EP1376039B1 - Multi tubular heat exchangers and process for making same - Google Patents

Multi tubular heat exchangers and process for making same Download PDF

Info

Publication number
EP1376039B1
EP1376039B1 EP03358008A EP03358008A EP1376039B1 EP 1376039 B1 EP1376039 B1 EP 1376039B1 EP 03358008 A EP03358008 A EP 03358008A EP 03358008 A EP03358008 A EP 03358008A EP 1376039 B1 EP1376039 B1 EP 1376039B1
Authority
EP
European Patent Office
Prior art keywords
shell
bundle
heat exchanger
wall
exchanger according
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.)
Expired - Lifetime
Application number
EP03358008A
Other languages
German (de)
French (fr)
Other versions
EP1376039A1 (en
Inventor
Gérard Mota
Jean-Claude Ebren
Michel Cremieux
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.)
MOTA
Original Assignee
MOTA
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 MOTA filed Critical MOTA
Publication of EP1376039A1 publication Critical patent/EP1376039A1/en
Application granted granted Critical
Publication of EP1376039B1 publication Critical patent/EP1376039B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/16Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation
    • 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
    • F28F9/005Other auxiliary members within casings, e.g. internal filling means or sealing means
    • 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
    • F28F9/0219Arrangements for sealing end plates into casing or header box; Header box sub-elements
    • 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
    • F28F9/0246Arrangements for connecting header boxes with flow lines
    • 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
    • F28F9/0246Arrangements for connecting header boxes with flow lines
    • F28F9/0248Arrangements for sealing connectors to header boxes
    • 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
    • F28F9/22Arrangements for directing heat-exchange media into successive compartments, e.g. arrangements of guide plates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2255/00Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes
    • F28F2255/16Heat exchanger elements made of materials having special features or resulting from particular manufacturing processes extruded
    • 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
    • F28F2265/32Safety or protection arrangements; Arrangements for preventing malfunction for limiting movements, e.g. stops, locking means

Definitions

  • the present invention relates to improvements made to shell-and-tube heat exchangers and methods of manufacturing such exchangers.
  • the invention is particularly applicable to heat exchangers between a first fluid circulating in a plurality of tubes forming a multitubular bundle, and a second fluid circulating around the tubes, in a cylindrical cavity delimited by a hollow body (or calender) in which extends the bundle of tubes;
  • the invention applies in particular to heat exchangers for heat engines, reducers, inverters, compressors, hydraulic units, etc .; in this type of exchanger, the transfer of heat energy between the hot source and the cold source is effected in particular by conduction through the wall of the tubes; in order to obtain a sufficient energy transfer flux (and / or a heat exchange coefficient), the tubes are made of a material having a high thermal conductivity, such as a copper-based metal alloy, aluminum, nickel, titanium or stainless steels.
  • the invention applies in particular to such exchangers comprising two tubular plates pierced with a plurality of orifices; each of the two ends of each of the tubes is engaged in one of the orifices of a tubular plate and is sealed to this plate in particular by brazing, welding or swaging.
  • the tubular bundle may comprise, in addition to the tubes and the end tube plates, baffles for guiding the flow of the second fluid inside the hollow body; these baffles generally consist essentially of thin plates extending transversely to the tubes and parallel to the end tube plates, are regularly spaced along the tubes and close part of the cross section - generally circular - of the hollow body, to guide the second fluid; the beam may also comprise fins crimped or otherwise related to the outer surface of the tubes of the beam; it may include other secondary surfaces.
  • Such exchangers generally further comprise, at each of its two longitudinal ends, a cap (water box) respectively covering one of said tubular plates, and allowing either the connection of the exchanger to two ducts (external to the exchanger) of transport of the first fluid, ie the guidance of this fluid in the case of a cap "blind", that is to say devoid of connection to an external conduit.
  • the hollow body is provided with an inlet orifice of the second fluid in said cavity as well as an outlet orifice of this fluid;
  • the hollow body is generally constituted by a generally tubular piece provided at each of its two longitudinal ends with an annular flange; each flange is pierced with a plurality of orifices extending along the longitudinal axis of the exchanger and receiving screws - or similar fastening members - for fastening to the body, in a sealed manner, at least one of the tubular plates, as well as the two caps.
  • the body of small exchangers (particularly larger diameter less than 0.25 meters) is generally manufactured by molding (without pressure) a metal alloy, the body and the flanges being molded in one piece; this technique has drawbacks: the inner face of the body must be machined over its entire length to have a roughness and geometric quality compatible with the use that is made of it; the outer faces of the flanges must also be erected; these moldings often have defects in their mass resulting in a porosity incompatible with the function of sealed wall they must fill; moreover, these defects can only be validly checked after mechanical machining (boring, turning, etc.); it is thus necessary to discard expensive parts; the pressure-free molding technique (in sand molds) also prevents the production of thin walls.
  • An object of the invention is to provide such exchangers that are improved, and a method of manufacturing these exchangers that reduces the cost.
  • the invention consists in proposing such exchangers in which a mutual engagement of the shell and the beam forms an abutment inside the cavity delimited by the shell, which prevents or limits a displacement of the beam relative to at the front grille; said exchangers being in accordance with claim 1.
  • This mutual engagement can result from a deformation of a part of the beam and / or part of the shell, or the insertion of a member forming a stop (or shoulder) inside the cylindrical cavity bounded by the grille; in all cases, these deformations and / or insertions are made after the beam has been introduced and correctly positioned inside the shell.
  • this stop is partly at least provided by a projection provided on the inner face of the calender wall, so that it is not necessary to manufacture for this purpose a separate part of the calender.
  • this projection or narrowing forming a stop extends over only a portion of the inner transverse circular contour of the shell.
  • the realization of this abutment is further simplified by making it around one of the fluid inlet and outlet ports in the cavity defined in the shell, in particular by pushing at least a portion of a flange, towards the inside.
  • the projection may be made at the periphery of a thin wall of the bundle, in particular of a tab integral with a tubular plate of the bundle, by pushing this thin wall or tongue towards the outside of the cavity , so as to obtain either a rigid frictional connection between the beam and the shell, or a blockage by penetration of the wall or tongue into an orifice formed in the wall of the shell, in particular in one of said inlet or outlet orifices. fluid outlet.
  • this projection may be incorporated at the end of a connecting part of the shell to a conduit for transporting this fluid - hereinafter referred to as second fluid -; for example, this projection may consist of a tubular portion extending a connection screwed into a threaded hole provided in the wall of the calender; this may allow to obtain a rigid connection between the beam and the shell, which is reversible (removable).
  • this projection consists essentially of a portion of the wall of the shell, and is provided (and / or extends) around one of said orifices (inlet and outlet fluid) to less; preferably, the abutment or projection is adapted to engage in a depression or indentation provided at the periphery of a part of the tubular bundle - preferably at the periphery of a portion of a tubular plate.
  • this part which comprises a first disk-shaped portion pierced with holes for passing and fixing the tubes of the bundle, and a second portion in the form of a tube or circular flange extending longitudinally to from the inner face of the first disk-shaped portion, preferably comprises a notch or depression of substantially circular profile and a diameter adapted to the dimensions of the abutment protruding on the inner face of the calender, this notch or depression being integrated in the second part of the tube plate.
  • such integrated protruding abutments are formed by deformation of a flange provided in the wall of the calender, at the inner end of a passage duct of the second fluid provided in this wall; this production method is particularly simple and inexpensive; this deformation must generally be performed after putting the tube bundle at its final location in the cavity defined by the shell.
  • this method may further include the features of claim 19.
  • a tubular shell-and-tube heat exchanger is described hereinafter, the bundle having two tubular plates, at least one plate - and preferably each - plate comprising: i) a first disk-shaped portion pierced with orifices receiving the tubes of the beam; if necessary ii) a second part extending from the internal face of the first part and incorporating either a housing provided to receive a stop protruding from the inner face of the shell, or an expandable wall or tongue provided for s engage - after deformation - in an orifice formed in the wall of the calender; iii) a third portion of tubular form extending from the outer face of the first portion, and adapted to be engaged in an end of a transport duct of the first fluid fixed to the third part of the plate by forced fitting and / or by strapping; preferably, the third tubular portion comprises for this purpose an outer annular rib.
  • the exchanger 1 comprises a shell 2 of longitudinal axis 3, and a tubular bundle housed in the cavity defined in the shell; the shell has a plurality of flat outer faces 4 to 13 (see figure 3 ) elongate and parallel to the axis 3; on the face 10 open two channels 14 and 15 connecting the cavity defined by the shell to a fluid such as oil to be cooled.
  • the calender is obtained by extrusion of aluminum; the resulting profile is soaked and cut into sections such as that illustrated Figures 2 and 3 ; each longitudinal end is machined to obtain a chamfer 16, 17 facilitating the introduction of the tubular bundle equipped with two annular sealing seals (pins 19, 20 figure 8 ) in the cavity 18 defined by the calender, without damaging the seals.
  • the walls 10 to 12 delimit a longitudinal rib 23 parallel to the axis 3, in which are drilled the channels 14, 15 of axes 21 and 22 radial.
  • each conduit 14, 15 has a threaded outer portion 24 extending from the face 10 to allow the screwing of a not shown fitting; the inner portion of the conduit through which the latter opens on the cylindrical inner face 25 of the cavity 18, has a diameter 26 smaller than the diameter 27 of the orifice through which the conduit opens on the face 10; this results from the presence of an annular flange 28 formed in the wall 23 during the drilling of the ducts 14, 15 by a profiled drill for this purpose; the flange 28 has a thickness 29 sufficiently low (for example of the order of 1 to 2 millimeters) to be deformed by the action of a tool supported on the inner face 30 inclined, according to the arrow 31 figure 4 ; this makes it possible to pass at least part of this flange of the initial configuration - reference 28 figure 4 - where the flange is flush with the face 25, the final configuration - marked 28a figure 4 - Where the deformed flange protrudes from the face 25, a value 32, for example close to one or two mill
  • This mode of deformation of the collar requires the use of a material having sufficient elongation at break, for producing the calender; for this purpose, the use of extruded and tempered aluminum is more favorable than that of cast aluminum and / or injected.
  • the hollow section (or tubular bar) used to form the shell may be obtained by extrusion of plastic material, or by hot spinning or cold drawing of a metal, in particular an aluminum alloy, of copper or steel.
  • the beam 34 comprises a plurality of tubes 35 parallel to its longitudinal axis 33, a plurality of flat baffles 36, 37 perpendicular to the axis 33, and two end pieces 38.
  • the contour of the baffles 36, 37 is largely circular (of diameter adapted to that of the cavity 18) and partly rectilinear 36a, 37a, so that the baffles have a truncated disk shape; the baffles 36 having their rectilinear edge 36a in the lower part are arranged, along the axis 33, alternately with the baffles 37 having their rectilinear edge 37a in the upper part, so that these baffles delimit with the calender a labyrinth forcing the second fluid to follow a sinuous path 39 figure 5 .
  • Each piece 38 has a first portion 380 in the form of a thick disc in which holes are drilled receiving the ends 350 of the tubes 35; this part, which extends transversely to the axis 33, forms the tubular plate itself.
  • the first portion 380 is extended at the periphery of its inner face 3800 by a second portion 381 of the workpiece 38, which is in the form of a short section of thin tube with an axis 33; at one end of this section, a notch 3810 is formed in the tubular wall of the section, which extends in a circular pattern whose diameter 40 is adapted to the dimensions (in particular to the diameter) of the projection 28a ( figure 4 ) formed on the inner face of the shell.
  • the first part 380 of the part 38 is further extended at the periphery of its external face 3801 by a third part 382 of the part 38 which is roughly in the shape of a tube section with an axis 33 and whose external face comprises an annular groove 41 provided for receiving one of the seals (19, 20 figure 8 ) sealing with the calender, and an annular rib 42 which protrudes from the central portion 3820 of this portion 382; the latter can thus, as illustrated figure 7 , receiving one end of a connection tube 43 force-fitted around the rib 42 and the cylindrical portion 3820 against which the tube 43 can be held tight by a strapping collar not shown.
  • each of the notches provided in the end pieces is respectively disposed opposite the inlet and outlet ports 14, 15 and receives a portion of the annular protrusions extending-these orifices, so that the beam is immobilized in the calender.
  • the tubular portion 381 of axis 33 extending tubular plate 380 of the bundle comprises a tongue-shaped portion 3811 which has been deformed after positioning the bundle in the shell, so that it extends inside the the orifice 14 for fluid passage, bearing against the wall delimiting this orifice; the tongue 3811 prevents the beam from sliding in the shell, along their common axis 3, 33 in the direction indicated by the arrow 100; by also equipping the second tube plate (not shown) of the same heat exchanger of such a tongue, it is also prohibited such sliding in the opposite direction, and a rotation of the beam.
  • a tubular sleeve 99 extends inside the conduit 14 for fluid passage drilled in the rib 23 of the shell, along the axis 21 of the conduit 14, on the walls of which leads this sleeve is supported.
  • the sleeve 99 protrudes from the inner face of the calender; therefore, it is engaged in a notch 3810 identical or similar to that described above, so that it limits the sliding of the beam in the calender; by further equipping a second conduit (as marked 15) by a second sleeve projecting inside the calender, the sliding and rotation of the beam in the calender is prevented.

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

An abutment is formed inside a cavity defined by a shell to prevent or restrict movement of a multi-tube bundle (34) relative to the shell. An Independent claim is included for a heat exchanger manufacturing method.

Description

La présente invention est relative à des améliorations apportées aux échangeurs de chaleur multitubulaires à calandre et à des procédés de fabrication de ces échangeurs.The present invention relates to improvements made to shell-and-tube heat exchangers and methods of manufacturing such exchangers.

L'invention s'applique particulièrement aux échangeurs de chaleur entre un premier fluide circulant dans une pluralité de tubes formant un faisceau multitubulaire, et un deuxième fluide circulant autour des tubes, dans une cavité cylindrique délimitée par un corps creux (ou calandre) dans lequel s'étend le faisceau de tubes ; l'invention s'applique notamment aux échangeurs pour moteurs thermiques, réducteurs, inverseurs, compresseurs, groupes hydrauliques... ; dans ce type d'échangeur, le transfert d'énergie thermique entre la source chaude et la source froide s'effectue notamment par conduction au travers de la paroi des tubes ; afin d'obtenir un flux de transfert d'énergie (et/ou un coefficient d'échange thermique) suffisant, les tubes sont réalisés en un matériau ayant une conductivité thermique élevée, tel qu'un alliage métallique à base de cuivre, d'aluminium, de nickel, de titane ou d'aciers inoxydables.The invention is particularly applicable to heat exchangers between a first fluid circulating in a plurality of tubes forming a multitubular bundle, and a second fluid circulating around the tubes, in a cylindrical cavity delimited by a hollow body (or calender) in which extends the bundle of tubes; the invention applies in particular to heat exchangers for heat engines, reducers, inverters, compressors, hydraulic units, etc .; in this type of exchanger, the transfer of heat energy between the hot source and the cold source is effected in particular by conduction through the wall of the tubes; in order to obtain a sufficient energy transfer flux (and / or a heat exchange coefficient), the tubes are made of a material having a high thermal conductivity, such as a copper-based metal alloy, aluminum, nickel, titanium or stainless steels.

L'invention s'applique en particulier à de tels échangeurs comportant deux plaques tubulaires percées d'une pluralité d'orifices ; chacune des deux extrémités de chacun des tubes est engagée dans un des orifices d'une plaque tubulaire et est solidarisé de façon étanche à cette plaque notamment par brasage, soudage ou dudgeonnage.The invention applies in particular to such exchangers comprising two tubular plates pierced with a plurality of orifices; each of the two ends of each of the tubes is engaged in one of the orifices of a tubular plate and is sealed to this plate in particular by brazing, welding or swaging.

Le faisceau tubulaire peut comporter, outre les tubes et les plaques tubulaires d'extrémité, des chicanes pour le guidage de l'écoulement du deuxième fluide à l'intérieur du corps creux ; ces chicanes sont généralement essentiellement constituées par des plaques minces s'étendant transversalement aux tubes et parallèlement aux plaques tubulaires d'extrémité, sont régulièrement espacées le long des tubes et ferment une partie de la section transversale - généralement circulaire - du corps creux, pour guider le deuxième fluide ; le faisceau peut également comporter des ailettes serties ou autrement liées à la surface externe des tubes du faisceau ; il peut comporter d'autres surfaces secondaires.The tubular bundle may comprise, in addition to the tubes and the end tube plates, baffles for guiding the flow of the second fluid inside the hollow body; these baffles generally consist essentially of thin plates extending transversely to the tubes and parallel to the end tube plates, are regularly spaced along the tubes and close part of the cross section - generally circular - of the hollow body, to guide the second fluid; the beam may also comprise fins crimped or otherwise related to the outer surface of the tubes of the beam; it may include other secondary surfaces.

De tels échangeurs comportent généralement en outre, à chacune de ses deux extrémités longitudinales, une calotte (boîte à eau) recouvrant respectivement une desdites plaques tubulaires, et permettant soit le raccordement de l'échangeur à deux conduits (externes à l'échangeur) de transport du premier fluide, soit le guidage de ce fluide dans le cas d'une calotte « borgne », c'est à dire dénuée de raccordement à un conduit externe.Such exchangers generally further comprise, at each of its two longitudinal ends, a cap (water box) respectively covering one of said tubular plates, and allowing either the connection of the exchanger to two ducts (external to the exchanger) of transport of the first fluid, ie the guidance of this fluid in the case of a cap "blind", that is to say devoid of connection to an external conduit.

Le corps creux est doté d'un orifice d'entrée du deuxième fluide dans ladite cavité ainsi que d'un orifice de sortie de ce fluide ; le corps creux est généralement constitué par une pièce de forme générale tubulaire pourvue à chacune de ses deux extrémités longitudinales d'une bride annulaire ; chaque bride est percée de plusieurs orifices s'étendant selon l'axe longitudinal de l'échangeur et recevant des vis - ou organes similaires de fixation - permettant de solidariser au corps, de façon étanche, au moins une des plaques tubulaires ainsi que les deux calottes.The hollow body is provided with an inlet orifice of the second fluid in said cavity as well as an outlet orifice of this fluid; the hollow body is generally constituted by a generally tubular piece provided at each of its two longitudinal ends with an annular flange; each flange is pierced with a plurality of orifices extending along the longitudinal axis of the exchanger and receiving screws - or similar fastening members - for fastening to the body, in a sealed manner, at least one of the tubular plates, as well as the two caps.

Le corps des petits échangeurs (en particulier de plus grand diamètre inférieur à 0,25 mètre) est généralement fabriqué par moulage (sans pression) d'un alliage métallique, le corps et les brides étant moulés en une seule pièce ; cette technique présente des inconvénients : la face interne du corps doit être usinée sur toute sa longueur pour présenter une rugosité et une qualité géométrique compatibles avec l'usage qui en est fait ; les faces extérieures des brides doivent également être dressées ; ces pièces moulées présentent fréquemment des défauts dans leur masse d'où résulte une porosité incompatible avec la fonction de paroi étanche qu'elles doivent remplir ; au surplus, ces défauts ne peuvent être valablement contrôlés qu'après usinage mécanique (alésage, tournage...) ; on est ainsi amené à mettre au rebut des pièces coûteuses ; la technique de moulage sans pression (dans des moules en sable) empêche en outre de réaliser des parois minces.The body of small exchangers (particularly larger diameter less than 0.25 meters) is generally manufactured by molding (without pressure) a metal alloy, the body and the flanges being molded in one piece; this technique has drawbacks: the inner face of the body must be machined over its entire length to have a roughness and geometric quality compatible with the use that is made of it; the outer faces of the flanges must also be erected; these moldings often have defects in their mass resulting in a porosity incompatible with the function of sealed wall they must fill; moreover, these defects can only be validly checked after mechanical machining (boring, turning, etc.); it is thus necessary to discard expensive parts; the pressure-free molding technique (in sand molds) also prevents the production of thin walls.

Il a été proposé dans le brevet FR 623 803 un échangeur multitubulaire dont le corps est constitué d'un tronçon de tuyau ordinaire et est dénué de brides d'extrémité ; cette technique rend difficile et/ou coûteuse la réalisation de raccords étanches d'entrée et de sortie du deuxième fluide dans la cavité.It has been proposed in the patent FR 623803 a multitubular exchanger whose body consists of an ordinary pipe section and is devoid of end flanges; this technique makes it difficult and / or expensive to produce sealed connections for entering and leaving the second fluid in the cavity.

Il a été décrit dans le document EP-A-1 146 310 un échangeur dont la calandre extrudée présente une nervure externe dans laquelle sont prévus les orifices d'entrée et de sortie du deuxième fluide, qui remédie à ce problème ; cet échangeur ne comporte pas de moyen de liaison rigide entre le corps creux et le faisceau tubulaire, la liaison mécanique entre ces éléments résultant essentiellement des forces de contact (d'appui) s'exerçant entre ces deux pièces par l'intermédiaire d'organes d'étanchéité tels que deux joints toriques, qui sont aplatis (comprimés) entre deux faces cylindriques d'appui (ou portées) prévues respectivement sur chacune de ces deux pièces; en l'absence de ces organes d'étanchéité, le faisceau peut librement coulisser dans la cavité du corps ; en présence de ces organes d'étanchéité le faisceau peut coulisser dans la cavité sous l'action d'un effort suffisant, en particulier sous l'action de l'allongement des tubes du faisceau, du fait de leur dilatation thermique ; chacun des organes d'étanchéité est logé dans une gorge annulaire prévue sur la face externe des plaques tubulaires ; ceci permet d'éviter la réalisation de gorges sur la face interne de la paroi du corps creux qui ne nécessite alors que la réalisation d'un chanfrein à son (ses) extrémité(s) interne(s) ; cela permet d'introduire par coulissement un faisceau dont la plaque tubulaire est munie du joint d'étanchéité sans détériorer ce joint et en facilitant son écrasement.It was described in the document EP-A-1 146 310 an exchanger whose extruded calender has an external rib in which are provided the inlet and outlet ports of the second fluid, which overcomes this problem; this exchanger does not comprise rigid connection means between the hollow body and the tubular bundle, the mechanical connection between these elements resulting essentially from the contact forces (of support) exerted between these two parts by means of organs such as two O-rings, which are flattened (compressed) between two cylindrical bearing faces (or spans) provided respectively on each of these two pieces; in the absence of these sealing members, the beam can slide freely in the body cavity; in the presence of these sealing members the beam can slide in the cavity under the action of a sufficient force, in particular under the action of the elongation of the tubes of the beam, because of their thermal expansion; each of the sealing members is housed in an annular groove provided on the outer face of the tubular plates; this avoids the realization of grooves on the inner face of the wall of the hollow body which then only requires the realization of a chamfer at its (their) end (s) internal (s); this allows to introduce by sliding a beam whose tubular plate is provided with the seal without damaging the seal and facilitating its crushing.

On connaît également des documents US 1 994 779 et US 3 363 680 , des échangeurs à faisceaux multitubulaires dans lesquels le blocage du faisceau est effectué par insertion en butée d'embouts tubulaires intercalaires entre le faisceau et la calandre de l'échangeur.Documents are also known US 1,994,779 and US 3,363,680 , multitubular beam exchangers in which the blocking of the beam is carried out by insertion abutting intermediate tubular ends between the beam and the shell of the exchanger.

Un objectif de l'invention est de proposer de tels échangeurs qui soient améliorés, ainsi qu'un procédé de fabrication de ces échangeurs qui permet d'en réduire le coût.An object of the invention is to provide such exchangers that are improved, and a method of manufacturing these exchangers that reduces the cost.

Selon un premier aspect, l'invention consiste à proposer de tels échangeurs dans lesquels un engagement mutuel de la calandre et du faisceau forme une butée à l'intérieur de la cavité délimitée par la calandre, qui empêche ou limite un déplacement du faisceau par rapport à la calandre ; lesdits échangeurs étant conformes à la revendication 1.According to a first aspect, the invention consists in proposing such exchangers in which a mutual engagement of the shell and the beam forms an abutment inside the cavity delimited by the shell, which prevents or limits a displacement of the beam relative to at the front grille; said exchangers being in accordance with claim 1.

Cet engagement mutuel peut résulter d'une déformation d'une pièce du faisceau et/ou d'une partie de la calandre, ou bien de l'insertion d'un organe formant butée (ou épaulement) à l'intérieur de la cavité cylindrique délimitée par la calandre ; dans tous les cas, ces déformations et/ou insertions sont effectuées après que le faisceau a été introduit et correctement positionné à l'intérieur de la calandre.This mutual engagement can result from a deformation of a part of the beam and / or part of the shell, or the insertion of a member forming a stop (or shoulder) inside the cylindrical cavity bounded by the grille; in all cases, these deformations and / or insertions are made after the beam has been introduced and correctly positioned inside the shell.

Ceci permet d'empêcher ou de limiter la rotation et/ou la translation du faisceau tubulaire à l'intérieur de la calandre. Ceci permet par conséquent d'utiliser des chicanes ne présentant pas une symétrie centrale comme c'est le cas des chicanes en forme de disques décrites dans le document EP 1 146 310 ; ceci permet notamment d'utiliser des chicanes en forme de portion de disque - ou de disque coupé -, et un faisceau multitubulaire comportant un ou plusieurs tubes s'étendant selon - ou à proximité immédiate de - l'axe longitudinal central du faisceau ; par conséquent, la répartition et/ou le nombre des tubes du faisceau peut être amélioré (augmenté) - pour une cavité de volume déterminé -, et le rendement et/ou la compacité de l'échangeur est ainsi également augmenté(e).This makes it possible to prevent or limit the rotation and / or the translation of the tubular bundle inside the shell. This therefore makes it possible to use baffles that do not have central symmetry, as is the case with the disk-shaped baffles described in the document. EP 1 146 310 ; this makes it possible in particular to use baffles in the shape of a portion of a disc - or disc cut - and a multitubular bundle having one or more tubes extending along - or in close proximity to - the central longitudinal axis of the bundle; therefore, the distribution and / or the number of tubes of the beam can be improved (increased) - for a cavity of a given volume -, and the efficiency and / or compactness of the exchanger is thus also increased (e).

De préférence, cette butée est en partie au moins réalisée par une saillie prévue sur la face interne de la paroi de la calandre, de sorte qu'il n'est pas nécessaire de fabriquer à cet effet une pièce séparée de la calandre.Preferably, this stop is partly at least provided by a projection provided on the inner face of the calender wall, so that it is not necessary to manufacture for this purpose a separate part of the calender.

De préférence encore, cette saillie ou rétrécissement formant butée s'étend sur une partie seulement du contour circulaire transversal interne de la calandre. La réalisation de cette butée est encore simplifiée en la réalisant autour d'un des orifices d'entrée et de sortie de fluide dans la cavité délimitée dans la calandre, en particulier en repoussant une partie au moins d'une collerette, vers l'intérieur de la cavité ; en complément ou alternativement, la saillie peut être réalisée à la périphérie d'une paroi mince du faisceau, en particulier d'une languette solidaire d'une plaque tubulaire du faisceau, en repoussant cette paroi mince ou languette vers l'extérieur de la cavité, de façon à obtenir soit une liaison rigide par friction entre le faisceau et la calandre, soit un blocage par pénétration de la paroi ou languette dans un orifice formé dans la paroi de la calandre, en particulier dans un desdits orifices d'entrée ou de sortie de fluide.More preferably, this projection or narrowing forming a stop extends over only a portion of the inner transverse circular contour of the shell. The realization of this abutment is further simplified by making it around one of the fluid inlet and outlet ports in the cavity defined in the shell, in particular by pushing at least a portion of a flange, towards the inside. cavity; in addition or alternatively, the projection may be made at the periphery of a thin wall of the bundle, in particular of a tab integral with a tubular plate of the bundle, by pushing this thin wall or tongue towards the outside of the cavity , so as to obtain either a rigid frictional connection between the beam and the shell, or a blockage by penetration of the wall or tongue into an orifice formed in the wall of the shell, in particular in one of said inlet or outlet orifices. fluid outlet.

Selon un autre mode possible de réalisation, cette saillie peut être incorporée à l'extrémité d'une pièce de raccordement de la calandre à un conduit de transport de ce fluide - ci-avant dénommé deuxième fluide - ; par exemple, cette saillie peut consister en une portion tubulaire prolongeant un raccord vissé dans un trou taraudé prévu dans la paroi de la calandre ; ceci peut permettre d'obtenir une liaison rigide entre le faisceau et la calandre, qui est réversible (démontable).According to another possible embodiment, this projection may be incorporated at the end of a connecting part of the shell to a conduit for transporting this fluid - hereinafter referred to as second fluid -; for example, this projection may consist of a tubular portion extending a connection screwed into a threaded hole provided in the wall of the calender; this may allow to obtain a rigid connection between the beam and the shell, which is reversible (removable).

Selon un mode préféré de réalisation, cette saillie est essentiellement constituée par une portion de la paroi de la calandre, et est prévue (et/ou s'étend) autour d'un desdits orifices (d'entrée et de sortie de fluide) au moins ; de préférence, la butée ou saillie est apte à s'engager dans une dépression ou échancrure prévue à la périphérie d'une pièce du faisceau tubulaire - de préférence à la périphérie d'une partie d'une plaque tubulaire.According to a preferred embodiment, this projection consists essentially of a portion of the wall of the shell, and is provided (and / or extends) around one of said orifices (inlet and outlet fluid) to less; preferably, the abutment or projection is adapted to engage in a depression or indentation provided at the periphery of a part of the tubular bundle - preferably at the periphery of a portion of a tubular plate.

Dans ce dernier cas, cette pièce qui comporte une première partie en forme de disque percée de trous de passage et de fixation des tubes du faisceau, et une deuxième partie en forme de tube ou bride circulaire s'étendant longitudinalement à partir de la face interne de la première partie en forme de disque, comporte de préférence une échancrure ou dépression de profil sensiblement circulaire et d'un diamètre adapté aux dimensions de la butée saillante sur la face interne de la calandre, cette échancrure ou dépression étant intégrée à la deuxième partie de la plaque tubulaire.In the latter case, this part which comprises a first disk-shaped portion pierced with holes for passing and fixing the tubes of the bundle, and a second portion in the form of a tube or circular flange extending longitudinally to from the inner face of the first disk-shaped portion, preferably comprises a notch or depression of substantially circular profile and a diameter adapted to the dimensions of the abutment protruding on the inner face of the calender, this notch or depression being integrated in the second part of the tube plate.

Dans le cas où deux telles butées saillantes faisant partie intégrante de la calandre sont prévues autour de chacun des deux orifices de passage du deuxième fluide, ces butées coopérant respectivement avec deux échancrures prévues dans deux plaques tubulaires, le faisceau ne peut alors être extrait de la cavité, la liaison étant généralement irréversible.In the case where two such protruding abutments forming an integral part of the calender are provided around each of the two orifices for the passage of the second fluid, these abutments cooperating respectively with two indentations provided in two tubular plates, the beam can not then be extracted from the cavity, the bond being generally irreversible.

De préférence, de telles butées saillantes intégrées sont réalisées par déformation d'une collerette prévue dans la paroi de la calandre, à l'extrémité interne d'un conduit de passage du deuxième fluide prévu dans cette paroi ; ce procédé de réalisation est particulièrement simple et peu coûteux ; cette déformation doit généralement être réalisée après avoir mis le faisceau tubulaire à son emplacement définitif dans la cavité délimitée par la calandre.Preferably, such integrated protruding abutments are formed by deformation of a flange provided in the wall of the calender, at the inner end of a passage duct of the second fluid provided in this wall; this production method is particularly simple and inexpensive; this deformation must generally be performed after putting the tube bundle at its final location in the cavity defined by the shell.

Ainsi, selon un autre aspect, l'invention propose un procédé de fabrication d'un échangeur à faisceau multitubulaire et calandre selon la revendication 17. Selon un mode particulier de mise en oeuvre du procédé selon l'invention, pour fabriquer un échangeur de chaleur multitubulaire comportant une calandre extrudée et un faisceau multitubulaire comportant deux plaques tubulaires équipées d'une dépression ou échancrure à leur périphérie, on effectue successivement les opérations suivantes :

  • On perce la paroi de la calandre d'un orifice d'entrée et d'un orifice de sortie de fluide de façon à réaliser deux conduits de passage du fluide dans cette paroi, chaque conduit présentant, du côté de la face interne de la calandre, une ouverture rétrécie résultant d'une collerette annulaire obtenue lors du perçage de la paroi à l'aide d'un foret profilé (épaulé),
  • On taraude une partie de chaque conduit de passage - à l'exclusion de la collerette -, de façon à permettre le vissage d'un raccord dans chaque orifice taraudé,
  • On engage le faisceau dans la calandre et on positionne les échancrures ou dépressions dans le prolongement respectif de chaque conduit de passage percé dans la calandre,
  • En empêchant le déplacement du faisceau dans la calandre, on déforme chaque collerette en exerçant sur elles - à l'aide d'un outil présentant de préférence une portée sphérique - un effort (radial) suffisant, jusqu'à ce qu'une partie au moins de chaque collerette faisant saillie sur la face interne de la paroi de la calandre, soit respectivement engagée dans la dépression ou échancrure correspondante, de sorte que le faisceau est immobilisé dans la calandre.
Thus, according to another aspect, the invention proposes a method for manufacturing a shell-and-tube heat exchanger according to claim 17. According to a particular embodiment of the method according to the invention, for manufacturing a heat exchanger multitubular comprising an extruded calender and a multitubular bundle comprising two tubular plates equipped with a depression or indentation at their periphery, the following operations are carried out successively:
  • The wall of the shell is pierced with an inlet orifice and a fluid outlet orifice so as to produce two fluid passage ducts in this wall, each duct having, on the side of the internal face of the shell a narrowed opening resulting from an annular flange obtained during the drilling of the wall using a profiled drill (shouldered),
  • One part of each passage duct is screwed - excluding the flange -, so as to allow the screwing of a connection in each threaded orifice,
  • The beam is engaged in the calender and the indentations or depressions are positioned in the respective extension of each passage duct pierced in the calender,
  • By preventing the displacement of the beam in the calender, each flange is deformed by exerting on them - with the aid of a tool preferably having a spherical bearing - a sufficient (radial) force, until a portion of less than each flange protruding from the inner face of the wall of the calender, is respectively engaged in the corresponding depression or notch, so that the beam is immobilized in the calender.

Selon un autre aspect, ce procédé peut en outre comprendre les caractéristiques de la revendication 19.In another aspect, this method may further include the features of claim 19.

On décrit, ci-après, un échangeur à faisceau multitubulaire et à calandre tubulaire, le faisceau comportant deux plaques tubulaires, au moins une plaque - et de préférence chaque - plaque comportant : i) une première partie en forme de disque percé d'orifices recevant les tubes du faisceau ; le cas échéant ii) une deuxième partie s'étendant à partir de la face interne de la première partie et incorporant soit un logement prévu pour recevoir une butée faisant saillie sur la face interne de la calandre, soit une paroi ou languette expansible prévue pour s'engager - après déformation - dans un orifice formé dans la paroi de la calandre ; iii) une troisième partie de forme tubulaire s'étendant à partir de la face externe de la première partie, et prévue pour être engagée dans une extrémité d'un conduit de transport du premier fluide fixé à la troisième partie de la plaque par emmanchement forcé et/ou par cerclage ; de préférence, la troisième partie tubulaire comporte à cet effet une nervure annulaire externe.A tubular shell-and-tube heat exchanger is described hereinafter, the bundle having two tubular plates, at least one plate - and preferably each - plate comprising: i) a first disk-shaped portion pierced with orifices receiving the tubes of the beam; if necessary ii) a second part extending from the internal face of the first part and incorporating either a housing provided to receive a stop protruding from the inner face of the shell, or an expandable wall or tongue provided for s engage - after deformation - in an orifice formed in the wall of the calender; iii) a third portion of tubular form extending from the outer face of the first portion, and adapted to be engaged in an end of a transport duct of the first fluid fixed to the third part of the plate by forced fitting and / or by strapping; preferably, the third tubular portion comprises for this purpose an outer annular rib.

Ceci permet notamment de diminuer le nombre de joints d'étanchéité nécessaires.This allows in particular to reduce the number of seals required.

D'autres avantages et caractéristiques de l'invention seront compris au travers de la description suivante qui se réfère aux dessins annexés, et qui illustre sans aucun caractère limitatif des modes préférentiels de réalisation de l'invention.

  • La figure 1 est une vue en perspective d'un mode préféré de réalisation d'un échangeur selon l'invention.
  • La figure 2 est une vue en coupe longitudinale d'une calandre d'un échangeur selon l'invention.
  • La figure 3 est une vue en coupe transversale - selon III - de la calandre illustrée figure 2 ; la figure 4 est une vue de détail à échelle agrandie - selon IV - d'un des passages de fluide percés dans la paroi de la calandre illustrée figure 2.
  • La figure 5 est une vue en coupe longitudinale d'un faisceau tubulaire d'un échangeur selon l'invention.
  • La figure 6 est une vue schématique en coupe transversale - selon VI - VI du faisceau illustré figure 5.
  • La figure 7 est une vue de côté d'une pièce formant plaque tubulaire et manchon de raccordement, qui comporte une échancrure demi-circulaire de positionnement à sa périphérie interne.
  • La figure 8 est une vue de côté montrant schématiquement l'assemblage du faisceau et de la calandre.
  • Les figures 9 et 10 illustrent une variante de réalisation de l'invention dans laquelle une languette solidaire d'une plaque tubulaire du faisceau est engagée dans un orifice de passage de fluide percé dans une nervure de la calandre ; la figure 10 est une vue en coupe longitudinale - selon X-X- de la figure 9 ; cette dernière est une vue de dessus d'une extrémité d'un échangeur.
  • Les figures 11 et 12 illustrent une variante de réalisation de l'invention dans laquelle un manchon tubulaire de raccordement servant de butée d'immobilisation du faisceau est engagé dans un orifice de passage de fluide percé dans une nervure de la calandre ; la figure 12 est une vue en coupe longitudinale - selon XII-XII- de la figure 11 ; cette dernière est une vue de dessus d'une extrémité d'un échangeur.
Other advantages and features of the invention will be understood through the following description which refers to the accompanying drawings, and which illustrates without any limiting nature of the preferred embodiments of the invention.
  • The figure 1 is a perspective view of a preferred embodiment of an exchanger according to the invention.
  • The figure 2 is a longitudinal sectional view of a shell of an exchanger according to the invention.
  • The figure 3 is a cross-sectional view - according to III - of the illustrated grille figure 2 ; the figure 4 is a detail view on an enlarged scale - according to IV - of one of the fluid passages pierced in the wall of the illustrated grille figure 2 .
  • The figure 5 is a longitudinal sectional view of a tubular bundle of an exchanger according to the invention.
  • The figure 6 is a schematic cross-section - along VI - VI of the illustrated beam figure 5 .
  • The figure 7 is a side view of a piece forming a tubular plate and connecting sleeve, which has a semicircular positioning notch at its inner periphery.
  • The figure 8 is a side view schematically showing the assembly of the beam and the shell.
  • The Figures 9 and 10 illustrate an alternative embodiment of the invention in which a tab integral with a tubular plate of the bundle is engaged in a fluid passage hole pierced in a rib of the shell; the figure 10 is a longitudinal sectional view - according to XX- of the figure 9 ; the latter is a top view of one end of a heat exchanger.
  • The Figures 11 and 12 illustrate an alternative embodiment of the invention in which a tubular connecting sleeve serving as immobilizing stop beam is engaged in a fluid passage hole pierced in a rib of the calender; the figure 12 is a view in longitudinal section - according to XII-XII- of the figure 11 ; the latter is a top view of one end of a heat exchanger.

Sauf indication contraire, des éléments, pièces et organes identiques ou similaires illustrés sur plusieurs figures, sont repérés par un repère invariable d'une figure à une autre.Unless otherwise indicated, elements, parts and the same or similar members shown in several figures, are identified by an invariable reference from one figure to another.

Par référence à la figure 1, l'échangeur 1 comporte une calandre 2 d'axe longitudinal 3, et un faisceau tubulaire logé dans la cavité délimitée dans la calandre ; la calandre présente une pluralité de faces externes planes 4 à 13 (voir figure 3) allongées et parallèles à l'axe 3 ; sur la face 10 débouchent deux canaux 14 et 15 de raccordement de la cavité délimitée par la calandre à un fluide tel que de l'huile à refroidir.By reference to the figure 1 , the exchanger 1 comprises a shell 2 of longitudinal axis 3, and a tubular bundle housed in the cavity defined in the shell; the shell has a plurality of flat outer faces 4 to 13 (see figure 3 ) elongate and parallel to the axis 3; on the face 10 open two channels 14 and 15 connecting the cavity defined by the shell to a fluid such as oil to be cooled.

La calandre est obtenue par extrusion d'aluminium ; le profilé résultant est trempé et coupé en tronçons tels que celui illustré figures 2 et 3 ; chaque extrémité longitudinale est usinée pour obtenir un chanfrein 16, 17 facilitant l'introduction du faisceau tubulaire équipé de deux joints annulaires d'étanchéité (repères 19, 20 figure 8) dans la cavité 18 délimitée par la calandre, sans détériorer les joints.The calender is obtained by extrusion of aluminum; the resulting profile is soaked and cut into sections such as that illustrated Figures 2 and 3 ; each longitudinal end is machined to obtain a chamfer 16, 17 facilitating the introduction of the tubular bundle equipped with two annular sealing seals (pins 19, 20 figure 8 ) in the cavity 18 defined by the calender, without damaging the seals.

Les parois 10 à 12 délimitent une nervure longitudinale 23 parallèle à l'axe 3, dans laquelle sont percés les canaux 14, 15 d'axes 21 et 22 radiaux.The walls 10 to 12 delimit a longitudinal rib 23 parallel to the axis 3, in which are drilled the channels 14, 15 of axes 21 and 22 radial.

Par référence aux figures 2 à 4, chaque conduit 14, 15 comporte une partie externe 24 filetée s'étendant à partir de la face 10 pour permettre le vissage d'un raccord non représenté ; la partie interne du conduit par laquelle celui-ci débouche sur la face interne cylindrique 25 de la cavité 18, présente un diamètre 26 inférieur au diamètre 27 de l'orifice par lequel le conduit débouche sur la face 10 ; ceci résulte de la présence d'une collerette 28 annulaire formée dans la paroi 23 lors du perçage des conduits 14, 15 par un foret profilé à cet effet ; la collerette 28 présente une épaisseur 29 suffisamment faible (par exemple de l'ordre de 1 à 2 millimètres) pour pouvoir être déformée par l'action d'un outil appuyé sur la face interne 30 inclinée, selon la flèche 31 figure 4 ; ceci permet de faire passer une partie au moins de cette collerette de la configuration initiale - repère 28 figure 4 - où la collerette est affleurante à la face 25, à la configuration finale - repérée 28a figure 4 - où la collerette déformée fait saillie par rapport à la face 25, d'une valeur 32, par exemple voisine d'un ou deux millimètres ; dans cette dernière configuration, la collerette est engagée dans une dépression prévue à la périphérie de la plaque tubulaire - comme décrit ci-après - de sorte qu'elle immobilise le faisceau dans la calandre.By reference to Figures 2 to 4 each conduit 14, 15 has a threaded outer portion 24 extending from the face 10 to allow the screwing of a not shown fitting; the inner portion of the conduit through which the latter opens on the cylindrical inner face 25 of the cavity 18, has a diameter 26 smaller than the diameter 27 of the orifice through which the conduit opens on the face 10; this results from the presence of an annular flange 28 formed in the wall 23 during the drilling of the ducts 14, 15 by a profiled drill for this purpose; the flange 28 has a thickness 29 sufficiently low (for example of the order of 1 to 2 millimeters) to be deformed by the action of a tool supported on the inner face 30 inclined, according to the arrow 31 figure 4 ; this makes it possible to pass at least part of this flange of the initial configuration - reference 28 figure 4 - where the flange is flush with the face 25, the final configuration - marked 28a figure 4 - Where the deformed flange protrudes from the face 25, a value 32, for example close to one or two millimeters; in this latter configuration, the flange is engaged in a depression provided at the periphery of the tube plate - as described below - so that it immobilizes the beam in the calender.

Ce mode de déformation de la collerette nécessite d'utiliser un matériau présentant un allongement à la rupture suffisant, pour la réalisation de la calandre ; à cet effet, l'utilisation d'aluminium extrudé et trempé est plus favorable que celle d'aluminium moulé et/ou injecté.This mode of deformation of the collar requires the use of a material having sufficient elongation at break, for producing the calender; for this purpose, the use of extruded and tempered aluminum is more favorable than that of cast aluminum and / or injected.

Selon des variantes de réalisation, le profilé creux (ou barre tubulaire) utilisé pour former la calandre peut être obtenu par extrusion de matière plastique, ou par filage à chaud ou étirage à froid d'un métal, en particulier un alliage d'aluminium, de cuivre ou d'acier.According to alternative embodiments, the hollow section (or tubular bar) used to form the shell may be obtained by extrusion of plastic material, or by hot spinning or cold drawing of a metal, in particular an aluminum alloy, of copper or steel.

Par référence aux figures 5 à 7 en particulier, le faisceau 34 comporte une pluralité de tubes 35 parallèles à son axe longitudinal 33, une pluralité de chicanes 36, 37 planes perpendiculaires à l'axe 33, et deux pièces 38 d'extrémité.By reference to Figures 5 to 7 in particular, the beam 34 comprises a plurality of tubes 35 parallel to its longitudinal axis 33, a plurality of flat baffles 36, 37 perpendicular to the axis 33, and two end pieces 38.

Le contour des chicanes 36, 37 est en grande partie circulaire (de diamètre adapté à celui de la cavité 18) et en partie rectiligne 36a, 37a, de sorte que les chicanes ont une forme de disque tronqué ; les chicanes 36 présentant leur bord rectiligne 36a en partie inférieure sont disposées, le long de l'axe 33, en alternance avec les chicanes 37 présentant leur bord rectiligne 37a en partie supérieure, de sorte que ces chicanes délimitent avec la calandre un labyrinthe obligeant le deuxième fluide à suivre un trajet sinueux 39 figure 5.The contour of the baffles 36, 37 is largely circular (of diameter adapted to that of the cavity 18) and partly rectilinear 36a, 37a, so that the baffles have a truncated disk shape; the baffles 36 having their rectilinear edge 36a in the lower part are arranged, along the axis 33, alternately with the baffles 37 having their rectilinear edge 37a in the upper part, so that these baffles delimit with the calender a labyrinth forcing the second fluid to follow a sinuous path 39 figure 5 .

Chaque pièce 38 comporte une première partie 380 en forme de disque épais dans laquelle sont percés des orifices recevant les extrémités 350 des tubes 35 ; cette partie, qui s'étend transversalement à l'axe 33, forme la plaque tubulaire proprement dite.Each piece 38 has a first portion 380 in the form of a thick disc in which holes are drilled receiving the ends 350 of the tubes 35; this part, which extends transversely to the axis 33, forms the tubular plate itself.

La première partie 380 est prolongée à la périphérie de sa face interne 3800 par une deuxième partie 381 de la pièce 38, qui est en forme d'un court tronçon de tube mince d'axe 33 ; à une extrémité de ce tronçon, une encoche 3810 est formée dans la paroi tubulaire du tronçon, qui s'étend selon un tracé circulaire dont le diamètre 40 est adapté aux dimensions (en particulier au diamètre) de la saillie 28a (figure 4) formée sur la face interne de la calandre.The first portion 380 is extended at the periphery of its inner face 3800 by a second portion 381 of the workpiece 38, which is in the form of a short section of thin tube with an axis 33; at one end of this section, a notch 3810 is formed in the tubular wall of the section, which extends in a circular pattern whose diameter 40 is adapted to the dimensions (in particular to the diameter) of the projection 28a ( figure 4 ) formed on the inner face of the shell.

La première partie 380 de la pièce 38 est en outre prolongée à la périphérie de sa face externe 3801 par une troisième partie 382 de la pièce 38 qui est grossièrement en forme d'un tronçon de tube d'axe 33 et dont la face externe comporte une rainure annulaire 41 prévue pour recevoir un des joints (19, 20 figure 8) d'étanchéité avec la calandre, ainsi qu'une nervure 42 annulaire qui fait saillie par rapport à la portion 3820 centrale de cette partie 382 ; cette dernière peut ainsi, comme illustré figure 7, recevoir une extrémité d'un tube 43 de raccordement emmanché en force autour de la nervure 42 et de la partie cylindrique 3820 contre laquelle le tube 43 peut être maintenu serré par un collier de cerclage non représenté.The first part 380 of the part 38 is further extended at the periphery of its external face 3801 by a third part 382 of the part 38 which is roughly in the shape of a tube section with an axis 33 and whose external face comprises an annular groove 41 provided for receiving one of the seals (19, 20 figure 8 ) sealing with the calender, and an annular rib 42 which protrudes from the central portion 3820 of this portion 382; the latter can thus, as illustrated figure 7 , receiving one end of a connection tube 43 force-fitted around the rib 42 and the cylindrical portion 3820 against which the tube 43 can be held tight by a strapping collar not shown.

Dans la configuration d'assemblage illustrée figure 8, chacune des encoches prévues dans les pièces d'extrémité est disposée respectivement en regard des orifices d'entrée et de sortie 14, 15 et reçoit une partie des saillies annulaires prolongeant-ces orifices, de sorte que le faisceau est immobilisé dans la calandre.In the illustrated assembly configuration figure 8 , each of the notches provided in the end pieces is respectively disposed opposite the inlet and outlet ports 14, 15 and receives a portion of the annular protrusions extending-these orifices, so that the beam is immobilized in the calender.

Par référence aux figures 9 et 10, la partie tubulaire 381 d'axe 33 prolongeant la plaque tubulaire 380 du faisceau, comporte une portion 3811 en forme de languette qui a été déformée après positionnement du faisceau dans la calandre, de sorte qu'elle s'étend à l'intérieur de l'orifice 14 de passage de fluide, en appui contre la paroi délimitant cet orifice ; la languette 3811 empêche un coulissement du faisceau dans la calandre, selon leur axe commun 3, 33 dans la direction repérée par la flèche 100 ; en équipant en outre la deuxième plaque tubulaire (non représentée) du même échangeur d'une telle languette, on interdit également un tel coulissement dans la direction opposée, ainsi qu'une rotation du faisceau.By reference to Figures 9 and 10 the tubular portion 381 of axis 33 extending tubular plate 380 of the bundle comprises a tongue-shaped portion 3811 which has been deformed after positioning the bundle in the shell, so that it extends inside the the orifice 14 for fluid passage, bearing against the wall delimiting this orifice; the tongue 3811 prevents the beam from sliding in the shell, along their common axis 3, 33 in the direction indicated by the arrow 100; by also equipping the second tube plate (not shown) of the same heat exchanger of such a tongue, it is also prohibited such sliding in the opposite direction, and a rotation of the beam.

Par référence aux figures 11 et 12, un manchon tubulaire 99 s'étend à l'intérieur du conduit 14 de passage de fluide percé dans la nervure 23 de la calandre, selon l'axe 21 du conduit 14, sur les parois duquel conduit ce manchon s'appuie.By reference to Figures 11 and 12 , a tubular sleeve 99 extends inside the conduit 14 for fluid passage drilled in the rib 23 of the shell, along the axis 21 of the conduit 14, on the walls of which leads this sleeve is supported.

Le manchon 99 fait saillie par rapport à la face interne 25 de la calandre ; de ce fait, il est engagé dans une encoche 3810 identique ou similaire à celle décrite ci-avant, de sorte qu'il limite le coulissement du faisceau dans la calandre ; en équipant en outre un deuxième conduit (tel que repéré 15) par un deuxième manchon faisant saillie à l'intérieur de la calandre, on empêche le coulissement et la rotation du faisceau dans la calandre.The sleeve 99 protrudes from the inner face of the calender; therefore, it is engaged in a notch 3810 identical or similar to that described above, so that it limits the sliding of the beam in the calender; by further equipping a second conduit (as marked 15) by a second sleeve projecting inside the calender, the sliding and rotation of the beam in the calender is prevented.

Claims (19)

  1. A heat exchanger comprising a multi-tube bundle and a shell, in which direct mutual engagement between the shell and the bundle forms an abutment inside a cavity defined by the shell, the said shell presenting an inlet orifice (14) for admitting fluid into the cavity and an outlet orifice (15) for exhausting fluid from the cavity, and a projection (28a, 3811, 99) placed around or within at least one of said orifices forms, at least in part, said abutment, and prevents any movement in rotation and/or translation of the bundle relative to the shell.
  2. A heat exchanger according to claim 1, wherein the said projection is a result of deforming of a portion (3811) of the bundle and/or a part (28a) of the shell.
  3. A heat exchanger according to claim 1, wherein the said projection is a result of inserting and abutment-forming member 99 inside the shell.
  4. A heat exchanger according to claim 1 or 2, wherein the said abutment is made by a projection (28a, 3811) made by chasing of a portion (28) of the inside wall (25) of the shell towards the inside of the cavity (18) or of a thin wall (3811) of the bundle towards the outside of the cavity.
  5. A heat exchanger according to claim 4, wherein the said projection extends over a fraction only of the inside transverse circular outline of the shell.
  6. A heat exchanger according to anyone of claims 1 to 5, wherein said orifices (14, 15) present a collar (28) of small thickness to allow it to be deformed under drive from a tool pressed against inside of the cavity (18) defined by the shell and to form a said projection (28).
  7. A heat exchanger according to anyone of claims 1 to 6, in which the shell presents at least one outside longitudinal spline (23) through which the orifices (14, 15) are pierced.
  8. A heat exchanger according to anyone of claims 1 to 7, in which the bundle includes baffles (36, 37) in the form of truncated disks and/or in the form of disk portions, and in which the said deformation of the bundle or the shell forms an abutment preventing or restricting movement in rotation and/or translation of the bundle in the cavity.
  9. A heat exchanger according to anyone of claims 1 to 8, in which the bundle has an end tube plate (380) and a cap (382) for coupling the heat exchanger to a duct (43) for transporting fluid that flows in the tubes of the bundle, and in which the tube plate and the cap form a single piece (38).
  10. A heat exchanger according to claim 9, in which the cap presents an annular rib (42) situated on an external tubular and/or cylindrical portion of the cap so as to enable a duct (43) to be secured to the cap by forced engagement and/or by clamping.
  11. A heat exchanger according to anyone of claims 1 to 10, in which the abutment co-operates with a part secured to the tube plate of the bundle to prevent or restrict sliding and/or turning of the bundle of tubes inside the cavity.
  12. A heat exchanger according to claim 11, in which the tube plate presents a setback or notch (3810) co-operating with an abutment (28a) projecting from the inside face of the wall (25) of the shell.
  13. A heat exchanger according to anyone of claims 1 to 12, in which the bundle (34) has two tube plates (38, 380), each having an annular groove (41) in its outside face receiving a seal bearing against a cylindrical bearing surface of the shell.
  14. A heat exchanger according to anyone of claims 1 to 13, in which the shell is constituted essentially by at least a segment of hollow section member defining a cylindrical cavity.
  15. A heat exchanger according to claim 14, in which the section member is made of metal which has been drawn or extruded.
  16. a heat exchanger according to claim 15, wherein the section member is made of aluminum which has been extruded or quenched.
  17. A method of manufacturing a heat exchanger with a multi-tube bundle and a shell according to anyone of claims 1 to 16, in which a portion of the bundle or of the shell is deformed so as to cause the shell and the bundle to be mutually engaged, thereby forming an abutment inside the cavity defined by the shell for limiting or restricting movement into rotation and/or translation of the bundle inside the shell, the said shell presenting said inlet and outlet orifices for fluid and the said abutment is made by a said projection (28a, 3811, 99) placed around or in at least one of said orifices, by deforming of a portion (3811) of the bundle and/or a part (28a) of the shell or by inserting and abutment-forming member 99 inside the shell.
  18. A method according to claim 17 for making a multi-tube heat exchanger comprising a shell (2) and a multi-tube bundle (34) having two tube plates each fitted with a setback or notch (3810) at its periphery, in which method, the following operations are performed in succession:
    · piercing the wall (23) of the shell by means of a shaped drill bit to form an inlet orifice (14) and an outlet orifice (15) for fluid so as to provide two fluid flow ducts through said wall, each duct presenting adjacent to the inside face of the shell, a narrowed opening that results from an annular collar (28) obtained while piercing the wall;
    · tapping each fluid flow duct over a portion excluding its collar so as to enable a coupling to be screwed into each tapped orifice;
    · engaging the bundle in the shell and positioning the notches or setbacks respectively in line with each of the fluid flow ducts pierced through the shell; and
    · while preventing the bundle from moving inside the shell, deforming at least a portion of each collar by exerting sufficient force thereon until at least a portion of each collar projects (28a) from the inside face of the wall (25) of the shell and is engaged in the corresponding setback or notch so that the bundle is prevented from moving inside the shell.
  19. A method according to claim 17 for manufacturing a multi-tube heat exchanger comprising a shell (2) and a multi-tube bundle (34) comprising two tubular plates (380) equipped with a tongue (3811), in which the successive following steps are carried out :
    · piercing the wall (23) of the shell to form an inlet orifice (14) and an outlet orifice (15) for fluid so as to provide two fluid flow ducts through said wall, each duct presenting adjacent to the inside face of the shell, a opening obtained while piercing the wall by means of a shaped drill bit,
    · positioning the bundle inside the shell and deforming a portion at least of each tongue (3811) so as to extend respectively inside each orifice (14, 15) in the wall of the shell, and press against the wall defining each said orifice, the tongues (3811) preventing the bundle from sliding or rotating inside the shell.
EP03358008A 2002-06-21 2003-06-18 Multi tubular heat exchangers and process for making same Expired - Lifetime EP1376039B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0207708A FR2841331B1 (en) 2002-06-21 2002-06-21 MULTITUBULAR EXCHANGERS AND METHOD OF MANUFACTURING THESE EXCHANGERS
FR0207708 2002-06-21

Publications (2)

Publication Number Publication Date
EP1376039A1 EP1376039A1 (en) 2004-01-02
EP1376039B1 true EP1376039B1 (en) 2008-11-12

Family

ID=29717077

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03358008A Expired - Lifetime EP1376039B1 (en) 2002-06-21 2003-06-18 Multi tubular heat exchangers and process for making same

Country Status (5)

Country Link
US (1) US6840306B2 (en)
EP (1) EP1376039B1 (en)
AT (1) ATE414252T1 (en)
DE (1) DE60324631D1 (en)
FR (1) FR2841331B1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7243711B2 (en) * 2004-03-30 2007-07-17 Caterpillar Inc. Efficient heat exchanger and engine using same
FR2871559B1 (en) * 2004-06-14 2006-09-22 Georges Favier COMPACT HEAT PUMP HEAT OF WATER / WATER TYPE
US8794299B2 (en) * 2007-02-27 2014-08-05 Modine Manufacturing Company 2-Pass heat exchanger including thermal expansion joints
DE102008011558B4 (en) * 2007-12-12 2010-04-01 GEA MASCHINENKüHLTECHNIK GMBH heat exchangers
US8517086B2 (en) * 2008-02-29 2013-08-27 Caterpillar Inc. Composite heat exchanger end structure
SE533394C2 (en) * 2008-10-15 2010-09-14 Alfa Laval Corp Ab A plate heat exchanger
US20110083619A1 (en) * 2009-10-08 2011-04-14 Master Bashir I Dual enhanced tube for vapor generator
KR102001250B1 (en) * 2013-07-12 2019-07-19 한국전력공사 Heat exchanger with multi flow path
EA029786B1 (en) * 2016-08-05 2018-05-31 Общество с ограниченной ответственностью Урало-Сибирская Компания "НЕКСАН" Shell-and-tube condenser
EP3564613A1 (en) * 2018-05-03 2019-11-06 Mann+Hummel GmbH Heat exchanger, air intake system with a heat exchanger and method for mounting a heat exchanger
JP7042383B1 (en) * 2021-10-29 2022-03-25 岩井機械工業株式会社 Multi-tube heat exchanger and heat exchange system

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR623803A (en) 1925-11-02 1927-07-01 Improvements to tube bundle heat exchangers
US1994779A (en) * 1932-04-16 1935-03-19 Andale Co Heat exchange apparatus
US1955006A (en) * 1932-12-02 1934-04-17 Standard Oil Dev Co Lubricated baffle for heat exchangers
GB734008A (en) * 1952-02-05 1955-07-20 Bristol Aeroplane Co Ltd Improvements in or relating to heat exchangers
US2956704A (en) * 1957-05-15 1960-10-18 Griscom Russell Co Removable tube sheet construction for heat exchangers
US3079992A (en) * 1961-02-06 1963-03-05 Baldwin Lima Hamilton Corp Heat exchanger closure construction
US3223154A (en) * 1962-01-25 1965-12-14 Young Radiator Co Shell-and-tube heat-exchanger
US3363680A (en) * 1966-07-21 1968-01-16 Du Pont Plastic tube heat exchanger with novel header construction
US3915337A (en) * 1972-12-05 1975-10-28 Foster Wheeler Energy Corp Pressure vessel with shear stud closure assembly and method of assembling same
US3863713A (en) * 1973-08-27 1975-02-04 Stewart Warner Corp Heat exchanger
US3948315A (en) * 1974-08-13 1976-04-06 Brown Fintube Company Closure for heat exchanger
US4421160A (en) * 1980-10-16 1983-12-20 Chicago Bridge & Iron Company Shell and tube heat exchanger with removable tubes and tube sheets
JPS60169094A (en) * 1984-02-10 1985-09-02 Hitachi Ltd Heat exchanger
US4589478A (en) * 1985-08-19 1986-05-20 United Aircraft Products, Inc. Pressure protected tubular heat exchanger
DE3610314A1 (en) * 1986-03-26 1987-10-01 Vni I Pk I Atomnogo Energet Ma Spiral pipe heat exchanger
FR2699656B1 (en) * 1992-12-23 1995-01-13 Framatome Sa Heat exchanger with anti-seismic holding device and anti-flight support for the envelope surrounding the bundle of tubes.
FR2807508B1 (en) 2000-04-11 2002-12-13 Mota IMPROVEMENT IN CALENDERED MULTITUBULAR HEAT EXCHANGERS AND METHOD FOR MANUFACTURING SUCH EXCHANGERS

Also Published As

Publication number Publication date
EP1376039A1 (en) 2004-01-02
ATE414252T1 (en) 2008-11-15
US6840306B2 (en) 2005-01-11
FR2841331A1 (en) 2003-12-26
FR2841331B1 (en) 2005-02-25
DE60324631D1 (en) 2008-12-24
US20030234099A1 (en) 2003-12-25

Similar Documents

Publication Publication Date Title
EP1376039B1 (en) Multi tubular heat exchangers and process for making same
FR2465942A1 (en) FITTING FOR TUBULAR ELEMENTS
EP2514980A2 (en) Insert for thermoplastic support and method for assembling the insert with the support
FR2967250A1 (en) HEAT EXCHANGER WITH CONNECTING DEVICE
WO2011007075A1 (en) Assembly of coaxial pipes including junction parts with sealed inner cavities, and method for making same
EP1146310B1 (en) Improvements related to multitubular shell-type heat exchangers and method of producing the same
EP0014107A1 (en) Method of manufacturing a cylindrical sleeve with inner grooves, closed at least at one end
EP1533558B1 (en) Coaxial pipe coupling
FR2905452A1 (en) Coolant i.e. glycolated water, distributing box for heat exchanger i.e. engine cooling radiator, of motor vehicle, has collecting container including joints and orifices that receive pipes, and formed of single part of plastic material
FR2484875A1 (en)
CA2198566C (en) Casting roll for continuous casting on one or between two cylinders
EP2893278B1 (en) Exchanger element for a heat exchanger, heat exchanger comprising such an exchanger element and method for the production of such an exchanger element
FR2916828A1 (en) Three-way connector for e.g. turbo-prop of aircraft, has convex boss extending towards exterior and diametrically opposite to endpiece, where endpiece's height is two/three times pipe diameter, and thickness of pipe wall is quasi-constant
WO2008025615A1 (en) Method for manufacturing a heat exchanger tube
FR2524110A1 (en) METHOD OF MANUFACTURING A TUBE WITH CONDUITS PLACED IN ITS WALL
EP2015016A1 (en) Heat exchanger for heating tank
EP3071916A1 (en) Manifold for a heat exchanger
FR2914411A1 (en) Heat-carrier fluid e.g. glycol water, distribution housing for e.g. radiator of motor vehicle`s engine, has tubes for circulating fluid, and fluid collection casing with openings for receiving tubes and constituted of single plastic piece
WO2018138459A1 (en) Device for thermally insulating a machining attachment and machining attachment provided with such a device
FR2852543A1 (en) Connection support fixing process for heat exchanger e.g. air-conditioning condenser, involves deforming wall to penetrate hole for connection by mechanical clinching operation and brazing support with lid
FR3057946B1 (en) THERMAL EXCHANGER AND METHOD OF MANUFACTURING A HEAT EXCHANGER
EP4257912A1 (en) Split profile for fluid circulation tube insertion and heat exchanger thereof
FR3045773A1 (en) MAIN CONDUIT OF A FLUID CIRCUIT CIRCUIT COMPRISING A FLUID SAMPLE ELEMENT
EP0633442A1 (en) Security annular heat exchanger for incompatible fluids
EP1503112B1 (en) Adapter ring between motor and transmission of an automobil

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL LT LV MK

17P Request for examination filed

Effective date: 20040512

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

17Q First examination report despatched

Effective date: 20060420

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REF Corresponds to:

Ref document number: 60324631

Country of ref document: DE

Date of ref document: 20081224

Kind code of ref document: P

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

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

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090223

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

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

Ref country code: IE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090212

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

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

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090413

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

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

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

26N No opposition filed

Effective date: 20090813

BERE Be: lapsed

Owner name: MOTA

Effective date: 20090630

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

Ref country code: MC

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

Effective date: 20090630

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

Ref country code: CH

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

Effective date: 20090630

Ref country code: LI

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

Effective date: 20090630

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

Ref country code: BE

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

Effective date: 20090630

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

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090213

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

Ref country code: LU

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

Effective date: 20090618

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

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090513

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

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

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

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20081112

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 14

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 15

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 16

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

Ref country code: FR

Payment date: 20220323

Year of fee payment: 20

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

Ref country code: SE

Payment date: 20220623

Year of fee payment: 20

Ref country code: IT

Payment date: 20220608

Year of fee payment: 20

Ref country code: GB

Payment date: 20220616

Year of fee payment: 20

Ref country code: DE

Payment date: 20220607

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 60324631

Country of ref document: DE

Representative=s name: CBDL PATENTANWAELTE GBR, DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 60324631

Country of ref document: DE

REG Reference to a national code

Ref country code: GB

Ref legal event code: PE20

Expiry date: 20230617

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

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

Ref country code: GB

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20230617