US20160201998A1 - Frameless cooling module - Google Patents

Frameless cooling module Download PDF

Info

Publication number
US20160201998A1
US20160201998A1 US15/075,362 US201615075362A US2016201998A1 US 20160201998 A1 US20160201998 A1 US 20160201998A1 US 201615075362 A US201615075362 A US 201615075362A US 2016201998 A1 US2016201998 A1 US 2016201998A1
Authority
US
United States
Prior art keywords
core
plate
heat exchanger
core units
bend
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US15/075,362
Inventor
Joseph L. Kennedy
Neil A. Terry
Mahesh K. Mokire
Bradley Wrage
Deepak B. Thakkar
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.)
Caterpillar Inc
Original Assignee
Caterpillar Inc
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 Caterpillar Inc filed Critical Caterpillar Inc
Priority to US15/075,362 priority Critical patent/US20160201998A1/en
Assigned to CATERPILLAR INC. reassignment CATERPILLAR INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: KENNEDY, JOSEPH L., MOKIRE, MAHESH K., TERRY, NEIL A., THAKKAR, DEEPAK B., WRAGE, BRADLEY
Publication of US20160201998A1 publication Critical patent/US20160201998A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • 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
    • F28F9/001Casings in the form of plate-like arrangements; Frames enclosing a heat exchange core
    • 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
    • F28F9/007Auxiliary supports for elements
    • F28F9/0075Supports for plates or plate assemblies
    • 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
    • F28D1/0408Multi-circuit heat exchangers, e.g. integrating different heat exchange sections in the same unit or heat exchangers for more than two fluids
    • F28D1/0426Multi-circuit heat exchangers, e.g. integrating different heat exchange sections in the same unit or heat exchangers for more than two fluids with units having particular arrangement relative to the large body of fluid, e.g. with interleaved units or with adjacent heat exchange units in common air flow or with units extending at an angle to each other or with units arranged around a central element
    • F28D1/0443Combination of units extending one beside or one above the other
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • 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
    • 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
    • F28F9/001Casings in the form of plate-like arrangements; Frames enclosing a heat exchange core
    • F28F2009/004Common frame elements for multiple cores
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2240/00Spacing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2265/00Safety or protection arrangements; Arrangements for preventing malfunction
    • F28F2265/26Safety or protection arrangements; Arrangements for preventing malfunction for allowing differential expansion between elements
    • 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
    • F28F2280/06Adapter frames, e.g. for mounting heat exchanger cores on other structure and for allowing fluidic connections

Definitions

  • the present disclosure relates to heat exchangers and more specifically, to an assembly of heat exchangers.
  • Heat exchangers are utilized across various machines for exchanging heat.
  • the heat exchangers include multiple tubes having an outlet port, and an inlet port.
  • the heat exchangers include fins on the outer surface of the tubes. As fluid flows through the tubes, the heat is dissipated away into ambient air with the help of fins.
  • cores of the heat exchangers exhibit thermal expansion/contraction in all directions.
  • the heat exchangers are mounted within a rigid framed structure.
  • the framed structure utilizes various types of isolators that are able to compress to account for the thermal expansion/contraction of the cores.
  • the framed structure is expensive due to cost of frames and the isolators.
  • frameless designs are also known for mounting the cores of the heat exchangers. The frameless designs are cheaper, but uneven rates of expansion of the cores reduces overall thermal life. Further, there are also challenges in controlling uneven expansion of the cores. Therefore, there is a need for packaging or assembly of such frameless heat exchangers to accommodate the uneven expansion of the cores.
  • U.S. Pat. No. 6,523,603 discloses a double heat exchanger.
  • the double heat exchanger includes a multi-core radiator which consists of a condenser and a radiator for heat dissipation. Further, a connecting member is provided with a slit and a wavy shaped flexible member, As the condenser and the radiator begin to heat, expansion and contraction of the flexible member allows the thermal expansion within the frame,
  • '603 reference fails to provide a cheaper and easily fabricable solution for controlling uneven expansion of the core units. Therefore, there is a need for a cost effective plate to accommodate uneven expansion of the core units of the heat exchangers.
  • a heat exchanger adapted to be coupled with a platform.
  • the heat exchanger comprises two or more core units having an upper surface and a lower surface, the lower surface of each core unit being fixed to the platform.
  • the heat exchanger further includes a plate disposed along the upper surface of the core units, the plate having a plurality of bend enhancement regions and a plurality of holes, each bend enhancement region being placed at a predetermined distance from the nearest adjacent holes, and a plurality of spacers interposed between the plate and the upper surface to couple the plate to the upper surface, the plurality of spacers adapted to provide offset between the plate from the core units.
  • each bend enhancement region is configured to facilitate flexibility of the plate to accommodate any uneven expansion of the two or more core units.
  • FIG. 1 is a perspective view of a heat exchanger having east two core units and a plate mounted on an upper surface of the at least two core units, in accordance with the concepts of the present disclosure
  • FIG. 2 is a perspective view of the plate of FIG. 1 , in accordance with the concepts of the present disclosure
  • FIG. 3 is a top view of the plate of FIG. 1 , in accordance with the concepts of the present disclosure
  • FIG. 4 is a front view of the heat exchanger of FIG. 1 with the plate mounted on the upper surface of the core units in a first configuration, in accordance with the concepts of the present disclosure.
  • FIG. 5 is a front view of the heat exchanger of FIG. 1 with the plate mounted on the upper surface of the core units in a second configuration, in accordance with the concepts of the present disclosure.
  • a heat exchanger 10 is shown without specific reference to one or more outlet ports and one or more inlet ports for coolant, and a plurality of fins coupled to outer surface of a plurality of tubes.
  • the heat exchanger 10 can include one or more cores 28 , 30 and/or 32 forming a core assembly 20 , and a plate 12 disposed along an upper surface 22 of the core assembly 20 and a platform 26 disposed along a lower surface 24 of the core assembly 20 .
  • the plate 12 may be disposed along the lower surface 24 and the platform 26 may be disposed along the upper surface 22 .
  • the plate 12 may be disposed offset at a distance from the upper surface 22 to define a spacing therebetween.
  • a plurality of spacers 16 can be interposed between a second surface 38 of the plate 12 and the upper surface 22 .
  • a plurality of fasteners 14 can be used to couple the plate 12 to the core assembly 20 . As shown in FIG. 1 , the fasteners 14 can be integrated with the locations of the spacers 16 , so that the fastener 14 is extended through a hole formed into the plate 12 , is extended through a corresponding spacer 16 , and terminated into the core assembly 20 .
  • the plate 12 may also include a plurality of bend enhancement regions 18 , as will be discussed.
  • the core assembly 20 may include one or more cores, such, for example, shown: a first core 28 (also called a first core unit), a second core 30 (also called a second core unit) and a third core 32 (also called a third core unit).
  • the core assembly 20 may include oil cooling core, turbo compressed air core, engine coolant core, among others and other components, such as inlets, outlets, fins (not shown in FIG. 1 ). It will be apparent to one skilled in the art that the heat exchanger 10 may have any other configuration or have more number of cores without departing from the meaning and scope of the disclosure.
  • the lower surface 24 of the core assembly 20 can be coupled to the platform 26 .
  • the platform 26 is fixedly secured to the lower surface 24 of the core assembly 20 or lower surface 24 of each of the cores 28 , 30 or 32 .
  • the platform 26 is utilized for mounting onto a machine, a vehicle frame or any other implement which requires the heat exchanger 10 .
  • the spacers 16 are provided for preventing interference between the plate 12 and the core assembly 20 . During thermal expansion, the spacers 16 are adapted to provide offset between the core assembly 20 and the plate 12 . It will be apparent to one skilled in the art that the spacers 16 may be of different shapes, configuration and material, but not limited to steel, stainless steel, iron, copper, among others.
  • the spacers 16 may be separate components or may be a part of the core assembly 20 without departing from the meaning and scope of the disclosure.
  • the spacers 16 are inboard on the first core 28 , the second core 30 , and the third core 32 to reduce the overall stiffness of the plate 12 . As a result, thermal stress is reduced as the first core 28 , the second core 30 , the third core 32 expand or contract.
  • various other components of the heat exchanger 10 are not labeled in FIG. 1 .
  • the plate 12 can have a plurality of holes 34 formed therein.
  • the plate 12 includes a first surface 36 , the second surface 38 , a first edge 40 , a second edge 42 , a third edge 44 and a fourth edge 46 .
  • the plate 12 may have a predetermined width W defined as the distance between the first and second edges 40 , 42 , a predetermined thickness T defined as the distance between the first and the second surfaces 36 , 38 , and a predetermined length L defined as the distance between the third and fourth edges 44 , 46 . It will be apparent to one skilled in the art that the predetermined width W, the predetermined thickness T, and the predetermined length L are defined as per the design requirements and may also he varied without departing from the meaning and scope of the disclosure.
  • the bend enhancement regions 18 are positioned at a predetermined distance ‘D’ from holes 34 that are the nearest adjacent thereto, generally each along a line X-X′. It will be apparent to one skilled in the art that the predetermined distance D is defined as per the design requirements (shown in FIG. 1 ) and may also be varied without departing from the meaning and scope of the disclosure.
  • the plate 12 is constructed from materials that include, but is not limit to, steel, stainless steel, copper, among others.
  • the bend enhancement regions 18 is defined as a region within the plate 12 at which a portion of material is removed or added to facilitate relative movement or flexing along the line X-X′ along with the region is formed at a predetermined location.
  • This predetermined location for flexing of the plate 12 is generally located to overlap the outer boundary of the core unit, i.e. the first core 28 , the second core 30 and/or the third core 32 .
  • the predetermined location can he positioned along the lateral space or boundary between adjacent core units so as not to overlap the outer boundary of the core unit, i.e. the first core 28 , the second core 30 and/or the third core 32 .
  • the bend enhancement region 18 facilitates in modifying the surface area of the plate 12 and adding flexibility around the line X-X′, that typically extends between the first and second edges 40 , 42 or along the third and fourth edges 44 , 46 .
  • the bend enhancement region 18 has a predetermined shape in form of a series of scallops or ovalic shapes removed from the plate, in other examples, this region can be perforated or material removed having rounded, rectangular or other shapes. It will he apparent to one skilled in the art that the bend enhancement regions 18 may have any other suitable shape, depth variation, and patterns around the plate 12 that allows flexibility to the plate 12 without departing from the meaning and scope of the disclosure.
  • the holes 34 are adapted to receive the fasteners 14 (as shown in FIG. 1 ) for attaching the plate 12 to the core assembly 20 (as shown in FIG. 1 ).
  • fasteners 14 may be other kind of fasteners, such as bolts, screws, among others without departing from the meaning and scope of the disclosure.
  • fasteners 14 may be constructed of materials includes, but not limited to, steel, stainless steel, iron, copper, among others.
  • the plate 12 is mounted on the first core 28 , the second core 30 , and the third core 32 via the fasteners 14 .
  • the plate 12 is mounted on the upper surface 22 (as shown in FIG. 1 ) of the first core 28 , the second core 30 and the third core 32 .
  • the plate 12 is mounted on the first core 28 , the second core 30 and the third core 32 a first configuration.
  • the first core 28 , and the third core 32 are in a cold state, while the second core 30 is in a hot state.
  • prolonged thermal exposure causes the second core 30 to expand.
  • the plate 12 bends or flexes around the line X-X′ of the bend enhancement regions 18 .
  • the bend enhancement regions 18 are at the predetermined distance D from the spacers 16 or the fasteners 14 .
  • the plate 12 is mounted on the first core 28 , the second core 30 and the third core 32 in a second configuration.
  • the first core 28 , and the third core 32 are in a hot state, while the second core 30 is in a cold state.
  • prolonged thermal exposure causes the first core 28 and the third core 32 to expand.
  • the plate 12 bends around the line X-X′ of the bend enhancement regions 18 .
  • the bend enhancement regions 18 are at the predetermined distance D from the number of spacers 16 or the fasteners 14 .
  • the plate 12 having the bend enhancement regions 18 that offer flexibility to the plate 12 to accommodate any uneven expansion of the first core 28 , the second core 30 and the third core 32 .
  • the plate 12 is made from a sheet metal that is manufactured easily and mounted within any frameless configuration without requiring a complete dismantling of the core assembly 20 . As a result, the maintenance cost and machine down time is reduced.
  • the plate 12 is light weight, and easily fabricable.
  • the plate 12 flexes as per the expansion rates of the first core 28 and the third core 32 ,
  • the flexibility is obtained by bending the plates at the line X-X′.
  • the bend enhancement regions 18 are subjected to a tensile load along the first edge 40 , which causes a deformation in the shape of the bend enhancement regions 18 while providing the bend along the line X-X′ in the plate 12 .

Landscapes

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

Abstract

A heat exchanger adapted to be coupled with a platform is disclosed. The heat exchanger comprises two or more core units having an upper surface and a lower surface, the lower surface of each core unit being fixed to the platform. The heat exchanger further includes a plate disposed along the upper surface of the core units, the plate having a plurality of bend enhancement regions and a plurality of holes, each bend enhancement region being placed at a predetermined distance from the nearest adjacent holes, and a plurality of spacers interposed between the plate and the upper surface to couple the plate to the upper surface, the plurality of spacers adapted to provide offset between the plate from the core units. During operation of the heat exchanger, each bend enhancement region is configured to facilitate flexibility of the plate to accommodate any uneven expansion of the core units.

Description

    TECHNICAL FIELD
  • The present disclosure relates to heat exchangers and more specifically, to an assembly of heat exchangers.
  • BACKGROUND
  • Heat exchangers are utilized across various machines for exchanging heat. The heat exchangers include multiple tubes having an outlet port, and an inlet port. The heat exchangers include fins on the outer surface of the tubes. As fluid flows through the tubes, the heat is dissipated away into ambient air with the help of fins.
  • Due to prolonged heat dissipation, cores of the heat exchangers exhibit thermal expansion/contraction in all directions. Currently, the heat exchangers are mounted within a rigid framed structure. The framed structure utilizes various types of isolators that are able to compress to account for the thermal expansion/contraction of the cores. However, the framed structure is expensive due to cost of frames and the isolators. Moreover, frameless designs are also known for mounting the cores of the heat exchangers. The frameless designs are cheaper, but uneven rates of expansion of the cores reduces overall thermal life. Further, there are also challenges in controlling uneven expansion of the cores. Therefore, there is a need for packaging or assembly of such frameless heat exchangers to accommodate the uneven expansion of the cores.
  • U.S. Pat. No. 6,523,603 (hereinafter referred to as '603) discloses a double heat exchanger. The double heat exchanger includes a multi-core radiator which consists of a condenser and a radiator for heat dissipation. Further, a connecting member is provided with a slit and a wavy shaped flexible member, As the condenser and the radiator begin to heat, expansion and contraction of the flexible member allows the thermal expansion within the frame, However, '603 reference fails to provide a cheaper and easily fabricable solution for controlling uneven expansion of the core units. Therefore, there is a need for a cost effective plate to accommodate uneven expansion of the core units of the heat exchangers.
  • SUMMARY OF THE DISCLOSURE
  • In one aspect of the present disclosure, a heat exchanger adapted to be coupled with a platform is disclosed. The heat exchanger comprises two or more core units having an upper surface and a lower surface, the lower surface of each core unit being fixed to the platform. The heat exchanger further includes a plate disposed along the upper surface of the core units, the plate having a plurality of bend enhancement regions and a plurality of holes, each bend enhancement region being placed at a predetermined distance from the nearest adjacent holes, and a plurality of spacers interposed between the plate and the upper surface to couple the plate to the upper surface, the plurality of spacers adapted to provide offset between the plate from the core units. During operation of the heat exchanger, each bend enhancement region is configured to facilitate flexibility of the plate to accommodate any uneven expansion of the two or more core units.
  • Other features and aspects of this disclosure will be apparent from the following description and the accompanying drawings.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a perspective view of a heat exchanger having east two core units and a plate mounted on an upper surface of the at least two core units, in accordance with the concepts of the present disclosure;
  • FIG. 2 is a perspective view of the plate of FIG. 1, in accordance with the concepts of the present disclosure;
  • FIG. 3 is a top view of the plate of FIG. 1, in accordance with the concepts of the present disclosure;
  • FIG. 4 is a front view of the heat exchanger of FIG. 1 with the plate mounted on the upper surface of the core units in a first configuration, in accordance with the concepts of the present disclosure; and
  • FIG. 5 is a front view of the heat exchanger of FIG. 1 with the plate mounted on the upper surface of the core units in a second configuration, in accordance with the concepts of the present disclosure.
  • DETAILED DESCRIPTION
  • Referring to FIG. 1, a heat exchanger 10 is shown without specific reference to one or more outlet ports and one or more inlet ports for coolant, and a plurality of fins coupled to outer surface of a plurality of tubes. The heat exchanger 10 can include one or more cores 28, 30 and/or 32 forming a core assembly 20, and a plate 12 disposed along an upper surface 22 of the core assembly 20 and a platform 26 disposed along a lower surface 24 of the core assembly 20. In some embodiments, the plate 12 may be disposed along the lower surface 24 and the platform 26 may be disposed along the upper surface 22. The plate 12 may be disposed offset at a distance from the upper surface 22 to define a spacing therebetween. To facilitate maintaining the spacing or offset distance, a plurality of spacers 16 (also can be called bosses) can be interposed between a second surface 38 of the plate 12 and the upper surface 22. A plurality of fasteners 14 can be used to couple the plate 12 to the core assembly 20. As shown in FIG. 1, the fasteners 14 can be integrated with the locations of the spacers 16, so that the fastener 14 is extended through a hole formed into the plate 12, is extended through a corresponding spacer 16, and terminated into the core assembly 20. The plate 12 may also include a plurality of bend enhancement regions 18, as will be discussed.
  • The terms “core” and “core unit” have similar meaning and interpretations and may be interchangeably used with the description without departing from the meaning and scope of the disclosure. The core assembly 20 may include one or more cores, such, for example, shown: a first core 28 (also called a first core unit), a second core 30 (also called a second core unit) and a third core 32 (also called a third core unit). In an embodiment, the core assembly 20 may include oil cooling core, turbo compressed air core, engine coolant core, among others and other components, such as inlets, outlets, fins (not shown in FIG. 1). It will be apparent to one skilled in the art that the heat exchanger 10 may have any other configuration or have more number of cores without departing from the meaning and scope of the disclosure.
  • The lower surface 24 of the core assembly 20 can be coupled to the platform 26. In one example, the platform 26 is fixedly secured to the lower surface 24 of the core assembly 20 or lower surface 24 of each of the cores 28, 30 or 32. The platform 26 is utilized for mounting onto a machine, a vehicle frame or any other implement which requires the heat exchanger 10. The spacers 16 are provided for preventing interference between the plate 12 and the core assembly 20. During thermal expansion, the spacers 16 are adapted to provide offset between the core assembly 20 and the plate 12. It will be apparent to one skilled in the art that the spacers 16 may be of different shapes, configuration and material, but not limited to steel, stainless steel, iron, copper, among others. The spacers 16 may be separate components or may be a part of the core assembly 20 without departing from the meaning and scope of the disclosure. The spacers 16 are inboard on the first core 28, the second core 30, and the third core 32 to reduce the overall stiffness of the plate 12. As a result, thermal stress is reduced as the first core 28, the second core 30, the third core 32 expand or contract. For the purpose of simplicity various other components of the heat exchanger 10 are not labeled in FIG. 1.
  • Referring to FIG. 2, the plate 12 can have a plurality of holes 34 formed therein. The plate 12 includes a first surface 36, the second surface 38, a first edge 40, a second edge 42, a third edge 44 and a fourth edge 46. The plate 12 may have a predetermined width W defined as the distance between the first and second edges 40, 42, a predetermined thickness T defined as the distance between the first and the second surfaces 36, 38, and a predetermined length L defined as the distance between the third and fourth edges 44, 46. It will be apparent to one skilled in the art that the predetermined width W, the predetermined thickness T, and the predetermined length L are defined as per the design requirements and may also he varied without departing from the meaning and scope of the disclosure.
  • Referring to FIG. 2, the bend enhancement regions 18 are positioned at a predetermined distance ‘D’ from holes 34 that are the nearest adjacent thereto, generally each along a line X-X′. It will be apparent to one skilled in the art that the predetermined distance D is defined as per the design requirements (shown in FIG. 1) and may also be varied without departing from the meaning and scope of the disclosure. The plate 12 is constructed from materials that include, but is not limit to, steel, stainless steel, copper, among others. The bend enhancement regions 18 is defined as a region within the plate 12 at which a portion of material is removed or added to facilitate relative movement or flexing along the line X-X′ along with the region is formed at a predetermined location. This predetermined location for flexing of the plate 12 is generally located to overlap the outer boundary of the core unit, i.e. the first core 28, the second core 30 and/or the third core 32. In some examples, the predetermined location can he positioned along the lateral space or boundary between adjacent core units so as not to overlap the outer boundary of the core unit, i.e. the first core 28, the second core 30 and/or the third core 32. The bend enhancement region 18 facilitates in modifying the surface area of the plate 12 and adding flexibility around the line X-X′, that typically extends between the first and second edges 40, 42 or along the third and fourth edges 44, 46. In an embodiment, the bend enhancement region 18 has a predetermined shape in form of a series of scallops or ovalic shapes removed from the plate, in other examples, this region can be perforated or material removed having rounded, rectangular or other shapes. It will he apparent to one skilled in the art that the bend enhancement regions 18 may have any other suitable shape, depth variation, and patterns around the plate 12 that allows flexibility to the plate 12 without departing from the meaning and scope of the disclosure. The holes 34 are adapted to receive the fasteners 14 (as shown in FIG. 1) for attaching the plate 12 to the core assembly 20 (as shown in FIG. 1). It will be apparent to one skilled in the art that the fasteners 14 may be other kind of fasteners, such as bolts, screws, among others without departing from the meaning and scope of the disclosure. Also the fasteners 14 may be constructed of materials includes, but not limited to, steel, stainless steel, iron, copper, among others.
  • Referring to FIG. 3, the plate 12 is mounted on the first core 28, the second core 30, and the third core 32 via the fasteners 14. The plate 12 is mounted on the upper surface 22 (as shown in FIG. 1) of the first core 28, the second core 30 and the third core 32.
  • Referring to FIG. 4, the plate 12 is mounted on the first core 28, the second core 30 and the third core 32 a first configuration. In the first configuration, the first core 28, and the third core 32 are in a cold state, while the second core 30 is in a hot state. During operations, prolonged thermal exposure causes the second core 30 to expand. During expansion of the second core 30, the plate 12 bends or flexes around the line X-X′ of the bend enhancement regions 18. The bend enhancement regions 18 (not shown in FIG. 4) are at the predetermined distance D from the spacers 16 or the fasteners 14.
  • Referring to FIG. 5, the plate 12 is mounted on the first core 28, the second core 30 and the third core 32 in a second configuration. In the second configuration, the first core 28, and the third core 32 are in a hot state, while the second core 30 is in a cold state. During operations, prolonged thermal exposure causes the first core 28 and the third core 32 to expand. During expansion of the first core 28 and the third core 32, the plate 12 bends around the line X-X′ of the bend enhancement regions 18. The bend enhancement regions 18 (not shown in FIG. 5) are at the predetermined distance D from the number of spacers 16 or the fasteners 14.
  • INDUSTRIAL APPLICABILITY
  • Currently, there are challenges for controlling uneven thermal expansion of the core assembly 20 of the heat exchanger 10 having various cores for oil cooling, turbo compressed air cooling, engine coolant core, among others and other components for an engine. During operation of the heat exchanger 10, the plate 12 having the bend enhancement regions 18 that offer flexibility to the plate 12 to accommodate any uneven expansion of the first core 28, the second core 30 and the third core 32. The plate 12 is made from a sheet metal that is manufactured easily and mounted within any frameless configuration without requiring a complete dismantling of the core assembly 20. As a result, the maintenance cost and machine down time is reduced. The plate 12 is light weight, and easily fabricable.
  • Referring to FIGS. 4 and 5, in an exemplary embodiment, if the first core 28 and the third core 32 are expanded more with respect to the second core 30, then the plate 12 flexes as per the expansion rates of the first core 28 and the third core 32, The flexibility is obtained by bending the plates at the line X-X′. During expansion or contraction, the bend enhancement regions 18 are subjected to a tensile load along the first edge 40, which causes a deformation in the shape of the bend enhancement regions 18 while providing the bend along the line X-X′ in the plate 12.
  • While aspects of the present disclosure have been particularly shown and described with reference to the embodiments above, it will be understood by those skilled in the art that various additional embodiments may be contemplated by the modification of the disclosed machines, systems and methods without departing from the spirit and scope of what is disclosed. Such embodiments should be understood to fall within the scope of the present disclosure as determined based upon the claims and any equivalents thereof.

Claims (1)

What is claimed is:
1. A heat exchanger adapted to be coupled with a platform, the heat exchanger comprising:
two or more core units having an upper surface and a lower surface, the lower surface of each core unit being fixed to the platform;
a plate disposed along the upper surface of the core units, the plate having a plurality of bend enhancement regions and a plurality of holes, each bend enhancement region being placed at a predetermined distance from the nearest adjacent holes; and
a plurality of spacers interposed between the plate and the upper surface to couple the plate to the upper surface, the plurality of spacers adapted to provide offset between the plate from the core units;
wherein, during operation of the heat exchanger, each bend enhancement region is configured to facilitate flexibility of the plate to accommodate any uneven expansion of the two or more core units.
US15/075,362 2016-03-21 2016-03-21 Frameless cooling module Abandoned US20160201998A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US15/075,362 US20160201998A1 (en) 2016-03-21 2016-03-21 Frameless cooling module

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15/075,362 US20160201998A1 (en) 2016-03-21 2016-03-21 Frameless cooling module

Publications (1)

Publication Number Publication Date
US20160201998A1 true US20160201998A1 (en) 2016-07-14

Family

ID=56367314

Family Applications (1)

Application Number Title Priority Date Filing Date
US15/075,362 Abandoned US20160201998A1 (en) 2016-03-21 2016-03-21 Frameless cooling module

Country Status (1)

Country Link
US (1) US20160201998A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180038652A1 (en) * 2016-08-04 2018-02-08 Hanon Systems Heat exchanger element with thermal expansion feature
US20180244127A1 (en) * 2017-02-28 2018-08-30 General Electric Company Thermal management system and method
US10830540B2 (en) 2017-02-28 2020-11-10 General Electric Company Additively manufactured heat exchanger

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE9420825U1 (en) * 1993-12-28 1995-02-09 Joh. Vaillant Gmbh U. Co, 42859 Remscheid bracket
US5992514A (en) * 1995-11-13 1999-11-30 Denso Corporation Heat exchanger having several exchanging portions
US6328098B1 (en) * 1998-11-10 2001-12-11 Valeo Inc. Side member for heat exchanger and heat exchanger incorporating side plate
WO2003085348A1 (en) * 2002-04-09 2003-10-16 Behr Gmbh & Co. Heat transfer unit, especially for a motor vehicle
US20140202670A1 (en) * 2013-01-21 2014-07-24 Denso International America, Inc. Stamped thermal expansion relief feature for heat exchangers

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE9420825U1 (en) * 1993-12-28 1995-02-09 Joh. Vaillant Gmbh U. Co, 42859 Remscheid bracket
US5992514A (en) * 1995-11-13 1999-11-30 Denso Corporation Heat exchanger having several exchanging portions
US6328098B1 (en) * 1998-11-10 2001-12-11 Valeo Inc. Side member for heat exchanger and heat exchanger incorporating side plate
WO2003085348A1 (en) * 2002-04-09 2003-10-16 Behr Gmbh & Co. Heat transfer unit, especially for a motor vehicle
US20140202670A1 (en) * 2013-01-21 2014-07-24 Denso International America, Inc. Stamped thermal expansion relief feature for heat exchangers

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180038652A1 (en) * 2016-08-04 2018-02-08 Hanon Systems Heat exchanger element with thermal expansion feature
US10429133B2 (en) * 2016-08-04 2019-10-01 Hanon Systems Heat exchanger element with thermal expansion feature
US20180244127A1 (en) * 2017-02-28 2018-08-30 General Electric Company Thermal management system and method
US10830540B2 (en) 2017-02-28 2020-11-10 General Electric Company Additively manufactured heat exchanger

Similar Documents

Publication Publication Date Title
KR102255779B1 (en) Heat exchanger and manufacturing method therefor, heat exchange module, heat exchange device and heat source unit
US20160201998A1 (en) Frameless cooling module
US20130014923A1 (en) Battery cooler
CN100356131C (en) Heat exchanger, especially a heat exchanging module for a motor vehicle
CN102272547A (en) Fin for a heat exchanger, and heat exchanger including such a fin
CN102498362A (en) Heat exchanger with end plate providing mounting flange
US3982587A (en) Vehicular radiator assembly
JP6065927B2 (en) Air conditioning indoor unit
SE529769C2 (en) Plate heat exchanger comprising at least one reinforcing plate disposed outside one of the outer heat exchanger plates
JP6615118B2 (en) Vehicle heat exchanger tube and vehicle radiator comprising such a tube
US11230968B2 (en) Frameless cooling module
US20150300757A1 (en) Heat exchanger tube insert
CN104937362A (en) Heat exchange system
US20120037349A1 (en) Heat exchange element
US10378827B2 (en) Heat exchanger
US10281222B2 (en) Heat exchanger
EP3106819A1 (en) Heat exchanger
JP2017183421A (en) Heat exchanger
CN203785517U (en) Coil end plate of heat exchange coil pack
EP3473961B1 (en) Heat exchanger
KR101371641B1 (en) Support Panel And Heat Exchanger adopting the same
WO2014176194A1 (en) Core device of a heat exchanger and heat exchanger with the core device
JPH08165928A (en) Fan shroud for heat exchanger
KR101897514B1 (en) heat exchanger plate for plate type heat exchanger
CN105008847A (en) Coil end plate for heat exchanger coil assembly

Legal Events

Date Code Title Description
AS Assignment

Owner name: CATERPILLAR INC., ILLINOIS

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:KENNEDY, JOSEPH L.;TERRY, NEIL A.;MOKIRE, MAHESH K.;AND OTHERS;REEL/FRAME:038047/0382

Effective date: 20160310

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION