WO2013078531A1 - Heat exchanger with end seal for blocking off air bypass flow - Google Patents

Heat exchanger with end seal for blocking off air bypass flow Download PDF

Info

Publication number
WO2013078531A1
WO2013078531A1 PCT/CA2011/050740 CA2011050740W WO2013078531A1 WO 2013078531 A1 WO2013078531 A1 WO 2013078531A1 CA 2011050740 W CA2011050740 W CA 2011050740W WO 2013078531 A1 WO2013078531 A1 WO 2013078531A1
Authority
WO
WIPO (PCT)
Prior art keywords
heat exchanger
seal
side faces
front face
spaced
Prior art date
Application number
PCT/CA2011/050740
Other languages
French (fr)
Inventor
Lee M. KINDER
Desmond Magill
Original Assignee
Dana Canada Corporation
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 Dana Canada Corporation filed Critical Dana Canada Corporation
Priority to DE112011105882.9T priority Critical patent/DE112011105882T5/en
Priority to CA2857084A priority patent/CA2857084A1/en
Priority to GB1409186.2A priority patent/GB2512218A/en
Priority to PCT/CA2011/050740 priority patent/WO2013078531A1/en
Priority to CN201180075107.7A priority patent/CN103959002B/en
Publication of WO2013078531A1 publication Critical patent/WO2013078531A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F27/00Control arrangements or safety devices specially adapted for heat-exchange or heat-transfer apparatus
    • F28F27/02Control arrangements or safety devices specially adapted for heat-exchange or heat-transfer apparatus for controlling the distribution of heat-exchange media between different channels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K13/00Arrangement in connection with combustion air intake or gas exhaust of propulsion units
    • B60K13/02Arrangement in connection with combustion air intake or gas exhaust of propulsion units concerning intake
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/04Cooling of air intake supply
    • F02B29/045Constructional details of the heat exchangers, e.g. pipes, plates, ribs, insulation, materials, or manufacturing and assembly
    • F02B29/0462Liquid cooled heat exchangers
    • 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
    • F28D1/03Heat-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 plate-like or laminated conduits
    • 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
    • F28D9/00Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/0006Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the plate-like or laminated conduits being enclosed within a pressure vessel
    • 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
    • F28D9/00Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/0031Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other
    • F28D9/0043Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another
    • F28D9/0056Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another with U-flow or serpentine-flow inside conduits; with centrally arranged openings on the plates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/08Elements constructed for building-up into stacks, e.g. capable of being taken apart for cleaning
    • F28F3/10Arrangements for sealing the margins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02Header boxes; End plates
    • F28F9/04Arrangements for sealing elements into header boxes or end plates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/26Arrangements for connecting different sections of heat-exchange elements, e.g. of radiators
    • 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
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/008Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for vehicles
    • F28D2021/0082Charged air coolers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2230/00Sealing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2280/00Mounting arrangements; Arrangements for facilitating assembling or disassembling of heat exchanger parts
    • F28F2280/04Means for preventing wrong assembling of parts
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • the specification relates to a heat exchanger having an air bypass seal, and a heat exchanger assembly having the heat exchanger and the seal.
  • Charge air cooler heat exchangers are well known in the art for mounting along the flow path of charge air supplied to a combustion engine.
  • This charge air typically comprises ambient air which has been compressed by apparatus such as a supercharger or turbocharger to provide an increased mass flow of air to the engine to permit the engine to combust increased quantities of fuel and thereby operate at an increased level of power and performance.
  • the charge air cooler is constructed from a plurality of lightweight heat transfer elements of a heat conductive material, such as copper or aluminum, shaped to provide extended heat transfer surfaces and defining a flow path for the charge air in heat transfer relation with a suitable coolant, such as ambient air or a liquid coolant.
  • a suitable coolant such as ambient air or a liquid coolant.
  • the charge air cooler may be constructed from a network of finned tubes such that charge air flowing over the fins is associated with a coolant flowing through the tubes resulting in adequate heat transfer for some engine system applications.
  • the charge air cooler is constructed from a stacked array of plates and fins which cooperate to define a heat exchanger core having separate flow paths for passage of the charge air and the coolant in close heat transfer relation with each other. In either case, however, the charge air cooler is desirably mounted directly into the intake manifold of the engine wherein charge air passing through the intake manifold is reduced in
  • the current heat exchanger products can allow air bypass past the ends of the fins (the plate lap joints extend beyond the end of the fins, or extend beyond the liquid fluid manifold, leaving unintended air bypass channels), or require additional brazed on components to compensate by blocking off these regions, which adds significant cost and/or may be impossible for certain cooler configurations.
  • wide elastomer seals can be provided, such as adhesively bonded or mechanically trapped seals, as part of the ducting installation - to minimize such bypass. But these seal materials are expensive, add assembly complexity, and have service durability limitations.
  • Another compensating alternative is to overdesign the heat exchanger, either by over-sizing or adding much higher fin density (pressure drop penalty) so that performance is maintained even with bypass flow, which can have other disadvantages.
  • the specification discloses a heat exchanger, containing :
  • each plate pair defines a flow passage for the flow of a first fluid; one or more fins thermally coupled and sandwiched by the spaced-apart plate pairs for flow of a second fluid; a fluid manifold being fluidly coupled to the flow passages of the spaced- apart plate pairs; the heat exchanger having a front face and side faces defined by at least the plurality of spaced-apart plate pairs and the one or more fins; and a bypass seal complementary to the front face or one of the side faces and engagingly coupled to the front face or one of the side faces for blocking a gap between the heat exchanger and a housing for receiving the heat
  • a heat exchanger assembly containing a housing having a cavity in communication with an opening for receiving a heat exchanger; and the heat exchanger as disclosed herein.
  • Figure 1 shows an air intake manifold for receiving a heat exchanger in accordance with the specification
  • Figure 2(a) shows a heat exchanger having a clip-on bypass seal in accordance with a second embodiment of the specification
  • Figures 2(b) and (c) show an alternative clip-on bypass seal attachable to a heat exchanger in accordance with the second embodiment of the specification ;
  • Figure 2(d) shows a sectional view of a heat exchanger with the clip-on bypass seal in accordance with the second embodiment of the
  • Figure 2(e) shows a top view of the heat exchanger in an air-intake manifold in accordance with the second embodiment of the specification
  • Figure 3(a) shows a schematic elevational view of a heat exchanger having a clip-on bypass seal in accordance with one embodiment of the specification ;
  • Figure 3(b) shows a top plan view of the heat exchanger of Figure 3(a);
  • Figure 4 shows the clip-on bypass seal in accordance with one embodiment of the specification for use with a heat exchanger
  • Figure 5 is a perspective view of the air intake manifold having a cut-out within the manifold for receiving the bypass seal present on a heat exchanger;
  • Figure 6(a) shows a heat exchanger having a clip-on bypass seal in accordance with a third embodiment of the specification
  • Figure 6(b) shows an expanded view of clip-on bypass seal used with the heat exchanger in accordance with the third embodiment of the specification ;
  • Figures 7 (a)-(d) shows views of an end section of heat exchanger having a retainer for clipping in place the clip-on bypass seal in accordance with a fourth embodiment of the specification
  • Figures 8 shows a heat exchanger having a brazed-on bypass seal in accordance with a fifth embodiment of the specification
  • Figure 9 shows an expanded view of an end portion of the heat exchanger having the brazed-on seal as shown in Figure 8;
  • Figure 10 shows an embodiment of a seal for use with the heat exchanger shown in Figure 8.
  • Figure 11 another view of the seal shown in Figure 10.
  • the specification generally relates to heat exchanger (2), such as a charge air cooler for reducing the temperature of air inflow to a combustion engine.
  • the heat exchanger (2) is typically placed in an air intake manifold (4), as shown in Figure 1, which has a cavity (6) for placing the heat exchanger (2) through an opening (8).
  • Incoming air enters the manifold (4) through an air intake aperture (10) and passes the heat exchanger (2) before being directed to the combustion engine.
  • the heat exchanger (2) used in accordance with the disclosure is not particularly limited.
  • the heat exchanger (2) has a plurality of spaced-apart plate pairs (12), where each plate pair defines a flow passage for the flow of a first fluid, such as a coolant.
  • a fluid manifold (14) (more clearly seen Figure 6) having an inlet (16) and outlet (18) is also provided; where the fluid manifold (14) is connected to the flow passage of each plate pair (12) to allow fluid, such as the coolant, to enter through the inlet (16) pass through the flow passages of the plate pairs (12) and exit through the outlet (18).
  • the position of the fluid manifold (14) and the inlet (16) and outlet (18) are not particularly limited.
  • the inlet and outlet can be present on a top plate (20). While in another embodiment, as shown in Figure 6, the inlet (16) and outlet (18) can be present on a side face (22) of the heat exchanger (2).
  • each spaced-apart plate pair (12) is provided with a fin (24).
  • the fins (24) can provide for a second fluid flow passage, generally the air entering through the air intake aperture (10); and where the second flow passage is perpendicular to the flow passage defined by the plate pairs (12) to allow for heat exchange.
  • the heat exchanger (2) as disclosed herein has a front face (26) such that when the heat exchanger (2) is positioned in the air intake manifold (4), the front face (26) is positioned at the air intake aperture (10) and allows for the second fluid, the air, to pass through the fins (24) and undergo heat exchange before entering the combustion engine.
  • the heat exchanger (2) as disclosed herein are provided with side faces (22).
  • one of the side faces is formed by the fluid manifold ( 14) while the other side face is formed by the ends of the plate pairs (12) along with the ends of the fins (24).
  • the heat exchanger (2) as disclosed herein, is also provided with a bypass seal (28) that is complementary to the front face (26) or one of the side faces (22) of the heat exchanger.
  • the complementary bypass seal (28) is coupled to the front face (26) or one of the side faces (22) of the heat
  • each seal (28) is complementary to the side face (22) of the heat exchanger (2) to which it is attached.
  • the seals (28) are provided with a heat exchanger engaging face (30) and a sealing face (32). It is the heat exchanger engaging face (30) that is complementary in profile to the side face (22) or the front face (26), whichever it engages.
  • the heat exchanger engaging face (30) is provided with notches (34) ( Figures 3 and 4), such that when the seal engages the side face (22) or the front face (26), the grooves formed by the plate pairs (12) and the fins (24) are blocked. While the sealing face (32) helps to block any gaps between the ends of the heat exchanger (2) and the manifold (4).
  • the sealing face (32) of the bypass seal (28) provides a flat surface. While in another embodiment as shown in Figures 3 and 4, the sealing face (32) is inclined; tapering and becoming narrower as it goes from the top plate (20) towards the bottom of the heat exchanger. For example, in one embodiment, the sealing face (32) is inclined at 1-2°. The angle can help to ensure that the seal (28) does not need to be compressed until the heat exchanger (2) is almost completely inserted in the manifold (4), and hence, assist with installation.
  • the shape and dimension of the heat exchanger engaging face (30) is not particularly limited and would depend upon, among other factors, the particular application and heat exchanger to which the seal (28) is applied to.
  • the notches (34) present on the heat exchanger engaging face (30) can be deeper, while in other case, the notches (34) can be shallow, depending upon the particular application and heat exchanger used.
  • the manifold (4) is provided with a recess (36) that is complementary to the sealing face (32) of the bypass seal (28) to block the gap between the heat exchanger (2) and the manifold (4).
  • the recess (36) is tapered, which can assist in both sealing and mounting of the heat exchanger (2) in the manifold (4).
  • the recess (36) can also assist in retaining the position of the heat exchanger (2) by resisting movement within the manifold.
  • the heat exchanger (2) has a bypass seal (28) positioned on the front face (26) of the heat exchanger (2), as shown, for example in Figures 6-9. In such
  • the seal (28) is also provided with a sealing face (32) and a heat exchanger engaging face (30) that has a profile, which is complementary to the front face (26) of the heat exchanger (2) to which it engages. Further, the seal (28) can be present at an edge (38) of the front face adjacent to the side face (22) of the heat exchanger (2). In the embodiments shown in Figures 6-9, the seal (28) is present at an edge (38), which is adjacent to a side face (22) that has the ends of the plate pairs (12) and the fins (24). However, it would be understood that a second seal (28) can also be provided at the opposing end of the front face (26) of the heat exchanger (2).
  • the manifold (4) can be prepared or appropriately manufactured to accommodate a heat exchanger (2) where the seal (28) is present at the front face (26) of the heat exchanger (2).
  • a similar recess (36), as described above, can also be provided to accommodate the seal (28) present on the front face (26).
  • the method for attaching the seal (28) to the heat exchanger (2) is not particularly, and can depend upon the particular application, among other factors.
  • the seal (28) is frictionally attached to the heat exchanger.
  • the seal (28) is clipped in place and is provided with means for clipping the seal (28) to the heat exchanger (2), as shown in Figure 6.
  • the heat exchanger can be provided with tabs (40) for retaining the seal, as shown in Figure 7.
  • the tabs (40) and the seal (28) can be provided with additional means, such as an arm and a gap for insertion of the arm into the gap, to lock the seal (28) in place.
  • the seal (28) can also be bolted on the heat exchanger (2), as shown in Figures 8- 11.
  • the seal (28) can be brazed-on to the heat exchanger (2).
  • a combination of methods can be used to position the seal (28) with the heat exchanger (2).
  • the material of construction of the seal (28) is not particularly limited and can depend upon the particular application.
  • the seal (28) is made of plastic, such as a thermoplastic.
  • the seal (28) can be made of a similar material as the heat exchanger (2) to allow for brazing of the seal (28) to the heat exchanger (2).
  • a heat exchanger assembly which contains the housing (4) and the heat exchanger (2) as described herein.
  • the entire assembly can be provided and be fitted into an engine for use.
  • the heat exchanger (2) and the manifold (4) can be provided separately.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

A heat exchanger having a plurality of spaced-apart plate pairs, where each plate pair defines a flow passage for the flow of a first fluid. One or more fins are thermally coupled and sandwiched by the spaced-apart plate pairs for flow of a second fluid. A fluid manifold being fluidly coupled to the flow passages of the spaced-apart plate pairs is also provided. The heat exchanger has a front face and side faces defined by at least the plurality of spaced-apart plate pairs and the one or more fins. And, a bypass seal complementary to the front face or one of the side faces and engagingly coupled to the front face or one of the side faces for blocking a gap between the heat exchanger and a housing for receiving the heat exchanger. Also disclosed is a heat exchanger assembly having the heat exchanger disclosed.

Description

HEAT EXCHANGER WITH END SEAL FOR BLOCKING OFF
AIR BYPASS FLOW
FIELD
[0001] The specification relates to a heat exchanger having an air bypass seal, and a heat exchanger assembly having the heat exchanger and the seal.
BACKGROUND
[0002] Charge air cooler heat exchangers are well known in the art for mounting along the flow path of charge air supplied to a combustion engine. This charge air typically comprises ambient air which has been compressed by apparatus such as a supercharger or turbocharger to provide an increased mass flow of air to the engine to permit the engine to combust increased quantities of fuel and thereby operate at an increased level of power and performance.
However, compression of ambient air also elevates the air temperature such that the charge air has a relatively high temperature which, if not reduced, undesirably increases total engine heat load. It is therefore desirable to cool the charge air prior to supply thereof to the engine, and charge air coolers are provided for this purpose.
[0003] In general, the charge air cooler is constructed from a plurality of lightweight heat transfer elements of a heat conductive material, such as copper or aluminum, shaped to provide extended heat transfer surfaces and defining a flow path for the charge air in heat transfer relation with a suitable coolant, such as ambient air or a liquid coolant. More specifically, the charge air cooler may be constructed from a network of finned tubes such that charge air flowing over the fins is associated with a coolant flowing through the tubes resulting in adequate heat transfer for some engine system applications. Alternatively, when improved heat transfer capacity is required, the charge air cooler is constructed from a stacked array of plates and fins which cooperate to define a heat exchanger core having separate flow paths for passage of the charge air and the coolant in close heat transfer relation with each other. In either case, however, the charge air cooler is desirably mounted directly into the intake manifold of the engine wherein charge air passing through the intake manifold is reduced in
temperature by flow through the charge air cooler immediately prior to ingestion by the engine.
[0004] The current heat exchanger products can allow air bypass past the ends of the fins (the plate lap joints extend beyond the end of the fins, or extend beyond the liquid fluid manifold, leaving unintended air bypass channels), or require additional brazed on components to compensate by blocking off these regions, which adds significant cost and/or may be impossible for certain cooler configurations. To address the above problem, wide elastomer seals can be provided, such as adhesively bonded or mechanically trapped seals, as part of the ducting installation - to minimize such bypass. But these seal materials are expensive, add assembly complexity, and have service durability limitations. Another compensating alternative is to overdesign the heat exchanger, either by over-sizing or adding much higher fin density (pressure drop penalty) so that performance is maintained even with bypass flow, which can have other disadvantages.
[0005] There is a need in the art for a heat exchanger and a heat exchanger assembly, where the heat exchanger has a seal that can reduce or prevent air bypass around the ends of the heat exchanger.
SUMMARY OF THE INVENTION
[0006] In one aspect, the specification discloses a heat exchanger, containing :
a plurality of spaced-apart plate pairs, where each plate pair defines a flow passage for the flow of a first fluid; one or more fins thermally coupled and sandwiched by the spaced-apart plate pairs for flow of a second fluid; a fluid manifold being fluidly coupled to the flow passages of the spaced- apart plate pairs; the heat exchanger having a front face and side faces defined by at least the plurality of spaced-apart plate pairs and the one or more fins; and a bypass seal complementary to the front face or one of the side faces and engagingly coupled to the front face or one of the side faces for blocking a gap between the heat exchanger and a housing for receiving the heat
exchanger.
[0007] In another aspect, disclosed is a heat exchanger assembly containing a housing having a cavity in communication with an opening for receiving a heat exchanger; and the heat exchanger as disclosed herein.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] Reference will now be made, by way of example, to the
accompanying drawings which show example embodiments of the present application, and in which :
[0009] Figure 1 shows an air intake manifold for receiving a heat exchanger in accordance with the specification;
[0010] Figure 2(a) shows a heat exchanger having a clip-on bypass seal in accordance with a second embodiment of the specification;
[0011] Figures 2(b) and (c) show an alternative clip-on bypass seal attachable to a heat exchanger in accordance with the second embodiment of the specification ;
[0012] Figure 2(d) shows a sectional view of a heat exchanger with the clip-on bypass seal in accordance with the second embodiment of the
specification in an air intake manifold;
[0013] Figure 2(e) shows a top view of the heat exchanger in an air-intake manifold in accordance with the second embodiment of the specification;
[0014] Figure 3(a) shows a schematic elevational view of a heat exchanger having a clip-on bypass seal in accordance with one embodiment of the specification ; [0015] Figure 3(b) shows a top plan view of the heat exchanger of Figure 3(a);
[0016] Figure 4 shows the clip-on bypass seal in accordance with one embodiment of the specification for use with a heat exchanger;
[0017] Figure 5 is a perspective view of the air intake manifold having a cut-out within the manifold for receiving the bypass seal present on a heat exchanger;
[0018] Figure 6(a) shows a heat exchanger having a clip-on bypass seal in accordance with a third embodiment of the specification;
[0019] Figure 6(b) shows an expanded view of clip-on bypass seal used with the heat exchanger in accordance with the third embodiment of the specification ;
[0020] Figures 7 (a)-(d) shows views of an end section of heat exchanger having a retainer for clipping in place the clip-on bypass seal in accordance with a fourth embodiment of the specification;
[0021] Figures 8 shows a heat exchanger having a brazed-on bypass seal in accordance with a fifth embodiment of the specification;
[0022] Figure 9 shows an expanded view of an end portion of the heat exchanger having the brazed-on seal as shown in Figure 8;
[0023] Figure 10 shows an embodiment of a seal for use with the heat exchanger shown in Figure 8; and
[0024] Figure 11 another view of the seal shown in Figure 10.
[0025] Similar reference numerals may have been used in different figures to denote similar components.
DESCRIPTION
[0026] The specification generally relates to heat exchanger (2), such as a charge air cooler for reducing the temperature of air inflow to a combustion engine. [0027] The heat exchanger (2) is typically placed in an air intake manifold (4), as shown in Figure 1, which has a cavity (6) for placing the heat exchanger (2) through an opening (8). Incoming air enters the manifold (4) through an air intake aperture (10) and passes the heat exchanger (2) before being directed to the combustion engine.
[0028] The heat exchanger (2) used in accordance with the disclosure is not particularly limited. In one example embodiment, as shown in Figure 2a, the heat exchanger (2) has a plurality of spaced-apart plate pairs (12), where each plate pair defines a flow passage for the flow of a first fluid, such as a coolant. A fluid manifold (14) (more clearly seen Figure 6) having an inlet (16) and outlet (18) is also provided; where the fluid manifold (14) is connected to the flow passage of each plate pair (12) to allow fluid, such as the coolant, to enter through the inlet (16) pass through the flow passages of the plate pairs (12) and exit through the outlet (18). The position of the fluid manifold (14) and the inlet (16) and outlet (18) are not particularly limited. In one embodiment, as shown in Figure 2(a), the inlet and outlet can be present on a top plate (20). While in another embodiment, as shown in Figure 6, the inlet (16) and outlet (18) can be present on a side face (22) of the heat exchanger (2).
[0029] The space between each spaced-apart plate pair (12) is provided with a fin (24). The fins (24) can provide for a second fluid flow passage, generally the air entering through the air intake aperture (10); and where the second flow passage is perpendicular to the flow passage defined by the plate pairs (12) to allow for heat exchange.
[0030] The heat exchanger (2) as disclosed herein, has a front face (26) such that when the heat exchanger (2) is positioned in the air intake manifold (4), the front face (26) is positioned at the air intake aperture (10) and allows for the second fluid, the air, to pass through the fins (24) and undergo heat exchange before entering the combustion engine.
[0031] In addition, the heat exchanger (2) as disclosed herein, are provided with side faces (22). In the embodiment shown in figure 6a, one of the side faces is formed by the fluid manifold ( 14) while the other side face is formed by the ends of the plate pairs (12) along with the ends of the fins (24).
[0032] The heat exchanger (2), as disclosed herein, is also provided with a bypass seal (28) that is complementary to the front face (26) or one of the side faces (22) of the heat exchanger. The complementary bypass seal (28) is coupled to the front face (26) or one of the side faces (22) of the heat
exchanger to block a gap that can be present between the heat exchanger (2) and the inside of a housing, such as the air intake manifold (4). This can help to prevent air bypass along the side faces (22) of the heat exchanger (2) and improve the overall efficiency of heat exchange.
[0033] In the embodiments shown in Figures 2 and 4, two bypass seals (28) are used, with each seal (28) being complementary to the side face (22) of the heat exchanger (2) to which it is attached. The seals (28) are provided with a heat exchanger engaging face (30) and a sealing face (32). It is the heat exchanger engaging face (30) that is complementary in profile to the side face (22) or the front face (26), whichever it engages. In one embodiment, the heat exchanger engaging face (30) is provided with notches (34) (Figures 3 and 4), such that when the seal engages the side face (22) or the front face (26), the grooves formed by the plate pairs (12) and the fins (24) are blocked. While the sealing face (32) helps to block any gaps between the ends of the heat exchanger (2) and the manifold (4).
[0034] The exact shape and dimensions of the seal (28) used in
accordance with the heat exchanger (2) disclosed are not particularly limited. In one embodiment as shown in Figure 2, the sealing face (32) of the bypass seal (28) provides a flat surface. While in another embodiment as shown in Figures 3 and 4, the sealing face (32) is inclined; tapering and becoming narrower as it goes from the top plate (20) towards the bottom of the heat exchanger. For example, in one embodiment, the sealing face (32) is inclined at 1-2°. The angle can help to ensure that the seal (28) does not need to be compressed until the heat exchanger (2) is almost completely inserted in the manifold (4), and hence, assist with installation. [0035] Similarly, the shape and dimension of the heat exchanger engaging face (30) is not particularly limited and would depend upon, among other factors, the particular application and heat exchanger to which the seal (28) is applied to. In the embodiment shown in Figures 3 and 4, the notches (34) present on the heat exchanger engaging face (30) can be deeper, while in other case, the notches (34) can be shallow, depending upon the particular application and heat exchanger used.
[0036] In one embodiment as shown in Figure 5, the manifold (4) is provided with a recess (36) that is complementary to the sealing face (32) of the bypass seal (28) to block the gap between the heat exchanger (2) and the manifold (4). In the embodiment of Figure 5, the recess (36) is tapered, which can assist in both sealing and mounting of the heat exchanger (2) in the manifold (4). In addition, the recess (36) can also assist in retaining the position of the heat exchanger (2) by resisting movement within the manifold. [0037] In further embodiments in accordance with the description, the heat exchanger (2) has a bypass seal (28) positioned on the front face (26) of the heat exchanger (2), as shown, for example in Figures 6-9. In such
embodiments, and as described previously, the seal (28) is also provided with a sealing face (32) and a heat exchanger engaging face (30) that has a profile, which is complementary to the front face (26) of the heat exchanger (2) to which it engages. Further, the seal (28) can be present at an edge (38) of the front face adjacent to the side face (22) of the heat exchanger (2). In the embodiments shown in Figures 6-9, the seal (28) is present at an edge (38), which is adjacent to a side face (22) that has the ends of the plate pairs (12) and the fins (24). However, it would be understood that a second seal (28) can also be provided at the opposing end of the front face (26) of the heat exchanger (2).
[0038] The manifold (4) can be prepared or appropriately manufactured to accommodate a heat exchanger (2) where the seal (28) is present at the front face (26) of the heat exchanger (2). A similar recess (36), as described above, can also be provided to accommodate the seal (28) present on the front face (26).
[0039] The method for attaching the seal (28) to the heat exchanger (2) is not particularly, and can depend upon the particular application, among other factors. In one embodiment, the seal (28) is frictionally attached to the heat exchanger. In another embodiment, the seal (28) is clipped in place and is provided with means for clipping the seal (28) to the heat exchanger (2), as shown in Figure 6. In a further embodiment, the heat exchanger can be provided with tabs (40) for retaining the seal, as shown in Figure 7. The tabs (40) and the seal (28) can be provided with additional means, such as an arm and a gap for insertion of the arm into the gap, to lock the seal (28) in place. Alternatively, the seal (28) can also be bolted on the heat exchanger (2), as shown in Figures 8- 11. In a still further embodiment, the seal (28) can be brazed-on to the heat exchanger (2). Moreover, a combination of methods can be used to position the seal (28) with the heat exchanger (2).
[0040] The material of construction of the seal (28) is not particularly limited and can depend upon the particular application. In one embodiment, for example and without limitation, the seal (28) is made of plastic, such as a thermoplastic. While in another embodiment, the seal (28) can be made of a similar material as the heat exchanger (2) to allow for brazing of the seal (28) to the heat exchanger (2).
[0041] In another aspect in accordance with the description, a heat exchanger assembly is provided, which contains the housing (4) and the heat exchanger (2) as described herein. The entire assembly can be provided and be fitted into an engine for use. Alternatively, the heat exchanger (2) and the manifold (4) can be provided separately.
[0042] Certain adaptations and modifications of the described
embodiments can be made. Therefore, the above discussed embodiments are considered to be illustrative and not restrictive.

Claims

WHAT IS CLAIMED IS :
A heat exchanger, comprising : a plurality of spaced-apart plate pairs, where each plate pair defines a flow passage for the flow of a first fluid; one or more fins thermally coupled and sandwiched by the spaced-apart plate pairs for flow of a second fluid; a fluid manifold being fluidly coupled to the flow passages of the spaced- apart plate pairs; the heat exchanger having a front face and side faces defined by at least the plurality of spaced-apart plate pairs and the one or more fins; and a bypass seal complementary to the front face or one of the side faces and engagingly coupled to the front face or one of the side faces for blocking a gap between the heat exchanger and a housing for receiving the heat exchanger.
The heat exchanger according to claim 1, wherein the bypass seal is complementary to one of the side faces and engagingly couples to the one of the side faces of the heat exchanger.
The heat exchanger according to claim 2, wherein the bypass seal is present on both side faces of the heat exchanger.
The heat exchanger according to any one of claims 1 to 3, wherein the seal has a heat exchanger engaging face and a sealing face, the heat exchanger engaging face having notches for receiving ends of the plurality of the spaced-apart plate pairs. 5. The heat exchanger according to claim 4, wherein the sealing face permits mounting of the heat exchanger in the housing.
6. The heat exchanger according to claim 4, wherein the sealing face is tapered for slidingly mounting into a recess in the housing.
7. The heat exchanger according to claim 1, wherein the bypass seal is
complementary to the front face and engagingly couples to the front face of the heat exchanger.
8. The heat exchanger according to claim 1, wherein the bypass seal is
complementary to the front face and positioned at an edge of the front face adjacent to one of the side faces of the heat exchanger.
9. The heat exchanger according to any one of claims 1 to 8, further
comprising a tab for coupling the seal to the heat exchanger.
10. The heat exchanger according to any one of claims 1 to 9, wherein the seal is clipped-on the heat exchanger.
11. The heat exchanger according to any one of claims 1 to 9, wherein the seal is brazed, bolted or brazed and bolted on the heat exchanger.
12. A heat exchanger assembly, comprising : a housing having a cavity in communication with an opening; and a heat exchanger receivable in the cavity of the housing, the heat exchanger comprising : a plurality of spaced-apart plate pairs, where each plate pair defines a flow passage for the flow of a first fluid; one or more fins thermally coupled and sandwiched by the spaced- apart plate pairs for flow of a second fluid; a fluid manifold being fluidly coupled to the flow passages of the spaced-apart plate pairs; the heat exchanger having a front face and side faces defined by at least the plurality of spaced-apart plate pairs and the one or more fins; and a bypass seal complementary to the front face or one of the side faces and engagingly coupled to the front face or one of the side faces for blocking a gap between the heat exchanger and the housing.
13. The heat exchanger assembly according to claim 12, wherein the bypass seal is complementary to one of the side faces and engagingly couples to the one of the side faces of the heat exchanger.
14. The heat exchanger assembly according to claim 12 or 13, wherein the seal has a heat exchanger engaging face and a sealing face, the heat exchanger engaging face having notches for receiving ends of the plurality of the spaced-apart plate pairs.
15. The heat exchanger assembly according to claim 14, wherein the sealing face permits mounting of the heat exchanger in the housing.
16. The heat exchanger assembly according to claim 14, wherein the sealing face is tapered for slidingly mounting into a recess in the housing.
17. The heat exchanger assembly according to claim 12, wherein the bypass seal is complementary to the front face and engagingly couples to the front face of the heat exchanger at an edge of the front face adjacent to one of the side faces of the heat exchanger.
18. The heat exchanger assembly according to any one of claims 12 to 17, further comprising a tab for coupling the seal to the heat exchanger.
19. The heat exchanger assembly according to any one of claims 12 to 18, wherein the seal is clipped-on the heat exchanger.
20. The heat exchanger assembly according to any one of claims 12 to 18, wherein the seal is brazed, bolted or brazed and bolted on the heat exchanger.
PCT/CA2011/050740 2011-11-28 2011-11-28 Heat exchanger with end seal for blocking off air bypass flow WO2013078531A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
DE112011105882.9T DE112011105882T5 (en) 2011-11-28 2011-11-28 End-seal heat exchanger for blocking an air bypass flow
CA2857084A CA2857084A1 (en) 2011-11-28 2011-11-28 Heat exchanger with end seal for blocking off air bypass flow
GB1409186.2A GB2512218A (en) 2011-11-28 2011-11-28 Heat exchanger with end seal for blocking off air bypass flow
PCT/CA2011/050740 WO2013078531A1 (en) 2011-11-28 2011-11-28 Heat exchanger with end seal for blocking off air bypass flow
CN201180075107.7A CN103959002B (en) 2011-11-28 2011-11-28 There is the heat exchanger of end seal for blocking air bypass flow

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CA2011/050740 WO2013078531A1 (en) 2011-11-28 2011-11-28 Heat exchanger with end seal for blocking off air bypass flow

Publications (1)

Publication Number Publication Date
WO2013078531A1 true WO2013078531A1 (en) 2013-06-06

Family

ID=48534551

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CA2011/050740 WO2013078531A1 (en) 2011-11-28 2011-11-28 Heat exchanger with end seal for blocking off air bypass flow

Country Status (5)

Country Link
CN (1) CN103959002B (en)
CA (1) CA2857084A1 (en)
DE (1) DE112011105882T5 (en)
GB (1) GB2512218A (en)
WO (1) WO2013078531A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015149951A1 (en) * 2014-04-04 2015-10-08 Valeo Systemes Thermiques Heat exchanger for a motor vehicle
WO2015149949A1 (en) * 2014-04-04 2015-10-08 Valeo Systemes Thermiques Heat exchanger for a motor vehicle
US9671168B2 (en) 2013-09-11 2017-06-06 Modine Manufacturing Company Heat exchanger arrangement and production method
JP2018059705A (en) * 2016-09-30 2018-04-12 ハンオン システムズ Heat exchanger
JP2020516846A (en) * 2017-04-14 2020-06-11 ヴァレオ、オートシステミ、エスピー.ゼット.オー.オー.Valeo Autosystemy Sp.Z.O.O. Heat exchanger for motor vehicles

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016049776A1 (en) * 2014-10-03 2016-04-07 Dana Canada Corporation Heat exchanger with self-retaining bypass seal
DE102016011254A1 (en) 2016-09-20 2018-03-22 Modine Manufacturing Company Bypass blocking device for heat exchangers
DE102017000183A1 (en) * 2017-01-12 2018-07-12 Modine Manufacturing Company Guiding / steering device for heat exchangers flowing through fluid streams
DE102017125394A1 (en) * 2017-10-30 2019-05-02 Deutsches Zentrum für Luft- und Raumfahrt e.V. Heat transfer device, use and tool
WO2020161727A1 (en) * 2019-02-05 2020-08-13 Pranav Vikas India Pvt Limited Universal heat exchanger

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2903543A1 (en) * 1979-01-31 1980-08-07 Daimler Benz Ag Water cooled vehicle oil cooler - has end water entries and bottom oil entries with tube bundle units between
US4303052A (en) * 1980-03-24 1981-12-01 The Garrett Corporation Charge air cooler mounting arrangement
EP0492047A1 (en) * 1990-12-20 1992-07-01 KÜHLERFABRIK LÄNGERER & REICH GmbH & Co. KG. Oil cooler
US20080185136A1 (en) * 2007-02-07 2008-08-07 Vastine Gerard W Heat exchanger with bypass seal

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3322778B2 (en) * 1995-08-22 2002-09-09 東芝キヤリア株式会社 Outdoor unit of air conditioner
DE102004013682A1 (en) * 2003-03-26 2004-12-16 Behr Industrietechnik Gmbh & Co. Kg Heat-exchange air/air cooler has first flow channels connected on inlet and outlet side to collection containers on block, and fins in second flow channels
US8225852B2 (en) * 2008-04-30 2012-07-24 Dana Canada Corporation Heat exchanger using air and liquid as coolants

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2903543A1 (en) * 1979-01-31 1980-08-07 Daimler Benz Ag Water cooled vehicle oil cooler - has end water entries and bottom oil entries with tube bundle units between
US4303052A (en) * 1980-03-24 1981-12-01 The Garrett Corporation Charge air cooler mounting arrangement
EP0492047A1 (en) * 1990-12-20 1992-07-01 KÜHLERFABRIK LÄNGERER & REICH GmbH & Co. KG. Oil cooler
US20080185136A1 (en) * 2007-02-07 2008-08-07 Vastine Gerard W Heat exchanger with bypass seal

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9671168B2 (en) 2013-09-11 2017-06-06 Modine Manufacturing Company Heat exchanger arrangement and production method
WO2015149951A1 (en) * 2014-04-04 2015-10-08 Valeo Systemes Thermiques Heat exchanger for a motor vehicle
WO2015149949A1 (en) * 2014-04-04 2015-10-08 Valeo Systemes Thermiques Heat exchanger for a motor vehicle
FR3019638A1 (en) * 2014-04-04 2015-10-09 Valeo Systemes Thermiques HEAT EXCHANGER FOR MOTOR VEHICLE
FR3019639A1 (en) * 2014-04-04 2015-10-09 Valeo Systemes Thermiques HEAT EXCHANGER FOR MOTOR VEHICLE
CN106414944A (en) * 2014-04-04 2017-02-15 法雷奥热系统公司 Heat exchanger for a motor vehicle
JP2017511460A (en) * 2014-04-04 2017-04-20 ヴァレオ システム テルミク Heat exchanger for motor vehicles
JP2017516051A (en) * 2014-04-04 2017-06-15 ヴァレオ システム テルミク Heat exchanger for motor vehicles
KR101906698B1 (en) * 2014-04-04 2018-10-10 발레오 시스템므 떼르미끄 Heat exchanger for a motor vehicle
CN106414944B (en) * 2014-04-04 2019-11-19 法雷奥热系统公司 Heat exchanger for motor vehicles
JP2018059705A (en) * 2016-09-30 2018-04-12 ハンオン システムズ Heat exchanger
JP2020516846A (en) * 2017-04-14 2020-06-11 ヴァレオ、オートシステミ、エスピー.ゼット.オー.オー.Valeo Autosystemy Sp.Z.O.O. Heat exchanger for motor vehicles

Also Published As

Publication number Publication date
GB2512218A (en) 2014-09-24
CA2857084A1 (en) 2013-06-06
DE112011105882T5 (en) 2014-10-02
CN103959002A (en) 2014-07-30
CN103959002B (en) 2016-10-12
GB201409186D0 (en) 2014-07-09

Similar Documents

Publication Publication Date Title
WO2013078531A1 (en) Heat exchanger with end seal for blocking off air bypass flow
US20130133869A1 (en) Heat Exchanger With End Seal For Blocking Off Air Bypass Flow
US20130133866A1 (en) Heat Exchanger Plates with Integral Bypass Blocking Tabs
KR101341469B1 (en) Egr cooler with dual coolant loop
CN102213554B (en) Heat exchanger and manufacture method thereof
EP2766687B1 (en) Stacked plate exhaust gas recovery device
US10619946B2 (en) Heat exchanger for cooling a flow of compressed air using a liquid coolant
US8695574B2 (en) Intake manifold having an integrated charge air cooler
CA2857079A1 (en) Heat exchanger plates with integral bypass blocking tabs
CN108369078B (en) Heat exchanger
US9920686B2 (en) Water-cooled charge air cooler with integrated multi-stage cooling
US11274884B2 (en) Heat exchanger module with an adapter module for direct mounting to a vehicle component
CN108603729A (en) Heat exchanger and core for heat exchanger
US20180128555A1 (en) Heat exchanger having bypass seal with retention clip
US10151231B2 (en) Manifold integrated intercooler with structural core
KR101777027B1 (en) Internal degas feature for plate-fin heat exchangers
US10337801B2 (en) Heat exchanger for cooling a flow of charge air, and method of assembling the same
US20140338873A1 (en) Stacked-Plate Heat Exchanger Including A Collector
US9551274B2 (en) Heat exchanger for cooling charge air
KR20190022308A (en) Housing and core assembly for plate fin heat exchangers
US20080185136A1 (en) Heat exchanger with bypass seal
US11156406B2 (en) Heat exchanger
KR100389699B1 (en) Water Cooling Heat Exchanger
CN109519272B (en) Intercooler and chip thereof
EP4166767B1 (en) A heat exchanger

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 11876761

Country of ref document: EP

Kind code of ref document: A1

ENP Entry into the national phase

Ref document number: 1409186

Country of ref document: GB

Kind code of ref document: A

Free format text: PCT FILING DATE = 20111128

WWE Wipo information: entry into national phase

Ref document number: 1409186.2

Country of ref document: GB

ENP Entry into the national phase

Ref document number: 2857084

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 1120111058829

Country of ref document: DE

Ref document number: 112011105882

Country of ref document: DE

122 Ep: pct application non-entry in european phase

Ref document number: 11876761

Country of ref document: EP

Kind code of ref document: A1