EP1129224B1 - Device and process for cooling metal components which were subjected to high temperatures - Google Patents

Device and process for cooling metal components which were subjected to high temperatures Download PDF

Info

Publication number
EP1129224B1
EP1129224B1 EP99959191A EP99959191A EP1129224B1 EP 1129224 B1 EP1129224 B1 EP 1129224B1 EP 99959191 A EP99959191 A EP 99959191A EP 99959191 A EP99959191 A EP 99959191A EP 1129224 B1 EP1129224 B1 EP 1129224B1
Authority
EP
European Patent Office
Prior art keywords
metal components
chamber
regions
cooling
gas
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
EP99959191A
Other languages
German (de)
French (fr)
Other versions
EP1129224A1 (en
Inventor
Lutz Wolkers
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.)
Siemens AG
Original Assignee
Siemens AG
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 Siemens AG filed Critical Siemens AG
Publication of EP1129224A1 publication Critical patent/EP1129224A1/en
Application granted granted Critical
Publication of EP1129224B1 publication Critical patent/EP1129224B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/84Controlled slow cooling
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/56General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering characterised by the quenching agents
    • C21D1/613Gases; Liquefied or solidified normally gaseous material
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0068Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/62Quenching devices
    • C21D1/667Quenching devices for spray quenching
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/74Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material
    • C21D1/767Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material with forced gas circulation; Reheating thereof

Definitions

  • Pre-process heating is often required to the metal components then provided with a coating, for example to be able to.
  • the heating of the metal components and their coating usually take place in a completed Chamber, often in a vacuum chamber.
  • After treating the Metal components must be cooled, which is why offers to open the chamber easily and the metal components thereby exposing to the ambient temperature. This will, however an uncontrolled thermal shock applied to the metal components, which is why it seems advisable to place the components in the chamber with an inert cooling gas, often called quench gas is referred to cool by the chamber with the inert Cooling gas is flooded.
  • EP-A-0 119 186 and FR-A-5 766 95 describe a method for cooling highly heated ones targeted metal components in the areas of the metal components according to the size of their mass are acted upon with an inert cooling gas to such an extent that a uniform Cooling of the entire metal component occurs.
  • a treatment device for cooling metal components is further out DE-A-1 274 151 and DE-C-3 405 244 are known.
  • the invention has for its object a method for Cooling of metal components heated up in a chamber to propose, regardless of the design of the metal components even cooling of the whole Metal component can be reached.
  • the invention is based on a method for cooling metal components that have been heated up in a chamber from in the chamber with the highly heated
  • An inert cooling gas is introduced into metal components, and Areas of metal components specifically so different according to the size of their mass are heavily charged with the inert cooling gas, that even cooling of the entire metal component entry provides according to the invention that the areas of metal components with relatively large Mass to be provided with enclosures and the enclosures of areas of different sizes for be individually charged with the inert cooling gas.
  • metal components are not just that pure metal components but also coated metal components, how to understand ceramic metal components.
  • the different levels of exposure to the individual areas of the metal components to be treated with the inert Cooling gas can be carried out in different ways; for example it is possible through a targeted attachment of more or less gas supply nozzles for the inert cooling gas near the individual areas of the metal components a different amount of exposure to the cooling gas to reach.
  • the housings can be compared with Realize little effort, especially if you at the same time to hold the metal components in the chamber be used.
  • metal components can be very different design and different Cool mass distribution.
  • Metal components are advantageously foot and Provide the top plate of the gas turbine blades with housings, because these parts compared to what lies between them Blade of the turbine blade has a relatively large mass exhibit.
  • the method according to the invention also offers the advantageous one Possibility of customizing the metal components on the inside to act with the inert cooling gas, whereby a uniform Cooling of the component is also promoted.
  • the invention is also based on the object of a treatment device for cooling metal components with a to propose the chamber containing metal components with which constructively and technically proportionate even cooling of the metal components with little effort can be achieved.
  • the solution to this problem is in a treatment facility for cooling metal components with the metal components receiving chamber seen with a reservoir for an inert cooling gas, wherein the metal component has at least two areas, in the invention the chamber has at least two housings, the chamber for areas of the Metal component, which is a relative to other areas of the metal component have a large mass, each has a separate housing, every enclosure is provided with an inlet opening, and the inlet openings are individually connected to the reservoir.
  • a major advantage of the treatment device according to the invention is that this is relatively simple can be produced because - usually existing facilities with chamber - only additionally with housings for the metal components with connections of their inlet openings are to be provided.
  • the treatment device 1 shown has a chamber 2, preferably a vacuum chamber, in which, with additional devices, for the sake of clarity in the FIG. Not shown, a metal component 3 is highly heated, for example, has been heated to 1100 ° C to carry out a coating.
  • the housing 4 is an inlet opening 9 with a inert cooling gas filled in the direction of arrow 10 a gas supply control device 11 and a tube 12 in the housing 4 streams.
  • a pipe 16 and an inlet opening 17 in the housing 6 this also filled with the intertening cooling gas that is not over shown column on the edge of the further housing 6 - as in the case of 4 - in the interior of the chamber 2 can flow out.
  • each enclosure 4 or 6 via a gas supply control device 11 or 15 can be supplied individually with the cooling gas, it is possible to make each enclosure 4 or 6 as strong by itself with inert cooling gas, as is the case with regard to the masses of the areas surrounded by housings 4 and 6 5 or 7 of the metal component 3 to achieve a uniform Cooling is required. If you also take into account caused by the inert gas in chamber 2 Cooling of the area 8 of the metal component 3, then by operating the gas supply control devices accordingly 11 and 15 achieve that the metal component 3 itself cools evenly overall.

Description

Im Zuge der Herstellung von Metallbauteilen, insbesondere von mechanisch und thermisch hochbelasteten Metallbauteilen, ist häufig eine Vorprozeßerwärmung erforderlich, um die Metallbauteile danach beispielsweise mit einer Beschichtung versehen zu können. Das Erwärmen der Metallbauteile und ihre Beschichtung erfolgen in der Regel in einer abgeschlossenen Kammer, häufig in einer Vakuumkammer. Nach der Behandlung der Metallbauteile müssen diese abgekühlt werden, wozu es sich anbietet, die Kammer einfach zu öffnen und die Metallbauteile damit der Umgebungstemperatur auszusetzen. Dadurch wird aber ein unkontrollierter Thermoschock auf die Metallbauteile ausgeübt, weshalb es ratsam erscheint, die Bauteile in der Kammer mit einem inerten Kühlgas, das häufig auch als Quenchgas bezeichnet wird, abzukühlen, indem die Kammer mit dem inerten Kühlgas geflutet wird.In the course of the production of metal components, in particular of mechanically and thermally highly stressed metal components Pre-process heating is often required to the metal components then provided with a coating, for example to be able to. The heating of the metal components and their coating usually take place in a completed Chamber, often in a vacuum chamber. After treating the Metal components must be cooled, which is why offers to open the chamber easily and the metal components thereby exposing to the ambient temperature. This will, however an uncontrolled thermal shock applied to the metal components, which is why it seems advisable to place the components in the chamber with an inert cooling gas, often called quench gas is referred to cool by the chamber with the inert Cooling gas is flooded.

EP-A-0 119 186 und FR-A-5 766 95 verchreiben ein Verfahren zum Abkühlen von hocherwärmten metallbauteilen bei dem Bereiche der Metallbauteile entsprechend der Größe ihrer Masse gezielt derart unterschiedlich stark mit einem inerten Kühlgas beaufschlagt werden, daß eine gleichmäßige Abkühlung des gesamten Metallbauteils eintriff.EP-A-0 119 186 and FR-A-5 766 95 describe a method for cooling highly heated ones targeted metal components in the areas of the metal components according to the size of their mass are acted upon with an inert cooling gas to such an extent that a uniform Cooling of the entire metal component occurs.

Eine Behandlungseinrichtung zum Abkühlen von metallbauteilen ist weiter aus DE-A-1 274 151 und DE-C-3 405 244 bekannt.A treatment device for cooling metal components is further out DE-A-1 274 151 and DE-C-3 405 244 are known.

Der Erfindung liegt die Aufgabe zugrunde, ein Verfahren zum Abkühlen von in einer Kammer hocherwärmten Metallbauteilen vorzuschlagen, mit dem sich unabhängig von der Ausgestaltung der Metallbauteile eine gleichmäßige Abkühlung des gesamten Metallbauteils erreichen läßt.The invention has for its object a method for Cooling of metal components heated up in a chamber to propose, regardless of the design of the metal components even cooling of the whole Metal component can be reached.

Zur Lösung dieser Aufgabe geht die Erfindung von einem Verfahren zum Abkühlen von in einer Kammer hocherwärmten Metallbauteilen aus, bei dem in die Kammer mit den hocherwärmten Metallbauteilen ein inertes Kühlgas eingebracht wird, und Bereiche der Metallbauteile entsprechend der Größe ihrer Masse gezielt derart unterschiedlich stark mit dem inerten Kühlgas beaufschlagt werden, daß eine gleichmäßige Abkühlung des gesamten Metallbauteils eintritt sieht erfindungsgemäß vor, daß die Bereiche der Metallbauteile mit relativ großer Masse mit Einhäusungen versehen werden und die Einhäusungen von Bereichen mit unterschiedlich großer Masse jeweils für sich mit dem inerten Kühlgas individuell beaufschlagt werden. Unter Metallbauteilen sind dabei nicht nur reine Metallbauteile sondern auch beschichtete Metallbauteile, wie Keramik-Metallbauteile zu verstehen.To achieve this object, the invention is based on a method for cooling metal components that have been heated up in a chamber from in the chamber with the highly heated An inert cooling gas is introduced into metal components, and Areas of metal components specifically so different according to the size of their mass are heavily charged with the inert cooling gas, that even cooling of the entire metal component entry provides according to the invention that the areas of metal components with relatively large Mass to be provided with enclosures and the enclosures of areas of different sizes for be individually charged with the inert cooling gas. Among metal components are not just that pure metal components but also coated metal components, how to understand ceramic metal components.

Ein wesentlicher Vorteil des erfindungsgemäßen Verfahrens besteht darin, daß durch die gezielte Zuführung von inertem Kühlgas zu den Bereichen der Metallbauteile entsprechend ihrer Massenkonzentration eine Reduktion von Thermospannungen in dem jeweiligen Metallbauteil beim Abkühlungsvorgang erreicht wird. Dadurch lassen sich auch sehr komplex mit sehr unterschiedlicher Masseverteilung gestaltete Bauteile verhältnismäßig schnell unter Vermeidung von Thermospannungen abkühlen, wodurch auch eine bessere Ausnutzung von zur Durchführung des Verfahrens benötigten Behandlungseinrichtungen erreicht wird. Ein weiterer Vorteil ist darin zu sehen, daß durch die gezielte Abkühlung einzelner Bereiche insgesamt eine gleichmäßige Abkühlung des gesamten Metallbauteils eintritt, wodurch sich das erfindungsgemäße Verfahren gut und einfach in ein umfassendes Verfahren mit beispielsweise einer weiteren Wärmebehandlung integrieren läßt.There is a significant advantage of the method according to the invention in that through the targeted supply of inert Cooling gas to the areas of the metal components according to their Mass concentration a reduction of thermal stresses reached in the respective metal component during the cooling process becomes. This can also be very complex with very different mass distribution designed components proportionally quickly while avoiding thermal stress cool down, which also makes better use of Implementation of the procedure required treatment facilities is achieved. Another advantage is that that through the targeted cooling of individual areas as a whole uniform cooling of the entire metal component occurs, whereby the inventive method good and easy in a comprehensive process using for example a further heat treatment can be integrated.

Bei der Durchführung des erfindungsgemäßen Verfahrens kann die unterschiedlich starke Beaufschlagung der einzelnen Bereiche der zu behandelnden Metallbauteile mit dem inerten Kühlgas in unterschiedlicher Weise durchgeführt werden; beispielsweise ist es möglich, durch eine gezielte Anbringung von mehr oder weniger Gaszuführungsdüsen für das inerte Kühlgas in der Nähe der einzelnen Bereiche der Metallbauteile eine unterschiedlich starke Beaufschlagung mit dem Kühlgas zu erreichen. Die Einhäusungen lassen sich mit verhältnismä-ßig wenig Aufwand realisieren, insbesondere dann, wenn sie gleichzeitig zur Halterung der Metallbauteile in der Kammer verwendet werden.When carrying out the method according to the invention the different levels of exposure to the individual areas of the metal components to be treated with the inert Cooling gas can be carried out in different ways; for example it is possible through a targeted attachment of more or less gas supply nozzles for the inert cooling gas near the individual areas of the metal components a different amount of exposure to the cooling gas to reach. The housings can be compared with Realize little effort, especially if you at the same time to hold the metal components in the chamber be used.

Mit dem erfindungsgemäßen Verfahren lassen sich Metallbau-teile sehr unterschiedlicher Ausgestaltung und unterschiedlicher Massenverteilung kühlen. Bei Gasturbinenschaufeln darstellenden Metallbauteilen werden vorteilhafterweise Fuß und Kopfplatte der Gasturbinenschaufeln mit Einhäusungen versehen, da diese Teile im Vergleich zu dem zwischen ihnen liegenden Blatt der Turbinenschaufel eine relativ große Masse aufweisen.With the method according to the invention, metal components can be very different design and different Cool mass distribution. Representing gas turbine blades Metal components are advantageously foot and Provide the top plate of the gas turbine blades with housings, because these parts compared to what lies between them Blade of the turbine blade has a relatively large mass exhibit.

Das erfindungsgemäße Verfahren bietet ferner die vorteilhafte Möglichkeit, die Metallbauteile an Innenseiten individuell mit dem inerten Kühlgas zu beaufschlagen, wodurch ein gleichmäßiges Abkühlen des Bauteils zusätzlich gefördert wird.The method according to the invention also offers the advantageous one Possibility of customizing the metal components on the inside to act with the inert cooling gas, whereby a uniform Cooling of the component is also promoted.

Der Erfindung liegt ferner die Aufgabe zugrunde, eine Behandlungseinrichtung zum Abkühlen von Metallbauteilen mit einer die Metallbauteile aufnehmenden Kammer vorzuschlagen, mit der sich mit konstruktiv und herstellungstechnisch verhältnismäßig geringen Aufwand eine gleichmäßige Abkühlung der Metallbauteile erreichen läßt.The invention is also based on the object of a treatment device for cooling metal components with a to propose the chamber containing metal components with which constructively and technically proportionate even cooling of the metal components with little effort can be achieved.

Die Lösung dieser Aufgabe wird in einer Behandlungseinrichtung zum Abkühlen von Metallbauteilen mit einer die Metallbauteile aufnehmenden Kammer gesehen, die mit einem Reservoir für ein inertes Kühlgas verbunden ist, wobei das Metallbauteil zumindest zwei Bereiche aufweist, bei der erfindungsgemäß die Kammer zumindest zwei Einhäusungen aufweist, die Kammer für Bereiche des Metallbauteils, die im vergleich zu anderen Bereichen der Metallbauteils eine relativ große Masse aufweisen, jeweils eine separate Einhausung aufweist, jede Einhausung mit einer Einlaßöffnung versehen ist, und die Einlaßöffnungen für sich mit dem Reservoir verbunden sind. The solution to this problem is in a treatment facility for cooling metal components with the metal components receiving chamber seen with a reservoir for an inert cooling gas, wherein the metal component has at least two areas, in the invention the chamber has at least two housings, the chamber for areas of the Metal component, which is a relative to other areas of the metal component have a large mass, each has a separate housing, every enclosure is provided with an inlet opening, and the inlet openings are individually connected to the reservoir.

Ein wesentlicher Vorteil der erfindungsgemäßen Behandlungseinrichtung besteht darin, daß diese verhältnismäßig einfach herstellbar ist, weil -in der Regel bereits vorhandene Einrichtungen mit Kammer - lediglich zusätzlich mit Einhäusungen für die Metallbauteile mit Anschlüssen ihrer Einlaßöffnungen zu versehen sind.A major advantage of the treatment device according to the invention is that this is relatively simple can be produced because - usually existing facilities with chamber - only additionally with housings for the metal components with connections of their inlet openings are to be provided.

Als besonders vorteilhaft wird es angesehen, wenn in den Verbindungen zwischen den Einlaßöffnungen und dem Reservoir Gaszuführungsregeleinrichtungen vorhanden sind.It is considered particularly advantageous if in the compounds between the inlet openings and the reservoir gas supply control devices available.

Zur Erläuterung der Erfindung ist in der Figur in schematischer Darstellung ein Ausführungsbeispiel einer erfindungsgemäßen Behandlungseinrichtung zum Abkühlen von Metallbauteilen dargestellt.To explain the invention is in the figure in a schematic Representation of an embodiment of an inventive Treatment device for cooling metal components shown.

Die dargestellte Behandlungseinrichtung 1 weist eine Kammer 2, vorzugsweise eine Vakuumkammer, auf, in der mit Zusatzeinrichtungen, die der besseren Übersichtlichkeit halber in der Figur nicht dargestellt sind, ein Metallbauteil 3 hocherwärmt, beispielsweise bis auf 1100°C erwärmt worden ist, um eine Beschichtung durchzuführen.The treatment device 1 shown has a chamber 2, preferably a vacuum chamber, in which, with additional devices, for the sake of clarity in the FIG. Not shown, a metal component 3 is highly heated, for example, has been heated to 1100 ° C to carry out a coating.

Zum Abkühlen des Metallbauteiles 3 wird dieses beispielsweise über nicht dargestellte Manipulatoren mit einer Einhäusung 4 an einem Bereich 5 und mit einer weiteren Einhäusung 6 an einem weiteren Bereich 7 umgeben. Handelt es sich bei dem Bauteil 3 beispielsweise um eine Gasturbinenschaufel, dann bildet der Bereich 5 den Fuß und der Bereich 7 die Kopfplatte der Turbinenschaufel; zwischen dem Fuß 5 und der Kopfplatte 7 erstreckt im Falle einer Gasturbinenschaufel das Blatt 8. Sowohl der Bereich 5 bzw. der Fuß einer Gasturbinenschaufel als auch der Bereich 7 bzw. die Kopfplatte einer Gasturbinenschaufel haben im Vergleich zu dem dazwischen liegenden Bereich 8 bzw. dem Blatt relativ große Massen und sind deshalb mit den Einhäusungen 4 und 6 versehen.To cool the metal component 3, this is for example via manipulators, not shown, with a housing 4 at an area 5 and with a further housing 6 at one surrounding area 7. Is it the component? 3, for example, around a gas turbine blade, then forms area 5 the foot and area 7 the top plate the turbine blade; between the foot 5 and the head plate 7 extends the blade 8 in the case of a gas turbine blade. Both the area 5 and the base of a gas turbine blade as well as the area 7 or the top plate of a gas turbine blade compared to the area in between 8 or the sheet relatively large masses and are therefore with housings 4 and 6.

Die Einhäusung 4 wird über eine Einlaßöffnung 9 mit einem inerten Kühlgas gefüllt, das in Richtung des Pfeiles 10 über eine Gaszuführungsregeleinrichtung 11 und ein Rohr 12 in die-Einhäusung 4 strömt.The housing 4 is an inlet opening 9 with a inert cooling gas filled in the direction of arrow 10 a gas supply control device 11 and a tube 12 in the housing 4 streams.

Über eine weitere Gaszuführungsregeleinrichtung 15, ein Rohr 16 und eine Einlaßöffnung 17 in der Einhäusung 6 wird diese ebenfalls mit dem interten Kühlgas gefüllt, das über nicht dargestellte Spalte am Rande der weiteren Einhausung 6 - ebenso wie bei der Einhausung 4 - in den Innenraum der Kammer 2 ausströmen kann.Via a further gas supply control device 15, a pipe 16 and an inlet opening 17 in the housing 6 this also filled with the intertening cooling gas that is not over shown column on the edge of the further housing 6 - as in the case of 4 - in the interior of the chamber 2 can flow out.

Mittels einer nicht dargestellten, geregelten Gasabsaugeinrichtung kann der Durchsatz an inertem Kühlgas durch die Kammer 2 geregelt werden.By means of a regulated gas suction device, not shown the throughput of inert cooling gas through the chamber 2 are regulated.

Da bei der dargestellten Behandlungseinrichtung 1 jede Einhausung 4 bzw. 6 über eine Gaszuführungsregeleinrichtung 11 bzw. 15 individuell mit dem Kühlgas beaufschlagt werden kann, ist es möglich, jede Einhausung 4 bzw. 6 für sich so stark mit inertem Kühlgas zu beaufschlagen, wie es im Hinblick auf die Massen der von den Einhäusungen 4 und 6 umgebenen Bereiche 5 bzw. 7 des Metallbauteils 3 zum Erreichen einer gleichmäßigen Abkühlung erforderlich ist. Berücksichtigt man zusätzlich das durch das inerte Gas in der Kammer 2 bewirkte Abkühlen des Bereichs 8 des Metallbauteils 3, dann läßt sich durch entsprechendes Betätigen der Gaszuführungsregeleinrichtungen 11 und 15 erreichen, daß das Metallbauteil 3 sich insgesamt gleichmäßig abkühlt.Since in the treatment device 1 shown each enclosure 4 or 6 via a gas supply control device 11 or 15 can be supplied individually with the cooling gas, it is possible to make each enclosure 4 or 6 as strong by itself with inert cooling gas, as is the case with regard to the masses of the areas surrounded by housings 4 and 6 5 or 7 of the metal component 3 to achieve a uniform Cooling is required. If you also take into account caused by the inert gas in chamber 2 Cooling of the area 8 of the metal component 3, then by operating the gas supply control devices accordingly 11 and 15 achieve that the metal component 3 itself cools evenly overall.

Claims (5)

  1. Method for the cooling of metal components highly heated in a chamber, in which an inert cooling gas is introduced into the chamber with the highly heated metal components, and
       regions (5, 7) of the metal components (3) are subjected in a controlled manner to the inert cooling gas to a differing extent according to the size of their mass, in such a way that a uniform cooling of the entire metal component (3) takes place,
    characterized in that
    the regions (5, 7) of the metal components (3) with relatively large mass are provided with housings (4, 6), and
    the housings (4, 6) of regions (5, 7) with different mass are each individually subjected separately to the inert cooling gas.
  2. Method according to Claim 1,
    characterized in that
    in the case of metal components which constitute gas turbine blades (3), the foot plate (5) and head plate (7) of the gas turbine blades are provided with housings (4, 6).
  3. Method according to Claims 1 or 2,
    characterized in that
    the metal components are subjected individually to the inert cooling gas on inner faces.
  4. Treatment device for the cooling of metal components with a chamber which receives the metal components and which is connected to a reservoir for an inert cooling gas, where the metal component has at least two regions,
    characterized in that the chamber (2) has at least two housings (4,6),
    in that the chamber (2) has a separate housing (4, 6) in each case for regions (5, 7) of the metal component (3) which have a relatively large mass in comparison with other regions of the metal component (3),
    in that each housing (4, 6) is provided with an inlet orifice (9, 17), and
    in that the inlet orifices (9, 17) are connected independently to the reservoir.
  5. Treatment device according to Claim 4,
    characterized in that
    gas supply regulating devices (11, 15) are present in the connections between the inlet orifices (9, 17) and the reservoir.
EP99959191A 1998-09-30 1999-09-30 Device and process for cooling metal components which were subjected to high temperatures Expired - Lifetime EP1129224B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19845805A DE19845805C1 (en) 1998-09-30 1998-09-30 Method and treatment device for cooling highly heated metal components
DE19845805 1998-09-30
PCT/DE1999/003237 WO2000018972A1 (en) 1998-09-30 1999-09-30 Device and process for cooling metal components which were subjected to high temperatures

Publications (2)

Publication Number Publication Date
EP1129224A1 EP1129224A1 (en) 2001-09-05
EP1129224B1 true EP1129224B1 (en) 2003-11-12

Family

ID=7883454

Family Applications (1)

Application Number Title Priority Date Filing Date
EP99959191A Expired - Lifetime EP1129224B1 (en) 1998-09-30 1999-09-30 Device and process for cooling metal components which were subjected to high temperatures

Country Status (5)

Country Link
US (1) US6434949B2 (en)
EP (1) EP1129224B1 (en)
JP (1) JP2003531958A (en)
DE (2) DE19845805C1 (en)
WO (1) WO2000018972A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE262598T1 (en) 2000-04-14 2004-04-15 Ipsen Int Gmbh METHOD AND DEVICE FOR THE HEAT TREATMENT OF METAL WORKPIECES
JP2005523200A (en) 2002-04-23 2005-08-04 オートリブ ディヴェロプメント アクチボラゲット Night vision device
WO2014130150A1 (en) * 2013-02-20 2014-08-28 Rolls-Royce Corporation Wall member useful in quenching

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR576695A (en) * 1924-02-01 1924-08-25 Cie Des Forges De Chatillon Thermal self-dressing of metal bars of asymmetric cross-section and in particular of steel rails
DE1274151B (en) * 1960-04-07 1968-08-01 Bochumer Eisen Heintzmann Quenching device for the heat treatment of profile steel
DE2839807C2 (en) * 1978-09-13 1986-04-17 Degussa Ag, 6000 Frankfurt Vacuum furnace with gas cooling device
AT376914B (en) * 1983-03-10 1985-01-25 Ver Edelstahlwerke Ag METHOD FOR PRODUCING TURBINE BLADES
DE3322386A1 (en) * 1983-06-22 1985-01-10 Schmetz Industrieofenbau und Vakuum-Hartlöttechnik KG, 5750 Menden METHOD FOR COOLING A BATCH AFTER A HEAT TREATMENT, AND OVEN SYSTEM FOR CARRYING OUT THE METHOD
DE3405244C1 (en) * 1984-02-15 1985-04-11 Aichelin GmbH, 7015 Korntal-Münchingen Industrial furnace, especially a multi-chamber vacuum furnace for the heat treatment of batches of metallic workpieces
US5173124A (en) * 1990-06-18 1992-12-22 Air Products And Chemicals, Inc. Rapid gas quenching process
DE4208485C2 (en) * 1992-03-17 1997-09-04 Wuenning Joachim Method and device for quenching metallic workpieces
US5226982A (en) * 1992-05-15 1993-07-13 The United States Of America As Represented By The Secretary Of The Air Force Method to produce hollow titanium alloy articles
JP3651490B2 (en) * 1993-12-28 2005-05-25 株式会社東芝 Turbine cooling blade
US5568833A (en) * 1995-06-07 1996-10-29 Allison Engine Company, Inc. Method and apparatus for directional solidification of integral component casting
DE19539770A1 (en) * 1995-06-20 1997-01-02 Abb Research Ltd Process for producing a directionally solidified casting and device for carrying out this process

Also Published As

Publication number Publication date
US6434949B2 (en) 2002-08-20
JP2003531958A (en) 2003-10-28
US20010029680A1 (en) 2001-10-18
DE19845805C1 (en) 2000-04-27
EP1129224A1 (en) 2001-09-05
WO2000018972A1 (en) 2000-04-06
DE59907749D1 (en) 2003-12-18

Similar Documents

Publication Publication Date Title
EP0562250B1 (en) Process and device for quenching of metal pieces
DE112009001953B4 (en) Silicon purification process
DE2703169C2 (en) Process for the production of metal powder and device for carrying out the process
DE112012005534T5 (en) Vacuum heat treatment device
DE102006019854A1 (en) Crucible apparatus and method for solidifying a molten material
DE102006029593A1 (en) Method and device for producing a solder joint
EP0474604A2 (en) Apparatus for thermal plasma processing of workpiece surfaces
DE102006044626A1 (en) Carburizing treatment apparatus and method
EP1129224B1 (en) Device and process for cooling metal components which were subjected to high temperatures
DE3819803C1 (en)
DE2952978C1 (en) Device for gas-dynamic mixing of liquid metal and simultaneous refining with a treatment gas in a container
EP1943364B1 (en) Method and installation for the dry transformation of a material structure of semifinished products
EP0103705B1 (en) Method of heat treating work pieces
DE19526882A1 (en) Process for cooling a hot surface and device for carrying out the process
DE102019206103A1 (en) Method and device for manufacturing a component by additive manufacturing using a free space method
CH659315A5 (en) VACUUM FURNACE FOR DEWAXING AND SINTERING CARBIDES.
DE10237494B4 (en) Method and apparatus for soldering in the vapor phase
DE2717360C3 (en) Process for producing granules of a semiconductor compound from arsenic selenide
EP1785206A1 (en) Method and apparatus for cooling a continuous casting mould by steam
DE102020131314B3 (en) Process and heat treatment system for the heat treatment of cast components
DE102008012931B4 (en) Method and device for cooling substrates
DE3322485A1 (en) Apparatus and process for metal processing or refining
EP1236403A2 (en) Process and apparatus for the preparation of particles from foodstuff, in particular chocolate
AT407846B (en) Metallurgical vessel
EP1743725A1 (en) Vapor soldering apparatus, in particular condensation apparatus.

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

17P Request for examination filed

Effective date: 20010215

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

17Q First examination report despatched

Effective date: 20011004

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

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): CH DE FR GB IT LI

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

REF Corresponds to:

Ref document number: 59907749

Country of ref document: DE

Date of ref document: 20031218

Kind code of ref document: P

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: GERMAN

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20040117

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

ET Fr: translation filed
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

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

Ref country code: FR

Payment date: 20040921

Year of fee payment: 6

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

Ref country code: LI

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

Effective date: 20040930

Ref country code: CH

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

Effective date: 20040930

26N No opposition filed

Effective date: 20040813

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: FR

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

Effective date: 20060531

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20060531

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

Ref country code: DE

Payment date: 20101119

Year of fee payment: 12

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

Ref country code: GB

Payment date: 20110915

Year of fee payment: 13

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

Ref country code: IT

Payment date: 20110927

Year of fee payment: 13

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 59907749

Country of ref document: DE

Effective date: 20120403

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

Ref country code: DE

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

Effective date: 20120403

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20120930

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 NON-PAYMENT OF DUE FEES

Effective date: 20120930

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

Ref country code: IT

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

Effective date: 20120930