EP0823610A1 - Heat exchanger - Google Patents

Heat exchanger Download PDF

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Publication number
EP0823610A1
EP0823610A1 EP96202233A EP96202233A EP0823610A1 EP 0823610 A1 EP0823610 A1 EP 0823610A1 EP 96202233 A EP96202233 A EP 96202233A EP 96202233 A EP96202233 A EP 96202233A EP 0823610 A1 EP0823610 A1 EP 0823610A1
Authority
EP
European Patent Office
Prior art keywords
tube
heat exchanger
ratio
section
wall thickness
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.)
Withdrawn
Application number
EP96202233A
Other languages
German (de)
French (fr)
Inventor
Björn Vestergaard
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.)
Norsk Hydro ASA
Original Assignee
Norsk Hydro ASA
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 Norsk Hydro ASA filed Critical Norsk Hydro ASA
Priority to EP96202233A priority Critical patent/EP0823610A1/en
Priority to AU37686/97A priority patent/AU3768697A/en
Priority to PCT/EP1997/003874 priority patent/WO1998006995A1/en
Publication of EP0823610A1 publication Critical patent/EP0823610A1/en
Withdrawn legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/02Tubular elements of cross-section which is non-circular
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
    • F28F1/24Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely
    • F28F1/32Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending transversely the means having portions engaging further tubular elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2275/00Fastening; Joining
    • F28F2275/12Fastening; Joining by methods involving deformation of the elements
    • F28F2275/125Fastening; Joining by methods involving deformation of the elements by bringing elements together and expanding

Definitions

  • the present invention relates to a heat exchanger, more precisely to a heat exchanger of the type defined in the preamble of Claim 1.
  • Such a heat exchanger is known from EP - A - 0 633 435. According to said publication the ratio between the maximum dimension of the cross-section and the minimum dimension of the cross section must be between 2.5 and 3.75, the ratio between maximum dimension of the cross-section and the thickness of the tube must be between 15 and 30 and the ratio between the distance between the fins and the thickness of each fin must be less than or equal to 11.
  • an improved heat exchanger is obtained by the characteristic portion of claim 1.
  • a heat exchanger is obtained in which the pressure transmitted by the tube to the fins is more evenly distributed, thereby obtaining a more evenly distributed heat exchange contact between the tubes and the fins.
  • the heat exchanger shown in the drawing is of the type disclosed in EP - A - 0 633 435 and for the general information about that construction, reference is made to that publication.
  • part of one fin 10 containing perpendicular to its surface a so-called oval tube 12, i.e. a tube having an oblong cross section without any flat walls.
  • the tube has in cross section a maximum dimension b and a minimum dimension a.
  • the wall thickness of the tube may vary according to the location. In this way four locations are important with respect to the tension when the tube is under internal pressure. These locations are the places with largest radius indicated by their thickness S 1 and S 2 and the places with the smaller radius indicated by their thickness S 3 and S 4 .
  • Fig. 2 there is shown the tube 12 and in the left hand part of the drawing there is shown the stress T 0 in the wall of the tube 12 when no pressurised fluid is present within the tube. In this situation the fins exert from the outer side a pressure on the wall of the tube 12, which pressure is the highest in the small diameter portions.
  • the stress T p in the tube wall when a pressurised fluid is present within the tube in which case the fluid exerts a pressure on the tube wall as shown in that part of fig. 2, the stress being the smallest in the small radius portion of the tube.
  • the tension T 0 in the left hand side and the stress T p in the right hand side of fig. 2 are differently oriented, in the left hand side being from the outside to the inside and in the right hand side being from the inside to the outside.
  • the schematic representation of fig. 2 is based upon calculations made with respect to a simplified model of a so called flat oval tube.
  • the simplification has primarily to do with the fact that it was accepted that the tube has an ellipse shape with a major axis of 12 mm and a minor axis of 3.2 mm and an average wall thickness of 0.5 mm. In the normal use of a heat exchanger this is quit often switched on and off, which means that with the same frequency a pressurised fluid is supplied to the interior of the tube 12 and the pressure relieved after switching off.
  • the stress T occurring in a small radius portion of the tube wall is represented in fig. 4 in function of the time t. Every time the heat exchanger is switched on the stress increases nearly stepwise, and after switching off it decreases more or less in the same way.

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

Abstract

Heat exchanger, comprising a group of tubes secured to a pack of fins by means of mechanical expansion of the tubes following their insertion in holes aligned in the fins, the tubes having an oblong cross-section without any flat walls, wherein a first ratio between the maximum dimension (b) and the minimum dimension (a) of the cross-section, is of between 2.80 and 5.20 and a second ratio between the maximum dimension (b) of the cross-section and the thickness (s) of the tube is between 15 and 38; and wherein the wall thickness of the tube fulfils the equation {[S3 + S4) / (S1 + S2)] - 1}* 100 > 5 wherein S3 and S4 are the wall thickness in the area of the tube with the smallest radius, and S1 and S2 are the wall thickness in the area of the tube with the largest radius.

Description

The present invention relates to a heat exchanger, more precisely to a heat exchanger of the type defined in the preamble of Claim 1.
Such a heat exchanger is known from EP - A - 0 633 435.
According to said publication the ratio between the maximum dimension of the cross-section and the minimum dimension of the cross section must be between 2.5 and 3.75, the ratio between maximum dimension of the cross-section and the thickness of the tube must be between 15 and 30 and the ratio between the distance between the fins and the thickness of each fin must be less than or equal to 11.
It has been found that the support given by the fins to the tubes when these are filled with a pressurised heat exchanging fluidum is subordinate if compared with the self-supporting characteristics of the tube. It has even been possible to use tubes with different dimensions, provided special measurements are taken with respect to the wall thickness of the tube.
According to the invention an improved heat exchanger is obtained by the characteristic portion of claim 1.
By using the dimensions according to the invention a heat exchanger is obtained in which the pressure transmitted by the tube to the fins is more evenly distributed, thereby obtaining a more evenly distributed heat exchange contact between the tubes and the fins.
Other advantages and characteristics will become obvious from the following description of an example reference being made to the annexed drawing in
Fig. 1
which is a part of a heat exchanger shown in cross section,.
Fig. 2
is a schematic representation of the stress on the tube wall in operative and non-operative condition,
Fig. 3
is a schematic representation of the tube form in operative and non-operative condition, and
Fig. 4
is a diagram showing the variations in stress in the tube wall.
The heat exchanger shown in the drawing is of the type disclosed in EP - A - 0 633 435 and for the general information about that construction, reference is made to that publication.
In the drawing there is shown part of one fin 10 containing perpendicular to its surface a so-called oval tube 12, i.e. a tube having an oblong cross section without any flat walls.
As shown in the drawing the tube has in cross section a maximum dimension b and a minimum dimension a. According to the invention the wall thickness of the tube may vary according to the location. In this way four locations are important with respect to the tension when the tube is under internal pressure. These locations are the places with largest radius indicated by their thickness S1 and S2 and the places with the smaller radius indicated by their thickness S3 and S4. By providing the wall thickness S1 and S2, S3 and S4 in such a way that they fulfil the claimed equation and when at the same time the first ratio b/a lies between 2,80 and 5,20 and second ratio b/s lies between 15 and 38, S being the average wall thickness
[e.g. = S = (S1 + S2 + S3 + S4)/4] the tube is optimised with respect to its strength against internal pressure and lowest material consumption.
The following explanation shows that the stress in the area with the smallest radius is higher than in the one with the largest radius, and that
In Fig. 2 there is shown the tube 12 and in the left hand part of the drawing there is shown the stress T0 in the wall of the tube 12 when no pressurised fluid is present within the tube. In this situation the fins exert from the outer side a pressure on the wall of the tube 12, which pressure is the highest in the small diameter portions. In the right hand side of figure 2 there is shown the stress Tp in the tube wall when a pressurised fluid is present within the tube, in which case the fluid exerts a pressure on the tube wall as shown in that part of fig. 2, the stress being the smallest in the small radius portion of the tube. It should however be noted that the tension T0 in the left hand side and the stress Tp in the right hand side of fig. 2 are differently oriented, in the left hand side being from the outside to the inside and in the right hand side being from the inside to the outside.
The schematic representation of fig. 2 is based upon calculations made with respect to a simplified model of a so called flat oval tube. The simplification has primarily to do with the fact that it was accepted that the tube has an ellipse shape with a major axis of 12 mm and a minor axis of 3.2 mm and an average wall thickness of 0.5 mm.
In the normal use of a heat exchanger this is quit often switched on and off, which means that with the same frequency a pressurised fluid is supplied to the interior of the tube 12 and the pressure relieved after switching off.
In Fig. 3 there is shown the shape of the tube 12 either in the non operative condition of the heat exchanger, in which situation the tube has the shape 12A and most of the stress is concentrated in the small radius portion of the wall. Upon applying a pressurised fluid in the tube 12 it takes the shape 12B. As can clearly be seen in fig. 3 the wall is moving as if it is articulating around the small diameter portion of the wall. This adds to the tensions which apply to these portions, and requires fatigue properties for these portions. By using the wall thickness ratio's according to the invention these improved fatigue properties have been obtained.
To further elucidate this phenomena, the stress T occurring in a small radius portion of the tube wall is represented in fig. 4 in function of the time t. Every time the heat exchanger is switched on the stress increases nearly stepwise, and after switching off it decreases more or less in the same way.

Claims (5)

  1. Heat exchanger, comprising a group of tubes secured to a pack of fins by means of mechanical expansion of the tubes following their insertion in holes aligned in the fins, the tubes having an oblong cross-section without any flat walls,
    characterised in that
    a first ratio between the maximum dimension (b) and the minimum dimension (a) of the cross-section, is of between 2.80 and 5.20 and a second ratio between the maximum dimension (b) of the cross-section and the thickness (s) of the tube is between 15 and 38; and in that the wall thickness of the tube fulfils the equation {[S3 + S4) / (S1 + S2)] - 1}* 100 > 5 wherein S3 and S4 are the wall thickness in the area of the tube with the smallest radius, and S1 and S2 are the wall thickness in the area of the tube with the largest radius.
  2. Heat exchanger according to claim 1,
    characterised in that
    the first ratio is between 3.75 and 5.20.
  3. Heat exchanger according to claim 1,
    characterised in that
    the first ratio is between 3.75 and 5.00.
  4. Heat exchanger according to any of the claims 1 to 3,
    characterised in that
    the second ratio is between 17 and 26.
  5. Heat exchanger according to any of the claims 1 to 4,
    characterised in that
    the equation is larger or equal to 6.
EP96202233A 1996-08-08 1996-08-08 Heat exchanger Withdrawn EP0823610A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP96202233A EP0823610A1 (en) 1996-08-08 1996-08-08 Heat exchanger
AU37686/97A AU3768697A (en) 1996-08-08 1997-07-15 Heat exchanger
PCT/EP1997/003874 WO1998006995A1 (en) 1996-08-08 1997-07-15 Heat exchanger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP96202233A EP0823610A1 (en) 1996-08-08 1996-08-08 Heat exchanger

Publications (1)

Publication Number Publication Date
EP0823610A1 true EP0823610A1 (en) 1998-02-11

Family

ID=8224266

Family Applications (1)

Application Number Title Priority Date Filing Date
EP96202233A Withdrawn EP0823610A1 (en) 1996-08-08 1996-08-08 Heat exchanger

Country Status (3)

Country Link
EP (1) EP0823610A1 (en)
AU (1) AU3768697A (en)
WO (1) WO1998006995A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998053265A1 (en) 1997-05-16 1998-11-26 Norsk Hydro Asa Flat oval tube

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3239002A (en) * 1964-01-06 1966-03-08 Young Radiator Co Tube formation for structuring heatexchanger core-units
FR2269053A1 (en) * 1974-04-25 1975-11-21 Chausson Usines Sa
FR2406794A1 (en) * 1977-10-21 1979-05-18 Volkswagenwerk Ag Heat exchanger with light alloy tubes - has unequal wall thickness tubes to prevent seal fracture on expansion
EP0633435A1 (en) * 1993-07-06 1995-01-11 MAGNETI MARELLI CLIMATIZZAZIONE S.r.l. Condenser for air-conditioning systems, in particular for motor vehicles

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3239002A (en) * 1964-01-06 1966-03-08 Young Radiator Co Tube formation for structuring heatexchanger core-units
FR2269053A1 (en) * 1974-04-25 1975-11-21 Chausson Usines Sa
FR2406794A1 (en) * 1977-10-21 1979-05-18 Volkswagenwerk Ag Heat exchanger with light alloy tubes - has unequal wall thickness tubes to prevent seal fracture on expansion
EP0633435A1 (en) * 1993-07-06 1995-01-11 MAGNETI MARELLI CLIMATIZZAZIONE S.r.l. Condenser for air-conditioning systems, in particular for motor vehicles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998053265A1 (en) 1997-05-16 1998-11-26 Norsk Hydro Asa Flat oval tube

Also Published As

Publication number Publication date
WO1998006995A1 (en) 1998-02-19
AU3768697A (en) 1998-03-06

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