EP2778592B1 - Heat exchanger assembly having split mini-louvered fins - Google Patents

Heat exchanger assembly having split mini-louvered fins Download PDF

Info

Publication number
EP2778592B1
EP2778592B1 EP14159252.7A EP14159252A EP2778592B1 EP 2778592 B1 EP2778592 B1 EP 2778592B1 EP 14159252 A EP14159252 A EP 14159252A EP 2778592 B1 EP2778592 B1 EP 2778592B1
Authority
EP
European Patent Office
Prior art keywords
mini
louvers
louver
planar portion
heat exchanger
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.)
Not-in-force
Application number
EP14159252.7A
Other languages
German (de)
French (fr)
Other versions
EP2778592A1 (en
Inventor
Prasad S. Kadle
Lawrence P. Scherer
Scott LIPA
Lin-Jie Huang
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.)
Mahle International GmbH
Original Assignee
Mahle International GmbH
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 Mahle International GmbH filed Critical Mahle International GmbH
Publication of EP2778592A1 publication Critical patent/EP2778592A1/en
Application granted granted Critical
Publication of EP2778592B1 publication Critical patent/EP2778592B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
    • F28F1/126Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element consisting of zig-zag shaped fins
    • F28F1/128Fins with openings, e.g. louvered fins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D1/00Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
    • F28D1/02Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
    • F28D1/04Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
    • F28D1/053Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight
    • F28D1/0535Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight the conduits having a non-circular cross-section
    • F28D1/05366Assemblies of conduits connected to common headers, e.g. core type radiators

Definitions

  • the invention relates to heat exchanger assemblies, particularly to heat exchangers having fins, and more particularly to air cooled heat exchangers having louvered fins. It relates specifically to a split mini-louvered fin according to the preamble of claim 1. Fig 3A of US 2009/0173479 A1 discloses such fins.
  • Air cooled heat exchanger assemblies for automobiles are used for transferring heat from various working fluids, such as an engine coolant, an engine lubricating oil, an air conditioning refrigerant, and a transmission oil.
  • a typical air cooled heat exchanger assembly includes an inlet header, an outlet header spaced from the inlet header, a plurality of fluid tubes hydraulically connecting the inlet and outlet headers, and a plurality of corrugated fins disposed between adjacent fluid tubes.
  • the core of the heat exchanger assembly is defined by the plurality of fluid tubes and the corrugated fins disposed between adjacent tubes.
  • a stream of air is directed through the core of the heat exchanger assembly typically by a cooling fan or motion of the automobile. As the stream of air flows across the fins, heat in a fluid flowing through the fluid tubes is conducted through the walls of the tubes, into the fins, transferred to the stream of air flow.
  • louvers Various types of fins and louver designs are known in the art with the object of increasing the heat transfer efficiency of the heat exchanger assembly. Examples of these designs include increasing the numbers of louvers on a planar portion of the fin, forming louvers at a predetermined angle relative to the planar portion of the fin, forming louvers above and below the planar portion of the fin, and disposing louvers at predetermined locations on the planar portion of the fin to alter the air flow pattern through the core to increase the heat transfer coefficient of air encountered by the fluid tubes and fins.
  • a heat exchanger assembly having at least one header, a plurality of spaced apart fluid tubes in hydraulic communication with the header, and a plurality of corrugated fins disposed between and in thermal contact with the tubes.
  • the corrugated fins include a planar portion having a louver segment defined between a pair of primary slits, in which the louver segment includes an intermediate slit between the pair of primary slits splitting the louver segment into a pair of mini-louvers.
  • the primary slits and the at least one intermediate slit are parallel and each of the primary slit includes a length L1.
  • the at least one intermediate slit includes a length L2, and wherein the length L2 is less than the length L1, thereby defining a primary juncture transitioning the louver segment to the planar portion and defining a secondary juncture transitioning the mini-louvers to the primary juncture.
  • the louver segment includes a primary juncture transitioning the louver segment to the planar portion.
  • the louver segment is pivoted about such primary juncture such that the louver segment is oblique relative to the planar portion.
  • Each of the mini-louvers includes a secondary juncture transitioning the mini-louvers to the primary juncture.
  • the mini-louvers are counter-offset such that one of the mini-louvers is on one side of the planar portion and other one of the mini-louver is on the other side of the planar portion.
  • the mini-louvers may be pivoted about their respective junctures such that each of the mini-louvers is at an angle oblique relative to the planar portion.
  • Each of the mini-louvers includes a front edge and an opposite trailing edge, wherein the mini-louvers partially overlap one another such that the rear edge of one mini-louver extends past the front edge of the other mini-louver.
  • the planar portion includes a leading edge, and the front edges of the mini-louvers are parallel with the leading edge of the planar portion.
  • the intermediate slit defines an air passageway between the mini-louvers on either side of the planar portion.
  • a split mini-louvered fin for a heat exchanger assembly comprises a planar portion having a louver segment defined between a pair of primary slits.
  • the louver segment includes at least one intermediate slit between the pair of primary slits, thereby splitting the louver segment into at least two mini-louvers.
  • the mini-louvers are counter-offset such that one of the mini-louvers is on one side of the planar portion and the other one of the mini-louvers is on the other side of said planar portion.
  • the intermediate slit defines an air passageway between the mini-louvers.
  • Each of the mini-louvers includes a front edge and an opposite trailing edge.
  • the mini-louvers partially overlap one another such that the rear edge of one mini-louver extends past the front edge of the other mini-louver.
  • Each of the mini-louvers transitions into a secondary juncture.
  • Each of the secondary juncture transitions into primary juncture which transitions into the planar portion.
  • the counter off-setting of the mini-louvers onto both sides of the planar portion allows the mini-louvers to extend a greater distance from the planar portion into the air-flow channel than what a single larger louver would allow.
  • the greater louver penetration into the air flow channels increases the distance that the air flow has to travel and increases the number of boundary layer interruptions that the air flow has to encounter, thereby increasing heat transfer efficiency.
  • the intermediate slit separating the first from the second mini-louver in each pair of mini-louvers defines an air flow passageway, which allows greater air flow efficiency and less air pressure drop for air flow through the core of the heat exchanger assembly.
  • FIG. 1 , 4 , 5 , and 7-9 wherein like numerals indicate corresponding parts throughout the several views, is an exemplary embodiment of a heat exchanger assembly 20 having split mini-louvered fins 150 of the current invention.
  • the split mini-louvered fins 150 enable greater heat transfer efficiency by allowing greater louver penetration into the air flow channels 36 to increase the distance that the air flow has to travel through the heat exchanger core 34 and to increase the number of boundary layer interruptions that the air flow has to encounter, while minimizing the pressure drop.
  • FIG. 1 Shown in Fig. 1 is a perspective front view of an exemplary embodiment of the heat exchanger assembly 20 of the present invention, which includes a first manifold 22 extending along a manifold A-axis and a second manifold 24 extending in a spaced and substantially parallel relationship with the first manifold 22.
  • the first and second manifolds 22, 24 present a plurality of corresponding tube slots 26 axially spaced along the respective manifolds 22, 24.
  • a plurality of fluid tubes 28 is inserted into the corresponding tube slots 26 of the manifolds 22 in a spaced and parallel arrangement for hydraulic fluid communication between the manifolds 22, 24.
  • a plurality of corrugated fins 32 is disposed between and in thermal contact with adjacent fluid tubes 28 for increased heat transfer efficiency between the fluid in the tubes 28 and ambient air.
  • the plurality of tubes 28 and corrugated fins 32 between adjacent tubes 28 define the heat exchanger core 34.
  • the spaces between the corrugated fins 32 and the plurality of tubes 28 define a plurality of airflow channels 36 through the core 34.
  • a stream of ambient air is directed through the core 34 of the heat exchanger assembly 20 to transfer heat from a fluid flowing through the fluid tubes 28 to the ambient air. Heat is conducted through the walls of the tubes 28, into the fins, and transferred to the stream of air flow. It should be appreciated that heat may be transferred to the fluid flowing through the tubes 28 if the temperature of the stream of air is higher than the temperature of the fluid flowing through the tubes 28.
  • FIG. 2 Shown in Fig. 2 is a view of a prior art corrugated louvered fin 50 having single louvers 52 along a planar portion 54 of the fin 50.
  • the corrugated louvered fin 50 is formed from a thin strip of heat conductive material into corner portions 56 and planar portions 54 that are alternately continuously arranged to define a corrugation.
  • Each of the planar portions 54 includes a leading edge 58 oriented into the oncoming air flow, an opposite trailing edge 60 spaced from the leading edge 58, and a plurality of louvers 52 therebetween.
  • Each louver 52 is defined by a louver segment 62 of the planar portion 54 between a pair of slits 64. Best shown in Figs.
  • the single louvers 52 are formed by pivoting the louver segments 62 about the junctures 66 such that the louver segments 62 are oblique to the planar portion 54. Best shown in Fig. 3 , the pivoting of the louver segment 62 about the juncture 66 defines a twisted transition that connects the single louver 52 to the planar portion 54.
  • the louver 52 includes a front edge 59 oriented toward the direction of air flow and an opposite rear edge 60. The front edges 59 of the louvers 52 are substantially parallel with each other and may be parallel with the leading edge 58 of the planar portion 54.
  • each pair of split mini-louvers 152 is defined by pivoting a louver segment 162 about a primary juncture 166 to a predetermined first angle relative to the planar portion 154, splitting the louver segment 162 into a first mini-louver 176 and a second mini-louver 178, counter off-setting the mini-louvers 176, 178 onto both sides of the planar portion 154, and pivoting the mini-louvers 176,178 about their respective secondary junctures 172 to a predetermine second angle with respect to the planar portion 154.
  • the mini-louvers 176, 178 may also be off-set in the axial direction with respect to the direction of airflow such that a portion of one mini-louver overlaps with a portion of the other mini-louver.
  • the split mini-louvered fin 150 includes a planar portion 154 having a leading edge 158 and an opposite trailing edge 160.
  • the planar portion 154 includes a louver segment 162 defined between a pair of primary slits 164 having a first length L1.
  • On opposite ends of the louver segment 162 is a primary juncture 166 that transitions the louver segment 162 to the planar portion 154.
  • the louver segment 162 is split into a first segment 168 and a second segment 170 by an intermediate slit 165 having a length L2 between the pair of primary slits 164.
  • the length L2 of the intermediate slit is shorter than the length of the primary slit L1, thereby defining a secondary juncture 172 on opposite sides of each of the first and second segments 168, 170.
  • the secondary junctures 172 transition the respective segments 168, 170 into the primary juncture 166, which then transitions into the planar portion 154.
  • the pair of primary slits 164 and intermediate slit 165 may be parallel with each other and as well as with the leading edge 158 of the planar portion 154.
  • Fig. 7 Shown in Fig. 7 is a cross-sectional view of the split mini-louvered fins 150 of Fig. 5 along line 7-7.
  • the louver segment 162 is pivoted in a first direction about the primary juncture 166 to a first angle that is oblique to the planar portion 154.
  • a first mini-louver 176 and a second mini-louver 178 are then defined by counter-offsetting the first and second segments 168, 170 onto opposite sides of the planar portion 154.
  • mini-louvers 176, 178 While only two mini-louvers 176, 178 are shown per louver segment 162, it should be appreciated that additional mini-louvers 176 may be formed on the same louver segment 162 by providing additional intermediate splits 165 between the pair of primary slits 164.
  • the counter-offsetting of the first and second segments 168, 170 to define the first and second mini-louvers 176, 178 may be accomplished by mechanically displacing the material defining the secondary junctures 172 such that one of the first and second mini-louvers 176, 178 is on one side of the planar portion 154 and the other of the first and second mini-louvers 176, 178 is on the other side of the planar portion 154.
  • the first and second mini-louvers 176, 178 may be individually pivoted about their respective secondary junctures 172 to a predetermined angle with respect to the planar portion 154.
  • the predetermined degree of angle for the first and second mini-louvers 176, 178 may be the same or offset from each other.
  • the counter-offsetting of the first and second segments 168, 170 to define the first and second mini-louvers 176, 178 may be accomplished by pivoting the first and second segments 168, 170 in a second direction opposite that of the first pivot direction of the louver segment 162 such that one of the first and second mini-louvers 176, 178 is on one side of the planar portion 154 and the other of the first and second mini-louvers 176, 178 is on the other side of the planar portion 154.
  • the pivoting of the first and second segments 168, 170 in a second direction opposite that of the first pivot direction may be varied according to the desired angle of the mini-louvers 176, 178 with respect to the planar portion 154.
  • Fig. 8 shows a cross-sectional view of an embodiment belonging to the of the split mini-louvered fins 150 of Fig. 5 along line 7-7.
  • the first mini-louver 176 includes a front edge 159a oriented in the direction of air flow and a downstream rear edge 161 a.
  • the associated second mini-louver 178 includes a front edge 159b oriented in the direction of air flow and a downstream trailing edge 161b.
  • the offset first and second mini-louvers 176, 178 are displaced axially relative to the direction of air flow from the leading edge 158 to the trailing edge 160 such that a portion of the first and second mini-louvers 176, 178 overlaps each other in way that the rear edge 161 a of the first mini-louver 176 extends rearward pass the front edge 159b of the second mini-louver 178.
  • Fig. 9 shows a cross-sectional view of the alternative embodiment of the split mini-louvered fins 150 of Fig. 5 along line 9-9.
  • the counter off-setting of the first and second mini-louvers 176, 178 onto both sides of the planar portion 154 allows the mini-louvers 176, 178 to extend at a greater distance from the planar portion 154 into the flow channel 36 than what a single larger louver 52 would allow.
  • the greater louver penetration into the air flow channels 36 increases the distance that the air flow has to travel and increases the number of boundary layer interruptions that the air flow has to encounter, thereby increasing heat transfer efficiency.
  • the intermediate slit 165 separating the first from the second mini-louver 176, 178 in each pair of mini-louvers 176, 178 defines an air flow passageway 190 thereby allowing greater air flow efficiency, resulting in less air pressure drop associated with the change in airflow direction caused by the fins and louvers.

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Geometry (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Blinds (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Description

    TECHNICAL FIELD
  • The invention relates to heat exchanger assemblies, particularly to heat exchangers having fins, and more particularly to air cooled heat exchangers having louvered fins. It relates specifically to a split mini-louvered fin according to the preamble of claim 1. Fig 3A of US 2009/0173479 A1 discloses such fins.
  • BACKGROUND OF THE INVENTION
  • Air cooled heat exchanger assemblies for automobiles are used for transferring heat from various working fluids, such as an engine coolant, an engine lubricating oil, an air conditioning refrigerant, and a transmission oil. A typical air cooled heat exchanger assembly includes an inlet header, an outlet header spaced from the inlet header, a plurality of fluid tubes hydraulically connecting the inlet and outlet headers, and a plurality of corrugated fins disposed between adjacent fluid tubes. The core of the heat exchanger assembly is defined by the plurality of fluid tubes and the corrugated fins disposed between adjacent tubes. A stream of air is directed through the core of the heat exchanger assembly typically by a cooling fan or motion of the automobile. As the stream of air flows across the fins, heat in a fluid flowing through the fluid tubes is conducted through the walls of the tubes, into the fins, transferred to the stream of air flow.
  • Various types of fins and louver designs are known in the art with the object of increasing the heat transfer efficiency of the heat exchanger assembly. Examples of these designs include increasing the numbers of louvers on a planar portion of the fin, forming louvers at a predetermined angle relative to the planar portion of the fin, forming louvers above and below the planar portion of the fin, and disposing louvers at predetermined locations on the planar portion of the fin to alter the air flow pattern through the core to increase the heat transfer coefficient of air encountered by the fluid tubes and fins.
  • It is desirable to continuously improve fin and louver designs for a heat exchanger assembly to increase the heat transfer efficiency by maximizing the heat transfer coefficient of air encountered by the fluid tubes and fins while minimizing the pressure drop through the core.
  • SUMMARY OF THE INVENTION
  • In concordance with the instant disclosure, a heat exchanger assembly is provided having at least one header, a plurality of spaced apart fluid tubes in hydraulic communication with the header, and a plurality of corrugated fins disposed between and in thermal contact with the tubes. The corrugated fins include a planar portion having a louver segment defined between a pair of primary slits, in which the louver segment includes an intermediate slit between the pair of primary slits splitting the louver segment into a pair of mini-louvers. The primary slits and the at least one intermediate slit are parallel and each of the primary slit includes a length L1. The at least one intermediate slit includes a length L2, and wherein the length L2 is less than the length L1, thereby defining a primary juncture transitioning the louver segment to the planar portion and defining a secondary juncture transitioning the mini-louvers to the primary juncture. The louver segment includes a primary juncture transitioning the louver segment to the planar portion. The louver segment is pivoted about such primary juncture such that the louver segment is oblique relative to the planar portion. Each of the mini-louvers includes a secondary juncture transitioning the mini-louvers to the primary juncture. The mini-louvers are counter-offset such that one of the mini-louvers is on one side of the planar portion and other one of the mini-louver is on the other side of the planar portion. The mini-louvers may be pivoted about their respective junctures such that each of the mini-louvers is at an angle oblique relative to the planar portion. Each of the mini-louvers includes a front edge and an opposite trailing edge, wherein the mini-louvers partially overlap one another such that the rear edge of one mini-louver extends past the front edge of the other mini-louver. The planar portion includes a leading edge, and the front edges of the mini-louvers are parallel with the leading edge of the planar portion. The intermediate slit defines an air passageway between the mini-louvers on either side of the planar portion.
  • A split mini-louvered fin for a heat exchanger assembly comprises a planar portion having a louver segment defined between a pair of primary slits. The louver segment includes at least one intermediate slit between the pair of primary slits, thereby splitting the louver segment into at least two mini-louvers. The mini-louvers are counter-offset such that one of the mini-louvers is on one side of the planar portion and the other one of the mini-louvers is on the other side of said planar portion. The intermediate slit defines an air passageway between the mini-louvers. Each of the mini-louvers includes a front edge and an opposite trailing edge. The mini-louvers partially overlap one another such that the rear edge of one mini-louver extends past the front edge of the other mini-louver. Each of the mini-louvers transitions into a secondary juncture. Each of the secondary juncture transitions into primary juncture which transitions into the planar portion.
  • The counter off-setting of the mini-louvers onto both sides of the planar portion allows the mini-louvers to extend a greater distance from the planar portion into the air-flow channel than what a single larger louver would allow. The greater louver penetration into the air flow channels increases the distance that the air flow has to travel and increases the number of boundary layer interruptions that the air flow has to encounter, thereby increasing heat transfer efficiency. The intermediate slit separating the first from the second mini-louver in each pair of mini-louvers defines an air flow passageway, which allows greater air flow efficiency and less air pressure drop for air flow through the core of the heat exchanger assembly.
  • Further features and advantages of the invention will appear more clearly on a reading of the following detailed description of an embodiment of the invention, which is given by way of non-limiting example only and with reference to the accompanying drawings.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • This invention will be further described with reference to the accompanying drawings in which:
    • Fig. 1 shows a perspective front view of an exemplary embodiment of a heat exchanger assembly having corrugated fins with louvers.
    • Fig. 2 shows a perspective view of single louvered fins known in the art.
    • Fig. 3 is a detailed perspective view of the prior art single louvered fins of Fig. 2.
    • Fig. 4 shows a perspective view of an exemplary embodiment of split mini-louvered fins not belonging to the current invention.
    • Fig. 5 is a detailed perspective view of the split mini-louvered fins of Fig. 4.
    • Fig. 6 is a schematic cross-sectional view of single louvered fins of Fig. 3 along line 6-6.
    • Fig. 7 is a schematic cross-sectional view of the split mini-louvered fins of Fig. 5 along line 7-7.
    • Fig. 8 is a schematic cross-sectional view of an embodiment of the split mini-louvered fins according to the invention.
    • Fig. 9 is a schematic cross-sectional view of an alternative embodiment of the split mini-louvered fins of Fig. 5 along line 9-9.
    DESCRIPTION OF THE PREFERRED EMBODIMENT
  • The following detailed description and appended drawings describe and illustrate various embodiments of the invention. The description and drawings serve to enable one skilled in the art to make and use the inventions, and are not intended to limit the scope of the invention in any manner.
  • Referring to Figures 1, 4, 5, and 7-9 wherein like numerals indicate corresponding parts throughout the several views, is an exemplary embodiment of a heat exchanger assembly 20 having split mini-louvered fins 150 of the current invention. The split mini-louvered fins 150 enable greater heat transfer efficiency by allowing greater louver penetration into the air flow channels 36 to increase the distance that the air flow has to travel through the heat exchanger core 34 and to increase the number of boundary layer interruptions that the air flow has to encounter, while minimizing the pressure drop.
  • Shown in Fig. 1 is a perspective front view of an exemplary embodiment of the heat exchanger assembly 20 of the present invention, which includes a first manifold 22 extending along a manifold A-axis and a second manifold 24 extending in a spaced and substantially parallel relationship with the first manifold 22. The first and second manifolds 22, 24 present a plurality of corresponding tube slots 26 axially spaced along the respective manifolds 22, 24. A plurality of fluid tubes 28 is inserted into the corresponding tube slots 26 of the manifolds 22 in a spaced and parallel arrangement for hydraulic fluid communication between the manifolds 22, 24. A plurality of corrugated fins 32 is disposed between and in thermal contact with adjacent fluid tubes 28 for increased heat transfer efficiency between the fluid in the tubes 28 and ambient air. The plurality of tubes 28 and corrugated fins 32 between adjacent tubes 28 define the heat exchanger core 34. The spaces between the corrugated fins 32 and the plurality of tubes 28 define a plurality of airflow channels 36 through the core 34.
  • In a normal operating state, a stream of ambient air is directed through the core 34 of the heat exchanger assembly 20 to transfer heat from a fluid flowing through the fluid tubes 28 to the ambient air. Heat is conducted through the walls of the tubes 28, into the fins, and transferred to the stream of air flow. It should be appreciated that heat may be transferred to the fluid flowing through the tubes 28 if the temperature of the stream of air is higher than the temperature of the fluid flowing through the tubes 28.
  • Shown in Fig. 2 is a view of a prior art corrugated louvered fin 50 having single louvers 52 along a planar portion 54 of the fin 50. The corrugated louvered fin 50 is formed from a thin strip of heat conductive material into corner portions 56 and planar portions 54 that are alternately continuously arranged to define a corrugation. Each of the planar portions 54 includes a leading edge 58 oriented into the oncoming air flow, an opposite trailing edge 60 spaced from the leading edge 58, and a plurality of louvers 52 therebetween. Each louver 52 is defined by a louver segment 62 of the planar portion 54 between a pair of slits 64. Best shown in Figs. 2 and 6, on opposite ends of the louver segment 62 is a juncture 66 that transitions the louver segment 62 to the planar portion 54. The single louvers 52 are formed by pivoting the louver segments 62 about the junctures 66 such that the louver segments 62 are oblique to the planar portion 54. Best shown in Fig. 3, the pivoting of the louver segment 62 about the juncture 66 defines a twisted transition that connects the single louver 52 to the planar portion 54. The louver 52 includes a front edge 59 oriented toward the direction of air flow and an opposite rear edge 60. The front edges 59 of the louvers 52 are substantially parallel with each other and may be parallel with the leading edge 58 of the planar portion 54.
  • Shown in Figs. 4, 5, and 7 are views of an embodiment of a corrugated split mini-louvered fin 150 not belonging to the invention. Best shown in Fig. 7, each pair of split mini-louvers 152 is defined by pivoting a louver segment 162 about a primary juncture 166 to a predetermined first angle relative to the planar portion 154, splitting the louver segment 162 into a first mini-louver 176 and a second mini-louver 178, counter off-setting the mini-louvers 176, 178 onto both sides of the planar portion 154, and pivoting the mini-louvers 176,178 about their respective secondary junctures 172 to a predetermine second angle with respect to the planar portion 154. Show in Figs. 8 and 9, the mini-louvers 176, 178 may also be off-set in the axial direction with respect to the direction of airflow such that a portion of one mini-louver overlaps with a portion of the other mini-louver.
  • Shown in Figs. 4 and 7, the split mini-louvered fin 150 includes a planar portion 154 having a leading edge 158 and an opposite trailing edge 160. The planar portion 154 includes a louver segment 162 defined between a pair of primary slits 164 having a first length L1. On opposite ends of the louver segment 162 is a primary juncture 166 that transitions the louver segment 162 to the planar portion 154. The louver segment 162 is split into a first segment 168 and a second segment 170 by an intermediate slit 165 having a length L2 between the pair of primary slits 164. The length L2 of the intermediate slit is shorter than the length of the primary slit L1, thereby defining a secondary juncture 172 on opposite sides of each of the first and second segments 168, 170. The secondary junctures 172 transition the respective segments 168, 170 into the primary juncture 166, which then transitions into the planar portion 154. The pair of primary slits 164 and intermediate slit 165 may be parallel with each other and as well as with the leading edge 158 of the planar portion 154.
  • Shown in Fig. 7 is a cross-sectional view of the split mini-louvered fins 150 of Fig. 5 along line 7-7. The louver segment 162 is pivoted in a first direction about the primary juncture 166 to a first angle that is oblique to the planar portion 154. A first mini-louver 176 and a second mini-louver 178 are then defined by counter-offsetting the first and second segments 168, 170 onto opposite sides of the planar portion 154. While only two mini-louvers 176, 178 are shown per louver segment 162, it should be appreciated that additional mini-louvers 176 may be formed on the same louver segment 162 by providing additional intermediate splits 165 between the pair of primary slits 164.
  • The counter-offsetting of the first and second segments 168, 170 to define the first and second mini-louvers 176, 178 may be accomplished by mechanically displacing the material defining the secondary junctures 172 such that one of the first and second mini-louvers 176, 178 is on one side of the planar portion 154 and the other of the first and second mini-louvers 176, 178 is on the other side of the planar portion 154. Once off-set, the first and second mini-louvers 176, 178 may be individually pivoted about their respective secondary junctures 172 to a predetermined angle with respect to the planar portion 154. The predetermined degree of angle for the first and second mini-louvers 176, 178 may be the same or offset from each other.
  • As an alternative to mechanically displacing the material defining the secondary junctures 172 such that one of the first and second mini-louvers 176, 178 are on opposite side of the planar portion 154, the counter-offsetting of the first and second segments 168, 170 to define the first and second mini-louvers 176, 178 may be accomplished by pivoting the first and second segments 168, 170 in a second direction opposite that of the first pivot direction of the louver segment 162 such that one of the first and second mini-louvers 176, 178 is on one side of the planar portion 154 and the other of the first and second mini-louvers 176, 178 is on the other side of the planar portion 154. The pivoting of the first and second segments 168, 170 in a second direction opposite that of the first pivot direction may be varied according to the desired angle of the mini-louvers 176, 178 with respect to the planar portion 154.
  • Fig. 8 shows a cross-sectional view of an embodiment belonging to the of the split mini-louvered fins 150 of Fig. 5 along line 7-7. The first mini-louver 176 includes a front edge 159a oriented in the direction of air flow and a downstream rear edge 161 a. Similarly, the associated second mini-louver 178 includes a front edge 159b oriented in the direction of air flow and a downstream trailing edge 161b. The offset first and second mini-louvers 176, 178 are displaced axially relative to the direction of air flow from the leading edge 158 to the trailing edge 160 such that a portion of the first and second mini-louvers 176, 178 overlaps each other in way that the rear edge 161 a of the first mini-louver 176 extends rearward pass the front edge 159b of the second mini-louver 178.
  • Fig. 9 shows a cross-sectional view of the alternative embodiment of the split mini-louvered fins 150 of Fig. 5 along line 9-9. The counter off-setting of the first and second mini-louvers 176, 178 onto both sides of the planar portion 154 allows the mini-louvers 176, 178 to extend at a greater distance from the planar portion 154 into the flow channel 36 than what a single larger louver 52 would allow. The greater louver penetration into the air flow channels 36 increases the distance that the air flow has to travel and increases the number of boundary layer interruptions that the air flow has to encounter, thereby increasing heat transfer efficiency. Furthermore, the intermediate slit 165 separating the first from the second mini-louver 176, 178 in each pair of mini-louvers 176, 178 defines an air flow passageway 190 thereby allowing greater air flow efficiency, resulting in less air pressure drop associated with the change in airflow direction caused by the fins and louvers.

Claims (7)

  1. A split mini-louvered fin (150) for a heat exchanger assembly (20), comprising:
    a planar portion (154) having a louver segment (162) defined between a pair of primary slits (164),
    wherein said louver segment (162) includes at least one intermediate slit (165) between said pair of primary slits (164), thereby splitting said louver segment (162) into at least two mini-louvers (176, 178),
    wherein
    each of said mini-louvers (176, 178) includes a front edge (159) and an opposite trailing edge (161), characterized in that wherein said mini-louvers (176, 178) partially overlap one another such that the rear edge (161) of one mini-louver (52) extends past the front edge (159) of the other said mini-louver (176, 178).
  2. Split mini-louvered fin (150) for a heat exchanger assembly (20) of claim 1 wherein said mini-louvers (176, 178) are counter-offset such that one of said mini-louvers (176, 178) is on one side of said planar portion (154) and other one of said mini-louvers (176, 178) is on the other side of said planar portion (154).
  3. Split mini-louvered fin (150) for a heat exchanger assembly (20) according to any one of the preceding claims wherein said intermediate slit (165) defines an air passageway between said mini-louvers (176).
  4. Split mini-louvered fin (150) for a heat exchanger assembly (20) according to any one of the preceding claims wherein each of said mini-louvers (176, 178) transitions into a secondary juncture (172).
  5. Split mini-louvered fin (150) for a heat exchanger assembly (20) of claim 4 wherein each of said secondary juncture (172) transitions into primary juncture (166) which transitions into said planar portion (154).
  6. A heat exchanger assembly (20) comprising:
    at least one header (22);
    a plurality of fluid tubes (28) in hydraulic communication with said header (22), wherein said tubes (28) are spaced apart; and
    a plurality of corrugated fins (32) disposed between and in thermal contact with said tubes (28), at least one of said corrugated fins (32) being a split mini-louvered fin (150) according to any one of the preceding claims.
  7. Heat exchanger assembly (20) of claim 6, wherein:
    said primary slits (164) and said at least one intermediate slit (165) are parallel,
    each of said primary slit includes a length L1,
    said at least one intermediate slit (165) includes a length L2, and
    wherein said length L2 is less than said length L1, thereby defining a primary juncture (166) transitioning said louver segment (162) to said planar portion (154) and defining a secondary juncture (172) transitioning said mini-louvers (176, 178) to said primary juncture (166).
EP14159252.7A 2013-03-15 2014-03-12 Heat exchanger assembly having split mini-louvered fins Not-in-force EP2778592B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/834,355 US20130199760A1 (en) 2008-08-06 2013-03-15 Heat exchanger assembly having split mini-louvered fins

Publications (2)

Publication Number Publication Date
EP2778592A1 EP2778592A1 (en) 2014-09-17
EP2778592B1 true EP2778592B1 (en) 2016-03-09

Family

ID=48901878

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14159252.7A Not-in-force EP2778592B1 (en) 2013-03-15 2014-03-12 Heat exchanger assembly having split mini-louvered fins

Country Status (5)

Country Link
US (1) US20130199760A1 (en)
EP (1) EP2778592B1 (en)
KR (1) KR20140113418A (en)
CN (1) CN104048522B (en)
BR (1) BR102014006089A8 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9518768B2 (en) 2009-06-10 2016-12-13 Mahle International Gmbh Evaporator having a phase change material louvered clam shell housing
ES2711572T3 (en) 2010-03-31 2019-05-06 Modine Mfg Co Heat exchanger
EP2846120A1 (en) * 2013-09-06 2015-03-11 Delphi Technologies, Inc. Evaporator having a phase change material louvered clam shell housings
US10209012B2 (en) * 2015-02-24 2019-02-19 Lgl France Heat exchanger with louvered fins
US10094624B2 (en) 2016-01-08 2018-10-09 Hanon Systems Fin for heat exchanger
USD852338S1 (en) 2016-07-05 2019-06-25 Danfoss Micro Channel Heat Exchanger (Jiaxing) Co., Ltd. Heat exchanger
USD839404S1 (en) * 2016-07-06 2019-01-29 Danfoss Micro Channel Heat Exchanger (Jiaxing) Co., Ltd. Heat exchanger
USD828910S1 (en) * 2016-07-07 2018-09-18 Danfoss Micro Channel Heat Exchanger (Jiaxing) Co., Ltd. Heat exchanger
US11326842B2 (en) * 2018-09-21 2022-05-10 Samsung Electronics Co., Ltd. Heat exchanger and air conditioner having the same
US20210063089A1 (en) 2019-09-03 2021-03-04 Mahle International Gmbh Curved heat exchanger and method of manufacturing

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5795595A (en) * 1980-12-03 1982-06-14 Hitachi Ltd Fin for heat exchanger unit
JPS6012088U (en) * 1983-06-30 1985-01-26 カルソニックカンセイ株式会社 Heat exchanger
JPS6256786A (en) * 1985-09-06 1987-03-12 Hitachi Ltd Heat exchanger
JPS63183390A (en) * 1987-01-22 1988-07-28 Kobe Steel Ltd Louver fin with slit
US5353866A (en) * 1987-12-04 1994-10-11 Hitachi, Ltd. Heat transfer fins and heat exchanger
JPH04324040A (en) * 1991-04-25 1992-11-13 Hitachi Cable Ltd Open air gravity fall type cooling device
CN1210583A (en) * 1996-12-04 1999-03-10 株式会社杰克塞尔 Heat exchanger
JP2000249485A (en) * 1999-02-26 2000-09-14 Sanyo Electric Co Ltd Heat exchanger
US6883598B2 (en) * 1999-03-16 2005-04-26 Outokumpu Oyj Cooling element for a heat exchanger
JP2004251554A (en) * 2003-02-20 2004-09-09 Matsushita Electric Ind Co Ltd Exterior heat exchanger for heat pump
EP1711769A1 (en) * 2004-02-05 2006-10-18 Calsonic Kansei UK Limited Heat exchanger
JP4614266B2 (en) * 2004-07-23 2011-01-19 臼井国際産業株式会社 Fins for fluid agitation, and heat transfer tubes and heat exchangers or heat exchange type gas cooling devices equipped with the fins
JP2006200788A (en) * 2005-01-19 2006-08-03 Denso Corp Heat exchanger
US20090173479A1 (en) * 2008-01-09 2009-07-09 Lin-Jie Huang Louvered air center for compact heat exchanger
CN101788241B (en) * 2009-03-25 2014-04-16 三花控股集团有限公司 Window type fin for heat exchanger and heat exchanger with window type fin
JP5545260B2 (en) * 2010-05-21 2014-07-09 株式会社デンソー Heat exchanger

Also Published As

Publication number Publication date
CN104048522B (en) 2017-12-12
US20130199760A1 (en) 2013-08-08
KR20140113418A (en) 2014-09-24
EP2778592A1 (en) 2014-09-17
CN104048522A (en) 2014-09-17
BR102014006089A2 (en) 2015-05-19
BR102014006089A8 (en) 2017-07-04

Similar Documents

Publication Publication Date Title
EP2778592B1 (en) Heat exchanger assembly having split mini-louvered fins
US6662861B2 (en) Heat exchanger
US8276652B2 (en) High performance louvered fin for heat exchanger
JP4674602B2 (en) Heat exchanger
US6213196B1 (en) Double heat exchanger for vehicle air conditioner
EP2697589B1 (en) Heat exchanger
US20100263847A1 (en) Microchannel heat exchanger
US8167028B2 (en) Heat exchanger fin with planar crests and troughs having slits
US9915481B2 (en) Fin for heat exchanger
JP2006200788A (en) Heat exchanger
EP3553446B1 (en) Shaped leading edge of cast plate fin heat exchanger
US20160054075A1 (en) Folded tube multiple bank heat exchange unit
EP2962055B1 (en) Fin solution related to micro channel based heat exchanger
EP1519133A2 (en) Heat exchanging apparatus
US6672376B2 (en) Twisted-louver high performance heat exchanger fin
US5975200A (en) Plate-fin type heat exchanger
EP2956728B1 (en) Multiple bank flattened tube heat exchanger
EP3575728B1 (en) A core of a heat exchanger comprising corrugated fins
EP2997322B1 (en) Method for manufacturing a multiple manifold assembly having internal communication ports
US20150000880A1 (en) Heat exchanger with varied louver angles
EP0803695B1 (en) Plate-fin heat exchanger
US20220128320A1 (en) Microchannel heat exchanger for a furnace
US10655530B2 (en) Intercooler
JP2008286446A (en) Heat transfer member and heat exchanger using the same
KR101100114B1 (en) Fin for heat exchanger

Legal Events

Date Code Title Description
17P Request for examination filed

Effective date: 20140312

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

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

R17P Request for examination filed (corrected)

Effective date: 20150317

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

RIC1 Information provided on ipc code assigned before grant

Ipc: F28F 1/12 20060101ALI20150915BHEP

Ipc: F28F 1/00 20060101AFI20150915BHEP

Ipc: F28D 1/053 20060101ALI20150915BHEP

INTG Intention to grant announced

Effective date: 20151002

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: MAHLE INTERNATIONAL GMBH

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): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 779833

Country of ref document: AT

Kind code of ref document: T

Effective date: 20160315

Ref country code: CH

Ref legal event code: EP

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: 602014001018

Country of ref document: DE

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 3

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20160309

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: 20160309

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: 20160610

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: 20160309

Ref country code: HR

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: 20160309

Ref country code: NO

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: 20160609

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 779833

Country of ref document: AT

Kind code of ref document: T

Effective date: 20160309

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: 20160309

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: 20160309

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: 20160309

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: 20160309

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: 20160309

Ref country code: RS

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: 20160309

Ref country code: BE

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

Effective date: 20160331

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

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: 20160309

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: 20160709

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

Ref country code: SM

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: 20160309

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: 20160309

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: 20160309

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: 20160309

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: 20160309

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: 20160711

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602014001018

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

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

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: 20160309

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: 20160309

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

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: 20160312

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: 20160309

26N No opposition filed

Effective date: 20161212

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: 20160609

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 4

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

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: 20160309

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: 20160309

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

Ref country code: LI

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

Effective date: 20170331

Ref country code: CH

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

Effective date: 20170331

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 5

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; INVALID AB INITIO

Effective date: 20140312

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: 20160331

Ref country code: LU

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

Effective date: 20160312

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: 20160309

Ref country code: MK

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: 20160309

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: 20160309

Ref country code: MC

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: 20160309

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

Ref country code: AL

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: 20160309

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

Effective date: 20180312

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

Ref country code: GB

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

Effective date: 20180312

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

Ref country code: FR

Payment date: 20190328

Year of fee payment: 6

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: 20200331

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

Ref country code: DE

Payment date: 20210427

Year of fee payment: 8

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602014001018

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: 20221001