EP0916897A2 - Heat shield - Google Patents
Heat shield Download PDFInfo
- Publication number
- EP0916897A2 EP0916897A2 EP98811060A EP98811060A EP0916897A2 EP 0916897 A2 EP0916897 A2 EP 0916897A2 EP 98811060 A EP98811060 A EP 98811060A EP 98811060 A EP98811060 A EP 98811060A EP 0916897 A2 EP0916897 A2 EP 0916897A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- felt
- heat shield
- fibers
- intermetallic
- heat
- 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.)
- Granted
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/04—Heavy metals
- F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
- F05C2201/0466—Nickel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
- F05D2300/2118—Zirconium oxides
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/614—Fibres or filaments
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12153—Interconnected void structure [e.g., permeable, etc.]
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12444—Embodying fibers interengaged or between layers [e.g., paper, etc.]
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12479—Porous [e.g., foamed, spongy, cracked, etc.]
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12611—Oxide-containing component
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12611—Oxide-containing component
- Y10T428/12618—Plural oxides
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12944—Ni-base component
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/131—Glass, ceramic, or sintered, fused, fired, or calcined metal oxide or metal carbide containing [e.g., porcelain, brick, cement, etc.]
Definitions
- the invention is based on a heat shield according to the preamble of the first Claim.
- Heat shields for example for use in thermal turbomachines and combustion chambers. These heat shields usually consist of a carrier material and a heat insulation layer which is connected to the carrier material via a binding layer. This bonding layer is applied in a vacuum-plasma process, which limits the size of the workable parts by the size of the vacuum chamber and makes production more expensive. Another problem is that at application temperatures above 900 ° C the bonding layer usually fails and the thermal insulation layer falls off. This will cause the heat shield to fail. From DE 3327216 A a heat protection layer made of a metallic felt which is infiltrated with zirconium oxide and filled up by means of CVD has become known.
- the metallic felt serves as a framework for the zirconium oxide coating.
- the disadvantage of this protective layer are the high manufacturing costs and the insufficient properties with regard to heat and oxidation resistance, especially the structure of the framework.
- the heat protection layer can also only with great difficulty, i.e. by means of large cooling air consumption can be cooled.
- the invention is based, with a heat shield of the aforementioned object Way of providing a cheap and efficient heat shield.
- the heat shield is made of a felt-like material consists of compressed and sintered intermetallic fibers.
- intermetallic fibers based felt-like material can be used at temperatures above 1000 ° C because the intermetallic fibers have a high heat resistance, a have high resistance to oxidation and advantageous thermal conductivity. These properties can also be determined by the selected intermetallic phase be set specifically and adapted to the respective conditions. Through the Porosity of the felt-like material can be a very efficient, low cooling air consuming Cooling are made possible.
- a heat shield 1 is shown in the single figure.
- a heat shield can Used in combustion chambers, thermal turbomachines such as gas turbines, etc. become.
- the heat shield consists of a carrier material 2, one on top of it arranged felt-like material 3 of intermetallic fibers and one Thermal insulation layer 4.
- the carrier material 2, which is usually metallic is, can have cooling channels 5.
- the thermal insulation layer 4 is, for example made of zirconium oxide which is partially mixed with yttrium oxide, calcium oxide or magnesium oxide or has been fully stabilized.
- the felt-like material 3 has become known, for example, from "VDI Report 1151, 1995, Metallische Hoch Temperaturfasem by Melt Extraction - Production, Properties and Applications, Stephani et al., Page 175ff". Fibers are produced there using the melt extraction process, the fibers are pressed and sintered. The felt-like material thus formed is used as a filter and as a catalyst carrier. According to the invention, this felt-like material is now made from intermetallic fibers. Intermetallic phases based on iron or nickel are advantageously used for this purpose. These have high heat resistance, high oxidation resistance and advantageous thermal conductivity. In addition, the abovementioned properties can be adjusted over a wide range by selecting an appropriate intermetallic phase. The felt-like material made of intermetallic fibers can also be produced very cheaply.
- the porosity of the felt-like material can be influenced by the parameters of the manufacturing process how press pressure and sintering parameters are set.
- the felt-like material made of intermetallic fibers is now on the carrier material attached.
- the carrier material serves as a fastening and stabilizing agent for the felt-like material.
- Thermal insulation layer applied this is done by known methods such as for example plasma sprays.
- the thermal insulation layer adheres excellently the rough and porous surface of the felt-like material.
- the thermal barrier layer reduces the temperature of the surface, the porous felt-like material is used for cooling. If the insulation layer fails, that is, if it is no longer available, the remaining is enough felt-like material due to the excellent properties in terms of heat resistance, Resistance to oxidation and advantageous thermal conductivity the intermetallic phases are still out. Even the felt-like material without a thermal barrier coating can thus be used as a heat shield, whereby here, however, in comparison to the additional use of a thermal barrier coating the cooling air consumption is somewhat higher.
- the invention is not limited to that shown and described Embodiment limited.
- the carrier material can also be omitted be when the felt-like material by a suitable choice of material and the porosity has sufficient inherent strength.
Abstract
Description
Die Erfindung geht aus von einem Hitzeschild nach dem Oberbegriff des ersten Anspruches.The invention is based on a heat shield according to the preamble of the first Claim.
Hitzeschilder, beispielsweise zur Verwendung in thermischen Strömungsmaschinen
und Brennkammern sind bekannt. Diese Hitzeschilder bestehen üblicherweise
aus einem Trägermaterial und einer Wärmedämmschicht, die über eine Bindeschicht
mit dem Trägermaterial verbunden ist. Diese Bindeschicht wird im Vakuum-Plasma-Verfahren
aufgetragen, was die Grösse der bearbeitbaren Teile durch
die Grösse der Vakuumkammer begrenzt und die Herstellung verteuert. Ein weiteres
Problem ist, dass bei Anwendungstemperaturen über 900°C die Bindeschicht
üblicherweise versagt und die Wärmedämmschicht abfällt. Dies führt zu einem
Versagen des Hitzeschildes.
Aus der DE 3327216 A ist eine Hitzeschutzschicht aus einem metallischen Filz
welcher mittels CVD mit Zirkonoxid infiltriert und aufgefüllt wird bekannt geworden. Heat shields, for example for use in thermal turbomachines and combustion chambers, are known. These heat shields usually consist of a carrier material and a heat insulation layer which is connected to the carrier material via a binding layer. This bonding layer is applied in a vacuum-plasma process, which limits the size of the workable parts by the size of the vacuum chamber and makes production more expensive. Another problem is that at application temperatures above 900 ° C the bonding layer usually fails and the thermal insulation layer falls off. This will cause the heat shield to fail.
From DE 3327216 A a heat protection layer made of a metallic felt which is infiltrated with zirconium oxide and filled up by means of CVD has become known.
Dadurch entsteht eine dichte feste Hitzeschutzschicht. Der metallische Filz dient als Gerüststruktur für die Zirkonoxidbeschichtung. Der Nachteil dieser Schutzschicht sind die hohen Herstellungskosten und die ungenügenden Eigenschaften bezüglich Hitze- und Oxidationsbeständigkeit, insbesondere der Gerüststruktur. Die Hitzeschutzschicht kann zudem nur mit grossen Schwierigkeiten, d.h. mittels grossem Kühlluftverbrauch gekühlt werden.This creates a tight, solid heat protection layer. The metallic felt serves as a framework for the zirconium oxide coating. The disadvantage of this protective layer are the high manufacturing costs and the insufficient properties with regard to heat and oxidation resistance, especially the structure of the framework. The heat protection layer can also only with great difficulty, i.e. by means of large cooling air consumption can be cooled.
Der Erfindung liegt die Aufgabe zugrunde, bei einem Hitzeschild der eingangs genannten Art einen billigen und effizienten Hitzeschild zur Verfügung zu stellen.The invention is based, with a heat shield of the aforementioned object Way of providing a cheap and efficient heat shield.
Erfindungsgemäss wird dies durch die Merkmale des ersten Anspruches erreicht.According to the invention, this is achieved by the features of the first claim.
Kern der Erfindung ist es also, dass der Hitzeschild aus einem filzähnlichen Material aus zusammengepressten und gesinterten intermetallischen Fasern besteht.The essence of the invention is therefore that the heat shield is made of a felt-like material consists of compressed and sintered intermetallic fibers.
Die Vorteile der Erfindung sind unter anderem dann zu sehen, dass durch die Verwendung von intermetallischen Fasern die zur Kühlung des Hitzeschildes benötigte Kühlluft deutlich reduziert werden kann. Das auf intermetallischen Fasern basierende filzähnliche Material kann bei Temperaturen von über 1000°C verwendet werden, da die intermetallischen Fasern eine hohe Hitzebeständigkeit, eine hohe Oxidationsbeständigkeit und vorteilhafte Wärmeleiteigenschaften aufweisen. Diese Eigenschaften können zudem durch die gewählte intermetallische Phase gezielt eingestellt und den jeweiligen Bedingungen angepasst werden. Durch die Porosität des filzähnlichen Materials kann eine sehr effiziente, wenig Kühlluft verbrauchende Kühlung ermöglicht werden. The advantages of the invention can be seen, inter alia, that by Use of intermetallic fibers needed to cool the heat shield Cooling air can be significantly reduced. That on intermetallic fibers based felt-like material can be used at temperatures above 1000 ° C because the intermetallic fibers have a high heat resistance, a have high resistance to oxidation and advantageous thermal conductivity. These properties can also be determined by the selected intermetallic phase be set specifically and adapted to the respective conditions. Through the Porosity of the felt-like material can be a very efficient, low cooling air consuming Cooling are made possible.
Es ist vorteilhaft auf dem filzähnlichen Material zusätzlich eine Wärmedämmschicht aufzutragen. Diese hält ohne spezielle Zwischenschichten auf dem filzähnlichen Material und verringert zusätzlich den Kühlungsbedarf und erhöht damit den Wirkungsgrad des Hitzeschildes zusätzlich.It is also advantageous to have a thermal barrier coating on the felt-like material to apply. This holds on the without special intermediate layers felt-like material and additionally reduces the cooling requirement and increases thus the efficiency of the heat shield in addition.
Weitere vorteilhafte Ausgestaltungen der Erfindung ergeben sich aus den weiteren Unteransprüchen.Further advantageous embodiments of the invention result from the others Subclaims.
In der Zeichnung ist ein schematisches Ausführungsbeispiel der Erfindung dargestellt.
Die einzige Figur zeigt einen Teillängsschnitt durch einen Hitzeschild. Es sind nur
die für das Verständnis der Erfindung wesentlichen Elemente gezeigt.In the drawing, a schematic embodiment of the invention is shown.
The only figure shows a partial longitudinal section through a heat shield. Only the elements essential for understanding the invention are shown.
In der einzigen Figur ist ein Hitzeschild 1 dargestellt. Ein solcher Hitzeschild kann
in Brennkammern, thermischen Strömungsmaschinen wie Gasturbinen, usw. Verwendet
werden. Der Hitzeschild besteht aus einem Trägermaterial 2, einem darauf
angeordneten filzähnlichen Material 3 aus intermetallischen Fasern und einer
Wärmedämmschicht 4. Das Trägermaterial 2, welches üblicherweise metallisch
ist, kann Kühlkanäle 5 aufweisen. Die Wärmedämmschicht 4 besteht beispielsweise
aus Zirkonoxid das mit Yttriumoxid, Calciumoxid oder Magnesiumoxid teil-
oder vollstabilisiert wurde.A heat shield 1 is shown in the single figure. Such a heat shield can
Used in combustion chambers, thermal turbomachines such as gas turbines, etc.
become. The heat shield consists of a
Das filzähnlichen Material 3 ist beispielsweise aus "VDI Bericht 1151, 1995, Metallische
Hochtemperaturfasem durch Schmelzextraktion - Herstellung, Eigenschaften
und Anwendungen, Stephani et al., Seite 175ff", bekannt geworden. Dort
werden Fasern im Schmelzextraktionsverfahren hergestellt, die Fasern verpresst
und gesintert. Das so gebildete filzähnliche Material wird als Filter und als Katalysator-Träger
verwendet.
Erfindungsgemäss wird nun dieses filzähnliche Material aus intermetallischen Fasern
hergestellt. Dazu werden vorteilhafterweise intermetallische Phasen auf Eisen-
oder Nickelbasis verwendet. Diese weisen eine hohe Hitzebeständigkeit, eine
hohe Oxidationsbeständigkeit und vorteilhafte Wärmeleiteigenschaften auf.
Zudem sind die vorgenannten Eigenschaften durch die Wahl einer entsprechenden
intermetallischen Phase in einem weiten Bereich einstellbar. Das filzähnliche
Material aus intermetallischen Fasern lässt sich zudem sehr billig herstellen.The felt-
According to the invention, this felt-like material is now made from intermetallic fibers. Intermetallic phases based on iron or nickel are advantageously used for this purpose. These have high heat resistance, high oxidation resistance and advantageous thermal conductivity. In addition, the abovementioned properties can be adjusted over a wide range by selecting an appropriate intermetallic phase. The felt-like material made of intermetallic fibers can also be produced very cheaply.
Die Porosität des filzähnlichen Materials kann durch die Parameter des Herstellungsprozesses wie Pressdruck und Sinterparameter eingestellt werden. Ein Vorteil dieser porösen Struktur ist, dass das filzähnliche Material sehr effizient direkt durch seine offene Porosität gekühlt werden kann. Durch die Porosität weist das filzähnliche Material eine grosse innere Oberfläche auf, die den Abwärmetransport vereinfacht.The porosity of the felt-like material can be influenced by the parameters of the manufacturing process how press pressure and sintering parameters are set. An advantage This porous structure is that the felt-like material is very efficient directly can be cooled by its open porosity. The porosity shows that felt-like material has a large inner surface, which the waste heat transport simplified.
Das filzähnliche Material aus intermetallischen Fasern wird nun auf dem Trägermaterial befestigt. Das Trägermaterial dient als Befestigungs- und Stabilisierungsmittel für das filzähnliche Material. Auf dem filzähnlichen Material wird die Wärmedämmschicht aufgebracht, dies geschieht durch bekannte Verfahren wie zum Beispiel Plasmasprayen. Die Wärmedämmschicht haftet hervorragend auf der rauhen und porösen Oberfläche des filzähnlichen Materials. The felt-like material made of intermetallic fibers is now on the carrier material attached. The carrier material serves as a fastening and stabilizing agent for the felt-like material. On the felt-like material Thermal insulation layer applied, this is done by known methods such as for example plasma sprays. The thermal insulation layer adheres excellently the rough and porous surface of the felt-like material.
Die Wärmedämmschicht reduziert die Temperatur der Oberfläche, das poröse filzähnlichen Material dient der Kühlung. Falls die Wärmedämmschicht ausfällt, das heisst wenn sie nicht mehr zur Verfügung steht, reicht das verbleibende filzähnliche Material aufgrund der hervorragenden Eigenschaften bezüglich Hitzebeständigkeit, Oxidationsbeständigkeit und vorteilhafter Wärmeleiteigenschaften der intermetallischen Phasen immer noch aus. Selbst das filzähnliche Material ohne Wärmedämmschicht kann somit als Hitzeschild verwendet werden, wobei hier jedoch im Vergleich zur zusätzlichen Verwendung einer Wärmedämmschicht der Kühlluftverbrauch etwas höher liegt.The thermal barrier layer reduces the temperature of the surface, the porous felt-like material is used for cooling. If the insulation layer fails, that is, if it is no longer available, the remaining is enough felt-like material due to the excellent properties in terms of heat resistance, Resistance to oxidation and advantageous thermal conductivity the intermetallic phases are still out. Even the felt-like material without a thermal barrier coating can thus be used as a heat shield, whereby here, however, in comparison to the additional use of a thermal barrier coating the cooling air consumption is somewhat higher.
Selbstverständlich ist die Erfindung nicht auf das gezeigte und beschriebene Ausführungsbeispiel beschränkt. Das Trägermaterial kann auch weggelassen werden, wenn das filzähnliche Material durch eine geeignete Wahl des Werkstoffes und der Porosität eine genügende Eigenfestigkeit aufweist.Of course, the invention is not limited to that shown and described Embodiment limited. The carrier material can also be omitted be when the felt-like material by a suitable choice of material and the porosity has sufficient inherent strength.
- 11
- HitzeschildHeat shield
- 22nd
- TrägermaterialBacking material
- 33rd
- filzähnliches Materialfelt-like material
- 44th
- WärmedämmschichtThermal insulation layer
- 55
- KühlkanäleCooling channels
Claims (5)
dadurch gekennzeichnet,
dass der Hitzeschild (1) aus einem filzähnlichen Material (3) aus zusammengepressten und gesinterten intermetallischen Fasern besteht.Heat shield (1), in particular for combustion chamber and for thermal flow machines,
characterized,
that the heat shield (1) consists of a felt-like material (3) made of compressed and sintered intermetallic fibers.
dadurch gekennzeichnet,
dass die intermetallischen Fasern aus einer intermetallischen Phase auf Eisenbasis oder Nickelbasis bestehen.Heat shield according to claim 1,
characterized,
that the intermetallic fibers consist of an iron-based or nickel-based intermetallic phase.
dadurch gekennzeichnet,
dass das filzähnliche Material (3) aus intermetallischen Fasern auf einem Trägermaterial (2) angeordnet ist und / oder dass auf dem filzähnlichen Material aus intermetallischen Fasern eine Wärmedämmschicht (4) angeordnet ist.Heat shield according to claim 1 or 2,
characterized,
that the felt-like material (3) made of intermetallic fibers is arranged on a carrier material (2) and / or that a thermal insulation layer (4) is arranged on the felt-like material made of intermetallic fibers.
dadurch gekennzeichnet,
dass die Wärmedämmschicht (4) aus teil- oder vollstabilisiertem Zirkonoxid besteht. Heat shield according to claim 3,
characterized,
that the thermal barrier coating (4) consists of partially or fully stabilized zirconium oxide.
dadurch gekennzeichnet,
dass der Hitzeschild (1) mittels einer offenen Porosität des filzähnlichen Materials (3) aus intermetallischen Fasern kühlbar istHeat shield according to one of claims 1 to 4,
characterized,
that the heat shield (1) can be cooled by means of an open porosity of the felt-like material (3) made of intermetallic fibers
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19750517A DE19750517A1 (en) | 1997-11-14 | 1997-11-14 | Heat shield |
DE19750517 | 1997-11-14 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0916897A2 true EP0916897A2 (en) | 1999-05-19 |
EP0916897A3 EP0916897A3 (en) | 2000-10-25 |
EP0916897B1 EP0916897B1 (en) | 2003-06-04 |
Family
ID=7848762
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP98811060A Expired - Lifetime EP0916897B1 (en) | 1997-11-14 | 1998-10-22 | Heat shield |
Country Status (4)
Country | Link |
---|---|
US (1) | US6492034B1 (en) |
EP (1) | EP0916897B1 (en) |
JP (1) | JPH11236995A (en) |
DE (2) | DE19750517A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1126221A1 (en) * | 2000-02-17 | 2001-08-22 | Siemens Aktiengesellschaft | Padded refactory tile as liner for a gas turbine combustor |
US7141128B2 (en) | 2002-08-16 | 2006-11-28 | Alstom Technology Ltd | Intermetallic material and use of this material |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005001502A1 (en) * | 2005-01-10 | 2006-07-20 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Radiation shield |
US20100272953A1 (en) * | 2009-04-28 | 2010-10-28 | Honeywell International Inc. | Cooled hybrid structure for gas turbine engine and method for the fabrication thereof |
DE102015215144B4 (en) * | 2015-08-07 | 2017-11-09 | MTU Aero Engines AG | Device and method for influencing the temperatures in inner ring segments of a gas turbine |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3327216A1 (en) | 1983-07-28 | 1985-02-07 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | METHOD FOR ARRANGING A HEAT INSULATION LAYER ON A METAL SUBSTRATE |
Family Cites Families (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3127668A (en) * | 1955-03-03 | 1964-04-07 | Iit Res Inst | High strength-variable porosity sintered metal fiber articles and method of making the same |
US3505038A (en) * | 1964-08-24 | 1970-04-07 | Brunswick Corp | Metal fibril compacts |
US3469297A (en) * | 1966-04-20 | 1969-09-30 | Brunswick Corp | Porous metal structure |
US3910039A (en) * | 1972-09-14 | 1975-10-07 | Nasa | Rocket chamber and method of making |
US4038815A (en) * | 1973-03-30 | 1977-08-02 | Northern Research And Engineering Corporation | Gas turbine |
GB1545584A (en) * | 1975-03-07 | 1979-05-10 | Onera (Off Nat Aerospatiale) | Processes and systems for the formation of surface diffusion alloys on perforate metal workpieces |
US4338380A (en) * | 1976-04-05 | 1982-07-06 | Brunswick Corporation | Method of attaching ceramics to metals for high temperature operation and laminated composite |
US4075364A (en) * | 1976-04-15 | 1978-02-21 | Brunswick Corporation | Porous ceramic seals and method of making same |
US4209334A (en) * | 1976-04-15 | 1980-06-24 | Brunswick Corporation | Porous ceramic seals and method of making same |
GB1545783A (en) * | 1976-05-03 | 1979-05-16 | Rolls Royce | Laminated metal material |
US4069171A (en) * | 1976-11-12 | 1978-01-17 | United Technologies Corporation | Metallic fibrous skeletal catalysts and process for producing them |
US4245469A (en) * | 1979-04-23 | 1981-01-20 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Heat exchanger and method of making |
US4273824A (en) * | 1979-05-11 | 1981-06-16 | United Technologies Corporation | Ceramic faced structures and methods for manufacture thereof |
US4615864A (en) * | 1980-05-01 | 1986-10-07 | Howmet Turbine Components Corporation | Superalloy coating composition with oxidation and/or sulfidation resistance |
DE3234376C1 (en) * | 1982-09-16 | 1984-03-01 | Goetze Ag, 5093 Burscheid | Sealing ring |
DE3247414C2 (en) * | 1982-12-22 | 1986-10-23 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Process for the production of an ablation layer interspersed with a mat |
DE3248661A1 (en) * | 1982-12-30 | 1984-07-05 | Grünzweig + Hartmann und Glasfaser AG, 6700 Ludwigshafen | Component provided with heat-resistant coating |
DE3321149A1 (en) * | 1983-06-11 | 1984-12-13 | Azo-Maschinenfabrik Adolf Zimmermann Gmbh, 6960 Osterburken | Combustion chamber, especially for nozzle burner |
DE3327218A1 (en) * | 1983-07-28 | 1985-02-07 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | THERMALLY HIGH-QUALITY, COOLED COMPONENT, IN PARTICULAR TURBINE BLADE |
DE3411924C2 (en) * | 1984-03-30 | 1994-01-13 | Gruenzweig & Hartmann Montage | Tile element for vibration-resistant thermal insulation of walls, and use for the formation of a vibration-resistant thermal insulation lining of walls |
DE3446649A1 (en) * | 1984-12-20 | 1986-06-26 | G + H Montage Gmbh, 6700 Ludwigshafen | Lining for high-temperature gas turbines |
US4729871A (en) * | 1985-06-21 | 1988-03-08 | Hiroshi Kawaguchi | Process for preparing porous metal plate |
US4956137A (en) * | 1986-09-16 | 1990-09-11 | Lanxide Technology Company, Lp | Porous ceramic composite with dense surface |
DE3638658C1 (en) * | 1986-11-12 | 1988-04-21 | Daimler Benz Ag | Heat-insulating lining for a gas turbine |
DE3718677A1 (en) * | 1987-06-04 | 1988-12-22 | Mtu Muenchen Gmbh | MOLDED BODY FROM A COMPOSITE OF METALS AND NON-METALS |
US4838031A (en) * | 1987-08-06 | 1989-06-13 | Avco Corporation | Internally cooled combustion chamber liner |
US4904546A (en) * | 1989-04-03 | 1990-02-27 | General Electric Company | Material system for high temperature jet engine operation |
JP2522604B2 (en) * | 1990-04-26 | 1996-08-07 | 株式会社ユニックス | Sound absorbing material and method for manufacturing the same |
EP0539011B1 (en) * | 1991-10-23 | 1997-05-07 | Inco Limited | Nickel coated carbon preforms |
DE4303135C2 (en) * | 1993-02-04 | 1997-06-05 | Mtu Muenchen Gmbh | Thermal insulation layer made of ceramic on metal components and process for their production |
DE4322431C2 (en) * | 1993-07-06 | 1997-04-10 | Mtu Muenchen Gmbh | Cooling structure and process for its manufacture |
BE1009485A3 (en) * | 1995-07-14 | 1997-04-01 | Bekaert Sa Nv | TEXTILE FABRIC INCLUDING MULTIPLE SCRAPED METAL filaments. |
US5665479A (en) * | 1995-12-12 | 1997-09-09 | N.V. Bekaert S.A. | Sintered multilayer metal fiber web |
DE19623300A1 (en) * | 1996-06-11 | 1997-12-18 | Siemens Ag | Heat shield arrangement, in particular for structural parts of gas turbine plants, with a layered structure |
US6210488B1 (en) * | 1998-12-30 | 2001-04-03 | General Electric Company | Method of removing a thermal barrier coating |
-
1997
- 1997-11-14 DE DE19750517A patent/DE19750517A1/en not_active Withdrawn
-
1998
- 1998-10-22 DE DE59808608T patent/DE59808608D1/en not_active Expired - Lifetime
- 1998-10-22 EP EP98811060A patent/EP0916897B1/en not_active Expired - Lifetime
- 1998-11-11 JP JP10320701A patent/JPH11236995A/en active Pending
- 1998-11-12 US US09/190,364 patent/US6492034B1/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3327216A1 (en) | 1983-07-28 | 1985-02-07 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | METHOD FOR ARRANGING A HEAT INSULATION LAYER ON A METAL SUBSTRATE |
Non-Patent Citations (1)
Title |
---|
STEPHANI ET AL: "METALLISCHE HOCHTEMPERATURFASERN DURCH SCHMELZEXTRAKTION- HERSTELLUNG, EIGENSCHAFTEN UND ANWENDUNGEN", VDI BERICHT 1151, 1 January 1995 (1995-01-01), pages 175FF |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1126221A1 (en) * | 2000-02-17 | 2001-08-22 | Siemens Aktiengesellschaft | Padded refactory tile as liner for a gas turbine combustor |
WO2001061250A1 (en) * | 2000-02-17 | 2001-08-23 | Siemens Aktiengesellschaft | Thermal shield stone and device for lining a combustion chamber, and gas turbine |
US7141128B2 (en) | 2002-08-16 | 2006-11-28 | Alstom Technology Ltd | Intermetallic material and use of this material |
Also Published As
Publication number | Publication date |
---|---|
EP0916897B1 (en) | 2003-06-04 |
JPH11236995A (en) | 1999-08-31 |
DE19750517A1 (en) | 1999-05-20 |
US6492034B1 (en) | 2002-12-10 |
DE59808608D1 (en) | 2003-07-10 |
EP0916897A3 (en) | 2000-10-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE602005003538T2 (en) | FURNACE AND METHOD FOR PRODUCING CERAMIC PARTS WITH THIS FUEL | |
DE19736560C2 (en) | Process for producing a porous body, body made of SiC, and use of the porous body | |
DE102005021006B4 (en) | Process for making a part of dense thermostructural composite | |
DE3843691C2 (en) | Mechanical seal with porous material and method of making the same | |
EP0887572B1 (en) | Friction element consisting of brake disc and lining | |
DE60127107T2 (en) | METHOD FOR PRODUCING AN ABRASION AND HIGH TEMPERATURE RESISTANT COATING AND MATERIAL CONTAINING COMPRESSED GEOMETRIC HOLLOW BODIES | |
DE102004009262B4 (en) | Method for producing a multiply perforated part made of a composite material with ceramic matrix | |
DE2108176A1 (en) | Fastening of ceramic turbine blades | |
DE19710105A1 (en) | Silicon carbide body reinforced with short graphite fibers | |
EP0995880A2 (en) | Turbine blade | |
DE2853397A1 (en) | MULTI-LAYER THERMAL INSULATION MATERIAL AND METHOD FOR MANUFACTURING IT | |
DE1558662A1 (en) | Ceramic composite material | |
DE2353551A1 (en) | CERAMIC TURBINE IMPELLER | |
DE1567489B2 (en) | DEVICE FOR SEPARATING HYDROGEN FROM GAS MIXTURES | |
DE10014418C5 (en) | Process for the production of a fiber-reinforced structural component and brake disk manufactured therefrom | |
EP0651698B1 (en) | Composites with at least two inorganic ceramic layers, and method of producing them | |
DE3307115C2 (en) | Cylinder head of a piston engine | |
EP0916897B1 (en) | Heat shield | |
DE3329250A1 (en) | FIREPROOF SILICON NITRIDE COMPOSITE | |
DE2631092C2 (en) | Ceramic alternating layer heat exchanger in modular design | |
DE3602132A1 (en) | Slide or friction element with functional part of ceramic material with incorporated stabiliser and process for its production | |
DE3028441A1 (en) | TURBOCHARGER ROTOR WITH CURVED SHOVEL BLADES | |
DE2845755C2 (en) | ||
DE3326728A1 (en) | LOAD-BEARING HEAT ISOLATOR | |
DE4405331C2 (en) | Method of manufacturing a ceramic component |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): DE GB |
|
AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
17P | Request for examination filed |
Effective date: 20010404 |
|
AKX | Designation fees paid |
Free format text: DE GB |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: ALSTOM |
|
17Q | First examination report despatched |
Effective date: 20020719 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: ALSTOM (SWITZERLAND) LTD |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Designated state(s): DE GB |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REF | Corresponds to: |
Ref document number: 59808608 Country of ref document: DE Date of ref document: 20030710 Kind code of ref document: P |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) | ||
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 |
|
26N | No opposition filed |
Effective date: 20040305 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59808608 Country of ref document: DE Representative=s name: UWE ROESLER, DE |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: 732E Free format text: REGISTERED BETWEEN 20120802 AND 20120808 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59808608 Country of ref document: DE Representative=s name: ROESLER, UWE, DIPL.-PHYS.UNIV., DE Effective date: 20120713 Ref country code: DE Ref legal event code: R081 Ref document number: 59808608 Country of ref document: DE Owner name: ANSALDO ENERGIA SWITZERLAND AG, CH Free format text: FORMER OWNER: ALSTOM (SWITZERLAND) LTD., BADEN, CH Effective date: 20120713 Ref country code: DE Ref legal event code: R081 Ref document number: 59808608 Country of ref document: DE Owner name: GENERAL ELECTRIC TECHNOLOGY GMBH, CH Free format text: FORMER OWNER: ALSTOM (SWITZERLAND) LTD., BADEN, CH Effective date: 20120713 Ref country code: DE Ref legal event code: R081 Ref document number: 59808608 Country of ref document: DE Owner name: ALSTOM TECHNOLOGY LTD., CH Free format text: FORMER OWNER: ALSTOM (SWITZERLAND) LTD., BADEN, CH Effective date: 20120713 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59808608 Country of ref document: DE Representative=s name: ROESLER, UWE, DIPL.-PHYS.UNIV., DE Ref country code: DE Ref legal event code: R081 Ref document number: 59808608 Country of ref document: DE Owner name: ANSALDO ENERGIA SWITZERLAND AG, CH Free format text: FORMER OWNER: ALSTOM TECHNOLOGY LTD., BADEN, CH Ref country code: DE Ref legal event code: R081 Ref document number: 59808608 Country of ref document: DE Owner name: GENERAL ELECTRIC TECHNOLOGY GMBH, CH Free format text: FORMER OWNER: ALSTOM TECHNOLOGY LTD., BADEN, CH |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20161020 Year of fee payment: 19 Ref country code: DE Payment date: 20161020 Year of fee payment: 19 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: 732E Free format text: REGISTERED BETWEEN 20170824 AND 20170830 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59808608 Country of ref document: DE Representative=s name: ROESLER, UWE, DIPL.-PHYS.UNIV., DE Ref country code: DE Ref legal event code: R081 Ref document number: 59808608 Country of ref document: DE Owner name: ANSALDO ENERGIA SWITZERLAND AG, CH Free format text: FORMER OWNER: GENERAL ELECTRIC TECHNOLOGY GMBH, BADEN, CH |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 59808608 Country of ref document: DE |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20171022 |
|
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: 20180501 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171022 |