DE2118848C3 - Rotationally symmetric, hollow composite body and process for its manufacture - Google Patents
Rotationally symmetric, hollow composite body and process for its manufactureInfo
- Publication number
- DE2118848C3 DE2118848C3 DE2118848A DE2118848A DE2118848C3 DE 2118848 C3 DE2118848 C3 DE 2118848C3 DE 2118848 A DE2118848 A DE 2118848A DE 2118848 A DE2118848 A DE 2118848A DE 2118848 C3 DE2118848 C3 DE 2118848C3
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- Germany
- Prior art keywords
- layer
- fibers
- metal
- composite body
- fiber
- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C41/00—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
- B29C41/02—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor for making articles of definite length, i.e. discrete articles
- B29C41/04—Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould
- B29C41/042—Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould by rotating a mould around its axis of symmetry
- B29C41/045—Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould by rotating a mould around its axis of symmetry the axis being placed vertically, e.g. spin casting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D13/00—Centrifugal casting; Casting by using centrifugal force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/02—Casting in, on, or around objects which form part of the product for making reinforced articles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/32—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core
- B29C70/323—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core on the inner surface of a rotating mould
- B29C70/326—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core on the inner surface of a rotating mould by rotating the mould around its axis of symmetry
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- 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
- Y10T428/12333—Helical or with helical component
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- 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.]
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- 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
- Y10T428/12465—All metal or with adjacent metals having magnetic properties, or preformed fiber orientation coordinate with shape
-
- 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
- Y10T428/12486—Laterally noncoextensive components [e.g., embedded, 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.]
- Y10T428/12736—Al-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
- Y10T428/12778—Alternative base metals from diverse categories
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Separation By Low-Temperature Treatments (AREA)
Description
b) Are Schicht besteht aus einem Faserwerkstoff, insbesondere aus Wolfram-, Beryllium-, Stahl-, Bor-, Kohlenstoff- oder SiU-ziumkarbidfasern, die als gewickelte Endlosfasern, als Stapelfasern oder als Fasermatten angeordnet sind, wobei die Fugen zwischen den einzelnen Fasern mit einem der unter (a) genannten Metalle vergossen sind, c) der Wärmeausdehnungskoeffizient des reinen Metalls der inneren Schicht ,st gleich groß oder größer als der des Matr.xmetalls der faserverstärkten äußeren Schicht.b) Are layer consists of a fiber material, in particular made of tungsten, beryllium, steel, boron, carbon or silicon carbide fibers, as wound continuous fibers, as staple fibers or as fiber mats are arranged, the joints between the individual fibers with one of the below (a) said metals are cast, c) the coefficient of thermal expansion of the pure Metal of the inner layer, st equal to or greater than that of the Matr.xmetalls the fiber reinforced outer layer.
2. Verfahren zur Herstellung eines rotationssymmetrischen Verbundkörpers nach Anspruch 1 durch Schleudergießen, wobei das zu vergießende Metall mit Hilfe eines rotierenden oder feststehenden, in der Achse einer rotierenden Kokille liegenden Gießvorrichtung auf die an der Kok. leninnenwand liegenden endlosen Fasern, Stapelfasern oder Fasermatten gegossen wird und wobei anschließend auf die mit dem Matnxmetall getränkte faserverstärkte Schicht eine zweite. Schicht aus einem Metall aufgegossen wird, das einen gleich großen oder größeren Warme ausdehnungskoeffizienten als das Matnxmetall be-SS, dadurch gekennzeichnet, daß die Rotation +o der Kokille so lange aufrechterhalten wird bis sich das Metall der inneren Schicht verfestigt hat.2. A method for producing a rotationally symmetrical composite body according to claim 1 by centrifugal casting, wherein the metal to be cast with the help of a rotating or stationary, lying in the axis of a rotating mold casting device on the Kok. Endless fibers, staple fibers or fiber mats lying on the inner wall is poured and then a second layer is applied to the fiber-reinforced layer impregnated with the Matnxmetall. Layer of a metal is poured on, which has an equal or greater thermal expansion coefficient than the Matnxmetall be-SS, characterized in that the rotation + o of the mold is maintained until the metal of the inner layer has solidified.
Werkstoffmaterial
g£}„ium> Bor, Kohals Faserwerkstoff Ver- ^ Matrix Metalle auf Nik- g £} "ium> Boron, Koh as a fiber material Ver ^ matrix metals on Nik-
VTtan oder Aluminiumbasis dienenServe VTtan or aluminum base
I970, 20, S. 1390 bis 1392).I 970 , 20, pp. 1390 to 1392).
^ " faserverstärkter Werkstoff seine^ "its fiber-reinforced material
Da em deramg z belastUng in Fasernch-As a result, there is a load in fiber
hohe ^st'gktu n. kbe]astung in Fasernchtunghigh strength in fiber direction
^ ί/Γ ^die Festigkeitswerte seines Matnxmaterials'und bei Zugbelastung senkrecht zur Fasernch- ^ ί / Γ ^ the strength values of its Matnxma ter ials' and with tensile load perpendicular to the fiber
ih einma, diese erreicht, w" e™ ^* 0^ Werkstoff tager^lit W^ ih einma , this achieved, w " e ™ ^ * 0 ^ material tager ^ lit W ^
Ser^fhende^ Wechselspannungen aufzu-The necessary alternating voltages
nehmen. , u„WVSrner mii,m take n., u " WVSrner mii , m
Zu einem schnell rotierenden Hohlkörper »« Fasem in tangentialerR.chtung verlaufen urn d, def Fliehkrafl resuH^renden Jangentialen Zug ngen aufzunehmen, es wirken da«e ™ T P ransver B saischwingungen <ffe^. senkrecht zum Faserverlauf; hiervon ist den A beautiful nell rotating hollow body "" fibers in tangentialerR.chtung run urn d, Fliehkrafl resuH ^ Governing Jangentialen def train nts record, it act as "e ™ T P ransver B sa i sc hwingungen <ff e ^. perpendicular to the grain; of this is the
ngen dadurch zu begegnen daß die haser. Necessary to meet the rabbits.
V aufeinanderliegen und sich gegen«mg^utee-D· Druckspannung wird also vom Matnxmatena und vom Fasenverkstoff aufgenommen.^ Anders heg V on one another and is against "mg ^ utee- D · Druckspa retr so absorbed by Fasenverkstoff from Matnxmatena and. ^ In other heg
der Fall bei ^^"Sdergedehnt, so daß die *eröanci aer ^ zwischen den Fasern be-the case at ^^ "sderstretched, so that the * er öanci aer ^ between the bevel rn
Spannung nur rial au{genommen werdenTension can only be perceived rial
f^lichai ^ai ^^ spannungsfrei bleiben,f ^ lichai ^ ai ^^ stay tension-free,
kam., <aa α f die Fasern völlig verMan7ß e e rrimaterial durch achsparallele Kett-Χ Dauerbrüche in Kauf nehmen.came. <aa α f the chamfer rn completely ver Man 7 ß e e rri material by axially parallel warp Χ fatigue fractures accepted.
rotationssymmetrischer Verbund- ^ Glas-Stapelfasern, Glasmatten "n 'eine rotierende Schleuderform o _g diesen Faserwerkstoff im rota tion symmetrical composite ^ glass staple fibers, glass mats "n 'ei ne rotating spinner o _g this Faserwer kstoff in
««gJ^Siverfahrcn einen flüssigen Kunststoff bc"ie"°. f"" fBecker, Schmitz, Weber: ^>ggJJ«k^ Kunststoffen«, C.Hansa»°as »chleuae g 58bis71).The use of a liquid plastic bc " ie " °. f "" fBec ker, Schmitz, Weber: ^> ggJJ « k ^ plastics«, C.Hansa »° as» chleuae g 58bis71) .
V er lag JMuncn {.ndun ist ^ dnen rotationssym-V he lay JMuncn { . ndun is dunes ^ ro t a tionssym-
Yih Hohlkörper zu finden, dessen Material ei-Yih to find hollow bodies, the material of which
Oie Erfindung bezieht sich auf einen rotationssym- ^SST^S. The invention relates to a rotationally symmetrical ^ SST ^ S.
metrischen, hohlen Verbundkörper, bestehend aus gungen ^^Aufgabe wird erfindungsgemäßmetric, hollow composite body, consisting of gungen ^^ Object is according to the invention
zwei ebenfalls rotationssymmetnschen ineinander ^"r J^nation folgender Merkmale vorgeschlagen:two also rotationally symmetrical in each other ^ " r J ^ nation of the following features are proposed:
angeordneten fugenlos ineinander übergehenden 5o die Kombination te, g wesentlichen ausarranged seamlessly merging 5 o the combination te, wesentl g i c h s from
Sn vTn GasTentrifugenanlagen, unterliegen ver-Sdenartigen Beanspruchungen. Zunächst ergibt sfch auf Gadder hohen Fliehkraft in der Wandung des Maschinenteils eine hohe Zugspannung, die taneential in der Rotationsebene auftritt. Diese im we-Sn liehen statische Spannung wird von weiteren oszinierenden Spannungen überlagtirt, die aus Biege-Schwingungen längs der Achse des Körpers folgen. Die resultierenden oszillierenden Spannungen ergeben Wechselbeanspruchungen, die zu alsbaldigem Dauerbruch führen.Sn vTn gas centrifuge systems are subject to ver-sden-like Stresses. First of all, there is a high centrifugal force in the wall on Gadder of the machine part has a high tensile stress, the taneential occurs in the plane of rotation. This static tension borrowed in the we-Sn is replaced by further oscillating Tensions superimposed from bending vibrations follow along the axis of the body. The resulting oscillating stresses result Alternating stresses that lead to fatigue failure in the near future.
Wenn die auftretenden Fliehkräfte sehr hoch werden, muß der Quotient der Zugfestigkeit zur Dichte im Material des Maschinente.ls «nen möglichst hohen Wert annehmen. Hierbei ist es bekannt, daß die-If the centrifugal forces that occur are very high, the quotient of tensile strength to density must in the material of the machine part should be as high as possible. It is known that the
b) Die außere Schicht besteht aus einem Faserwerkstoff, insbesondere aus Wolfram-, ΒβηΛ-Hunv> stahl-, Bor-, Kohkntoff oderStonr karbidfasern, die als ψ^Τ^^Ά. a,s stapelfasern oder als Fasermatten angeord net sin^ wobei die Fugen zwischen *n«niel· nen Fasem mit einem der unter (a) genannten Metalles vergossen sind. b) The exterior layer consists of a fiber who kstoff, in particular from tungsten, ΒβηΛ- Hunv> steel, boron, Kohkntoff oderStonr karbidfasern, as ψ ^ ^^ Τ Ά. a, s staple fibers or fiber mats angeord net sin ^ ei wove the joints are sealed between * n "niel · nen fibers with one of said (a) metal.
Der Wärmeausdehnungskoeffizient des reinen MetaHg der inneren Schicht ist gleich groß oder, größer als der des Matrixmetalls der faserver- The coefficient of thermal expansion of the pure MetaHg of the inner layer is equal to or greater than that of the matrix metal of the fiber-reinforced
stärkten äußeren Schicht.s Secretary kth outer layer.
Erfindung liegen darin, daß einInvention are that a
JJ«d v^her Quotient 6 der Zugfestigkeit zur besondersJJ « d v ^ her quotient 6 of the tensile strength to the particularly
Dichte im von der Fliehkraft besonders belasteten äußeren Teil des Rotationskörpers vorliegt; dieses ist dadurch erreicht, daß ein Verbundwerkstoff, wie er bereits oben genannt ist, die äußere Schicht bildet.Density is present in the outer part of the body of revolution that is particularly stressed by centrifugal force; this is achieved in that a composite material, as already mentioned above, forms the outer layer.
Diesem äußeren Teil des Verbundkörpers ist ein zwjiter, innerer Teil fugenlos eingebracht, der aus reinem Metall besteht und somit erheblich höhere axiale Zugspannungen aufnehmen kann als die Schicht aus Verbundmaterial, deren Fasern im wesentlichen in tangentialer Richtung verlaufen müssen. Hierbei nehmen bei hoher Drehzahl die Fasern die Z:ntrifugallast der inneren Schicht auf, die sich hierbei eng an die äußere anlegt und dadurch bei Biegesthwingungen die äußere Schicht stützt. Bei axialen Zugspannungen stützt die innere Schicht die äußere und verhindert deren Dehnung über die Schadensgrenze hinaus, wobei durch das enge Anliegen der beiden Schichten eine sichere Verbindung zwischen ihnen gewährleistet ist.This outer part of the composite body has a second, inner part that is seamlessly incorporated pure metal and can therefore absorb considerably higher axial tensile stresses than the Layer of composite material, the fibers of which must run essentially in a tangential direction. Here, at high speed, the fibers take on the centrifugal load of the inner layer, which is caused by this closely to the outer and therefore with flexural vibrations the outer layer supports. In the case of axial tensile stresses, the inner layer supports the outer one and prevents them from stretching beyond the limit of damage, whereby due to the close concern of the a secure connection between them is guaranteed between the two layers.
Lm aber auch bei niedrigen Drehzahlen ein Vers^ hieben der inneren Schicht gegenüber der äußeren zu verhindern, empfiehlt es sich, zwischen beiden Schichten eine radiale Vorspannung vorzusehen, d. h. die äußere Schicht auf die innere aufzuschrumpfen. Da man sich hierzu gewöhnlich thermischer Verfahi en bedient, sieht die Erfindung weiterhin vor, für die innere Schicht ein Metall zu verwenden, dessen Wärmeausdehnungskoeffizient gleich groß oder größer ist als der des Matrixmetalls der äußeren Schicht. Kommt es nämlich bei dem Ineinanderbringen der beiden hohlzylihdrischen Schichten zu einem Wärmeausgleich, dann wird sich beim Abkühlen die innere Schicht nicht weniger verkürzen als die äußere, es wird also von vornherein ein schädliches axiales Vorspannen der äußeren Schicht verhindert. Ein Nachlassen der radialen Vorspannung wird hierbei auch bei geringer Drehzahl durch die aus der Fliehkraft resultierende Andruckkraft ausgeglichen.Lm but also at low speeds a verse ^ To prevent chopping the inner layer against the outer, it is advisable to keep between the two Providing radial prestress to layers; d. H. to shrink the outer layer onto the inner one. Since this is usually used thermal Verahi en, the invention continues to provide for the inner layer to use a metal whose coefficient of thermal expansion is equal to or greater is than that of the matrix metal of the outer layer. It comes from bringing the two hollow-cylindrical layers to a heat balance, then the inner one becomes when it cools down Shorten the layer no less than the outer one, so it becomes a damaging axial one from the start Pre-tensioning the outer layer prevented. A decrease in the radial pretensioning occurs here balanced even at low speed by the pressure force resulting from the centrifugal force.
Als Material dient für die innere Schicht eines der Metalle, wie es als Matrix der äußeren Schicht dient. Hierdurch, insbesondere aber bei Verwendung des gleichen Materials für Martix und innere Schicht, ergibt sich der Vorteil, daß insbesondere durch thermische Behandlung eine innige Verbindung zwischen äußerer und innerer Schicht hergestellt wird, wodurch Ablösungserscheinungen verhindert werden.The material used for the inner layer is one of the metals as it is used as the matrix for the outer layer. This, but especially when using the same material for the Martix and inner layer, results the advantage that, in particular by thermal treatment, an intimate connection between outer and inner layer is produced, whereby delamination phenomena are prevented.
In einer weiteren Ausgestaltung der Erfindung wird der erfindungsgemäße Verbundkörper durch Schleudergießen hergestellt, wobei das zu vergießende Metall mit Hilfe eines rotierenden oder feststehenden, in der Achse einer rotierenden Kokille liegenden Gießvorrichtung auf die an der Kokilleninnenwand liegenden endlosen Fasern, Stapelfasern oder Fasermatten gegossen wird und wobei anschließend auch die mit dem Matrixmetall getränkte faserverstärkte Schicht eine rveite Schicht aus einem Metall aufgegossen wird, das einen gleich großen oder größeren Wärmeausdehnungskoeffizienten ak das Matrixmetall besitzt, indem dia Rotation der Kokille so lange aufrechterhalten wird, bis sich das Metall derIn a further embodiment of the invention, the composite body according to the invention is through Centrifugal casting produced, whereby the metal to be cast is made with the help of a rotating or stationary, Lying in the axis of a rotating mold casting device on the inside wall of the mold lying endless fibers, staple fibers or fiber mats is poured and then the fiber-reinforced layer impregnated with the matrix metal also has a second layer made of a metal is poured on, which has an equal or greater coefficient of thermal expansion ak that Matrix metal by maintaining the rotation of the mold until the metal is
inneren Schicht verfestigt hat. Es ermöglicht dieses Verfahren, die Fasern in der Gußtrommel in optimaler Weise anzuordnen und dann anschließend das Matrixmetall lunkerfrei und mit gleichmäßiger Schichtdicke auf die Fasern aufzutragen.solidified inner layer. It enables this process to optimize the fibers in the casting drum Way to arrange and then subsequently the matrix metal void-free and with more uniform Apply a layer thickness to the fibers.
ίο Während das Metall der inneren Schicht aufgetragen wird, ist das Matrixmetall bereits so weit erstarrt, daß es zwar noch die Bildung einer Diffusionszone zwischen den beiden Schichten gestattet, aber dem Druck der erkaltenden und sich verkürzenden inneren Schicht standhält, so daß sich in axialer Richtung in der äußeren Schicht eine hohe Druckspannung, in der inneren Schicht eine hohe Zugspannung ausbildet. Die Größenordnung dieser Spannung ist von Gießgeschwindigkeit, Art der Schmelzen, Materia!ίο While the metal is applied to the inner layer is, the matrix metal has already solidified to such an extent that a diffusion zone is still formed between the two layers, but the pressure of the cooling and shortening inner layers Layer withstands, so that there is a high compressive stress in the axial direction in the outer layer, in the inner layer forms a high tensile stress. The magnitude of this tension is of Casting speed, type of melts, materia!
so der Kokillenwand und von deren Dicke abhängig und über diese genannten Einflußgrößen derart beherrschbar, daß eine so große Vorspannung gewählt werden kann, die bei Transversalauslenkungen des fertigen Gußkörpers in der äußeren Schicht umso depends on the mold wall and its thickness and can be controlled using these influencing variables in such a way that such a large preload is selected can be that in the case of transverse deflections of the finished cast body in the outer layer
Druck-Schwellspannungen, in der inneren Schicht nur Zug-Schwellspannungen aufkommen läßt. Es ist hiermit nicht nur das Erreichen schädlicher Zugspannung in der äußeren Schicht verhindert, es entfällt darüber hinaus die besonders schnell zu Dauerschä-Pressure-threshold stresses, in the inner layer only allows tensile-threshold stresses to arise. It is This not only prevents damaging tensile stress from being reached in the outer layer, it is also eliminated in addition, the particularly fast to permanent damage
den führende Wechselbeanspruchung, in beiden Schichten. Um radiale Vorspannungen in günstiger Richtung zu erhalten, wird die schnelle Rotation der Kokille bis zum endgültigen Erkalten der inneren Schicht weitergeführt, wobei diese Schicht in Kraft-the leading alternating stress, in both shifts. To get radial biases in cheaper Direction is obtained by the rapid rotation of the mold until the inner mold has finally cooled down Shift continued, with this shift in force
richtung verfestigt, also radial nach außen plastisch verformt und gegen die äußere Schicht gepreßt wird, so daß nach dem Erkalten in radialer Richtung ein Spannungszustand geschaffen wird, wie er sich sonst erst bei höherer Drehzahl des fertigen Gußkörperssolidified in the direction, i.e. plastically deformed radially outwards and pressed against the outer layer, so that after cooling in the radial direction a state of tension is created, as it would otherwise only at a higher speed of the finished cast body
einstellen würde. Hier werden nicht nur Ablösungserscheinungen verhindert, die bei z.B. Torsionsschwingungen auftreten würden, sondern auch Einstülpungen bei transversalen Auslenkungen des langsam umlaufenden Gußkörpers und Umwandeln aller auftretenden radialen Wechselspannungen.would hire. This not only prevents the detachment phenomena caused by e.g. torsional vibrations would occur, but also invaginations with transverse deflections of the slowly rotating cast body and converting all occurring radial alternating voltages.
Es ist bei Anwendung des genannten Verfahrens vorteilhaft, in die Gußtrommel vor dem Gießen ein mit Faserwerkstoff belegtes und aus Matrixmaterial bestehendes Gerüst einzubringen. Hierdurch können die Fasern in dem späteren Spannungsverlauf entsprechenden Mustern angeordnet und während des . Anfahrens der Gußtrommel in ihrer Stellung festgehalten werden, bis Fliehkraft und flüssiges Matrixmaterial ein Verrutschen der Fasern verhindern; das Traggerüst wird dann mit dem Matrixmaterial homogen verschmolzen.When using the method mentioned, it is advantageous to insert it into the casting drum before casting to introduce a framework covered with fiber material and consisting of matrix material. This allows the fibers arranged in the later stress curve corresponding patterns and during the . Approaching the casting drum held in its position until centrifugal force and liquid matrix material prevent the fibers from slipping; the supporting structure then becomes homogeneous with the matrix material merged.
Claims (1)
lenstoff oder ^a) The inner layer consists essentially of metal, in particular of alloys based on nickel, titanium, cobalt or aluminum, "" - sen requirements
lenstoff or ^
Priority Applications (13)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2118848A DE2118848C3 (en) | 1971-04-19 | 1971-04-19 | Rotationally symmetric, hollow composite body and process for its manufacture |
AT313772A AT323915B (en) | 1971-04-19 | 1972-04-11 | ROTARY, HOLLOW COMPOSITE BODY AND PROCESS FOR ITS MANUFACTURING |
DK186472A DK141355C (en) | 1971-04-19 | 1972-04-17 | Rotationally symmetrical, hollow, fiber-reinforced composite bodies and methods of manufacture thereof |
BE782239A BE782239A (en) | 1971-04-19 | 1972-04-17 | METHOD AND DEVICE FOR MANUFACTURING A SYMMETRICAL COMPOSITE ENROTATION ELEMENT |
NO1340/72A NO130892C (en) | 1971-04-19 | 1972-04-18 | |
CH572072A CH566831A5 (en) | 1971-04-19 | 1972-04-18 | |
NL7205164.A NL162003C (en) | 1971-04-19 | 1972-04-18 | ROTATION SYMMETRICAL HOLLOW COMPOSITE BODY AND METHOD FOR MANUFACTURING SUCH BODY. |
FR7213593A FR2133852B1 (en) | 1971-04-19 | 1972-04-18 | |
JP3950072A JPS5516750B1 (en) | 1971-04-19 | 1972-04-19 | |
FI1103/72A FI52939C (en) | 1971-04-19 | 1972-04-19 | |
SE7205126A SE387874B (en) | 1971-04-19 | 1972-04-19 | ROTATION SYMMETRIC HOLY COMPOSITE BODY AND SET FOR ITS PREPARATION |
US00245575A US3849080A (en) | 1971-04-19 | 1972-04-19 | Rotationally symmetrical hollow compound body |
GB1821872A GB1393989A (en) | 1971-04-19 | 1972-04-19 | Methods of manufacturing rotationally symmetrical hollow composite bodies |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2118848A DE2118848C3 (en) | 1971-04-19 | 1971-04-19 | Rotationally symmetric, hollow composite body and process for its manufacture |
Publications (3)
Publication Number | Publication Date |
---|---|
DE2118848A1 DE2118848A1 (en) | 1972-11-02 |
DE2118848B2 DE2118848B2 (en) | 1973-06-20 |
DE2118848C3 true DE2118848C3 (en) | 1974-01-17 |
Family
ID=5805092
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE2118848A Expired DE2118848C3 (en) | 1971-04-19 | 1971-04-19 | Rotationally symmetric, hollow composite body and process for its manufacture |
Country Status (13)
Country | Link |
---|---|
US (1) | US3849080A (en) |
JP (1) | JPS5516750B1 (en) |
AT (1) | AT323915B (en) |
BE (1) | BE782239A (en) |
CH (1) | CH566831A5 (en) |
DE (1) | DE2118848C3 (en) |
DK (1) | DK141355C (en) |
FI (1) | FI52939C (en) |
FR (1) | FR2133852B1 (en) |
GB (1) | GB1393989A (en) |
NL (1) | NL162003C (en) |
NO (1) | NO130892C (en) |
SE (1) | SE387874B (en) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2523074A1 (en) * | 1975-05-24 | 1976-12-02 | Christensen Diamond Prod Co | PROCESS AND EQUIPMENT FOR MANUFACTURING WEAR-RESISTANT BODIES, IN PARTICULAR FOR DEEP DRILLING TECHNOLOGY |
JPS5292827A (en) * | 1976-01-16 | 1977-08-04 | Honda Motor Co Ltd | Method of manufacturing structures with fiber reinforced composite parts |
DE2929217A1 (en) * | 1979-07-19 | 1983-12-01 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | ROTATION-SYMMETRICAL HOLLOW COMPOSITE BODY |
JPS5630070A (en) * | 1979-08-17 | 1981-03-26 | Honda Motor Co Ltd | Manufacture of fiber-reinforced composite material |
US4258756A (en) * | 1979-08-27 | 1981-03-31 | Allied Chemical Corporation | Composite shell |
US4834693A (en) * | 1980-06-26 | 1989-05-30 | Avco Corporation | Hybrid drive shaft |
AU554140B2 (en) * | 1980-07-02 | 1986-08-07 | Dana Corporation | Thermally insulating coating on piston head |
JPS5893813U (en) * | 1981-12-18 | 1983-06-25 | トキコ株式会社 | turbine meter |
DE3478035D1 (en) * | 1984-01-27 | 1989-06-08 | Chugai Ro Kogyo Kaisha Ltd | Fiber reinforced metal alloy and method for the manufacture thereof |
GB8518909D0 (en) * | 1985-07-26 | 1985-09-04 | Ae Plc | Engineering components |
US4816347A (en) * | 1987-05-29 | 1989-03-28 | Avco Lycoming/Subsidiary Of Textron, Inc. | Hybrid titanium alloy matrix composites |
GB2222793A (en) * | 1988-09-16 | 1990-03-21 | British Aerospace | "Method of forming a fibre reinforced material" |
JP3179812B2 (en) * | 1991-09-17 | 2001-06-25 | トーカロ株式会社 | Carbon member having metal spray coating layer with excellent adhesion |
GB9413631D0 (en) * | 1994-07-06 | 1994-09-14 | Inco Engineered Prod Ltd | Manufacture of forged components |
JP3650183B2 (en) * | 1995-10-13 | 2005-05-18 | 栃木富士産業株式会社 | Screw rotor processing method |
DE19737601A1 (en) * | 1997-08-28 | 1999-03-04 | Bayerische Motoren Werke Ag | Process for increasing the damping of a cast component made of a light metal material |
EP1297400A4 (en) * | 2000-06-27 | 2005-02-16 | Univ Leland Stanford Junior | Composite rotors for flywheels and methods of fabrication thereof |
WO2002058917A2 (en) * | 2001-01-23 | 2002-08-01 | The Johns Hopkins University | Use of a liquid during centrifugal processing to improve consolidation of a composite structure |
GB201223198D0 (en) * | 2012-12-21 | 2013-02-06 | Jaguar Cars | Sleeve member and method of casting |
CN109203508A (en) * | 2018-08-29 | 2019-01-15 | 江苏赛图新材料科技有限公司 | Horizontal centrifugal forming device and forming process for fiber tube |
US11510283B2 (en) * | 2019-05-14 | 2022-11-22 | Intel Corporation | WLAN sensing using high-efficiency (HE) trigger- based (TB) PPDUs (HE TB PPDUs) |
CN112246586B (en) * | 2020-09-28 | 2023-03-10 | 镇江经纬输送装备有限公司 | Process for uniformly pouring polyurethane on inner wall of chute |
CN113400542B (en) * | 2021-07-20 | 2022-11-25 | 南通天木绝缘复合材料有限公司 | Make things convenient for glass steel grating production of raw materials flash mixed with centrifugal pouring device |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1280909A (en) * | 1916-02-05 | 1918-10-08 | Metalco Company | Manufacture of pipes. |
US2197916A (en) * | 1937-01-27 | 1940-04-23 | Detroit Gasket & Mfg Company | Gasket |
US3427185A (en) * | 1964-02-19 | 1969-02-11 | United Aircraft Corp | Composite structural material incorporating metallic filaments in a matrix,and method of manufacture |
US3419952A (en) * | 1966-09-12 | 1969-01-07 | Gen Electric | Method for making composite material |
NL6912700A (en) * | 1968-08-22 | 1970-02-24 | ||
US3575783A (en) * | 1968-11-13 | 1971-04-20 | United Aircraft Corp | Unidirectional fiber reinforced metal matrix tape |
US3608170A (en) * | 1969-04-14 | 1971-09-28 | Abex Corp | Metal impregnated composite casting method |
-
1971
- 1971-04-19 DE DE2118848A patent/DE2118848C3/en not_active Expired
-
1972
- 1972-04-11 AT AT313772A patent/AT323915B/en not_active IP Right Cessation
- 1972-04-17 DK DK186472A patent/DK141355C/en active
- 1972-04-17 BE BE782239A patent/BE782239A/en unknown
- 1972-04-18 CH CH572072A patent/CH566831A5/xx not_active IP Right Cessation
- 1972-04-18 FR FR7213593A patent/FR2133852B1/fr not_active Expired
- 1972-04-18 NL NL7205164.A patent/NL162003C/en not_active IP Right Cessation
- 1972-04-18 NO NO1340/72A patent/NO130892C/no unknown
- 1972-04-19 JP JP3950072A patent/JPS5516750B1/ja active Pending
- 1972-04-19 SE SE7205126A patent/SE387874B/en unknown
- 1972-04-19 US US00245575A patent/US3849080A/en not_active Expired - Lifetime
- 1972-04-19 FI FI1103/72A patent/FI52939C/fi active
- 1972-04-19 GB GB1821872A patent/GB1393989A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB1393989A (en) | 1975-05-14 |
FI52939B (en) | 1977-09-30 |
NL162003B (en) | 1979-11-15 |
NO130892B (en) | 1974-11-25 |
BE782239A (en) | 1972-08-16 |
SE387874B (en) | 1976-09-20 |
NO130892C (en) | 1975-03-05 |
CH566831A5 (en) | 1975-09-30 |
DK141355B (en) | 1980-03-03 |
JPS5516750B1 (en) | 1980-05-06 |
DK141355C (en) | 1980-08-18 |
US3849080A (en) | 1974-11-19 |
DE2118848A1 (en) | 1972-11-02 |
FR2133852B1 (en) | 1976-10-29 |
AT323915B (en) | 1975-08-11 |
NL162003C (en) | 1980-04-15 |
FR2133852A1 (en) | 1972-12-01 |
FI52939C (en) | 1978-01-10 |
DE2118848B2 (en) | 1973-06-20 |
NL7205164A (en) | 1972-10-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C3 | Grant after two publication steps (3rd publication) | ||
E77 | Valid patent as to the heymanns-index 1977 | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: M.A.N. MASCHINENFABRIK AUGSBURG-NUERNBERG AG, 8000 |
|
8339 | Ceased/non-payment of the annual fee |