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EP0313038B1 - Method for the manufacture of a heat exchanger tube plate structure - Google Patents

Method for the manufacture of a heat exchanger tube plate structure Download PDF

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Publication number
EP0313038B1
EP0313038B1 EP88117464A EP88117464A EP0313038B1 EP 0313038 B1 EP0313038 B1 EP 0313038B1 EP 88117464 A EP88117464 A EP 88117464A EP 88117464 A EP88117464 A EP 88117464A EP 0313038 B1 EP0313038 B1 EP 0313038B1
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EP
European Patent Office
Prior art keywords
tube
metallic
plate structure
fibres
profile
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
EP88117464A
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German (de)
French (fr)
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EP0313038A1 (en
Inventor
Klaus Hagemeister
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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Publication of EP0313038A1 publication Critical patent/EP0313038A1/en
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Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • F28D7/06Heat-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 having a single U-bend
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • 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
    • F28F9/0221Header boxes or end plates formed by stacked 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
    • F28F9/0243Header boxes having a circular cross-section
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2250/00Arrangements for modifying the flow of the heat exchange media, e.g. flow guiding means; Particular flow patterns
    • F28F2250/02Streamline-shaped elements
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00Heat exchange
    • Y10S165/454Heat exchange having side-by-side conduits structure or conduit section
    • Y10S165/471Plural parallel conduits joined by manifold
    • Y10S165/481Partitions in manifold define serial flow pattern for conduits/conduit groups
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4935Heat exchanger or boiler making
    • Y10T29/49366Sheet joined to sheet
    • Y10T29/49368Sheet joined to sheet with inserted tubes

Definitions

  • the invention relates to a method for producing a tube sheet structure of a heat exchanger according to the preamble of patent claim 1.
  • the tube sheet is to be composed of a large number of precisely pre-shaped or pre-profiled elements; According to the number and the desired spacing of the profile tubes of the matrix, the relevant layer-to-layer elements should be pre-deformed in such a way that they can enclose half of the arranged tube ends of the matrix in a form-fitting manner.
  • the invention is based on the object of specifying a method in which the tube ends of a profile tube matrix of a heat exchanger can be optimally integrally bonded into a floor or distributor tube structure which is to be created essentially free of predetermined solid component specifications.
  • the rings forming the central tube plate are not made from solid material as already known, but from a fiber mesh.
  • the fiber braid is compressed under the action of axial joining forces in such a way that it nestles completely around the enclosed heat exchanger tubes.
  • the compression of the fiber structure is strongest locally where the surfaces of adjacent pipes are at the smallest distance from each other in the joining area of the heat exchanger pipe field.
  • Metallic material (metal matrix) is then infiltrated into this initially porous structure of the central tube sheet in this way, which fills the cavities of the fiber structure and also creates a material connection to the surfaces of the enclosed tubes and the fibers of the wickerwork.
  • the formation of the fiber rings can be designed in detail as follows.
  • Orientation of a certain proportion of fibers in the circumferential direction is desirable in order to absorb the high circumferential forces during operation of the heat exchanger which result from the internal pressure load on the central tube with the relevant heat exchanger base.
  • Another part of the fiber structure should protrude like bristles from the side surfaces of said fiber ring. When they are joined, these bristle structures of adjacent rings penetrate each other and, after infiltrating the metallic matrix, transmit the forces in the longitudinal direction of the central tube; the bristle structures also ensure that the areas that are least compressed during assembly, in particular on the leading and trailing edges of the heat exchanger tubes, are filled correctly and with a sufficient volume of the fiber material.
  • the fiber material should preferably be heat-resistant in accordance with the temperature load on the component, but not necessarily resistant to oxidation and corrosion. The latter is not the case if the fibers are completely enclosed by the system of the matrix, so that they are protected against the entry of aggressive media. So metallic, but also ceramic and carbon fibers come into question.
  • the fiber rings For assembling the heat exchanger, it can also be advantageous to enclose the fiber rings with solid rings.
  • the width of these rings corresponds to the closest local distances of the heat exchanger tubes in the field, so that the rings can ensure the required distances when they are joined or pressed together. Since they have to follow the corrugated track of the tube field in the circumferential direction, it is necessary to make them correspondingly flexible or to impress the corrugated shape on the rings before joining.
  • the infiltration of the fiber matrix can also be carried out as follows.
  • a lance-like cast crockery is passed inside the resulting central tube over its inner jacket and the molten matrix material is injected which, due to the capillary action, fills the fiber structure, binds with fibers and tube surfaces and solidifies.
  • the molten matrix material is injected which, due to the capillary action, fills the fiber structure, binds with fibers and tube surfaces and solidifies.
  • the above-mentioned massive ring which surrounds the fiber structure on the outside, as well as a corresponding, if necessary, corresponding, arranged on the inside diameter of the fiber structure massive ring similar construction can also be made of a material that becomes molten when heated in the furnace like a solder and by capillary action in the fiber structure penetrates to fill the matrix volume and make the bonds.
  • Pipes of the matrix and fibers or fiber braiding can be subjected to a surface pretreatment in all cases in order to achieve improved wetting and integration into the matrix.
  • Fig. 1 illustrates a heat exchanger 1 for guiding gases of very different temperatures
  • the cross-countercurrent matrix 2 in the hot gas flow G consists of separate compressed air lines 3 (Fig. 2), which on the one hand to a first stationary pipe guide 4 for the supply of cold compressed air D in the matrix 2 (cold) and on the other hand connected to a second stationary pipe guide 5, from which the compressed air D (hot) heated via the matrix 2 can be fed to a consumer.
  • the two pipe guides 4, 5 are arranged separately from one another and integrated in a common header pipe 6.
  • Each profile tube 3 of the matrix 2 - starting from its tube-side connections to the first 4 and second tube guide 5 of the header tube 6 - should initially run parallel to a laterally extended header tube meridian plane before it turns into a common, U deflecting the compressed air D by 180 ° -shaped wiring harness merges.
  • the matrix 2 should also flow through the hot gas G transversely to the elongated manifold meridian plane and while ensuring the permissible hot gas blockage between the adjacent profile tubes 3.
  • each profile tube 3 of the matrix 2 (FIG. 2) also contains two compressed air channels 8, 9 separated from one another by a profile web 7, which have triangular flow cross sections in the sense of the two tapered outer wall sections of the profile tubes 3 concerned.
  • two or more separate manifolds or manifolds for the compressed air supply into the matrix can also be used instead of the common manifold 6, essentially arranged one above the other or next to one another 2 or for the compressed air discharge (hot) from the matrix 2.
  • the invention therefore relates to the manufacture of the relevant floor structure 10, but in particular to the manufacture of the header pipe 6 together with the floor structure 10 or the manufacture of one or more header or distributor pipes in a heat exchanger of the cross-countercurrent construction discussed at the beginning.
  • a method for producing a tube sheet structure 10 or a header tube 6 of a heat exchanger using strip-shaped layers 11, 12 or 12, 13 (FIG. 5) is thus specified, between which tube ends of the profile tubes 3 of the matrix 2 are firmly integrated in a fluid-tight manner; the strip-shaped layers 11, 12; 12, 13 are to be produced from fibers which are initially bundled uniformly (fiber bundles 11 ', 12'; 12 ' , 13') between the tube ends of adjacent rows of profile tubes (tubes 3) and are thus deformed under pressure (arrow direction P, P ') They should form an initially porous bottom structure (Fig. 5) under half-sided pipe wrapping, into which a metallic material is then infiltrated in a molten state, in which all fibers including the pipe ends are integrally bonded.
  • the fiber bundles e.g. 12 ', composed of interwoven fiber layers with main fibers 14 running in the circumferential direction of the tube sheet structure and transverse fibers 15 running transversely thereto, such that the latter - after the pressing and deformation phase (FIG. 5) have been completed - engage in a bristle-like manner essentially outside the tube encapsulation areas.
  • the secondary fibers 15 of the adjacent fiber layers e.g. 12, 13, intertwine like bristles.
  • a complete interweaving of fibers should also be achieved in the respective profile end or tip areas.
  • the aforementioned contact planes 16 are arranged in a longitudinally symmetrical alignment with the profile longitudinal center planes E.
  • the fiber bundles, e.g. 12 ', 13' (Fig. 3) layers, e.g. 12, 13 (FIG. 5) are covered entirely or partially by metallic ring elements 17, 18 (FIG. 7) or 18, 19 (FIG. 8) extending along the inside and / or outside of the floor structure.
  • the ring elements mentioned can e.g. can be provided to stiffen the floor or pipe structure, and to protect the fiber structures from local environmental influences such as temperature influences.
  • the ring elements mentioned can also be aids in the infiltration process in that they are intended to prevent the infiltration agent from flowing off. If e.g. the infiltration process of a molten metallic material from the outside of a tube sheet into the fiber material, the relevant ring elements, e.g. 19 (Fig. 8) can only be arranged on the inside of the tube sheet to prevent the metallic material from flowing away. After infiltration has been completed, the ring elements, e.g. 19 (Fig. 8) can be removed again.
  • the metallic ring elements e.g. 18, 19 (FIG. 8) are manufactured from a solder material which ensures metallic infiltration.
  • the ring elements, e.g. 18, 19 (FIG. 8) on the inside and outside of the porous tube sheet structure as elements corrugated in the sense of the profile tube profile (FIG. 7) are placed on the fiber bundles 12 '(FIG. 8).
  • a metallic composite material (matrix) can be melted within a vacuum furnace via a lance-shaped casting tableware that sweeps the corrugated porous floor structure (FIG. 5) along the inside and outside of the tube sheet be injected.
  • the ends of the profile tubes 3 of the matrix which are open on the inside of the tube sheet can be closed before metallic infiltration is carried out from the inside of the base structure and can be opened again by mechanical processing after the infiltration has been completed.
  • the fibers of the fiber bundles) 11 ' , 12' or 12 ', 13' can be made from a metallic material or from wires, from a ceramic material, for example from partially stabilized zirconium oxide or from carbon.
  • the metallic material infiltrated after the pressing and deformation phase can be made from an aluminum alloy.
  • a circular cylindrical (Fig. 1, 6 or 8), square or rectangular header or distributor pipe of a cross-countercurrent heat exchanger can be used with the collector or distributor pipes, e.g. 6-fig. 1, U-shaped protruding profile tube matrix 2 are produced, the fiber bundles 11 ', 12' or 12 ', 13' (FIG. 3) being compressed to the desired length of header or distributor tube, including the required mutual profile tube spacing of the matrix 2, and the metallic infiltration, for example by means of the aforementioned crockery, can be carried out continuously over the entire circumference of the porous collecting or distribution pipe structure (FIG. 5).
  • rings made of a suitable plastic e.g. can be provided from a fiber-reinforced plastic or from a suitable ceramic material.

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  • 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)
  • Details Of Heat-Exchange And Heat-Transfer (AREA)

Description

Die Erfindung bezieht sich auf ein Verfahren zur Herstellung einer Rohrbodenstruktur eines Wärmetauschers gemäß Oberbegriff des Patentanspruchs 1.The invention relates to a method for producing a tube sheet structure of a heat exchanger according to the preamble of patent claim 1.

Bei einem aus der DE-OS 33 10 061 bekannten Verfahren zur Herstellung einer Rohrverteileranordnung bzw. eines Verteilerrohrs eines Wärmetauschers soll der Rohrboden aus einer Vielzahl genauestens vorgeformter bzw. vorprofilierter Elemente zusammengesetzt werden; entsprechend der Anzahl und der gewünschten Beabstandung der Profilrohre der Matrix sollen dabei die betreffenden Schicht auf Schicht zusammenzufügenden Elemente also so vorverformt sein, daß sie die angeordneten Rohrenden der Matrix jeweils zur Hälfte formschlüssig umschließen können.In a method known from DE-OS 33 10 061 for producing a pipe distributor arrangement or a distributor pipe of a heat exchanger, the tube sheet is to be composed of a large number of precisely pre-shaped or pre-profiled elements; According to the number and the desired spacing of the profile tubes of the matrix, the relevant layer-to-layer elements should be pre-deformed in such a way that they can enclose half of the arranged tube ends of the matrix in a form-fitting manner.

Im bekannten Fall wird es als nachteilhaft angesehen, daß trotz verhältnismäßig genauer Fertigung der betreffenden, die Schichten bildenden Elemente Fertigungtoleranzen zu berücksichtigen sind, derart, daß die Gesamtlänge des zu erstellenden Bodens oder Rohrs mit der Summe der Dickentoleranz der Elemente schwankt; neben Boden- oder Rohrlängenschwankungen sind ferner im bekannten Fall örtliche Belochungsversätze gegenüber der normalen Profilrohrbeabstandung und -Anordnung nicht auszuschließen; durch die massive Formvorgabe der Elemente sind also grundsätzlich Fertigungstoleranzen nicht zu vermeiden und praktisch kaum oder nur mit extrem kostenaufwendiger Nachbearbeitung korrigierbar.In the known case, it is considered disadvantageous that despite relatively precise manufacture of the relevant elements forming the layers, manufacturing tolerances have to be taken into account such that the total length of the base or pipe to be produced fluctuates with the sum of the thickness tolerance of the elements; in addition to floor or pipe length fluctuations, local perforation offsets compared to the normal profile pipe spacing and arrangement cannot be ruled out; Due to the massive shape specification of the elements, manufacturing tolerances cannot be avoided and can hardly be corrected, or can only be corrected with extremely expensive post-processing.

Genannte Belochungsversätze wie aber auch schon geringfügige Belochungsformschwankungen setzen ein mühsames Feinjustieren bzw. Zentrieren der betreffenden Rohrenden der Matrix voraus, zumal das spätere Verlöten der Rohrenden im Schichtboden eine extrem genaue Sitzpassung der Rohrenden erzwingt, um örtliche Lotwertstoff-Verlagerungen möglichst zu vermeiden.The above-mentioned perforation offsets as well as slight fluctuations in the perforation form require laborious fine adjustment or centering of the relevant tube ends of the matrix, especially since the later soldering of the tube ends in the layered base forces an extremely precise fit of the tube ends in order to avoid local solder material displacements as far as possible.

Der Erfindung liegt die Aufgabe zugrunde, ein Verfahren anzugeben, bei dem die Rohrenden einer Profilrohrmatrix eines Wärmetauschers in eine im wesentlichen frei von vorgegebenen Massivbauteilvorgaben zu erstellende Boden- oder Verteilerrohrstruktur optimal stoffschlüssig einbindbar sind.The invention is based on the object of specifying a method in which the tube ends of a profile tube matrix of a heat exchanger can be optimally integrally bonded into a floor or distributor tube structure which is to be created essentially free of predetermined solid component specifications.

Bei einem Verfahren nach dem Oberbegriff des Patentanspruchs 1 ist die genannte Aufgabe durch die Merkmale des Kennzeichnungsteils des Patentanspruchs 1 erfindungsgemäß gelöst.In a method according to the preamble of patent claim 1, the stated object is achieved according to the invention by the features of the characterizing part of patent claim 1.

Gemäß der Erfindung ist es also vorgesehen, die den Zentralrohrboden bildenden Ringe nicht aus massivem Material wie bereits als bekannt erwähnt herzustellen, sondern aus einem Fasergeflecht. Beim Zusammenfügen der Schichten - gebildet aus ebenen Lagen von Wärmetauscherrohren und den den Zentralrohrboden darstellenden Faserringen - wird erfindungsgemäß das Fasergeflecht unter der Wirkung von axialen Fügekräften in der Weise komprimiert, daß es sich vollständig um die eingeschlossenen Wärmetauscherrohre schmiegt. Dabei ist die Verdichtung der Faserstruktur örtlich dort am stärksten, wo im Fügebereich des Wärmetauscherohrfeldes die Oberflächen benachbarter Rohre den geringsten Abstand zueinander haben.According to the invention, it is therefore provided that the rings forming the central tube plate are not made from solid material as already known, but from a fiber mesh. When joining the layers - formed from flat layers of heat exchanger tubes and the fiber rings representing the central tube plate - according to the invention, the fiber braid is compressed under the action of axial joining forces in such a way that it nestles completely around the enclosed heat exchanger tubes. The compression of the fiber structure is strongest locally where the surfaces of adjacent pipes are at the smallest distance from each other in the joining area of the heat exchanger pipe field.

In diese derart gebildete, zunächst noch poröse Struktur des Zentralrohrbodens wird anschließend metallisches Material (Metall-Matrix) schmelzflüssig infiltriert, das sowohl die Hohlräume der Faserstruktur ausfüllt als auch eine stoffschlüssige Verbindung zu den Oberflächen der umschlossenen Rohre und den Fasern des Flechtwerks herstellt.Metallic material (metal matrix) is then infiltrated into this initially porous structure of the central tube sheet in this way, which fills the cavities of the fiber structure and also creates a material connection to the surfaces of the enclosed tubes and the fibers of the wickerwork.

Die Ausbildung der Faserringe kann im Einzelnen wie folgt gestaltet werden.The formation of the fiber rings can be designed in detail as follows.

In Umfangsrichtung ist eine Orientierung eines gewissen Faseranteils anzustreben, um damit im Betrieb des Wärmetauschers die hohen Umfangskräfte aufzunehmen, die aus der Innendruckbelastung des Zentralrohres mit dem betreffenden Wärmetauscherboden resultieren. Ein anderer Teil der Faserstruktur sollte borstenartig aus den Seitenflächen des besagten Faserringes herausragen. Beim Zusammenfügen durchdringen sich diese Borstenstrukturen benachbarter Ringe und vermitteln, nach Infiltrieren der metallischen Matrix, die Kräfte übertragung in Längsrichtung des Zentralrohres; die Borstenstrukturen stellen außerdem sicher, daß die beim Zusammenfügen am geringsten komprimierten Gebiete, insbesondere an den Anström- und Abströmkanten der Wärmetauscherrohre, einwandfrei und mit einem genügenden Volumen des Fasermaterials ausgefüllt werden.Orientation of a certain proportion of fibers in the circumferential direction is desirable in order to absorb the high circumferential forces during operation of the heat exchanger which result from the internal pressure load on the central tube with the relevant heat exchanger base. Another part of the fiber structure should protrude like bristles from the side surfaces of said fiber ring. When they are joined, these bristle structures of adjacent rings penetrate each other and, after infiltrating the metallic matrix, transmit the forces in the longitudinal direction of the central tube; the bristle structures also ensure that the areas that are least compressed during assembly, in particular on the leading and trailing edges of the heat exchanger tubes, are filled correctly and with a sufficient volume of the fiber material.

Das Fasermaterial sollte vorzugsweise der Temperaturbelastung des Bauteils entsprechend warmfest sein, jedoch nicht unbedingt oxidations-und korrosionsfest. Letzteres dann nämlich nicht, wenn die Fasern vom System der Matrix völlig umschlossen werden, so daß sie vor Zutritt aggressiver Medien geschützt sind. In Frage kommen also metallische, aber auch keramische und Kohle-Fasern.The fiber material should preferably be heat-resistant in accordance with the temperature load on the component, but not necessarily resistant to oxidation and corrosion. The latter is not the case if the fibers are completely enclosed by the system of the matrix, so that they are protected against the entry of aggressive media. So metallic, but also ceramic and carbon fibers come into question.

Für das Zusammenfügen des Wärmetauschers kann es ferner vorteilhaft sein, die Faserringe mit massiven Ringen zu umfassen. Die Breite dieser Ringe entspricht den engsten örtlichen Abständen der Wärmetauscherrohre im Feld, so daß die Ringe beim Zusammenfügen bzw. -pressen die erforderlichen Abstände sicherstellen können. Da sie dabei der jeweils gewellten Spur des Rohrfeldes in Umfangsrichtung folgen müssen, ist es erforderlich, sie entsprechend biegeweich zu gestalten oder aber den Ringen die gewellte Form schon vor dem Fügen aufzuprägen.For assembling the heat exchanger, it can also be advantageous to enclose the fiber rings with solid rings. The width of these rings corresponds to the closest local distances of the heat exchanger tubes in the field, so that the rings can ensure the required distances when they are joined or pressed together. Since they have to follow the corrugated track of the tube field in the circumferential direction, it is necessary to make them correspondingly flexible or to impress the corrugated shape on the rings before joining.

Das Infiltrieren der Fasermatrix kann ferner wie folgt vorgenommen werden.The infiltration of the fiber matrix can also be carried out as follows.

1. In Vakuumöfen wird ein lanzenartiges Gießgeschirr im Inneren des entstehenden Zentralrohres über dessen Innenmantel geführt und das schmelzflüssige Matrixmaterial injiziert, das aufgrund der Kapillarwirkung die Faserstruktur ausfüllt, mit Fasern und Rohroberflächen Bindungen eingeht und erstarrt. Dazu kann es erforderlich sein, die in den Innenraum des Zentralrohres hineinreichenden Rohrenden der Wärmetauscher-Matrix zuvor zu verschließen, um sie nach Abschluß des Fertigungsprozesses abzuarbeiten und damit wieder zu öffenen.1. In vacuum ovens, a lance-like cast crockery is passed inside the resulting central tube over its inner jacket and the molten matrix material is injected which, due to the capillary action, fills the fiber structure, binds with fibers and tube surfaces and solidifies. For this purpose, it may be necessary to previously close the tube ends of the heat exchanger matrix that extend into the interior of the central tube, in order to process them after the completion of the manufacturing process and thus to reopen them.

2. Der oben erwähnte massive, die Faserstruktur außen um fassende Ring sowie auch ein gegebenenfalls entsprechender, am Innendurchmesser der Faserstruktur angeordneter massiver Ring ähnlicher Bauweise können ferner aus einem Material hergestellt sein, das beim Erhitzen im Ofen wie ein Lot schmelzflüssig wird und durch Kapillarwirkung in die Faserstruktur eindringt, um das Matrixvolumen auszufüllen und die Bindungen bzw. Verbindungen herzustellen.2. The above-mentioned massive ring, which surrounds the fiber structure on the outside, as well as a corresponding, if necessary, corresponding, arranged on the inside diameter of the fiber structure massive ring similar construction can also be made of a material that becomes molten when heated in the furnace like a solder and by capillary action in the fiber structure penetrates to fill the matrix volume and make the bonds.

Rohre der Matrix und Fasern bzw. Faserflechtwerke können in allen Fällen einer Oberflächenvorbehandlung unterzogen werden, um eine verbesserte Benetzung und Einbindung in die Matrix zu erzielen.Pipes of the matrix and fibers or fiber braiding can be subjected to a surface pretreatment in all cases in order to achieve improved wetting and integration into the matrix.

Die zuvor genannten Ausführungen beruhen auf dem Grundgedanken der Erfindung gemäß Anspruch 1 unter sachlicher Verdeutlichung weiterer Ausgestaltungen des Verfahrens nach Anspruch 1 im Rahmen der Patentansprüche 2 bis 17.The above-mentioned statements are based on the basic idea of the invention according to claim 1 with objective clarification of further refinements of the method according to claim 1 within the scope of claims 2 to 17.

Anhand der Zeichnungen ist die Erfindung beispielsweise weiter erläutert; es zeigen:

  • Fig. 1 die perspektivische Darstellung eines bekannten und für die Durchführung des erfindungsgemäßen Verfahrens geeigneten Profilrohr-Wärmetauschers in Kreuz-Gegenstrom-Bauweise,
  • Fig. 2 einen Profilausschnitt (geradschenkeliger Bereich) aus der Matrix des Wärmetauschers nach Fig.1,
  • Fig. 3 ein grob vorjustiertes, in die Zeichnungsebene projiziertes Profilrohrfeld für die Matrix des Wärmetauschers nach Fig. 1 mit in gleichmäßigen Abständen zwischen benachbarten Profilrohrenden lose angeordneten Faserbündeln im Rahmen einer Ausgangsphase des Herstellverfahrens für eine Boden- oder Zentralrohrausbildung,
  • Fig. 4 die perspektivische Darstellung eines Faserbündelabschnitts,
  • Fig. 5 ein aus der Ausgangsstufe des betreffenden Verfahrens nach Fig. 3 durch Pressung und Verformung der betreffenden Faserbündel unter jeweiliger Profilrohrendumschließung ausgebildeter Abschnitt eines Wärmetauscherbodens mit regulärer gewünschter gegenseitiger Profilrohrbeabstandung im Feld,
  • Fig. 6 ein im Wege der Pressung und Verformung nach Fig. 5 hergestelltes zylindrisches Sammel-oder Verteilerrohr mit beidseitig zwischen benachbarten Faserbündeln ins Rohrinnere einmündenden Profilrohrenden der Matrix, hier im Wege einer örtlich freigelegten Seitenansicht der betreffenden Profilrohrenden in Kombination mit einem innenliegenden zylindrischen Faserbündel verdeutlicht,
  • Fig. 7 die nach Fig. 5 hergestellte Bodenstruktur unter Verwendung zusätzlicher, hier entlang der Bodenaußenseite sich gewellt zwischen den Profilrohrenden erstreckenden metallischen Zwischenringen und
  • Fig. 8 eine gemäß Fig. 6 dargestellte Weiterentwicklung des Verfahrensgegenstandes unter Verwendung jeweils äußerer und innerer metallischer Zwischenringe an gemäß Fig. 5 verformten und gepressten Faserbündeln zwecks Ausbildung einer zylindrischen Sammel- oder Verteilerrohrstruktur.
The invention is further explained, for example, with the aid of the drawings; show it:
  • 1 is a perspective view of a known profile tube heat exchanger in a cross-countercurrent design which is suitable for carrying out the method according to the invention,
  • 2 shows a profile section (straight-leg region) from the matrix of the heat exchanger according to FIG. 1,
  • 3 shows a roughly pre-adjusted profile tube field for the matrix of the heat exchanger according to FIG. 1, projected into the plane of the drawing, with fiber bundles loosely arranged at uniform intervals between adjacent profile tube ends as part of an initial phase of the manufacturing process for bottom or central tube formation,
  • 4 shows the perspective illustration of a fiber bundle section,
  • 5 shows a section of a heat exchanger base which is formed from the initial stage of the relevant method according to FIG. 3 by pressing and deforming the relevant fiber bundle with the respective profile tube end enclosure, with a regular desired mutual profile tube spacing in the field,
  • Fig. 6 shows a cylindrical manifold or distributor tube produced by pressing and deforming according to Fig. 5 with profile tube ends of the matrix opening into the tube interior between adjacent fiber bundles, here illustrated by means of a locally exposed side view of the relevant profile tube ends in combination with an internal cylindrical fiber bundle ,
  • Fig. 7, the bottom structure produced according to Fig. 5 using additional, here along the bottom outside corrugated between the profile tube ends extending metallic intermediate rings and
  • FIG. 8 shows a further development of the subject of the method shown in FIG. 6 using outer and inner metallic intermediate rings on fiber bundles deformed and pressed according to FIG. 5 to form a cylindrical header or distributor pipe structure.

Fig. 1 veranschaulicht einen Wärmetauscher 1 zur Führung von Gasen stark unterschiedlicher Temperaturen, dessen im Heißgasstrom G liegende Kreuz-Gegenstrom-Matrix 2 aus seperaten Druckluftleitungen 3 (Fig. 2) besteht, die einerseits an eine erste stationäre Rohrführung 4 für die Zufuhr kalter Druckluft D in die Matrix 2 (kalt) und andererseits an eine zweite stationäre Rohrführung 5 angeschlossen sind, aus der die über die Matrix 2 aufgeheizte Druckluft D (heiß) einem Verbraucher zuführbar ist. Die beiden Rohrführungen 4, 5 sind voneinander getrennt angeordnet und in ein gemeinsames Sammelrohr 6 integriert. Dabei soll jedes Profilrohr 3 der Matrix 2 - ausgehend von deren rohrbodenseitigen Anschlüssen an die erste 4 und zweite Rohrführung 5 des Sammelrohrs 6 - zunächst parallel zu einer seitlich verlängerten Sammelrohrmeridianebene verlaufen, bevor sie in einen gemeinsamen, die Druckluft D um 180° umlenkenden, U-förmigen Leitungsstrang übergeht. Die Matrix 2 soll ferner quer zur verlängerten Sammelrohrmeridianebene sowie unter Gewährleistung der zulässigen Heißgasversperrung zwischen den einander benachbarten Profilrohren 3 vom Heißgas G durchströmt sein.Fig. 1 illustrates a heat exchanger 1 for guiding gases of very different temperatures, the cross-countercurrent matrix 2 in the hot gas flow G consists of separate compressed air lines 3 (Fig. 2), which on the one hand to a first stationary pipe guide 4 for the supply of cold compressed air D in the matrix 2 (cold) and on the other hand connected to a second stationary pipe guide 5, from which the compressed air D (hot) heated via the matrix 2 can be fed to a consumer. The two pipe guides 4, 5 are arranged separately from one another and integrated in a common header pipe 6. Each profile tube 3 of the matrix 2 - starting from its tube-side connections to the first 4 and second tube guide 5 of the header tube 6 - should initially run parallel to a laterally extended header tube meridian plane before it turns into a common, U deflecting the compressed air D by 180 ° -shaped wiring harness merges. The matrix 2 should also flow through the hot gas G transversely to the elongated manifold meridian plane and while ensuring the permissible hot gas blockage between the adjacent profile tubes 3.

Wie insbesondere aus Fig. 2 entnehmbar, weisen die mit strömungsgünstig zugespitzten Enden an-und abströmseitig in der Heißgasströmungsrichtung G liegenden Profilrohre 3 der Matrix einen linsenförmigen Querschnitt auf; dabei greifen die jeweils parallel zu einer gemeinsamen Matrixquerebene verlaufend angeordneten Profilrohre 3 mit ihren an- bzw. abströmseitig einander benachbarten Profilzuspitzungen unter Ausnutzung der infolge dieser Zuspitzungen sich räumlich ausbildenden Erweiterungen ineinander; jedes Profilrohr 3 der Matrix 2 (Fig. 2) enthält ferner zwei durch einen Profilsteg 7 voneinander getrennte Druckluftkanäle 8,9, die im Sinne der beiden zugespitzten Außenwandabschnitte der betreffenden Profilrohre 3 dreieckförmig ausgebildete Strömungsquerschnitte aufweisen.As can be seen in particular from FIG. 2, the profile tubes 3 of the matrix lying on the upstream and downstream sides in the hot gas flow direction G with streamlined pointed ends have a lenticular cross section; the profile tubes 3, which each run parallel to a common matrix transverse plane, engage with one another on the upstream and downstream side of the profile tapering, utilizing the expansions which form as a result of these tapering; each profile tube 3 of the matrix 2 (FIG. 2) also contains two compressed air channels 8, 9 separated from one another by a profile web 7, which have triangular flow cross sections in the sense of the two tapered outer wall sections of the profile tubes 3 concerned.

Beim eingangs beschriebenen Wärmetauscher, wie er im übrigen aus der DE-PS 29 07 810 bekannt ist, können ferner anstelle des gemeinsamen Sammelrohrs 6 zwei oder mehrere separate, im wesentlichen parallel über- oder nebeneinander angeordnete Verteiler- oder Sammelrohre für die Druckluftzufuhr in die Matrix 2 bzw. für die Druckluftableitung (heiß) aus der Matrix 2 vorgesehen werden.In the heat exchanger described at the outset, as is known from DE-PS 29 07 810, two or more separate manifolds or manifolds for the compressed air supply into the matrix can also be used instead of the common manifold 6, essentially arranged one above the other or next to one another 2 or for the compressed air discharge (hot) from the matrix 2.

Die Erfindung betrifft also die Herstellung der betreffenden Bodenstruktur 10, insbesondere aber die Herstellung des Sammelrohrs 6 nebst Bodenstruktur 10 bzw. die Herstellung einzelner oder mehrerer Sammel- oder Verteilerrohre bei einem eingangs behandelten Wärmetauscher in Kreuz-Gegenstrom-Bauweise.The invention therefore relates to the manufacture of the relevant floor structure 10, but in particular to the manufacture of the header pipe 6 together with the floor structure 10 or the manufacture of one or more header or distributor pipes in a heat exchanger of the cross-countercurrent construction discussed at the beginning.

Es wird also ein Verfahren zur Herstellung einer Rohrbodenstruktur 10 bzw. eines Sammelrohres 6 eines Wärmetauschers unter Anwendung streifenförmiger Schichten 11, 12 bzw. 12, 13 (Fig. 5) angegeben, zwischen denen Rohrenden der Profilrohre 3 der Matrix 2 fluiddicht fest eingebunden sind; die streifenförmigen Schichten 11,12; 12,13 sollen aus Fasern hergestellt werden, die zunächst gleichförmig gebündelt (Faserbündei 11',12'; 12',13') zwischen den Rohrenden benachbarter Profilrohrreihen (Rohre 3) angeordnet und unter Pressung (Pfeilrichtung P,P') so verformt werden sollen, daß sie unter jeweils halbseitiger Rohrumschmiegung eine zunächst poröse Bodenstruktur (Fig. 5) ausbilden, in die dann ein metallischer Werkstoff schmelzflüssig infiltriert wird, in den sämtliche Fasern einschließlich der Rohrenden stoffschlüssig eingebunden werden.A method for producing a tube sheet structure 10 or a header tube 6 of a heat exchanger using strip-shaped layers 11, 12 or 12, 13 (FIG. 5) is thus specified, between which tube ends of the profile tubes 3 of the matrix 2 are firmly integrated in a fluid-tight manner; the strip-shaped layers 11, 12; 12, 13 are to be produced from fibers which are initially bundled uniformly (fiber bundles 11 ', 12'; 12 ' , 13') between the tube ends of adjacent rows of profile tubes (tubes 3) and are thus deformed under pressure (arrow direction P, P ') They should form an initially porous bottom structure (Fig. 5) under half-sided pipe wrapping, into which a metallic material is then infiltrated in a molten state, in which all fibers including the pipe ends are integrally bonded.

Gemäß Fig. 4 können die Faserbündel, z.B. 12', aus miteinander verwobenen Faserlagen mit in Umfangsrichtung der Rohrbodenstruktur verlaufenden Hauptfasern 14 und quer dazu ver laufenden Nebenfasern 15 so zusammengesetzt werden, daß die letzteren - nach vollzogener Press- und Verformungsphase (Fig. 5) - im wesentlichen außerhalb der Rohrumschmiegungsbereiche borstenartig ineinandergreifen.4, the fiber bundles, e.g. 12 ', composed of interwoven fiber layers with main fibers 14 running in the circumferential direction of the tube sheet structure and transverse fibers 15 running transversely thereto, such that the latter - after the pressing and deformation phase (FIG. 5) have been completed - engage in a bristle-like manner essentially outside the tube encapsulation areas.

Im Bereich der gegenseitigen Kontaktebenen 16 sollen also die Nebenfasern 15 der jeweils benachbarten Faserschichten, z.B. 12, 13, borstenartig innig ineinandergreifen. Insbesondere soll dabei auch in den jeweiligen Profilend- oder -spitzenbereichen eine lückenlose Faserverflechtung erreicht werden. Die genannten Kontaktebenen 16 sind dabei längssymmetrisch fluchtend zu den Profillängsmittelebenen E angeordnet.In the area of the mutual contact planes 16, the secondary fibers 15 of the adjacent fiber layers, e.g. 12, 13, intertwine like bristles. In particular, a complete interweaving of fibers should also be achieved in the respective profile end or tip areas. The aforementioned contact planes 16 are arranged in a longitudinally symmetrical alignment with the profile longitudinal center planes E.

Gemäß Fig. 7 und 8 können die aus den Faserbündein, z.B. 12', 13' (Fig. 3) gebildeten Schichten, z.B. 12, 13 (Fig.5) gänzlich oder teilweise von sich entlang der Innen- und/oder Außenseite der Bodenstruktur erstreckenden metallischen Ringelementen 17, 18 (Fig. 7) bzw. 18, 19 (Fig. 8) abgedeckt werden.7 and 8, the fiber bundles, e.g. 12 ', 13' (Fig. 3) layers, e.g. 12, 13 (FIG. 5) are covered entirely or partially by metallic ring elements 17, 18 (FIG. 7) or 18, 19 (FIG. 8) extending along the inside and / or outside of the floor structure.

Die genannten Ringelemente können z.B. vorgesehen werden, um die Boden- oder Rohrstruktur zu versteifen, sowie, um die Faserstrukturen vor örtlichen Umgebungseinflüssen, wie Temperatureinflüssen, zu schützen.The ring elements mentioned can e.g. can be provided to stiffen the floor or pipe structure, and to protect the fiber structures from local environmental influences such as temperature influences.

Die genannten Ringelemente können aber auch Hilfsmittel beim Infiltrationsvorgang sein, indem sie ein Abfließen des Infiltriermittels verhüten sollen. Wenn z.B. der Infiltrationsvorgang eines schmelzflüssigen metallischen Materials von der Außenseite eines Rohrbodens aus in das Fasermaterial erfolgt, so können die betreffenden Ringelemente, z.B. 19 (Fig. 8) ausschließlich an der Rohrbodeninnenseite angeordnet werden, um das Abfließen des metallischen Materials zu verhindern. Nach vollzogener Infiltration können dann die Ringelemente, z.B. 19 (Fig. 8), wieder entfernt werden.The ring elements mentioned can also be aids in the infiltration process in that they are intended to prevent the infiltration agent from flowing off. If e.g. the infiltration process of a molten metallic material from the outside of a tube sheet into the fiber material, the relevant ring elements, e.g. 19 (Fig. 8) can only be arranged on the inside of the tube sheet to prevent the metallic material from flowing away. After infiltration has been completed, the ring elements, e.g. 19 (Fig. 8) can be removed again.

In einer weiteren Verfahrensausbildung besteht ferner die Möglichkeit, daß die metallischen Ringelemente, z.B. 17, 18 (Fig. 7), unter Gewährleistung der erforderlichen Profilbeabstandung, in der Bodenstruktur zusammen mit den Faserbündeln 12', 13' (Fig. 3) verformt werden, und zwar entsprechend gewellt verformt.In a further process training there is also the possibility that the metallic ring elements, e.g. 17, 18 (Fig. 7), while ensuring the required profile spacing, in the floor structure together with the fiber bundles 12 ', 13' (Fig. 3) are deformed, and accordingly corrugated deformed.

Anstelle der gemeinsamen Verpressung von Faserbündeln und Ringelementen wäre es auch möglich, daß im Sinne des endgültigen Profilrohrverlaufs vorgeformte oder gewellte metallische Ringelement, z.B. 18, 19 (Fig. 8), vor der metallischen Infiltration, an der Innen- und Außenseite des Rohrbodens auf die Faserschichten, z.B. 12, aufgesetzt werden.Instead of the joint pressing of fiber bundles and ring elements, it would also be possible for pre-shaped or corrugated metallic ring elements, e.g. 18, 19 (Fig. 8), before the metallic infiltration, on the inside and outside of the tube sheet onto the fiber layers, e.g. 12, to be put on.

Gemäß einer weiteren vorteilhaften Variante des Verfahrens können die metallischen Ringelemente, z.B. 18, 19 (Fig. 8), aus einem die metallische Infiltration gewährleistenden Lotwerkstoff gefertigt werden. Hierbei können also die Ringelemente, z.B. 18, 19 (Fig. 8) an der Innen- und Außenseite der porösen Rohrbodenstruktur als im Sinne des Profilrohrverlaufs gewellte Elemente (Fig. 7) auf die Faserbündel 12' (Fig. 8) aufgesetzt werden.According to a further advantageous variant of the method, the metallic ring elements, e.g. 18, 19 (FIG. 8), are manufactured from a solder material which ensures metallic infiltration. The ring elements, e.g. 18, 19 (FIG. 8) on the inside and outside of the porous tube sheet structure as elements corrugated in the sense of the profile tube profile (FIG. 7) are placed on the fiber bundles 12 '(FIG. 8).

Eine äußerst praktikable Handhabung des Infiltrationsvorgangs wird darin gesehen, daß die mit metallischen Ringelementen 17,18 (Fig. 7) bzw. 18,19 (Fig. 8) aus einem Lotwerkstoff bestückte Rohrbodenstruktur zur Schmelzverflüssigung und Infiltration des Lots in einem Ofen erhitzt wird.An extremely practical handling of the infiltration process is seen in the fact that the tube sheet structure, which is equipped with metallic ring elements 17, 18 (FIG. 7) or 18, 19 (FIG. 8) made of a solder material, is heated in an oven for melt liquefaction and infiltration of the solder.

Sofern beispielsweise keine den Lot- und Verbundwerkstoff breitstellenden Ringelemente angewendet werden sollten, kann ein metallischer Verbundwerkstoff (Matrix) innerhalb eines Vakuumofens über ein die gewellt verformte poröse Bodenstruktur (Fig. 5) bestreichendes, lanzenartig ausgebildetes Gießgeschirr entlang der Innen- und Außenseite des Rohrbodens schmelzflüssig injiziert werden.If, for example, no ring elements that extend the solder and composite material should be used, a metallic composite material (matrix) can be melted within a vacuum furnace via a lance-shaped casting tableware that sweeps the corrugated porous floor structure (FIG. 5) along the inside and outside of the tube sheet be injected.

In weiterer Verfahrensausgestaltung können die rohrbodeninnenseitig offenen Enden der Profilrohre 3 der Matrix vor einer von der Innenseite der Bodenstruktur aus durchgeführten metallischen Infiltration verschlossen und nach vollzogener Infiltration durch mechanische Bearbeitung wieder geöffnet werden.In a further embodiment of the method, the ends of the profile tubes 3 of the matrix which are open on the inside of the tube sheet can be closed before metallic infiltration is carried out from the inside of the base structure and can be opened again by mechanical processing after the infiltration has been completed.

Die Fasern der Faserbünde) 11', 12' bzw. 12', 13' (Fig. 3) können aus einem metallischen Werkstoff bzw. aus Drähten, aus einem keramischen Werkstoff, z.B. aus partiell stabilisiertem Zirkonoxid oder aus Kohlenstoff gefertigt sein.The fibers of the fiber bundles) 11 ' , 12' or 12 ', 13' (FIG. 3) can be made from a metallic material or from wires, from a ceramic material, for example from partially stabilized zirconium oxide or from carbon.

Der nach der Press- und Verformungsphase infiltrierte metallische Werkstoff kann aus einer Aluminiumlegierung hergestellt sein.The metallic material infiltrated after the pressing and deformation phase can be made from an aluminum alloy.

Im Rahmen des Verfahrens kann ein kreiszylindrisches (Fig. 1, 6 oder 8), quadratisches oder rechteckiges Sammel- oder Verteilerrohr eines Kreuz-Gegenstrom-Wärmetauschers mit von den Sammel- oder Verteilerrohren, z.B. 6-Fig. 1, U-förmig auskragender Profilrohrmatrix 2 hergestellt werden, wobei die Faserbündel 11', 12' bzw. 12', 13' (Fig. 3) auf das gewünschte Sammel- oder Verteilerrohrlängenmaß unter Einschluß der geforderten gegenseitigen Profilrohrbeabstandung der Matrix 2 zusammengepreßt werden und wobei die metallische Infiltration, z.B. mittels zuvor erwähnten Gießgeschirrs, fortlaufend über dem gesamten Umfang der porösen Sammel- oder Verteilerrohrstruktur (Fig. 5) durchgeführt werden kann.Within the scope of the method, a circular cylindrical (Fig. 1, 6 or 8), square or rectangular header or distributor pipe of a cross-countercurrent heat exchanger can be used with the collector or distributor pipes, e.g. 6-fig. 1, U-shaped protruding profile tube matrix 2 are produced, the fiber bundles 11 ', 12' or 12 ', 13' (FIG. 3) being compressed to the desired length of header or distributor tube, including the required mutual profile tube spacing of the matrix 2, and the metallic infiltration, for example by means of the aforementioned crockery, can be carried out continuously over the entire circumference of the porous collecting or distribution pipe structure (FIG. 5).

Anstelle der eingangs erwähnten metallischen Ringe können im übrigen auch Ringe aus einem geeigneten Kunststoff, z.B. aus einem faserverstärkten Kunststoff oder aus einem geeigneten keramischen Werkstoff vorgesehen werden.Instead of the metallic rings mentioned at the outset, rings made of a suitable plastic, e.g. can be provided from a fiber-reinforced plastic or from a suitable ceramic material.

Claims (17)

1. A method of producing a tube plate structure of a heat exchanger composed of strip-like layers between which tube ends of a profile tube matrix are fluid-tightly and rigidly bonded, characterised in that the strip-like layers (12, 13) are produced from fibres which are disposed between the tube ends of adjacent rows of profile tubes and which are pressed so that they become so shaped that fitting closely half way round a tube they initially form a porous plate structure into which a metallic material is infiltrated in the molten state, the fibre structure being filled by capillary action and entering into a bond with fibres and tube surfaces and solidifying, all the fibres including the tube ends being bonded as a result of material flow.
2. A method according to Claim 1, characterised in that fibre bundles (12') of interconnected layers of fibres comprising main fibres (14) extending in the peripheral direction of the tube plate structure and subsidiary fibres (15) extending transversely thereto are so assembled that, when the pressing and moulding phases are completed, the latter inter-engage like bristles outside the areas which fit around the tubes.
3. A method according to Claim 1 or 2, characterised in that the layers (12) produced from fibre bundles (12') are entirely or partially masked by ring elements (18, 19) extending along the inside and/or outside of the plate structure.
4. A method according to Claim 3, characterised in that ring elements (18, 19) provided on the inside and outside of the plate structure are removed once metallic infiltration is complete.
5. A method according to Claim 3, characterised in that the ring elements (17, 18) are moulded together with the fibre bundles (12', 13'), ensuring the required profile gap in the plate structure.
6. A method according to Claim 3 or 4, characterised in that ring elements (18, 19) pre-shaped or undulating according to the final pattern of the profile tubes are fitted onto the fibre layers (12) on the inside or outside of the tube plate prior to metallic infiltration.
7. A method according to Claim 3 or 5, characterised in that the ring elements (18, 19) are produced from a solder material which guarantees metallic infiltration.
8. A method according to Claim 7, characterised in that the metallic ring elements (18, 19) produced from a solder material are fitted onto the fibre bundles (12') on the inside and outside of the porous tube plate structure to serve as undulating elements according to the pattern of the profile tubes.
9. A method according to Claim 7 or 8, characterised in that the tube plate structure provided with metallic ring elements which consist of a solder material are heated in an oven to liquefy and allow infiltration of the solder.
10. A method according to one or more of Claims 1 to 6, characterised in that the metallic composite material is injected in molten-fluid form along the inside or outside of the tube plate inside a vacuum oven, by means of a pouring apparatus of lance like construction adapted to coat the undulatingly shaped porous plate structure.
11. A method according to Claim 10, characterised in that the tube ends of the matrix which are open towards the inside of the tube plate are closed by metallic infiltration carried out from inside the plate structure and, once infiltration is complete, are opened again by mechanical machining.
12. A method according to one or more of Claims 1 to 11, characterised in that the fibres of the fibre bundles are made from a metallic material or from wires.
13. A method according to one or more of Claims 1 to 11, characterised in that the fibres of the fibre bundles are made from a ceramic material.
14. A method according to Claim 13, characterised in that the fibres of the fibre bundles are made from partially stabilised zirkonium oxide.
15. A method according to Claim 13 or 14, characterised in that the metallic material infiltrated after the moulding and shaping phases is produced from an aluminium alloy.
16. A method according to one or more of Claims 1 to 11, characterised in that the fibres of the fibre bundles are made from carbon.
17. A method according to one or more of Claims 1 to 16, characterised in that a circularly cylindrical, quadratic or rectangular collecting or distributing tube (6) of a cross-counter current heat exchanger with a profile tube matrix (2) projecting in a U-shape from collecting or distributor tubes (6) is produced over the tube plate structure, the fibre bundles (11', 12'; 12', 13') being compressed to the desired collecting or distributor tube length with the inclusion of the required distance between the profile tubes in the matrix (2), metallic infiltration being carried out over the entire periphery of the porous collecting or distributor tube structure.
EP88117464A 1987-10-23 1988-10-20 Method for the manufacture of a heat exchanger tube plate structure Expired - Lifetime EP0313038B1 (en)

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DE19873735846 DE3735846A1 (en) 1987-10-23 1987-10-23 METHOD FOR PRODUCING A TUBE BOTTOM STRUCTURE OF A HEAT EXCHANGER
DE3735846 1987-10-23

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Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3914773C2 (en) * 1989-05-05 1994-03-03 Mtu Muenchen Gmbh Heat exchanger with at least two header pipes
US5177865A (en) * 1989-05-05 1993-01-12 Mtu Motoren-Und Turbinen-Union Method for making heat exchanger having at least two collecting pipes
US5269276A (en) * 1992-09-28 1993-12-14 Ford Motor Company Internal combustion engine fuel supply system
DE4322431C2 (en) * 1993-07-06 1997-04-10 Mtu Muenchen Gmbh Cooling structure and process for its manufacture
CN1228591C (en) * 2002-07-12 2005-11-23 株式会社电装 Heat exchanger for cooling air
US7117680B2 (en) * 2004-04-22 2006-10-10 United Technologies Corporation Cooling scheme for scramjet variable geometry hardware
DE102006021436A1 (en) * 2006-05-09 2007-11-15 Mtu Aero Engines Gmbh Gas turbine engine
DE102010025587A1 (en) * 2010-06-29 2011-12-29 Mtu Aero Engines Gmbh Gas turbine i.e. propeller gas turbine, has hollow sections with profile axles bent against series axles around profile angle, and exhausting passage bent against gas turbine around passage angle along longitudinal axis
DE102010025998A1 (en) * 2010-07-03 2012-03-29 Mtu Aero Engines Gmbh Profile heat exchanger, particularly for gas turbine, has a supply passage, discharge passage and multiple hollow sections, particularly elongated, oval or elliptical shaped cross sections
US10190828B2 (en) * 2015-10-22 2019-01-29 Hamilton Sundstrand Corporation Heat exchangers
US11092384B2 (en) * 2016-01-14 2021-08-17 Hamilton Sundstrand Corporation Thermal stress relief for heat sinks
US11892250B2 (en) * 2021-05-14 2024-02-06 Rtx Corporation Heat exchanger tube support
US11859910B2 (en) * 2021-05-14 2024-01-02 Rtx Corporation Heat exchanger tube support

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2026088A1 (en) * 1968-12-13 1970-09-11 Dunlop Co Ltd Metallic foam heat transfer element
US3825063A (en) * 1970-01-16 1974-07-23 K Cowans Heat exchanger and method for making the same
FR2337867A1 (en) * 1976-01-12 1977-08-05 Chausson Usines Sa HEAT EXCHANGER WITH THICK COLLECTORS
DE2907810C2 (en) * 1979-02-28 1985-07-04 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Heat exchangers for conducting gases with widely differing temperatures
DE3310061A1 (en) * 1982-11-19 1984-05-24 MTU Motoren- und Turbinen-Union München GmbH, 8000 München METHOD FOR PRODUCING A PIPE DISTRIBUTOR ARRANGEMENT AND A HEAT EXCHANGER TANK PRODUCED BY THIS METHOD
US4512069A (en) * 1983-02-04 1985-04-23 Motoren-Und Turbinen-Union Munchen Gmbh Method of manufacturing hollow flow profiles
DE3329202A1 (en) * 1983-08-12 1985-02-21 MTU Motoren- und Turbinen-Union München GmbH, 8000 München PROFILE TUBE HEAT EXCHANGER
DE3447145A1 (en) * 1984-12-22 1986-06-26 MTU Motoren- und Turbinen-Union München GmbH, 8000 München METHOD FOR PRODUCING CYLINDRICAL HEAT EXCHANGER COLLECTING PIPE STRUCTURES OF FORMING RING DISC-LIKE COMPONENTS
DE3543893A1 (en) * 1985-12-12 1987-06-25 Mtu Muenchen Gmbh HEAT EXCHANGER
DE3635548C1 (en) * 1986-10-20 1988-03-03 Mtu Muenchen Gmbh Heat exchanger

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JPH01147295A (en) 1989-06-08
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DE3861453D1 (en) 1991-02-07
US4893674A (en) 1990-01-16
EP0313038A1 (en) 1989-04-26

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