DE102019207617A1 - METHOD FOR MANUFACTURING A COMPONENT FROM A CERAMIC FIBER COMPOSITE MATERIAL - Google Patents
METHOD FOR MANUFACTURING A COMPONENT FROM A CERAMIC FIBER COMPOSITE MATERIAL Download PDFInfo
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Abstract
Die vorliegende Erfindung betrifft ein Verfahren zur Herstellung von Bauteilen aus keramischen Faserverbundwerkstoffen, bei welchen Fasern (8) aus Keramik oder Kohlenstoff in einer Matrix (11) aus Siliciumcarbid eingebettet sind, wobei Schichten (1,3,5) mit einem organische Werkstoff (6) und Silicium - Partikeln (7) und Schichten (2,4) mit Fasern (8) angeordnet und zu einem Grünkörper geformt werden, wobei anschließend der Grünkörper einer Wärmebehandlung oberhalb der Schmelztemperatur von Silicium unterzogen wird, bei der eine SiC - Matrix (11) gebildet wird, in der die Fasern (8) eingelagert sind.The present invention relates to a method for producing components made of ceramic fiber composite materials, in which fibers (8) made of ceramic or carbon are embedded in a matrix (11) made of silicon carbide, layers (1, 3, 5) with an organic material (6 ) and silicon particles (7) and layers (2,4) with fibers (8) are arranged and shaped into a green body, the green body then being subjected to a heat treatment above the melting temperature of silicon, in which a SiC matrix (11 ) is formed in which the fibers (8) are embedded.
Description
HINTERGRUND DER ERFINDUNGBACKGROUND OF THE INVENTION
GEBIET DER ERFINDUNGFIELD OF THE INVENTION
Die vorliegende Erfindung betrifft ein Verfahren zur Herstellung von Bauteilen aus keramischen Faserverbundwerkstoffen, bei welchen Fasern aus Keramik oder Kohlenstoff in einer Matrix aus Siliciumcarbid eingebettet sind.The present invention relates to a method for producing components made of ceramic fiber composite materials, in which fibers made of ceramic or carbon are embedded in a matrix made of silicon carbide.
STAND DER TECHNIKSTATE OF THE ART
Keramische Faserverbundwerkstoffe, die im englischen auch als Ceramic Matrix Composites CMC bezeichnet werden, werden aufgrund ihrer guten Hochtemperatur - sowie Korrosionsbeständigkeit und ihrer hervorragenden mechanischen Eigenschaften in vielen Bereichen der Technik eingesetzt, unter anderem bei Hochtemperaturanwendungen im Flugzeug - bzw. Flugtriebwerksbau. Allerdings ist die Herstellung von Bauteilen aus keramischen Faserverbundwerkstoffen schwierig, da häufig die Porenfreiheit und Homogenität der Matrix schwierig zu erreichen sind.Ceramic fiber composites, which are also known as Ceramic Matrix Composites CMC, are used in many areas of technology due to their good high temperature and corrosion resistance and their excellent mechanical properties, including high temperature applications in aircraft and aircraft engine construction. However, the production of components from ceramic fiber composite materials is difficult, since the absence of pores and homogeneity of the matrix are often difficult to achieve.
Beispielsweise wird bei der Herstellung von Bauteilen aus mit SiC - Fasern verstärktem Siliciumcarbid die Matrix häufig durch Infiltration von flüssigem Silicium in einen Faserrohling (Preform) hergestellt. Allerdings stellt die Durchdringung des Faserrohlings mit flüssigem Silicium eine Schwierigkeit dar, die umso schwerwiegender ist, je größer das Bauteil ist bzw. je mehr SiC - Matrix gebildet werden muss. Dies kann dazu führen, dass ein Teil des bereitgestellten Kohlenstoffs nicht zu Siliciumcarbid reagieren kann, sodass die Homogenität der Matrix beeinträchtigt wird. Außerdem kann es zu Porenbildung kommen, die ebenfalls die Anwendung von Bauteilen aus derartigen keramischen Faserverbundwerkstoffen, wie faserverstärktem Siliciumcarbid, beeinträchtigen kann.For example, in the production of components from silicon carbide reinforced with SiC fibers, the matrix is often produced by infiltration of liquid silicon into a fiber blank (preform). However, the penetration of the fiber blank with liquid silicon represents a difficulty which is more serious the larger the component is or the more SiC matrix has to be formed. This can mean that some of the carbon provided cannot react to form silicon carbide, so that the homogeneity of the matrix is impaired. In addition, pore formation can occur, which can also impair the use of components made of such ceramic fiber composite materials, such as fiber-reinforced silicon carbide.
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OFFENBARUNG DER ERFINDUNGDISCLOSURE OF THE INVENTION
AUFGABE DER ERFINDUNGOBJECT OF THE INVENTION
Es ist deshalb Aufgabe der vorliegenden Erfindung ein Verfahren zur Herstellung von keramischen Faserverbundwerkstoffen bzw. von Bauteilen daraus bereitzustellen, bei welchem auf die Infiltration von entsprechenden Stoffen in einen Faserrohling oder Grünkörper verzichtet werden kann und eine homogene und weitgehend porenfreie Matrix erzeugt werden kann. Insbesondere soll ein Verfahren angegeben werden, mit dem Bauteile aus faserverstärktem Siliciumcarbid in zuverlässiger und einfacher Weise hergestellt werden können.It is therefore the object of the present invention to provide a method for the production of ceramic fiber composite materials or of components therefrom, in which the infiltration of corresponding substances into a Fiber blank or green body can be dispensed with and a homogeneous and largely pore-free matrix can be produced. In particular, a method is to be specified with which components made of fiber-reinforced silicon carbide can be manufactured in a reliable and simple manner.
TECHNISCHE LÖSUNGTECHNICAL SOLUTION
Diese Aufgabe wird gelöst durch ein Verfahren mit den Merkmalen des Anspruchs 1. Vorteilhafte Ausgestaltungen sind Gegenstand der abhängigen Ansprüche.This object is achieved by a method with the features of
Die Erfindung schlägt zur Herstellung von Bauteilen aus keramischen Faserverbundwerkstoffen auf Basis von Siliciumcarbid vor, Schichten mit einem organischen Werkstoff und Silicium - Partikeln sowie Schichten mit Fasern, die in dem keramischen Faserverbundwerkstoff enthalten sein sollen, zu einem Grünkörper zu formen, wobei anschließend der Grünkörper einer Wärmebehandlung oberhalb der Schmelztemperatur von Silicium unterzogen wird, sodass eine SiC - Matrix aus dem Kohlenstoff des organischen Werkstoffs und den Silicium - Partikeln gebildet wird, in der die Fasern eingelagert sind. Mit dieser Vorgehensweise kann auf die Infiltration von Stoffen in einen Faserrohling verzichtet werden. Stattdessen wird durch die Bereitstellung des Kohlenstoffs über einen organischen Werkstoff und des Siliciums über die Silicium - Partikel in entsprechenden Schichten, die zusätzlich zu Schichten mit den einzulagernden Fasern angeordnet werden, die Bildung von Siliciumcarbid ermöglicht, welches homogen ohne Ausbildung von Poren an den Fasern ausgebildet werden kann.For the production of components from ceramic fiber composites based on silicon carbide, the invention proposes to form layers with an organic material and silicon particles as well as layers with fibers that are to be contained in the ceramic fiber composite material to form a green body, the green body then being one Heat treatment above the melting temperature of silicon is subjected, so that a SiC matrix is formed from the carbon of the organic material and the silicon particles in which the fibers are embedded. With this procedure, the infiltration of substances into a fiber blank can be dispensed with. Instead, the provision of the carbon via an organic material and the silicon via the silicon particles in appropriate layers, which are arranged in addition to layers with the fibers to be embedded, enables the formation of silicon carbide, which is homogeneous without the formation of pores on the fibers can be.
Die Silicium - Partikel können in den Schichten mit dem organischen Werkstoff und den Silicium - Partikeln in dem organischen Werkstoff eingebettet sein und / oder auf dem organischen Werkstoff angeordnet sein.The silicon particles can be embedded in the layers with the organic material and the silicon particles in the organic material and / or can be arranged on the organic material.
Bei dem organischen Werkstoff kann es sich um ein thermoplastisches Polymer handeln.The organic material can be a thermoplastic polymer.
Der organische Werkstoff kann bei der Wärmebehandlung pyrolysiert oder verbrannt werden, sodass lediglich der Kohlenstoff des organischen Werkstoffs bzw. des thermoplastischen Polymers für die Siliciumcarbid - Bildung bereitgestellt wird, während andere Bestandteile des organischen Werkstoffs bzw. thermoplastischen Polymers verbrennen und / oder ausgasen.The organic material can be pyrolyzed or burned during the heat treatment so that only the carbon of the organic material or thermoplastic polymer is provided for silicon carbide formation, while other components of the organic material or thermoplastic polymer burn and / or outgas.
Der organische Werkstoff kann insbesondere aus der Gruppe ausgewählt werden, die Wachse, insbesondere synthetische Wachse, Polyamide, Polyethylen und Polyolefine umfasst.The organic material can in particular be selected from the group comprising waxes, in particular synthetic waxes, polyamides, polyethylene and polyolefins.
Die Schichten mit einem organischen Werkstoff und Silicium - Partikeln sowie die Schichten mit Fasern können abwechselnd zueinander bzw. alternierend angeordnet werden, sodass die Fasern gleichmäßig von der Matrix, die durch die Bildung des Siliciumcarbid entsteht, umschlossen sind.The layers with an organic material and silicon particles as well as the layers with fibers can be arranged alternately with one another or alternately so that the fibers are evenly enclosed by the matrix that is created by the formation of the silicon carbide.
Der Grünkörper, der aus den Schichten mit einem organischen Werkstoff und Silicium - Partikeln sowie den Schichten mit Fasern gebildet wird, kann in einer Form entsprechend der Form des herzustellenden Bauteils hergestellt werden, sodass bereits eine endkonturnahe Form des Grünkörpers gegeben ist.The green body, which is formed from the layers with an organic material and silicon particles and the layers with fibers, can be produced in a shape corresponding to the shape of the component to be produced, so that the green body already has a near net shape.
Die Schichten mit einem organischen Werkstoff und Silicium - Partikeln sowie die Schichten mit Fasern aus Keramik und / oder Kohlenstoff können zur Bildung des Grünkörpers miteinander mithilfe eines Klebstoffs verklebt werden. Zusätzlich oder alternativ können auch die Bestandteile der einzelnen Schichten, also beispielsweise die Silicium - Partikel mit dem organischen Werkstoff oder untereinander sowie die Fasern aus Kohlenstoff und / oder Keramik miteinander verklebt werden. Zum Verkleben der Schichten mit einem organischen Werkstoff und Silicium - Partikeln sowie den Schichten mit Fasern aus Kohlenstoff und / oder Keramik und / oder von deren Bestandteilen kann ein Klebstoff aus der Gruppe verwendet werden, die Wachse, insbesondere synthetische Wachse, Polyamide, Polyethylen und Polyolefine umfasst.The layers with an organic material and silicon particles and the layers with fibers made of ceramic and / or carbon can be glued to one another with the aid of an adhesive to form the green body. Additionally or alternatively, the components of the individual layers, for example the silicon particles with the organic material or with one another, and the fibers made of carbon and / or ceramic, can be glued to one another. An adhesive from the group consisting of waxes, in particular synthetic waxes, polyamides, polyethylene and polyolefins, can be used to bond the layers with an organic material and silicon particles and the layers with fibers made of carbon and / or ceramic and / or their components includes.
Der Grünkörper kann während der Wärmebehandlung komprimiert werden, wobei insbesondere ein HIP - Prozess (heißisostatisches Pressen HIP) durchgeführt werden kann.The green body can be compressed during the heat treatment, in particular a HIP process (hot isostatic pressing HIP) can be carried out.
Als keramische Fasern können Siliciumcarbid - Fasern oder beschichtete Siliciumcarbid - Fasern verwendet werden, wobei die Beschichtung der Siliciumcarbid - Fasern mit einem Stoff erfolgen kann, der aus der Gruppe ausgewählt ist, die BN, Si3N4, SiC und C umfasst.Silicon carbide fibers or coated silicon carbide fibers can be used as ceramic fibers, it being possible for the silicon carbide fibers to be coated with a substance selected from the group consisting of BN, Si 3 N 4 , SiC and C.
FigurenlisteFigure list
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-
1 eine Querschnittsdarstellung eines Grünkörpers eines ersten Ausführungsbeispiels, -
2 eine Querschnittsdarstellung des aus dem Grünkörper der1 gefertigten Bauteils, -
3 eine Querschnittsdarstellung eines Grünkörpers eines zweiten Ausführungsbeispiels, -
4 eine Querschnittsdarstellung des aus dem Grünkörper der2 gefertigten Bauteils und in -
5 einen Querschnitt durch eine beschichtete Faser.
-
1 a cross-sectional representation of a green body of a first embodiment, -
2 a cross-sectional view of the from the green body of1 manufactured component, -
3 a cross-sectional representation of a green body of a second embodiment, -
4th a cross-sectional view of the from the green body of2 manufactured component and in -
5 a cross section through a coated fiber.
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
Die erste, dritte und fünfte Schicht
Die zweite und vierte Schicht
Sämtliche Schichten
Der Grünkörper aus
Die
Neben den ersten, dritten, fünften und siebten Schichten
Auch der Grünkörper gemäß den zweiten Ausführungsbeispiel, der in
Anstelle der in den vorangegangenen Ausführungsbeispielen gezeigten SiC - Fasern können auch andere Fasern, wie beispielsweise Kohlenstofffasern eingesetzt werden. Eine Möglichkeit besteht auch darin beschichtete Fasern
Anstelle der in den Ausführungsbeispielen 1 und 2 der
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
- erste Schichtfirst layer
- 22
- zweite Schichtsecond layer
- 33
- dritte Schichtthird layer
- 44th
- vierte Schichtfourth layer
- 55
- fünfte Schichtfifth layer
- 66
- ThermoplastThermoplastic
- 77th
- Silicium - PartikelSilicon particles
- 88th
- SiC - FaserSiC fiber
- 99
- Klebstoffadhesive
- 1010
- BauteilComponent
- 1111
- SiC - MatrixSiC matrix
- 2121st
- erste Schichtfirst layer
- 2222nd
- zweite Schichtsecond layer
- 2323
- dritte Schichtthird layer
- 2424
- vierte Schichtfourth layer
- 2525th
- fünfte Schichtfifth layer
- 2626th
- sechste Schichtsixth shift
- 2727
- siebte Schichtseventh shift
- 2828
- ThermoplastThermoplastic
- 2929
- Silicium - PartikelSilicon particles
- 3030th
- BauteilComponent
- 3131
- SiC - MatrixSiC matrix
- 3232
- FasergeflechtFiber braid
- 3333
- erste Fasernfirst fibers
- 3434
- zweite Fasernsecond fibers
- 3535
- beschichtete Fasercoated fiber
- 3636
- FaserkernFiber core
- 3737
- FaserbeschichtungFiber coating
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
- US 8980027 B2 [0004]US 8980027 B2 [0004]
- US 9440888 B2 [0005]US 9440888 B2 [0005]
- US 5589115 A [0006]US 5589115 A [0006]
- US 5476685 A [0007]US 5476685 A [0007]
- US 9512044 B2 [0008]US 9512044 B2 [0008]
- US 2016/0159066 A1 [0009]US 2016/0159066 A1 [0009]
- US 6773528 B2 [0010]US 6773528 B2 [0010]
Claims (11)
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Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2210771A1 (en) * | 1971-03-05 | 1972-09-28 | Secr Defence | Process for the production of a mixed material |
US4689188A (en) * | 1986-07-16 | 1987-08-25 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of preparing fiber reinforced ceramic material |
US5439627A (en) * | 1990-06-29 | 1995-08-08 | Flexline Services Ltd. | Process for manufacturing reinforced composites |
US5589115A (en) * | 1987-11-16 | 1996-12-31 | Corning Incorporated | Method for making fiber-reinforced ceramic matrix composite |
US6773528B2 (en) * | 1999-03-01 | 2004-08-10 | Agency Of Industrial Science And Technology | Process for producing fiber-reinforced-silicon carbide composites |
US20050202282A1 (en) * | 2002-07-30 | 2005-09-15 | Eads Space Transportation Sa | Manufacturing process for a refractory material, protective coating that can be obtained with this process and uses of this process and this coating |
US8980027B2 (en) * | 2006-10-17 | 2015-03-17 | Herakles | Process for manufacturing a part made of a ceramic matrix composite containing matrix phases for healing and deflecting cracks |
-
2019
- 2019-05-24 DE DE102019207617.3A patent/DE102019207617A1/en not_active Withdrawn
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2210771A1 (en) * | 1971-03-05 | 1972-09-28 | Secr Defence | Process for the production of a mixed material |
US4689188A (en) * | 1986-07-16 | 1987-08-25 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of preparing fiber reinforced ceramic material |
US5589115A (en) * | 1987-11-16 | 1996-12-31 | Corning Incorporated | Method for making fiber-reinforced ceramic matrix composite |
US5439627A (en) * | 1990-06-29 | 1995-08-08 | Flexline Services Ltd. | Process for manufacturing reinforced composites |
US6773528B2 (en) * | 1999-03-01 | 2004-08-10 | Agency Of Industrial Science And Technology | Process for producing fiber-reinforced-silicon carbide composites |
US20050202282A1 (en) * | 2002-07-30 | 2005-09-15 | Eads Space Transportation Sa | Manufacturing process for a refractory material, protective coating that can be obtained with this process and uses of this process and this coating |
US8980027B2 (en) * | 2006-10-17 | 2015-03-17 | Herakles | Process for manufacturing a part made of a ceramic matrix composite containing matrix phases for healing and deflecting cracks |
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