US20020023335A1 - Method for producing a bending-resistant, elongated body and an arrangement for a bending-resistant, elongated body - Google Patents
Method for producing a bending-resistant, elongated body and an arrangement for a bending-resistant, elongated body Download PDFInfo
- Publication number
- US20020023335A1 US20020023335A1 US09/445,450 US44545000A US2002023335A1 US 20020023335 A1 US20020023335 A1 US 20020023335A1 US 44545000 A US44545000 A US 44545000A US 2002023335 A1 US2002023335 A1 US 2002023335A1
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- Prior art keywords
- cavity
- elongated
- fibre composite
- cavities
- composite body
- Prior art date
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Links
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- 239000005011 phenolic resin Substances 0.000 claims description 3
- 229920000647 polyepoxide Polymers 0.000 claims description 3
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Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C13/00—Rolls, drums, discs, or the like; Bearings or mountings therefor
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H27/00—Special constructions, e.g. surface features, of feed or guide rollers for webs
-
- D—TEXTILES; PAPER
- D21—PAPER-MAKING; PRODUCTION OF CELLULOSE
- D21F—PAPER-MAKING MACHINES; METHODS OF PRODUCING PAPER THEREON
- D21F1/00—Wet end of machines for making continuous webs of paper
- D21F1/36—Guiding mechanisms
- D21F1/40—Rolls
-
- D—TEXTILES; PAPER
- D21—PAPER-MAKING; PRODUCTION OF CELLULOSE
- D21G—CALENDERS; ACCESSORIES FOR PAPER-MAKING MACHINES
- D21G1/00—Calenders; Smoothing apparatus
- D21G1/02—Rolls; Their bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/02—Shafts; Axles
- F16C3/026—Shafts made of fibre reinforced resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2401/00—Materials used for the handling apparatus or parts thereof; Properties thereof
- B65H2401/10—Materials
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2404/00—Parts for transporting or guiding the handled material
- B65H2404/10—Rollers
- B65H2404/11—Details of cross-section or profile
- B65H2404/111—Details of cross-section or profile shape
- B65H2404/1116—Polygonal cross-section
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2404/00—Parts for transporting or guiding the handled material
- B65H2404/10—Rollers
- B65H2404/11—Details of cross-section or profile
- B65H2404/115—Details of cross-section or profile other
- B65H2404/1152—Markings, patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2404/00—Parts for transporting or guiding the handled material
- B65H2404/10—Rollers
- B65H2404/13—Details of longitudinal profile
- B65H2404/137—Means for varying longitudinal profiles
- B65H2404/1372—Means for varying longitudinal profiles anti-deflection
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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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49622—Vehicular structural member making
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49623—Static structure, e.g., a building component
- Y10T29/49634—Beam or girder
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49716—Converting
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49801—Shaping fiber or fibered material
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49863—Assembling or joining with prestressing of part
- Y10T29/49865—Assembling or joining with prestressing of part by temperature differential [e.g., shrink fit]
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49885—Assembling or joining with coating before or during assembling
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49906—Metal deforming with nonmetallic bonding
Definitions
- the present invention relates to a method for producing a bending-resistant, elongated body, preferably a shaft or beam, as indicated in the preamble to claim 1 .
- the invention also relates to an arrangement for a bending-resistant, elongated body, preferably a shaft or beam, as indicated in the preamble to claim 7 .
- shafts which serve inter alia as spindles for carrying paper reels.
- These are now often manufactured as homogeneous or tubular aluminium or steel shafts, possibly with longitudinal circumferential recesses for air-activated clamping segments or the like. It is understood that a shaft of this kind can have a relatively great mass even in the case of comparatively short lengths, especially if the shaft is to carry large loads.
- a shaft of this kind can also come to produce natural frequencies in the speed range which is relevant for this type of application and by doing so possibly limit the velocity of the paper web.
- One aim of the present invention is therefore to provide a method for producing a bending-resistant, elongated body, preferably a shaft or beam, and an arrangement for a bending-resistant, elongated body, which method and which arrangement contribute to eliminating or at any rate reducing the aforementioned problems.
- a method is achieved for producing a bending-resistant, elongated body, preferably a shaft or beam, as indicated in claim 1 .
- a bending-resistant, elongated body can be produced, preferably a lightweight shaft or beam, the bending resistance of which is considerably increased and the natural frequency of which can be adapted to the current application.
- FIG. 1 shows a first embodiment of a bending-resistant, elongated body according to the invention in the form of a shaft, in a section at right angles to its longitudinal axis.
- FIG. 2 shows a second embodiment of a bending-resistant, elongated body according to the invention in the form of a beam, in a section at right angles to its longitudinal axis.
- FIG. 1, 1 generally describes a bending-resistant, elongated body in the form of a circular shaft of the type which is suitable as a spindle in a paper making machine or the like, for example.
- the circular shaft 1 has a number of circular cavities 2 , 2 a, extending essentially along the whole of its length, the inner surfaces of which, in a section at right angles to its longitudinal axis, are at a distance from the mass centre of the section.
- One of these cavities 2 a is arranged concentrically around the mass centre of the section. In comparison with a homogeneous metal shaft, for example, the cavities considerably reduce the weight of the shaft.
- Fibre composite bodies 3 , 3 a are applied to the cavities 2 , 2 a, preferably by gluing, which bodies have outer surfaces essentially congruent with the inner surfaces of the cavities 2 , 2 a, which outer surfaces due to the affixing are joined to the inner surfaces of the cavities by affixing.
- the fibre composite bodies 3 , 3 a may be homogeneous, as in the cavities 2 lying circumferentially, or tubular, like the fibre composite body 3 a, which is affixed in the hollow 2 a arranged concentrically with the mass centre.
- the majority of the fibres in the fibre composite bodies 3 , 3 a extend essentially parallel to the longitudinal axis of the shaft 1 and are elongated along the whole of its length.
- the fibre composite bodies 3 , 3 a consist preferably of carbon fibre in an epoxide matrix, but other fibres and matrices with similar properties are naturally conceivable.
- an epoxy-, acrylic-, polyurethane- or phenolic-resin based adhesive is used for gluing.
- FIG. 2 1 generally describes a bending-resistant, elongated body in the form of a rectangular beam.
- the rectangular beam 1 has a number of cavities 2 , 2 a extending essentially along its entire length, the inner surfaces of which cavities, in a section at right angles to its longitudinal axis, are at a distance from its mass centre.
- one of these cavities 2 a is arranged concentrically around the mass centre.
- the cavities 2 , 2 a as in the embodiment according to FIG.
- fibre composite bodies 3 , 3 a are affixed, preferably by gluing, which bodies have outer surfaces essentially congruent with the inner surfaces of the cavities, which outer surfaces are joined by affixing to the inner surfaces of the cavities
- the fibre composite bodies 3 , 3 a in all cavities are homogeneous in this embodiment.
- the majority of the fibres extend essentially parallel to the longitudinal axis of the elongated body and are elongated along the whole of its length.
- Bending-resistant, lightweight shafts and beams of an arbitrary cross-section can be produced by the invention
- the bending resistance of these can be increased by arranging the inner surfaces of the cavities 2 , 2 a connecting to the outer surfaces of the fibre composite bodies 3 , 3 a at a greater distance from the mass centre and reduced in the reverse manner, seen in a section at right angles to the longitudinal axis of the shaft/beam.
- the above may also be utilized to give the shafts/beams according to the invention the desired natural frequency.
- the cavities 2 , 2 a In the case of rotating shafts, it is normally suitable for the cavities 2 , 2 a to be arranged with an equal pitch, symmetrically around the mass centre of the shaft seen in a section at right angles to its longitudinal axis, while in the case of a beam, varying bending resistance in different directions can be achieved through asymmetrical positioning of the cavities 2 , 2 a. Due to the fact that the fibre composite bodies 3 , 3 a are normally of a lower density than the material which is used for the elongated body, a basic reduction in weight is achieved compared with a homogeneous body of the same dimensions. To reduce the weight further, it is possible for certain applications to arrange further cavities 2 , 2 a, in which fibre composite bodies 3 , 3 a are not arranged.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
- Rod-Shaped Construction Members (AREA)
- Shaping Of Tube Ends By Bending Or Straightening (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Paper (AREA)
Abstract
The present invention comprises a method for producing a bending-resistant, elongated body (1), preferably a shaft or beam. The invention is characterized in that an elongated blank is produced having at least one cavity (2, 2 a) extending essentially along the entire length of the blank, the inner surface of which cavity is at a distance from the mass center of the blank seen in a section at right angles to its longitudinal axis and that affixed in the cavity (2, 2 a) is a fiber composite body (3, 3 a) with an outer surface essentially congruent with the inner surface of the cavity and that the majority of the fibers in the fiber composite body (3, 3 a) both extend essentially parallel to the longitudinal axis of the elongated blank and are elongated along the whole of its length. The invention also relates to an arrangement produced according to the method.
Description
- The present invention relates to a method for producing a bending-resistant, elongated body, preferably a shaft or beam, as indicated in the preamble to claim 1.
- The invention also relates to an arrangement for a bending-resistant, elongated body, preferably a shaft or beam, as indicated in the preamble to claim 7.
- On paper making machines, for example, relatively long shafts occur, which serve inter alia as spindles for carrying paper reels. These are now often manufactured as homogeneous or tubular aluminium or steel shafts, possibly with longitudinal circumferential recesses for air-activated clamping segments or the like. It is understood that a shaft of this kind can have a relatively great mass even in the case of comparatively short lengths, especially if the shaft is to carry large loads. On rotation, a shaft of this kind can also come to produce natural frequencies in the speed range which is relevant for this type of application and by doing so possibly limit the velocity of the paper web. In addition, these shafts must often be handled manually when exchanging reels or the like, which means risking coming into conflict with working environment requirements imposed with regard to lifting heavy objects. In the case of large lengths and high stresses, it can also be difficult to obtain sufficient bending resistance with shafts produced according to the prior art
- One aim of the present invention is therefore to provide a method for producing a bending-resistant, elongated body, preferably a shaft or beam, and an arrangement for a bending-resistant, elongated body, which method and which arrangement contribute to eliminating or at any rate reducing the aforementioned problems.
- According to an embodiment of the present invention, a method is achieved for producing a bending-resistant, elongated body, preferably a shaft or beam, as indicated in
claim 1. - An arrangement for a bending-resistant, elongated body, preferably a shaft or beam, as indicated in claim 7, is also achieved according to the present invention.
- Preferred embodiments of the method or arrangement have in addition one or some of the features indicated in the respective sub-claims.
- The method or arrangement according to the invention have several advantages. By means of the method according to the invention, a bending-resistant, elongated body can be produced, preferably a lightweight shaft or beam, the bending resistance of which is considerably increased and the natural frequency of which can be adapted to the current application.
- The invention is to be explained in greater detail below by way of examples of embodiments of the invention and the arrangement and with reference to the enclosed drawings.
- FIG. 1 shows a first embodiment of a bending-resistant, elongated body according to the invention in the form of a shaft, in a section at right angles to its longitudinal axis.
- FIG. 2 shows a second embodiment of a bending-resistant, elongated body according to the invention in the form of a beam, in a section at right angles to its longitudinal axis.
- In FIG. 1, 1 generally describes a bending-resistant, elongated body in the form of a circular shaft of the type which is suitable as a spindle in a paper making machine or the like, for example. The
circular shaft 1 has a number of 2, 2 a, extending essentially along the whole of its length, the inner surfaces of which, in a section at right angles to its longitudinal axis, are at a distance from the mass centre of the section. One of thesecircular cavities cavities 2 a is arranged concentrically around the mass centre of the section. In comparison with a homogeneous metal shaft, for example, the cavities considerably reduce the weight of the shaft. 3, 3 a are applied to theFibre composite bodies 2, 2 a, preferably by gluing, which bodies have outer surfaces essentially congruent with the inner surfaces of thecavities 2, 2 a, which outer surfaces due to the affixing are joined to the inner surfaces of the cavities by affixing. Thecavities 3, 3 a may be homogeneous, as in thefibre composite bodies cavities 2 lying circumferentially, or tubular, like the fibrecomposite body 3 a, which is affixed in thehollow 2 a arranged concentrically with the mass centre. The majority of the fibres in the 3, 3 a extend essentially parallel to the longitudinal axis of thefibre composite bodies shaft 1 and are elongated along the whole of its length. - The
3, 3 a consist preferably of carbon fibre in an epoxide matrix, but other fibres and matrices with similar properties are naturally conceivable. For gluing, an epoxy-, acrylic-, polyurethane- or phenolic-resin based adhesive is used.fibre composite bodies - When manufacturing the shaft according to FIG. 1, one starts by producing a elongated shaft blank with the
2, 2 a extending essentially along the entire length of thecavities shaft 1. A fibre 3, 3 a, with an outer surface essentially congruent with the inner surface of the cavity is then fitted into eachcomposite body 2, 2 a. The majority of the fibres in the fibrecavity 3, 3 a should hereby be oriented essentially parallel to the longitudinal axis of the elongated shaft blank and such that they are elongated along the whole of its length.composite body - In FIG. 2, 1 generally describes a bending-resistant, elongated body in the form of a rectangular beam. Like the shaft according to FIG. 1, the
rectangular beam 1 has a number of 2, 2 a extending essentially along its entire length, the inner surfaces of which cavities, in a section at right angles to its longitudinal axis, are at a distance from its mass centre. As in the previous embodiment, one of thesecavities cavities 2 a is arranged concentrically around the mass centre. In the 2, 2 a, as in the embodiment according to FIG. 1,cavities 3, 3 a are affixed, preferably by gluing, which bodies have outer surfaces essentially congruent with the inner surfaces of the cavities, which outer surfaces are joined by affixing to the inner surfaces of the cavities The fibrefibre composite bodies 3, 3 a in all cavities are homogeneous in this embodiment. Here also the majority of the fibres extend essentially parallel to the longitudinal axis of the elongated body and are elongated along the whole of its length.composite bodies - The production of the beam 1 a according to FIG. 2 is performed in a corresponding manner to that for the
shaft 1 according to FIG. 1. - Bending-resistant, lightweight shafts and beams of an arbitrary cross-section can be produced by the invention The bending resistance of these can be increased by arranging the inner surfaces of the
2, 2 a connecting to the outer surfaces of the fibrecavities 3, 3 a at a greater distance from the mass centre and reduced in the reverse manner, seen in a section at right angles to the longitudinal axis of the shaft/beam. The above may also be utilized to give the shafts/beams according to the invention the desired natural frequency. In the case of rotating shafts, it is normally suitable for thecomposite bodies 2, 2 a to be arranged with an equal pitch, symmetrically around the mass centre of the shaft seen in a section at right angles to its longitudinal axis, while in the case of a beam, varying bending resistance in different directions can be achieved through asymmetrical positioning of thecavities 2, 2 a. Due to the fact that thecavities 3, 3 a are normally of a lower density than the material which is used for the elongated body, a basic reduction in weight is achieved compared with a homogeneous body of the same dimensions. To reduce the weight further, it is possible for certain applications to arrangefibre composite bodies 2, 2 a, in whichfurther cavities 3, 3 a are not arranged.fibre composite bodies - It is evident to a man skilled in the art that the invention is not restricted to the embodiments described above, but that it can instead undergo modifications in the scope of the inventive idea defined in the following patent claims. For example, in the case of the embodiments according to FIG. 1 or FIG. 2 it is possible to arrange the fibre
3, 3 a solely in thecomposite bodies cavities 2 lying circumferentially or alternatively only in thehollows 2 a executed concentrically with the mass centre. It is understood also that the 2, 2 a can have an arbitrary cross-section and that the fibre composite bodies can be affixed in the cavities by shrinking.cavities
Claims (13)
1. Method of producing a bending-resistant, elongated body (1), preferably a shaft or beam, characterized in that an elongated blank is produced having a number of cavities (2, 2 a) extending essentially along the entire length of the blank, the inner surface of which cavity is at a distance from the mass centre of the blank seen in a section at right angles to its longitudinal axis and that in a number of the cavities (2, 2 a) a fibre composite body (3, 3 a) is affixed with an outer surface essentially congruent with the inner surface of the cavity, and that the majority of the fibres in the fibre composite body (3, 3 a) both extend essentially parallel to the longitudinal axis of the elongated blank and are elongated along the whole of its length.
2. Method according to claim 1 , characterized in that the fibre composite body (3, 3 a) is affixed in the cavity (2, 2 a) by gluing.
3. Method according to claim 1 , characterized in that the fibre composite body (3, 3 a) is affixed in the cavity (2, 2 a) by shrinking.
4. Method according to claim 2 , characterized in that an epoxy-, acrylic-, polyurethane- or phenolic-resin-based adhesive is used for gluing.
5. Method according to any of the preceding claims, characterized in that fibre material in a plastic matrix, preferably carbon fibre in an epoxide matrix, is used as a fibre composite body (3, 3 a).
6. Method according to any of the preceding claims, characterized in that the blank is provided with a number of longitudinal cavities (2, 2 a), which are arranged with equal pitch, symmetrically around the mass centre of the blank seen in a section at right angles to its longitudinal axis.
7. Arrangement for a bending-resistant, elongated body (1), preferably a shaft or beam, characterized in that the elongated body (1) has a number of cavities (2, 2 a) extending essentially along the whole of its length, the inner surface of which cavity is at a distance from the body's mass centre seen in a section at right angles to its longitudinal axis and that affixed in a number ofthe cavities (2, 2 a) is a fibre composite body (3, 3 a) with an outer surface which is essentially congruent with the inner surface of the cavity, and that the majority of the fibres in the fibre composite body (3, 3 a) both extend essentially parallel to the longitudinal axis of the elongated body and are elongated along the whole of its length.
8. Arrangement according to claim 7 , characterized in that the fibre composite body (3, 3 a) consists of fibre material in a plastic matrix, preferably carbon fibre in an epoxide matrix.
9. Arrangement according to claim 7 or 8, characterized in that the outer surface of the fibre composite body is joined to the inner surface of the cavity by means of an adhesive.
10. Arrangement according to claim 9 , characterized in that the adhesive is epoxy-, acrylic-, polyurethane- or phenolic-resin-based.
11. Arrangement according to claim 7 or 8, characterized in that the outer surface of the fibre composite body is joined to the inner surface of the cavity by shrinking.
12. Arrangement according to any of the preceding claims, characterized in that the elongated body (1) with longitudinal cavities comprises an injection moulded profile beam or a tube.
13. Arrangement according to any of the preceding claims, characterized in that the elongated body (1) has a number of longitudinal cavities (2, 2 a) distributed with an equal pitch symmetrically around its mass centre seen in a section at right angles to its longitudinal axis.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/055,897 US6854171B2 (en) | 1997-06-16 | 2002-01-28 | Method for producing a bending-resistant, elongated body |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE9702284-2 | 1997-06-16 | ||
| SE9702284A SE511439C2 (en) | 1997-06-16 | 1997-06-16 | Method for providing a bending stiff, elongated body and a device for a bending stiff, elongated body |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/SE1998/001144 A-371-Of-International WO1998058182A1 (en) | 1997-06-16 | 1998-06-15 | Method for producing a bending-resistant, elongated body and an arrangement for a bending-resistant, elongated body |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/055,897 Continuation US6854171B2 (en) | 1997-06-16 | 2002-01-28 | Method for producing a bending-resistant, elongated body |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20020023335A1 true US20020023335A1 (en) | 2002-02-28 |
Family
ID=20407391
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US09/445,450 Abandoned US20020023335A1 (en) | 1997-06-16 | 1998-06-15 | Method for producing a bending-resistant, elongated body and an arrangement for a bending-resistant, elongated body |
| US10/055,897 Expired - Fee Related US6854171B2 (en) | 1997-06-16 | 2002-01-28 | Method for producing a bending-resistant, elongated body |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/055,897 Expired - Fee Related US6854171B2 (en) | 1997-06-16 | 2002-01-28 | Method for producing a bending-resistant, elongated body |
Country Status (8)
| Country | Link |
|---|---|
| US (2) | US20020023335A1 (en) |
| EP (1) | EP1027544B1 (en) |
| JP (1) | JP2002503325A (en) |
| CN (1) | CN1101898C (en) |
| AU (1) | AU7947898A (en) |
| DE (1) | DE69833374T2 (en) |
| SE (1) | SE511439C2 (en) |
| WO (1) | WO1998058182A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100166568A1 (en) * | 2006-08-17 | 2010-07-01 | Lin Sherman S | Composite-Steel Hybrid Mast for Rotorcraft |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6234912B1 (en) * | 1999-09-07 | 2001-05-22 | General Electric Company | High-stiffness composite shaft |
| WO2003051632A1 (en) * | 2001-12-19 | 2003-06-26 | Gallus Ferd. Rüesch AG | Pressure cylinder in the form of a hollow cylinder made of metal |
| FR2882421A1 (en) * | 2005-02-22 | 2006-08-25 | Freyssinet Internat Stup Soc P | METHOD FOR REINFORCING A METAL TUBULAR STRUCTURE AND RESULTING STRUCTURE |
| US20070117640A1 (en) * | 2005-11-21 | 2007-05-24 | Haka Raymond J | Composite clutch shaft assembly |
| US20080148708A1 (en) * | 2006-12-20 | 2008-06-26 | General Electric Company | Turbine engine system with shafts for improved weight and vibration characteristic |
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| US3487518A (en) | 1965-08-12 | 1970-01-06 | Henry Hopfeld | Method for making a reinforced structural member |
| US3508990A (en) * | 1965-10-24 | 1970-04-28 | Owens Corning Fiberglass Corp | Method of producing a multi-element glass cord construction |
| US3419952A (en) | 1966-09-12 | 1969-01-07 | Gen Electric | Method for making composite material |
| US3623203A (en) | 1970-03-24 | 1971-11-30 | Avco Corp | Reinforced structural members and method of making same |
| US3699623A (en) | 1970-10-20 | 1972-10-24 | United Aircraft Corp | Method for fabricating corrosion resistant composites |
| US3945555A (en) | 1972-05-24 | 1976-03-23 | The United States Of America As Represented By The Secretary Of The Navy | Production of beryllium reinforced composite solid and hollow shafting |
| US3820212A (en) * | 1972-10-05 | 1974-06-28 | United States Steel Corp | Method of forming composite rolls |
| US3942231A (en) | 1973-10-31 | 1976-03-09 | Trw Inc. | Contour formed metal matrix blade plies |
| US3889579A (en) * | 1974-01-07 | 1975-06-17 | Poly Trusions Inc | Oil well pumping system having reinforced plastic sucker rod |
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| US3953637A (en) * | 1974-10-31 | 1976-04-27 | United Technologies Corporation | Slender rod for fishing rods and method of making the same |
| CH602330A5 (en) | 1976-08-26 | 1978-07-31 | Bbc Brown Boveri & Cie | |
| US4111606A (en) | 1976-12-27 | 1978-09-05 | United Technologies Corporation | Composite rotor blade |
| GB1592310A (en) * | 1978-04-17 | 1981-07-01 | Asahi Dow Ltd | Glass fibre reinforced thermoplastic resin moulding material |
| GB2059546A (en) * | 1979-09-08 | 1981-04-23 | Advanced Composite Componenets | Lined Hollow Shafts |
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| CH666332A5 (en) * | 1984-02-28 | 1988-07-15 | Sigri Gmbh | Metal clad synthetic resin roller |
| NO850361L (en) * | 1985-01-30 | 1986-07-31 | Raufoss Ammunisjonsfabrikker | SHAFT OR STAG. |
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| US4841613A (en) * | 1987-06-15 | 1989-06-27 | The Mead Corporation | Pressure developer or press having a pressure roll containing composite material |
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| US5576081A (en) * | 1987-12-28 | 1996-11-19 | Sandt; Hartley | Composite structural element and process for making same |
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| US5411463A (en) * | 1993-10-13 | 1995-05-02 | Albany International Corp. | Composite roll and method of making |
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-
1997
- 1997-06-16 SE SE9702284A patent/SE511439C2/en unknown
-
1998
- 1998-06-15 US US09/445,450 patent/US20020023335A1/en not_active Abandoned
- 1998-06-15 JP JP50428399A patent/JP2002503325A/en active Pending
- 1998-06-15 WO PCT/SE1998/001144 patent/WO1998058182A1/en not_active Ceased
- 1998-06-15 AU AU79478/98A patent/AU7947898A/en not_active Abandoned
- 1998-06-15 EP EP98929990A patent/EP1027544B1/en not_active Expired - Lifetime
- 1998-06-15 CN CN98806288A patent/CN1101898C/en not_active Expired - Fee Related
- 1998-06-15 DE DE69833374T patent/DE69833374T2/en not_active Expired - Fee Related
-
2002
- 2002-01-28 US US10/055,897 patent/US6854171B2/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100166568A1 (en) * | 2006-08-17 | 2010-07-01 | Lin Sherman S | Composite-Steel Hybrid Mast for Rotorcraft |
| US7938628B2 (en) | 2006-08-17 | 2011-05-10 | Bell Helicopter Textron Inc. | Composite-steel hybrid mast for rotorcraft |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1027544A1 (en) | 2000-08-16 |
| JP2002503325A (en) | 2002-01-29 |
| US6854171B2 (en) | 2005-02-15 |
| SE9702284L (en) | 1998-12-17 |
| DE69833374D1 (en) | 2006-04-13 |
| AU7947898A (en) | 1999-01-04 |
| CN1101898C (en) | 2003-02-19 |
| CN1260865A (en) | 2000-07-19 |
| EP1027544B1 (en) | 2006-02-01 |
| DE69833374T2 (en) | 2006-09-28 |
| SE511439C2 (en) | 1999-09-27 |
| SE9702284D0 (en) | 1997-06-16 |
| US20020066173A1 (en) | 2002-06-06 |
| WO1998058182A1 (en) | 1998-12-23 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: AMAL AKTIEBOLAG, SWEDEN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:JERVANT, ULF;KROGAGER, MAX;REEL/FRAME:010658/0012;SIGNING DATES FROM 19991130 TO 19991202 |
|
| AS | Assignment |
Owner name: MEGTEC SYSTEMS AMAL AB, SWEDEN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:BALDWIN AMAL AB;REEL/FRAME:012621/0218 Effective date: 20010926 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |