and liquid in the coolant. In an embodiment, the separated gas may enter the separator 122 via the plurality of perforations provided along at least a portion of a length of the conduit 402. The air bubbles may then rise within the gas flow path towards the outlet end 404 of the conduit 402 under effect of buoyancy forces.
10027] Thereafter, the separated gas may exit the separator 122 via the gas outlet 128 which is connected to the conduit 402. The separated gas may then enter the expansion tank 118 via the communication line 132 which extends from the gas outlet 128 of thc scparator 122. Morcover, the separated liquid may cxit the separator 122 via the liquid outlet 130. The separated liquid may cnter the radiator 108 in the cooling system 100 or the pump 116 in the cooling system 200.
100281 Onc of ordinary skill in thc art will appreciatc that thc conduit 402 may promote better swirling characteristics in a flow field within the separator 122, thereby leading to improved separation efficiency. Moreover, the centrifugal force generated within the separator 122 may be directly proportional to the velocity of the coolant flowing within the separator 122 and inversely proportional to a radius of the hollow body 124. Thus, a rectangular shaped inlet 126, as shown in the accompanying figures, may provide a reduction in flow area of the inlet 126 and thereby cause an increase in the velocity of the coolant flow into the separator 122. Also, the reduction in the throat radius of the hollow body 124 may facilitate higher levels of swirl and therefore provide improved separation efficiency.
100291 Although the embodiments of this disclosure as described herein may be incorporated without departing from the scope of the following claims, it will be apparent to those skilled in the art that various modifications and variations can be made. Other embodiments will be apparent to those skilled in the art from consideration of the specification and practice of the disclosure. It is intended that the specification and cxamplcs be considered as exemplary only, with a true scope being indicated by the following claims and their equivalents.

Claims (13)

  1. Claims What is claimed is: 1. A separator for separating gas and liquid in a coolant, the separator comprising: a hollow body having a first end and a second cnd an inlet arranged towards the first end; a gas outlet; a liquid outlet arranged towards the second end; and a conduit mounted in the hollow body and defining a gas flow path at least partway between the first end and the second end.
  2. 2. The separator of claim I, wherein the conduit includes an outlet end proximal to the gas outlet and an inlet end distal to the gas outlet.
  3. 3. The separator of claim!, wherein the inlet is arranged substantially tangentially to the hollow body.
  4. 4. The separator of claim I, wherein the gas outlet is arranged substantially axially to the hollow body.
  5. 5. The separator of claim 1 further including ribs for mounting the conduit within the hollow body.
  6. 6. The separator of claim I, wherein the conduit is integral with the first end of the hollow body.
  7. 7. The separator of claim 1, wherein the hollow body has a substantially unifomi cmss section.
  8. 8. The separator of claim 1, wherein the hollow body includes a diametrically smaller portion to affect coolant speed.
  9. 9. The separator of claim 1, wherein the conduit is configured to generate a low velocity region in coolant flow for the separation of the gas and the liquid in the coolant.
  10. 10. The separator of claim 9, wherein the gas flow path directs the separated gas towards the gas outlet of the hollow body.
  11. 11. Theseparatorofclaim 1, whereinthe conduitisconflguredtohave a hollow cylindrical shapc or a hollow conical shape.
  12. 12. The separator of claim!, wherein the gas outlet is arranged towards the first end of the hollow body.
  13. 13. The separator of claim 1 further including a plurality of holes pmvided along at least a portion of a length of the conduit.
GB201213377A 2012-07-27 2012-07-27 Coolant separator Expired - Fee Related GB2504470B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB1420563.7A GB2517103B (en) 2012-07-27 2012-07-27 Coolant separator
GB201213377A GB2504470B (en) 2012-07-27 2012-07-27 Coolant separator
PCT/GB2013/051704 WO2014016554A1 (en) 2012-07-27 2013-06-27 Coolant separator
CN201390000606.4U CN204436567U (en) 2012-07-27 2013-06-27 Freezing mixture separator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB201213377A GB2504470B (en) 2012-07-27 2012-07-27 Coolant separator

Publications (3)

Publication Number Publication Date
GB201213377D0 GB201213377D0 (en) 2012-09-12
GB2504470A true GB2504470A (en) 2014-02-05
GB2504470B GB2504470B (en) 2014-12-31

Family

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Family Applications (2)

Application Number Title Priority Date Filing Date
GB1420563.7A Expired - Fee Related GB2517103B (en) 2012-07-27 2012-07-27 Coolant separator
GB201213377A Expired - Fee Related GB2504470B (en) 2012-07-27 2012-07-27 Coolant separator

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB1420563.7A Expired - Fee Related GB2517103B (en) 2012-07-27 2012-07-27 Coolant separator

Country Status (3)

Country Link
CN (1) CN204436567U (en)
GB (2) GB2517103B (en)
WO (1) WO2014016554A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2520680A (en) * 2013-11-27 2015-06-03 Cran Simpson Ltd Fluid processing device
JP2017160821A (en) * 2016-03-08 2017-09-14 マツダ株式会社 Cooling device of engine
DE102020120712A1 (en) 2020-08-05 2022-02-10 Audi Aktiengesellschaft Drive device for a motor vehicle

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106898800B (en) * 2015-12-21 2019-06-18 中国科学院大连化学物理研究所 A kind of minitype radiator and fuel cell system with gas-liquid separating function

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3481118A (en) * 1968-04-22 1969-12-02 Porta Test Mfg Cyclone separator
EP0654292A2 (en) * 1993-07-30 1995-05-24 Mitsubishi Oil Company, Limited Bubble separating apparatus
US5866000A (en) * 1997-11-21 1999-02-02 Yeh; George C. Apparatus for separating dispersed liquid from a continuous fluid
US20070084340A1 (en) * 2003-05-16 2007-04-19 Jianwen Dou Adjustable gas-liquid centrifugal separator and separating method
US20070163442A1 (en) * 2006-01-16 2007-07-19 Toyota Boshoku Kabushiki Kaisha Bubble separator
JP2010269250A (en) * 2009-05-21 2010-12-02 Yuzawa Enterprise:Kk Cyclone-type gas separator

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1283565A (en) * 1960-03-14 1962-02-02 Bird Machine Co Apparatus for separating solid particles and gas bubbles from liquid suspensions
US3163508A (en) * 1960-09-07 1964-12-29 Smith Paper Mills Ltd Howard Method and apparatus for separating gas from liquid rich foams or liquids containing entrained air
FR2086768A5 (en) * 1970-04-08 1971-12-31 Peugeot & Renault
DE4342295A1 (en) * 1993-12-11 1995-06-14 Bayerische Motoren Werke Ag Vaporising cooling system for IC engine
KR100613505B1 (en) * 2004-02-25 2006-08-17 엘지전자 주식회사 Cooling cycle apparatus
JP5102681B2 (en) * 2008-04-02 2012-12-19 日本サーモスタット株式会社 Fluid discharge structure of fluid control device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3481118A (en) * 1968-04-22 1969-12-02 Porta Test Mfg Cyclone separator
EP0654292A2 (en) * 1993-07-30 1995-05-24 Mitsubishi Oil Company, Limited Bubble separating apparatus
US5866000A (en) * 1997-11-21 1999-02-02 Yeh; George C. Apparatus for separating dispersed liquid from a continuous fluid
US20070084340A1 (en) * 2003-05-16 2007-04-19 Jianwen Dou Adjustable gas-liquid centrifugal separator and separating method
US20070163442A1 (en) * 2006-01-16 2007-07-19 Toyota Boshoku Kabushiki Kaisha Bubble separator
JP2010269250A (en) * 2009-05-21 2010-12-02 Yuzawa Enterprise:Kk Cyclone-type gas separator

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2520680A (en) * 2013-11-27 2015-06-03 Cran Simpson Ltd Fluid processing device
GB2520680B (en) * 2013-11-27 2018-07-25 Bisset James A central heating system device
JP2017160821A (en) * 2016-03-08 2017-09-14 マツダ株式会社 Cooling device of engine
DE102020120712A1 (en) 2020-08-05 2022-02-10 Audi Aktiengesellschaft Drive device for a motor vehicle

Also Published As

Publication number Publication date
WO2014016554A1 (en) 2014-01-30
GB201420563D0 (en) 2014-12-31
GB2517103A (en) 2015-02-11
GB201213377D0 (en) 2012-09-12
GB2517103B (en) 2015-04-08
GB2504470B (en) 2014-12-31
CN204436567U (en) 2015-07-01

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 20210727