WO2000018972A1 - Verfahren und behandlungseinrichtung zum abkühlen von hocherwärmten metallbauteilen - Google Patents
Verfahren und behandlungseinrichtung zum abkühlen von hocherwärmten metallbauteilen Download PDFInfo
- Publication number
- WO2000018972A1 WO2000018972A1 PCT/DE1999/003237 DE9903237W WO0018972A1 WO 2000018972 A1 WO2000018972 A1 WO 2000018972A1 DE 9903237 W DE9903237 W DE 9903237W WO 0018972 A1 WO0018972 A1 WO 0018972A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- metal components
- chamber
- gas
- cooling gas
- areas
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/84—Controlled slow cooling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/56—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering characterised by the quenching agents
- C21D1/613—Gases; Liquefied or solidified normally gaseous material
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/0068—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/62—Quenching devices
- C21D1/667—Quenching devices for spray quenching
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/74—Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material
- C21D1/767—Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material with forced gas circulation; Reheating thereof
Definitions
- pre-process heating is often necessary in order to be able to provide the metal components with a coating, for example.
- the heating of the metal components and their coating usually take place in a closed chamber, often in a vacuum chamber.
- this causes an uncontrolled thermal shock to the metal components, which is why it seems advisable to cool the components in the chamber with an inert cooling gas, which is often also referred to as quench gas, by flooding the chamber with the inert cooling gas.
- the invention is based on the object of proposing a method for cooling metal components which have been heated to a high temperature, by means of which a uniform cooling of the entire metal component can be achieved regardless of the configuration of the metal components.
- the invention is based on a method for cooling metal components that have been heated up in a chamber, in which an inert cooling gas is introduced into the chamber with the metal components that have been heated up, and according to the invention provides that the areas of the metal components correspond to the size
- the inert cooling gas is applied to the mass in such a targeted manner that the cooling of the entire metal structure is uniform. partly occurs.
- Metal components are " not only pure metal components but also coated metal components, such as ceramic metal components.
- An essential advantage of the method according to the invention is that the targeted supply of inert cooling gas to the areas of the metal components in accordance with their mass concentration reduces the thermal stresses in the respective metal component during the cooling process. As a result, even components that are designed to be very complex with very different mass distributions can be cooled relatively quickly while avoiding thermal stresses, as a result of which better use is made of the treatment devices required to carry out the method.
- Another advantage is that the targeted cooling of individual areas results in a uniform cooling of the entire metal component, which means that the method according to the invention can be easily and easily integrated into a comprehensive method with, for example, a further heat treatment.
- the inert cooling gas can be applied to the individual areas of the metal components to be treated in different ways; For example, it is possible to achieve a different level of exposure to the cooling gas by specifically attaching more or fewer gas supply nozzles for the inert cooling gas in the vicinity of the individual areas of the metal components.
- Such housings can namely with relatively Realize little effort, especially if they are used simultaneously to hold the metal components in the chamber.
- metal components of very different configurations and different mass distributions can be cooled.
- the base and top plate of the gas turbine blades are advantageously provided with housings, since these parts have a relatively large mass compared to the blade of the turbine blade lying between them.
- the method according to the invention also offers the advantageous possibility of individually applying the inert cooling gas to the inside of the metal components, which additionally promotes even cooling of the component.
- the invention is also based on the object of proposing a treatment device for cooling metal components with a chamber accommodating the metal components, with which a uniform cooling of the metal components can be achieved with relatively little effort in terms of construction and production technology.
- Mass are surrounded by a housing, each housing 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 it is relatively easy to manufacture because, as a rule, already existing devices with a chamber are only to be additionally provided with housings for the metal components with connections of their inlet openings.
- gas supply control devices are present in the connections between the inlet openings and the reservoir.
- the treatment device 1 shown has a chamber 2, preferably a vacuum chamber, in which, with additional devices, which are not shown in the figure for the sake of clarity, a metal component 3 has been heated up, for example up to 1100 ° C., for a coating perform.
- the metal component 3 it is surrounded, for example, by manipulators (not shown) with a housing 4 in a region 5 and with a further housing 6 in a further region 7.
- region 5 forms the base and region 7 the top plate of the turbine blade;
- the blade 8 extends between the foot 5 and the head plate 7. Both the region 5 or the foot of a gas turbine blade and the region 7 or the head plate of a gas turbine blade have compared to the intermediate layer rich 8 or the sheet relatively large masses and are therefore provided with the housings 4 and 6.
- the housing 4 is filled via an inlet opening 9 with an inert cooling gas which flows in the direction of the arrow 10 via a gas supply control device 11 and a pipe 12 into the housing 4.
- a tube 16 and an inlet opening 17 in the housing 6 this is also filled with the internal cooling gas, which - via gaps (not shown) on the edge of the further housing 6 - as well as in the housing 4 - into the interior of the chamber 2 can flow out.
- the throughput of inert cooling gas through the chamber 2 can be regulated by means of a regulated gas suction device (not shown).
- each casing 4 or 6 can be individually supplied with the cooling gas via a gas supply control device 11 or 15, it is possible for each casing 4 or 6 to be acted upon with inert cooling gas as strongly as it is in the With regard to the masses of the areas 5 and 7 of the metal component 3 surrounded by the housings 4 and 6, it is necessary to achieve uniform cooling. If one additionally takes into account the cooling of the area 8 of the metal component 3 caused by the inert gas in the chamber 2, then by correspondingly actuating the gas supply control devices 11 and 15 it can be achieved that the metal component 3 cools uniformly overall.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatments In General, Especially Conveying And Cooling (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP99959191A EP1129224B1 (de) | 1998-09-30 | 1999-09-30 | Verfharen und behandlungseinrichtung zum abkühlen von hocherwärmten metallbauteilen |
DE59907749T DE59907749D1 (de) | 1998-09-30 | 1999-09-30 | Verfharen und behandlungseinrichtung zum abkühlen von hocherwärmten metallbauteilen |
JP2000572419A JP2003531958A (ja) | 1998-09-30 | 1999-09-30 | 高温加熱された金属構造部材の冷却方法及び装置 |
US09/822,016 US6434949B2 (en) | 1998-09-30 | 2001-03-30 | Method and treatment device for the cooling of highly heated metal components |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19845805.3 | 1998-09-30 | ||
DE19845805A DE19845805C1 (de) | 1998-09-30 | 1998-09-30 | Verfahren und Behandlungseinrichtung zum Abkühlen von hocherwärmten Metallbauteilen |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/822,016 Continuation US6434949B2 (en) | 1998-09-30 | 2001-03-30 | Method and treatment device for the cooling of highly heated metal components |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2000018972A1 true WO2000018972A1 (de) | 2000-04-06 |
Family
ID=7883454
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DE1999/003237 WO2000018972A1 (de) | 1998-09-30 | 1999-09-30 | Verfahren und behandlungseinrichtung zum abkühlen von hocherwärmten metallbauteilen |
Country Status (5)
Country | Link |
---|---|
US (1) | US6434949B2 (de) |
EP (1) | EP1129224B1 (de) |
JP (1) | JP2003531958A (de) |
DE (2) | DE19845805C1 (de) |
WO (1) | WO2000018972A1 (de) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1154024A1 (de) * | 2000-04-14 | 2001-11-14 | Ipsen International GmbH | Verfahren und Vorrichtung zur Wärmebehandlung metallischer Werkstücke |
US7592592B2 (en) | 2002-04-23 | 2009-09-22 | Autoliv Development Ab | Night vision arrangement |
WO2014130150A1 (en) * | 2013-02-20 | 2014-08-28 | Rolls-Royce Corporation | Wall member useful in quenching |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR576695A (fr) * | 1924-02-01 | 1924-08-25 | Cie Des Forges De Chatillon | Auto-dressage thermique des barres métalliques de section dissymétrique et en particulier des rails en acier |
DE1274151B (de) * | 1960-04-07 | 1968-08-01 | Bochumer Eisen Heintzmann | Abschreckvorrichtung fuer die Waermebehandlung von Profilstahl |
EP0119186A2 (de) * | 1983-03-10 | 1984-09-19 | Vereinigte Edelstahlwerke Aktiengesellschaft (Vew) | Verfahren zur Herstellung von Turbinenschaufeln |
EP0129701A1 (de) * | 1983-06-22 | 1985-01-02 | Schmetz GmbH & Co. KG Unternehmensverwaltung | Ofenanlage zur Kühlung einer Charge, insbesondere aus metallischen Werkstücken |
DE3405244C1 (de) * | 1984-02-15 | 1985-04-11 | Aichelin GmbH, 7015 Korntal-Münchingen | Industrieofen,insbesondere Mehrkammer-Vakuumofen zur Waermebehandlung von Chargen metallischer Werkstuecke |
DE4208485C1 (de) * | 1992-03-17 | 1993-02-11 | Joachim Dr.-Ing. 7250 Leonberg De Wuenning |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2839807C2 (de) * | 1978-09-13 | 1986-04-17 | Degussa Ag, 6000 Frankfurt | Vakuumofen mit Gaskühleinrichtung |
US5173124A (en) * | 1990-06-18 | 1992-12-22 | Air Products And Chemicals, Inc. | Rapid gas quenching process |
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 (ja) * | 1993-12-28 | 2005-05-25 | 株式会社東芝 | タービン冷却翼 |
US5568833A (en) * | 1995-06-07 | 1996-10-29 | Allison Engine Company, Inc. | Method and apparatus for directional solidification of integral component casting |
DE19539770A1 (de) * | 1995-06-20 | 1997-01-02 | Abb Research Ltd | Verfahren zur Herstellung eines gerichtet erstarrten Gießkörpers und Vorrichtung zur Durchführung dieses Verfahrens |
-
1998
- 1998-09-30 DE DE19845805A patent/DE19845805C1/de not_active Expired - Fee Related
-
1999
- 1999-09-30 JP JP2000572419A patent/JP2003531958A/ja not_active Withdrawn
- 1999-09-30 DE DE59907749T patent/DE59907749D1/de not_active Expired - Lifetime
- 1999-09-30 EP EP99959191A patent/EP1129224B1/de not_active Expired - Lifetime
- 1999-09-30 WO PCT/DE1999/003237 patent/WO2000018972A1/de active IP Right Grant
-
2001
- 2001-03-30 US US09/822,016 patent/US6434949B2/en not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR576695A (fr) * | 1924-02-01 | 1924-08-25 | Cie Des Forges De Chatillon | Auto-dressage thermique des barres métalliques de section dissymétrique et en particulier des rails en acier |
DE1274151B (de) * | 1960-04-07 | 1968-08-01 | Bochumer Eisen Heintzmann | Abschreckvorrichtung fuer die Waermebehandlung von Profilstahl |
EP0119186A2 (de) * | 1983-03-10 | 1984-09-19 | Vereinigte Edelstahlwerke Aktiengesellschaft (Vew) | Verfahren zur Herstellung von Turbinenschaufeln |
EP0129701A1 (de) * | 1983-06-22 | 1985-01-02 | Schmetz GmbH & Co. KG Unternehmensverwaltung | Ofenanlage zur Kühlung einer Charge, insbesondere aus metallischen Werkstücken |
DE3405244C1 (de) * | 1984-02-15 | 1985-04-11 | Aichelin GmbH, 7015 Korntal-Münchingen | Industrieofen,insbesondere Mehrkammer-Vakuumofen zur Waermebehandlung von Chargen metallischer Werkstuecke |
DE4208485C1 (de) * | 1992-03-17 | 1993-02-11 | Joachim Dr.-Ing. 7250 Leonberg De Wuenning |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1154024A1 (de) * | 2000-04-14 | 2001-11-14 | Ipsen International GmbH | Verfahren und Vorrichtung zur Wärmebehandlung metallischer Werkstücke |
US7255829B1 (en) | 2000-04-14 | 2007-08-14 | Ipsen International Gmbh | Method and apparatus for treatment of metallic workpieces |
US7592592B2 (en) | 2002-04-23 | 2009-09-22 | Autoliv Development Ab | Night vision arrangement |
WO2014130150A1 (en) * | 2013-02-20 | 2014-08-28 | Rolls-Royce Corporation | Wall member useful in quenching |
US9840747B2 (en) | 2013-02-20 | 2017-12-12 | Rolls-Royce Corporation | Wall member useful in quenching |
US11001903B2 (en) | 2013-02-20 | 2021-05-11 | Rolls-Royce Corporation | Wall member useful in quenching |
Also Published As
Publication number | Publication date |
---|---|
JP2003531958A (ja) | 2003-10-28 |
DE59907749D1 (de) | 2003-12-18 |
DE19845805C1 (de) | 2000-04-27 |
US20010029680A1 (en) | 2001-10-18 |
EP1129224A1 (de) | 2001-09-05 |
EP1129224B1 (de) | 2003-11-12 |
US6434949B2 (en) | 2002-08-20 |
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