DE2118848C3 - Rotationally symmetric, hollow composite body and process for its manufacture - Google Patents

Rotationally symmetric, hollow composite body and process for its manufacture

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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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DE
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.)
Expired
Application number
DE2118848A
Other languages
German (de)
Other versions
DE2118848A1 (en
DE2118848B2 (en
Inventor
Hartwin Dipl.-Ing. 8000 Muenchen Zechmeister
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MAN AG
Original Assignee
MAN Maschinenfabrik Augsburg Nuernberg AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by MAN Maschinenfabrik Augsburg Nuernberg AG filed Critical MAN Maschinenfabrik Augsburg Nuernberg AG
Priority to DE2118848A priority Critical patent/DE2118848C3/en
Priority to AT313772A priority patent/AT323915B/en
Priority to BE782239A priority patent/BE782239A/en
Priority to DK186472A priority patent/DK141355C/en
Priority to NL7205164.A priority patent/NL162003C/en
Priority to FR7213593A priority patent/FR2133852B1/fr
Priority to CH572072A priority patent/CH566831A5/xx
Priority to NO1340/72A priority patent/NO130892C/no
Priority to SE7205126A priority patent/SE387874B/en
Priority to JP3950072A priority patent/JPS5516750B1/ja
Priority to FI1103/72A priority patent/FI52939C/fi
Priority to US00245575A priority patent/US3849080A/en
Priority to GB1821872A priority patent/GB1393989A/en
Publication of DE2118848A1 publication Critical patent/DE2118848A1/en
Publication of DE2118848B2 publication Critical patent/DE2118848B2/en
Application granted granted Critical
Publication of DE2118848C3 publication Critical patent/DE2118848C3/en
Expired legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C41/00Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
    • B29C41/02Shaping 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
    • B29C41/04Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould
    • B29C41/042Rotational or centrifugal casting, i.e. coating the inside of a mould by rotating the mould by rotating a mould around its axis of symmetry
    • B29C41/045Rotational 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D13/00Centrifugal casting; Casting by using centrifugal force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/02Casting in, on, or around objects which form part of the product for making reinforced articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping 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
    • B29C70/32Shaping 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
    • B29C70/323Shaping 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
    • B29C70/326Shaping 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
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12333Helical or with helical component
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12444Embodying fibers interengaged or between layers [e.g., paper, etc.]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12465All metal or with adjacent metals having magnetic properties, or preformed fiber orientation coordinate with shape
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12486Laterally noncoextensive components [e.g., embedded, etc.]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12736Al-base component
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12778Alternative 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. , uWVSrner 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«eT 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 "eT 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)

Patcntansprüche:Patent claims: 1 Rotationssymmetrischer, hohler Verbundkörper, bestehend aus zwei ebenfalls rotationssymmetrischen, ineinander angeordneten fugenlos ineinander übergehenden Schichten, gekennzeichnet durch die Kombination folgender Merkmale:1 rotationally symmetrical, hollow composite body, consisting of two rotationally symmetrical, layers arranged one inside the other, seamlessly merging into one another, marked by combining the following features: a) Die innere Schicht besteht im wesentlichen aus Metall, insbesondere aus Legierungen auf Nickel-, Titan-, Kobalt- oder Alum,«»- sen Anforderungen
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 ^
DE2118848A 1971-04-19 1971-04-19 Rotationally symmetric, hollow composite body and process for its manufacture Expired DE2118848C3 (en)

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

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DE2118848A Expired DE2118848C3 (en) 1971-04-19 1971-04-19 Rotationally symmetric, hollow composite body and process for its manufacture

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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)

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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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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