DE102019207621A1 - PROCESS FOR PRODUCING A COMPONENT FROM A CERAMIC FIBER COMPOSITE MATERIAL WITH A MODIFIED SLIDING OR FRICTION SURFACE - Google Patents
PROCESS FOR PRODUCING A COMPONENT FROM A CERAMIC FIBER COMPOSITE MATERIAL WITH A MODIFIED SLIDING OR FRICTION SURFACE Download PDFInfo
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Abstract
Die vorliegende Erfindung betrifft ein Bauteil aus einem Faserverbundwerkstoff sowie ein Verfahren zur Herstellung desselben, wobei bei dem Faserverbundwerkstoff Fasern (8) aus Keramik und / oder Kohlenstoff in einer Matrix (9) aus Keramik und / oder Kohlenstoff und / oder einem Polymer eingebettet sind und wobei das Bauteil eine Oberfläche aufweist, von der zumindest ein Teil als Kontaktfläche zum mechanischen Kontakt mit einem Kontaktpartner ausgebildet ist, und wobei Festschmierstoffpartikel (10) in mindestens einem Oberflächenrandbereich des Bauteils angrenzend an die Kontaktfläche in die Matrix (9) eingelagert sind, wobei die Festschmierstoffpartikel (10) im Gefüge mit der Matrix und / oder den Fasern verzahnt oder dispergiert sind. The present invention relates to a component made of a fiber composite material and a method for producing the same, wherein in the fiber composite material fibers (8) made of ceramic and / or carbon are embedded in a matrix (9) made of ceramic and / or carbon and / or a polymer and wherein the component has a surface, of which at least a part is designed as a contact surface for mechanical contact with a contact partner, and wherein solid lubricant particles (10) are embedded in at least one surface edge region of the component adjacent to the contact surface in the matrix (9), the Solid lubricant particles (10) are interlocked or dispersed in the structure with the matrix and / or the fibers.
Description
HINTERGRUND DER ERFINDUNGBACKGROUND OF THE INVENTION
GEBIET DER ERFINDUNGFIELD OF THE INVENTION
Die vorliegende Erfindung betrifft ein Bauteil aus einem keramischen Faserverbundwerkstoff sowie ein Verfahren zur Herstellung desselben, wobei bei dem Faserverbundwerkstoff Fasern aus Keramik und / oder Kohlenstoff in einer Matrix aus Keramik und / oder Kohlenstoff eingebettet sind.The present invention relates to a component made of a ceramic fiber composite material and a method for producing the same, wherein in the fiber composite material fibers made of ceramic and / or carbon are embedded in a matrix made of ceramic and / or carbon.
STAND DER TECHNIKSTATE OF THE ART
Faserverbundwerkstoffe, wie kohlenstofffaserverstärkter Kunststoff (CFK) und keramische Faserverbundwerkstoff, die im englischen auch als Ceramic Matrix Composites CMC bezeichnet werden, werden aufgrund ihrer hervorragenden mechanischen Eigenschaften in vielen Bereichen der Technik eingesetzt.Fiber composite materials such as carbon fiber reinforced plastic (CFRP) and ceramic fiber composite materials, which are also referred to as Ceramic Matrix Composites CMC, are used in many areas of technology due to their excellent mechanical properties.
Keramische Faserverbundwerkstoffe, die neben keramischen Stoffen zur Bildung der Matrix und / oder der Fasern auch solche aus Kohlenstoff mit einschließen sollen, werden aufgrund ihrer guten Hochtemperatur - sowie Korrosionsbeständigkeit unter anderem bei Hochtemperaturanwendungen im Flugzeug - bzw. Flugtriebwerksbau verwendet. Verfahren zur effizienten Herstellung von möglichst dichten keramischen Faserverbundwerkstoffen, die in Gasturbinen oder Flugtriebwerken eingesetzt werden können, sind beispielsweise in dem europäischen Patent
Darüber hinaus gelangen auch kohlenstofffaserverstärkte Kunststoffe zum Einsatz, bei denen Kohlenstofffasern in einer Matrix aus einem Polymer bzw. Kunstharz eingebettet sind. In addition, carbon fiber-reinforced plastics are also used, in which carbon fibers are embedded in a matrix made of a polymer or synthetic resin.
Allerdings müssen Bauteile aus Faserverbundwerkstoffen häufig mit Schutzschichten versehen werden, wenn die Faserverbundwerkstoffe bei mechanischem Kontakt mit anderen Bauteilen einem hohen Verschleiß unterliegen oder diesen bei benachbarten Bauteilen verursachen würden. Beispielsweise können bei Strömungsmaschinen, wie Gasturbinen oder Flugtriebwerken, hochbelastete Kontaktflächen vorliegen, wie z.B. an Laufschaufel, insbesondere an Laufschaufeldeckbändern oder Laufschaufel - Scheibe - Kontaktflächen, oder an dem den Strömungskanal umgebenden Gehäuse oder anderen Bauteilen, die gegeneinander anliegen.However, components made of fiber composite materials often have to be provided with protective layers if the fiber composite materials are subject to high wear in the event of mechanical contact with other components or if they would cause this in adjacent components. For example, in fluid flow machines, such as gas turbines or aircraft engines, highly stressed contact surfaces can exist, such as on moving blade, in particular on moving blade shrouds or moving blade - disk - contact surfaces, or on the housing surrounding the flow channel or other components that rest against one another.
Schutzschichten können jedoch bei zyklischer thermischer Beanspruchung oder Thermoschockbeanspruchung abplatzen, sodass die Schutzwirkung verloren geht und zudem die abgeplatzten Partikel Schädigungen in entsprechenden Maschinen bzw. Triebwerken verursachen können. Für einen dauerhaften und zuverlässigen Einsatz von Faserverbundwerkstoffen muss somit die Funktionalität der daraus hergestellten Bauteile über einen breiten Temperaturbereich sichergestellt werden. Darüber hinaus ist ein übermäßiger Verschleiß zu vermeiden, der die Lebensdauer der entsprechenden Bauteile stark beschränken würde.Protective layers can, however, flake off in the event of cyclical thermal stress or thermal shock stress, so that the protective effect is lost and the flaked particles can also cause damage to the corresponding machines or engines. For permanent and reliable use of fiber composite materials, the functionality of the components made from them must be ensured over a wide temperature range. In addition, excessive wear must be avoided, which would severely limit the service life of the relevant components.
Entsprechend ist es beispielsweise aus dem US - Patent
In der europäischen Patentanmeldung
OFFENBARUNG DER ERFINDUNGDISCLOSURE OF THE INVENTION
AUFGABE DER ERFINDUNGOBJECT OF THE INVENTION
Es ist deshalb Aufgabe der vorliegenden Erfindung einen Faserverbundwerkstoff, insbesondere einen keramischen Faserverbundwerkstoff, dessen Matrix aus Keramik und / oder Kohlenstoff und dessen Fasern ebenfalls aus Keramik und / oder Kohlenstoff gebildet sind, oder einen kohlenstofffaserverstärkten Kunststoff bereitzustellen, der in seinen tribologischen Eigenschaften gegenüber dem Stand der Technik verbessert ist, wobei insbesondere Reibung und Verschleiß an entsprechenden Oberflächen dauerhaft verringert sind. Darüber hinaus soll ein derartiger Faserverbundwerkstoff effizient herstellbar sein und eine hohe Lebensdauer aufweisen.It is therefore the object of the present invention to provide a fiber composite material, in particular a ceramic fiber composite material, the matrix of which is made of ceramic and / or carbon and the fibers of which are also made of ceramic and / or carbon, or a carbon fiber-reinforced plastic that has tribological properties compared to the prior art the technology is improved, in particular friction and wear on corresponding surfaces are permanently reduced. In addition, such a fiber composite material should be able to be produced efficiently and have a long service life.
TECHNISCHE LÖSUNGTECHNICAL SOLUTION
Diese Aufgabe wird gelöst durch ein Verfahren zur Herstellung eines Bauteils aus einem Faserverbundwerkstoff, welches die Merkmale des Anspruchs 1 umfasst, sowie durch ein Bauteil mit den Merkmalen des Anspruchs 4. Vorteilhafte Ausgestaltungen sind Gegenstand der abhängigen Ansprüche.This object is achieved by a method for producing a component from a fiber composite material, which comprises the features of claim 1, and by a component having the features of
Die Erfindung schlägt zur Verbesserung der tribologischen Eigenschaften eines Faserverbundwerkstoffs vor, direkt bei der Herstellung des Faserverbundwerkstoffs in der Matrix aus Keramik und / oder Kohlenstoff und / oder einem Polymer, in die die Fasern des Faserverbundwerkstoffs eingebettet werden, zusätzlich zumindest in entsprechenden Oberflächenrandbereichen des herzustellenden Bauteils, die in mechanischen Kontakt, z.B. Reib - oder Gleitkontakt, mit Kontaktpartnern, wie Reib - bzw. Gleitpartnern, gelangen können, Festschmierstoffpartikel einzulagern, sodass der Festschmierstoff an den entsprechenden Kontaktflächen eines aus dem modifizierten Faserverbundwerkstoff gebildeten Bauteils vorliegt und eine Schmierung bereitstellen kann. Durch die direkte Einlagerung der Festschmierstoffpartikel in das Gefüge mit der Matrix und den Fasern wird eine sichere und feste Anordnung der Festschmierstoffpartikel und somit eine zuverlässige und dauerhafte Bereitstellung des Festschmierstoffs an Kontaktflächen des entsprechend hergestellten Bauteils gewährleistet. Außerdem ist die Herstellung gegenüber dem Stand der Technik vereinfacht, da keine zusätzlichen Herstellschritte zur Aufbringung einer zusätzlichen Schutzschicht oder zur Vorbereitung eines Randbereichs des Bauteils zur Einbringung der Festschmierstoffpartikel vorgenommen werden müssen. Ferner besteht durch den Verzicht auf eine Beschichtung keine Gefahr von entsprechenden Abplatzungen der Schicht.In order to improve the tribological properties of a fiber composite material, the invention proposes, directly during the production of the fiber composite material in the matrix of ceramic and / or carbon and / or a polymer, in which the fibers of the fiber composite material are embedded, additionally at least in corresponding surface edge areas of the material to be produced Components that can come into mechanical contact, e.g. friction or sliding contact, with contact partners, such as friction or sliding partners, store solid lubricant particles so that the solid lubricant is present on the corresponding contact surfaces of a component formed from the modified fiber composite material and can provide lubrication. The direct embedding of the solid lubricant particles in the structure with the matrix and the fibers ensures a secure and solid arrangement of the solid lubricant particles and thus a reliable and permanent supply of the solid lubricant to the contact surfaces of the correspondingly manufactured component. In addition, the production is simplified compared to the prior art, since no additional production steps have to be carried out to apply an additional protective layer or to prepare an edge region of the component for the introduction of the solid lubricant particles. Furthermore, dispensing with a coating means that there is no risk of the layer flaking off.
Die Einbringung der Festschmierstoffpartikel erfolgt vor und / oder gleichzeitig mit der Anordnung des Matrixmaterials in einem Fasergebilde, z.B. durch Infiltration, wobei mit dem Fasergebilde die zur Verstärkung des Faserverbundwerkstoffs vorgesehenen Fasern bereitgestellt werden. Ein entsprechendes Fasergebilde kann beispielsweise als Fasergewebe, Fasergeflecht, Fasergewirk oder ähnliches bereitgestellt werden.The solid lubricant particles are introduced before and / or simultaneously with the arrangement of the matrix material in a fiber structure, e.g. by infiltration, the fibers provided for reinforcing the fiber composite material with the fiber structure. A corresponding fiber structure can be provided, for example, as a fiber fabric, fiber braid, fiber knitted fabric or the like.
Die Festschmierstoffpartikel können in dem Fasergebilde beschränkt auf die Oberflächenrandbereiche eingebracht werden, in denen ein mechanischer Kontakt, z.B. in Form eines Reib - oder Gleitkontakts, zu erwarten ist. Entsprechend kann eine lokal begrenzte Ausbildung von Oberflächenrandbereichen mit den Festschmierstoffpartikel verwirklicht werden.The solid lubricant particles can be incorporated in the fiber structure limited to the surface edge areas in which mechanical contact, e.g. in the form of frictional or sliding contact is to be expected. Correspondingly, a locally limited formation of surface edge regions with the solid lubricant particles can be realized.
Die Festschmierstoffpartikel können in den entsprechenden Oberflächenrandbereichen in unterschiedlicher Konzentration vorgesehen werden, also mit unterschiedlichem Volumenanteil, sodass Konzentrationsgradienten entlang der Oberfläche des Bauteils und / oder vertikal zur Oberfläche des Bauteils ausgebildet werden können. Beispielsweise kann der Volumenanteil der Festschmierstoffpartikel in dem Gefüge in den Oberflächenrandbereichen von einem inneren Bereich zur Oberfläche hin ansteigen.The solid lubricant particles can be provided in the corresponding surface edge areas in different concentrations, that is to say with different volume proportions, so that concentration gradients can be formed along the surface of the component and / or vertical to the surface of the component. For example, the volume fraction of the solid lubricant particles in the structure in the surface edge areas can increase from an inner area to the surface.
Die Ausbildung der Matrix kann durch unterschiedliche Verfahren verwirklicht werden. Angepasst an das gewählte Verfahren zur Ausbildung der Matrix um die Fasern bzw. in den Hohlräumen und Öffnungen des Fasergebildes kann die Einbringung der Festschmierstoffpartikel in die entsprechenden Oberflächenrandbereiche angepasst werden.The formation of the matrix can be realized by different methods. The introduction of the solid lubricant particles into the corresponding surface edge areas can be adapted to the selected method for forming the matrix around the fibers or in the cavities and openings of the fiber structure.
Beispielsweise ist es möglich die Abscheidung der Matrix aus der Gasphase vorzunehmen, z.B. durch chemische Dampfphasenabscheidung oder chemische Gasphaseninfiltration, wobei in diesem Fall die Festschmierstoffpartikel bereits im Fasergebilde, beispielsweise aus einem mit Harz verklebten Fasern ausgebildeten Fasergebilde, angeordnet sein können.For example it is possible to carry out the deposition of the matrix from the gas phase, e.g. by chemical vapor phase deposition or chemical gas phase infiltration, in which case the solid lubricant particles can already be arranged in the fiber structure, for example from a fiber structure made of fibers bonded with resin.
In dem Fasergebilde können auch Polymere zur anschließenden Pyrolyse, beispielsweise siliciumhaltige Polymere vorgesehen sein, wobei in den Oberflächenrandbereichen, in denen der Werkstoff entsprechend der Erfindung modifiziert werden soll, zusätzlich die Feststoffschmierpartikel angeordnet sind.Polymers for subsequent pyrolysis, for example silicon-containing polymers, can also be provided in the fiber structure, with the solid lubricant particles additionally being arranged in the surface edge areas in which the material is to be modified according to the invention.
Auch bei weiteren Infiltrationsverfahren, wie der Flüssiginfiltration, z.B. der Flüssigpolymerinfiltration oder der Infiltration über Schlicker oder Schmelzinfiltrationsverfahren, wie der Flüssigsiliciuminfiltration oder dergleichen, können die Festschmierstoffpartikel bereits im Fasergebilde vorgesehen sein, wobei zusätzlich weitere Bestandteile zur chemischen Reaktion mit dem infiltrierten Stoff zur Ausbildung der Matrix angeordnet sein können.Also in other infiltration processes, such as liquid infiltration, e.g. liquid polymer infiltration or infiltration via slurry or melt infiltration processes, such as liquid silicon infiltration or the like, the solid lubricant particles can already be provided in the fiber structure, with additional components for chemical reaction with the infiltrated substance to form the matrix.
Weitere Verfahren zur Ausbildung der Matrix, insbesondere einer Keramikmatrix sind die Elektrophorese oder Sinterverfahren, bei denen ebenfalls die Festschmierstoffpartikel bereits im Fasergebilde vorgesehen sein können, um in der sich ausbildenden Matrix eingelagert zu werden.Further methods for forming the matrix, in particular a ceramic matrix, are electrophoresis or sintering processes, in which the solid lubricant particles can also already be provided in the fiber structure in order to be embedded in the forming matrix.
Durch die Einlagerung der Festschmierstoffpartikel in das Gefüge aus einer Matrix aus Keramik und / oder Kohlenstoff und / oder einer organischen Matrix, insbesondere einem Polymer, und Fasern aus Keramik und / oder Kohlenstoff wird eine feste Einbindung der Festschmierstoffpartikel in die Oberfläche des Bauteils bewirkt, wobei z.B. durch ungleichmäßige, dreidimensionale Grenzflächen zwischen den Festschmierstoffpartikeln und den Körnern der Matrix und / oder den Fasern insbesondere mit Vorsprüngen und Vertiefungen oder Hinterschneidungen sowie durch die Dispersion in der Matrix eine feste Einbindung der Festschmierstoffpartikel im Gefüge bewirkt wird.By embedding the solid lubricant particles in the structure of a matrix made of ceramic and / or carbon and / or an organic matrix, in particular a polymer, and fibers made of ceramic and / or carbon, the solid lubricant particles are firmly embedded in the surface of the component, whereby e.g. uneven, three-dimensional interfaces between the solid lubricant particles and the grains of the matrix and / or the fibers, in particular with protrusions and depressions or undercuts, and the dispersion in the matrix cause the solid lubricant particles to be firmly integrated in the structure.
Die eingebrachten Festschmierstoffpartikel können unterschiedlicher Art sein und sollen lediglich den für die beabsichtigten tribologischen Eigenschaften entsprechenden Schmierstoff bereitstellen. Beispielsweise können Bornitrid, insbesondere amorphes Bornitrid oder hexagonales Bornitrid, Metalloxide, wie Molybdänoxid oder Wolframoxid, sowie Chalkogene oder Graphit hierfür eingesetzt werden.The solid lubricant particles introduced can be of different types and are only intended to provide the lubricant appropriate for the intended tribological properties. For example, boron nitride, in particular amorphous boron nitride or hexagonal boron nitride, metal oxides such as molybdenum oxide or tungsten oxide, and chalcogens or graphite can be used for this purpose.
FigurenlisteFigure list
Die beigefügten Zeichnungen zeigen in rein schematischer Weise in
-
1 eine Darstellung eines erfindungsgemäßen Bauteils, welches mit zwei anderen Bauteilen in mechanischem Kontakt ist, -
2 einen Schnitt durch einen erfindungsgemäß modifizierten Oberflächenrandbereich eines erfindungsgemäßen Bauteils, wie es in1 dargestellt ist, -
3 eine Darstellung eines Fasergebildes als Ausgangsmaterial für die Herstellung eines erfindungsgemäßen Bauteils, -
4 eine Darstellung des Fasergebildes aus3 nach Befüllen von Oberflächenrandbereichen mit Festschmierstoffpartikeln zur Ausbildung eines erfindungsgemäßen Bauteils und in -
5 eine Darstellung des fertig gestellten Bauteils aus einem Faserverbundwerkstoff, das modifizierte Oberflächenrandbereiche aufweist.
-
1 a representation of a component according to the invention which is in mechanical contact with two other components, -
2 a section through an inventive modified surface edge region of a component according to the invention, as shown in FIG1 is shown -
3 a representation of a fiber structure as a starting material for the production of a component according to the invention, -
4th a representation of thefiber structure 3 after filling surface edge areas with solid lubricant particles to form a component according to the invention and in -
5 a representation of the finished component made of a fiber composite material that has modified surface edge areas.
AUSFÜHRUNGSBEISPIELEEXAMPLES
Weitere Vorteile, Kennzeichen und Merkmale der vorliegenden Erfindung werden bei der nachfolgenden detaillierten Beschreibung der Ausführungsbeispiele ersichtlich. Allerdings ist die Erfindung nicht auf diese Ausführungsbeispiele beschränkt.Further advantages, characteristics and features of the present invention will become apparent in the following detailed description of the exemplary embodiments. However, the invention is not restricted to these exemplary embodiments.
Die
In den Oberflächenrandbereichen
Die
Die
Zunächst wird ein Fasergebilde
Gemäß der Darstellung in
Neben den Festschmierstoffpartikeln, die nur in den Oberflächenrandbereichen
Alternativ ist es auch möglich, Ausgangsstoffe für die anschließende Bildung der Matrix in dem Fasergebilde
Gleiches gilt für eine mögliche Abscheidung des Keramikmaterials über die Dampfphase, bei der mittels chemischer Dampfphasenabscheidung oder chemischer Dampfphaseninfiltration das Keramikmaterial in den Freiräumen des Fasergebildes
Die
Obwohl die vorliegende Erfindung anhand der Ausführungsbeispiele detailliert beschrieben worden ist, ist für den Fachmann selbstverständlich, dass die Erfindung nicht auf diese Ausführungsbeispiele beschränkt ist, sondern dass vielmehr Abwandlungen in der Weise möglich sind, dass einzelne Merkmale weggelassen oder andersartige Kombinationen von Merkmalen verwirklicht werden können, ohne dass der Schutzbereich der beigefügten Ansprüche verlassen wird. Insbesondere schließt die vorliegende Offenbarung sämtliche Kombinationen der in den verschiedenen Ausführungsbeispielen gezeigten Einzelmerkmale mit ein, sodass einzelne Merkmale, die nur in Zusammenhang mit einem Ausführungsbeispiel beschrieben sind, auch bei anderen Ausführungsbeispielen oder nicht explizit dargestellten Kombinationen von Einzelmerkmalen eingesetzt werden können.Although the present invention has been described in detail on the basis of the exemplary embodiments, it is obvious to the person skilled in the art that the invention is not limited to these exemplary embodiments, but rather that modifications are possible in such a way that individual features can be omitted or other types of combinations of features can be implemented without departing from the scope of protection of the appended claims. In particular, the present disclosure includes all combinations of the individual features shown in the various exemplary embodiments, so that individual features that are only described in connection with one exemplary embodiment can also be used in other exemplary embodiments or combinations of individual features that are not explicitly shown.
BezugszeichenlisteList of reference symbols
- 11
- BauteilComponent
- 22
- Reib - bzw. GleitpartnerFriction or sliding partner
- 33
- Reib - bzw. GleitpartnerFriction or sliding partner
- 44th
- KontaktflächeContact area
- 55
- KontaktflächeContact area
- 66
- OberflächenrandbereichSurface edge area
- 77th
- OberflächenrandbereichSurface edge area
- 88th
- FasernFibers
- 99
- Keramikkörner bzw. KeramikmatrixCeramic grains or ceramic matrix
- 1010
- FestschmierstoffpartikelSolid lubricant particles
- 1111
- FasergebildeFiber structures
- 1212
- OberflächenrandbereichSurface edge area
- 1313
- OberflächenrandbereichSurface edge area
- 1414th
- KontaktflächeContact area
- 1515th
- KontaktflächeContact area
- 1616
- OberflächenrandbereichSurface edge area
- 1717th
- OberflächenrandbereichSurface edge area
- 1818th
- keramischer Faserverbundwerkstoffceramic fiber composite
ZITATE ENTHALTEN IN DER BESCHREIBUNGQUOTES INCLUDED IN THE DESCRIPTION
Diese Liste der vom Anmelder aufgeführten Dokumente wurde automatisiert erzeugt und ist ausschließlich zur besseren Information des Lesers aufgenommen. Die Liste ist nicht Bestandteil der deutschen Patent- bzw. Gebrauchsmusteranmeldung. Das DPMA übernimmt keinerlei Haftung für etwaige Fehler oder Auslassungen.This list of the documents listed by the applicant was generated automatically and is included solely for the better information of the reader. The list is not part of the German patent or utility model application. The DPMA assumes no liability for any errors or omissions.
Zitierte PatentliteraturPatent literature cited
- EP 1999288 B1 [0003]EP 1999288 B1 [0003]
- US 2018/0187560 A1 [0003]US 2018/0187560 A1 [0003]
- US 9238595 B2 [0007]US 9238595 B2 [0007]
- EP 2535182 A1 [0008]EP 2535182 A1 [0008]
Claims (8)
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DE102019207621.1A DE102019207621A1 (en) | 2019-05-24 | 2019-05-24 | PROCESS FOR PRODUCING A COMPONENT FROM A CERAMIC FIBER COMPOSITE MATERIAL WITH A MODIFIED SLIDING OR FRICTION SURFACE |
PCT/DE2020/000095 WO2020239149A1 (en) | 2019-05-24 | 2020-05-18 | Method for producing a component from a ceramic fibre-reinforced composite material with a modified sliding or frictional surface |
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Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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DE3601569A1 (en) * | 1986-01-21 | 1987-07-23 | Kolbenschmidt Ag | COMPOSITE SLIDING BEARING MATERIAL |
DE102009032961A1 (en) * | 2009-07-14 | 2011-01-20 | Schaeffler Technologies Gmbh & Co. Kg | Rolling bearing cage |
DE102012205606A1 (en) * | 2011-04-04 | 2012-10-25 | Gwo S. Swei | Self-lubricating structure and method of making the same |
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JP2000081062A (en) * | 1998-09-08 | 2000-03-21 | Ngk Insulators Ltd | Brake member |
US6210786B1 (en) * | 1998-10-14 | 2001-04-03 | Northrop Grumman Corporation | Ceramic composite materials having tailored physical properties |
US20050276961A1 (en) * | 2003-08-04 | 2005-12-15 | Sherwood Walter J | Materials and methods for making ceramic matrix composites |
WO2007108793A1 (en) | 2006-03-20 | 2007-09-27 | Sulzer Metco Venture, Llc | Method for forming a ceramic containing composite structure |
FR2939430B1 (en) | 2008-12-04 | 2011-01-07 | Snecma Propulsion Solide | METHOD FOR SMOOTHING THE SURFACE OF A PIECE OF CMC MATERIAL |
US20120318448A1 (en) | 2011-06-16 | 2012-12-20 | General Electric Company | Method for manufacturing a composite surface |
US20160230570A1 (en) | 2015-02-11 | 2016-08-11 | Rolls-Royce High Temperature Composites Inc. | Modified atmosphere melt infiltration |
-
2019
- 2019-05-24 DE DE102019207621.1A patent/DE102019207621A1/en not_active Withdrawn
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Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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DE3601569A1 (en) * | 1986-01-21 | 1987-07-23 | Kolbenschmidt Ag | COMPOSITE SLIDING BEARING MATERIAL |
DE102009032961A1 (en) * | 2009-07-14 | 2011-01-20 | Schaeffler Technologies Gmbh & Co. Kg | Rolling bearing cage |
DE102012205606A1 (en) * | 2011-04-04 | 2012-10-25 | Gwo S. Swei | Self-lubricating structure and method of making the same |
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