EP2556518B1 - Flyer bow and method for the production thereof - Google Patents
Flyer bow and method for the production thereof Download PDFInfo
- Publication number
- EP2556518B1 EP2556518B1 EP11701763.2A EP11701763A EP2556518B1 EP 2556518 B1 EP2556518 B1 EP 2556518B1 EP 11701763 A EP11701763 A EP 11701763A EP 2556518 B1 EP2556518 B1 EP 2556518B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- cross
- rotor bow
- longitudinal groove
- sectional area
- rotor
- 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.)
- Active
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 16
- 238000000034 method Methods 0.000 title description 4
- 239000000463 material Substances 0.000 claims description 26
- 239000000835 fiber Substances 0.000 claims description 20
- 229920003023 plastic Polymers 0.000 claims description 10
- 239000004033 plastic Substances 0.000 claims description 10
- 239000011248 coating agent Substances 0.000 claims description 7
- 238000000576 coating method Methods 0.000 claims description 7
- 239000007787 solid Substances 0.000 claims description 5
- 229910010293 ceramic material Inorganic materials 0.000 claims description 2
- 239000012783 reinforcing fiber Substances 0.000 description 11
- 239000011159 matrix material Substances 0.000 description 8
- 230000002787 reinforcement Effects 0.000 description 8
- 239000003822 epoxy resin Substances 0.000 description 4
- 229920000647 polyepoxide Polymers 0.000 description 4
- 230000035882 stress Effects 0.000 description 4
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 3
- 238000005452 bending Methods 0.000 description 3
- 239000011151 fibre-reinforced plastic Substances 0.000 description 3
- 239000007769 metal material Substances 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 description 2
- 239000004641 Diallyl-phthalate Substances 0.000 description 2
- 239000004696 Poly ether ether ketone Substances 0.000 description 2
- 239000004697 Polyetherimide Substances 0.000 description 2
- 239000004734 Polyphenylene sulfide Substances 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 238000001746 injection moulding Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 229920001568 phenolic resin Polymers 0.000 description 2
- 229920002492 poly(sulfone) Polymers 0.000 description 2
- 229920002530 polyetherether ketone Polymers 0.000 description 2
- 229920001601 polyetherimide Polymers 0.000 description 2
- 229920000069 polyphenylene sulfide Polymers 0.000 description 2
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 2
- 239000004814 polyurethane Substances 0.000 description 2
- 229920002635 polyurethane Polymers 0.000 description 2
- 229920001187 thermosetting polymer Polymers 0.000 description 2
- 229920006337 unsaturated polyester resin Polymers 0.000 description 2
- 229920001567 vinyl ester resin Polymers 0.000 description 2
- 244000198134 Agave sisalana Species 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 244000025254 Cannabis sativa Species 0.000 description 1
- 235000012766 Cannabis sativa ssp. sativa var. sativa Nutrition 0.000 description 1
- 235000012765 Cannabis sativa ssp. sativa var. spontanea Nutrition 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 240000006240 Linum usitatissimum Species 0.000 description 1
- 235000004431 Linum usitatissimum Nutrition 0.000 description 1
- CERQOIWHTDAKMF-UHFFFAOYSA-M Methacrylate Chemical compound CC(=C)C([O-])=O CERQOIWHTDAKMF-UHFFFAOYSA-M 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- 229920005372 Plexiglas® Polymers 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 229920003180 amino resin Polymers 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- QUDWYFHPNIMBFC-UHFFFAOYSA-N bis(prop-2-enyl) benzene-1,2-dicarboxylate Chemical compound C=CCOC(=O)C1=CC=CC=C1C(=O)OCC=C QUDWYFHPNIMBFC-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 235000009120 camo Nutrition 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 235000005607 chanvre indien Nutrition 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000006355 external stress Effects 0.000 description 1
- 239000003733 fiber-reinforced composite Substances 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 239000011487 hemp Substances 0.000 description 1
- 229910010272 inorganic material Inorganic materials 0.000 description 1
- 239000011147 inorganic material Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 239000011368 organic material Substances 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- -1 polyethylene Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 239000004926 polymethyl methacrylate Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 210000003462 vein Anatomy 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 0.000 description 1
Images
Classifications
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B3/00—General-purpose machines or apparatus for producing twisted ropes or cables from component strands of the same or different material
- D07B3/08—General-purpose machines or apparatus for producing twisted ropes or cables from component strands of the same or different material in which the take-up reel rotates about the axis of the rope or cable or in which a guide member rotates about the axis of the rope or cable to guide the rope or cable on the take-up reel in fixed position and the supply reels are fixed in position
- D07B3/10—General-purpose machines or apparatus for producing twisted ropes or cables from component strands of the same or different material in which the take-up reel rotates about the axis of the rope or cable or in which a guide member rotates about the axis of the rope or cable to guide the rope or cable on the take-up reel in fixed position and the supply reels are fixed in position with provision for imparting more than one complete twist to the ropes or cables for each revolution of the take-up reel or of the guide member
- D07B3/103—General-purpose machines or apparatus for producing twisted ropes or cables from component strands of the same or different material in which the take-up reel rotates about the axis of the rope or cable or in which a guide member rotates about the axis of the rope or cable to guide the rope or cable on the take-up reel in fixed position and the supply reels are fixed in position with provision for imparting more than one complete twist to the ropes or cables for each revolution of the take-up reel or of the guide member characterised by the bow construction
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01H—SPINNING OR TWISTING
- D01H7/00—Spinning or twisting arrangements
- D01H7/02—Spinning or twisting arrangements for imparting permanent twist
- D01H7/24—Flyer or like arrangements
- D01H7/26—Flyer constructions
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B7/00—Details of, or auxiliary devices incorporated in, rope- or cable-making machines; Auxiliary apparatus associated with such machines
- D07B7/02—Machine details; Auxiliary devices
- D07B7/12—Machine details; Auxiliary devices for softening, lubricating or impregnating ropes, cables, or component strands thereof
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B2401/00—Aspects related to the problem to be solved or advantage
- D07B2401/40—Aspects related to the problem to be solved or advantage related to rope making machines
- D07B2401/401—Reducing wear
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B2401/00—Aspects related to the problem to be solved or advantage
- D07B2401/40—Aspects related to the problem to be solved or advantage related to rope making machines
- D07B2401/406—Increasing speed
Definitions
- the present invention relates to a rotor yoke for a machine for processing elongated strand material, wherein the rotor yoke is designed such that it can be rotatably mounted in the machine and wherein the rotor yoke is used for twisting the strand material. Furthermore, the invention relates to a method for producing such a rotor yoke.
- Machines with a rotatably mounted rotor bar for processing elongated extrudates are known from the prior art. Such machines are used for processing ladders, veins, threads or cords to cables or ropes and referred to as stranding or Verlitzmaschinen, in principle, a distinction is made between einschtagigen or doppelschlagigen machines. In the following, the invention will be described using the example of a Doppeltschverlitzmaschine, but it should be noted that the invention also relates to all other types of machinery, in which a rotor yoke is used in the manner described.
- Double weft-stranding machines are mainly used for the production of mass-produced goods, such as electrical cables for the automotive industry, and accordingly have an extremely high processing speed. Along with this, the rotational speed of the rotor yoke is high and sometimes amounts to several thousand revolutions per minute.
- Doppelschlagverlitzmaschinen are often involved in production lines, ie in the so-called in-line production. In this type of processing the Doppeltschverlitzmaschine are before and / or downstream production steps for the production of the final product necessary. In the manufacture of an electric cable, for example, insulating the cable is downstream of the stranding. If only one link in the production chain fails during in-line production, the entire production line comes to a standstill and high downtime costs arise. Therefore, the reliability of a Doppelschlagverlitzmaschine extraordinary requirements.
- rotor yokes So far rotatably mounted rotor yokes are used in Doppeltschverlitzmaschinen, which often consist of a high-strength metallic material, or rotor yoke, which are designed as a very complex hollow body profile, as for example in the US 2006/0196163 A1 is disclosed. From the US 2006/0196163 A1 It is also known to manufacture rotor yokes, also as a solid profile, from a fiber reinforced composite material, such as carbon fiber reinforced plastic, with a plurality of individual wire guide liners held in line in a recessed channel in the rotor yoke.
- a fiber reinforced composite material such as carbon fiber reinforced plastic
- a rotor yoke for a Verlitzmaschine is known with a longitudinal groove for guiding the strand material, which is preferably made of glass fiber fabric with epoxy resin in a vacuum container molding process.
- the object of the invention is to provide a rotor yoke for a machine for processing elongated extrudates, wherein the rotor yoke is designed such that it can be rotatably mounted in the machine and wherein the rotor yoke is used for twisting the strand, which ensures the functional reliability of the machine increases as well as a method for producing a rotor yoke according to the invention.
- the rotatably mounted rotor yoke serves to twist the strand material and extends starting from a cross-sectional area in the direction of a longitudinal axis.
- the rotor yoke extends at least partially bent in the direction of this longitudinal axis.
- the rotor yoke has in this direction a substantially perpendicular to this cross-sectional area extending longitudinal groove.
- This longitudinal groove is at least partially covered by at least one guide element.
- the extruded material is guided movably in the direction of the longitudinal axis.
- the rotor yoke according to the invention consists essentially of plastic with fiber reinforcement.
- the cross-sectional area of the rotor yoke is to be understood as an area which is arranged essentially perpendicular to the longitudinal axis of the rotor yoke and describes the cross section of the rotor yoke at least in sections.
- the rotor yoke extends at right angles to its cross-sectional area.
- the cross-sectional area may vary along the longitudinal axis of the rotor yoke.
- a rotor yoke is to be understood as meaning an elongated, partially bent component.
- the bending of the rotor yoke may be caused by individual kinks, wherein the rotor yoke is straight or bent between two consecutive kinks.
- Under a kink is a bend with a relatively small bending radius, preferably r ⁇ 100 mm to understand.
- the rotor yoke can have a continuous bend in one area in the direction of the longitudinal axis and run without bending in another area, in which case the radius of the bend can be variable.
- the rotor yoke is preferably rotatably mounted in the region of its ends and thus in particular rotatable about an axis of rotation.
- a longitudinal groove is to be understood as meaning a recess in this rotor yoke which runs essentially in the direction of the longitudinal axis.
- the longitudinal groove is intended to guide the elongated strand material in the direction of the longitudinal axis of the rotor yoke.
- a guide element is to be understood as meaning a component which at least partially covers this longitudinal groove.
- a guide element is provided to securely guide the elongate strand material in the longitudinal groove.
- a plastic with fiber reinforcement is to be understood as meaning a material which has at least one proportion of matrix material and one portion of reinforcing fibers.
- the reinforcing fibers of inorganic materials such as basalt, boron, glass, ceramic or silica; made of metallic materials such as steel, aluminum or titanium, as well as of metallic alloys; Made of natural materials such as wood, flax, hemp or sisal or preferably made of organic materials such as aramid, carbon, polyester, nylon, polyethylene or Plexiglas.
- the reinforcing fibers used can have different fiber lengths. Preferably short fibers are used with a fiber length of 0.1 to 1 mm, these reinforcing fibers can be used advantageously in particular when the rotor yoke is produced in an injection molding process. Long fibers with a length of 1 mm to 50 mm are particularly preferably used, in particular in combination with a thermoset matrix material. Long fibers in particular lead to an increase in the strength and rigidity of the plastic with fiber reinforcement. Very particular preference is given to using continuous fibers having a length of more than 50 mm. continuous fibers are used in particular in the form of rovings or fabrics. A plastic with fiber reinforcement by continuous fibers meets the highest demands, in particular on the strength and rigidity.
- the deformation behavior and / or the strength of the plastic can be influenced with fiber reinforcement.
- the reinforcing fibers are preferably arranged randomly, multidirectionally in the matrix material.
- an almost uniformly rigid and / or solid plastic with fiber reinforcement results in almost all spatial directions.
- the reinforcing fibers are aligned according to known stresses of the rotor yoke. This results in particular in a multidirectionally directed or preferably unidirectional orientation of the reinforcing fibers, so that the rotor hoop has a predeterminable deformation behavior in its main stress direction.
- the matrix material of a fiber-reinforced plastic preferably has as a constituent a thermoplastic such as polyether ether ketone (PEEK), polyphenylene sulfide (PPS), polysulfone (PSU), polyether imide (PEI) or polytetrafluoroethene (PTFE) or preferably a thermosetting plastic such as epoxy resin (EP), unsaturated polyester resin (UP), vinyl ester resin (VE), phenol-formaldehyde resin (PF), diallyl phthalate resin (DAP), methacrylate resin (MMA), polyurethane (PUR) or amino resin.
- a thermoplastic such as polyether ether ketone (PEEK), polyphenylene sulfide (PPS), polysulfone (PSU), polyether imide (PEI) or polytetrafluoroethene (PTFE) or preferably a thermosetting plastic such as epoxy resin (EP), unsaturated polyester resin (UP), vinyl ester resin (VE),
- the volume fraction of reinforcing fibers to matrix material is preferably adapted to the expected stress and the allowable deformation of the rotor yoke. In particular, a high proportion of longer fibers leads to an increase in rigidity and strength.
- a fiber-reinforced plastic preferably has a fiber content of from 3 to 95% by volume, preferably from 60 to 80% by volume and particularly preferably from 65 to 70% by volume.
- the rotor yoke is designed as a solid profile, d. H. he has no closed cavities.
- the cross-sectional area of the rotor yoke according to the invention has an elliptical basic shape.
- the cross-sectional area of the rotor yoke has a first and a second axis. Preferably, these first and second axes are perpendicular to each other. Preferably, the cross-sectional area is substantially symmetrical with respect to the first axis and / or to the second axis.
- a rotor bracket according to the invention has essentially the same coefficient of air resistance due to its cross-sectional area, in particular in both directions at right angles to the direction of the longitudinal axis, and thus can be independent of the direction of rotation be used. As a result, the risk of errors when using the rotor yoke is lowered and thus in particular increases the reliability of Doppelschlagverlitzmaschine.
- the rotor yoke has a longitudinal groove.
- the shape of this longitudinal groove is determined in part by a longitudinal groove cross-sectional area which is preferably in a common plane with the cross-sectional area of the rotor yoke.
- the longitudinal groove extends in the direction of the longitudinal axis of the rotor yoke.
- the longitudinal groove cross-sectional area intersects the first axis of the cross-sectional area of the rotor yoke and in particular is symmetrical with respect to the second axis of this cross-sectional area.
- the elongated extruded material is protected during the rotational movement, it is particularly exposed to external stresses, such as air currents, only slightly.
- external stresses such as air currents
- the surface of this longitudinal groove at least partially on a coating.
- the longitudinal groove is at least partially provided with a wear-reducing and / or friction-increasing coating.
- a wear-reducing and / or friction-increasing coating By increasing the friction to ⁇ > 0.1 at the longitudinal groove surface is achieved in particular that on the surface of the longitudinal groove a sliding material can be secured against slipping. Due to the anti-slip fastening, in particular the functional reliability of the double-tucked glittering machine is increased.
- the surface of the longitudinal groove is at least partially provided with a wear and / or friction-reducing coating.
- the friction-reducing coating achieves, in particular, that the elongate extruded material with a coefficient of friction of ⁇ ⁇ 0.1 can slide in the longitudinal groove. Due to this low coefficient of friction, the reliability of Doppelschlagverlitzmaschine is increased.
- the surface of the longitudinal groove is provided with no coating.
- the surface of this longitudinal groove is provided with a sliding plate.
- the sliding plate consists of a friction and / or wear-reducing material.
- this sliding plate lowers the coefficient of friction between the elongated extrudate and the sliding plate to ⁇ ⁇ 0.1.
- the sliding plate is made of a metallic material.
- a sliding plate is in particular prevents that caused by the sliding of the elongated winding material wear damages the structure of the rotor yoke and thus reduces the component strength.
- a sliding plate thus in particular the reliability of Doppelschlagverlitzmaschine is increased.
- a Doppelschlagverlitzmaschine a rotor bracket with a guide element made of a wear and / or friction-reducing material.
- this guide element is made of a metallic or preferably of a ceramic material.
- a guide element has at least a proportion of silicon carbide, preferably of aluminum oxide and particularly preferably of zirconium oxide.
- a guide element with a fastening element on this rotor bracket is releasably attached.
- the guide element is fastened by a pin, preferably by a rivet and more preferably by a screw.
- a guide element is fastened with 1 to 4 fastening elements, preferably with 2 to 3 and particularly preferably with 2 fastening elements such as a screw connection. Due to the detachable connection between the guide element and the rotor yoke, the guide element can be easily and safely replaced and thus prevents this from being used despite heavy wear. As a result, the reliability of Doppelschlagverlitzmaschine is increased.
- the guide element is integrally connected to the rotor yoke.
- the guide element partially overlaps the longitudinal groove so that an overall cross-sectional area with a substantially closed strand guide recess arises in this covered area.
- At least one of the attachment means does not protrude beyond the overall cross-sectional area.
- a fastening means is introduced by the guide member in the rotor yoke and no longer protrudes beyond the attachment of the guide member beyond this.
- the fastening element is a screw and the guide element has a recess for receiving a fastening means.
- the arrangement of the recess in the guide element of the rotor yoke is less weakened than in an arrangement of the recess in the rotor yoke. The rotor yoke thus has a less reduced component strength.
- a fastening means is inserted through the rotor bracket into the guide element and, after the fastening of the guide element has been completed, no longer projects beyond the rotor bracket.
- the fastening means is a screw and the rotor bracket has a recess for receiving the screw head and the guide element has a threaded portion.
- the guide elements are positioned so that the strand is deflected at least on two successive guide elements by the same angle, in particular to follow the course of the longitudinal groove.
- a plurality of but at least two guide elements are claimed substantially equal by this type of attachment of the guide elements.
- the same stress on identical guide elements causes a similar wear, so that inferred by the control of a guide element on the state of wear of several guide elements and thus their replacement can be simplified. In particular, by the simplified replacement of the guide elements, the reliability of Doppelschlagverlitzmaschine is increased.
- a rotor yoke according to the invention is first produced from a plastic, in particular with fiber reinforcement, on which a guide element is subsequently attached.
- this has in particular the steps of prototyping and curing or cooling of this rotor yoke.
- plastic with fiber reinforcement in a mold, which is preferably substantially a negative form of the rotor yoke to understand.
- the matrix material and the reinforcing fibers are introduced together, in particular by injection molding, in the negative mold.
- the matrix material and the reinforcing fibers are preferably introduced into the negative mold separately from one another.
- the rotor yoke has substantially the desired mechanical properties, in particular with regard to its rigidity and strength, especially after completion of this process.
- a guide element By attaching a guide element is to be understood that this is positively connected to the rotor bracket, for example by a fastener or that this is materially connected to the rotor yoke.
- a fastener is a rivet or a screw to understand.
- a guide element is fastened with two fastening elements on the rotor yoke, particularly preferably with two screws.
- a rotor yoke 1 for use in a Doppelschlagberitzmaschine is shown.
- the rotor yoke 1 extends in the direction of the longitudinal axis 3, at right angles to its cross-sectional area 4 (not shown) and has a bend in the middle region.
- the rotor yoke 1 is rotatably mounted in the region of its ends 14 and can rotate about the axis of rotation 13.
- Fig. 2 is the cross-sectional area 4 of the rotor yoke 1 shown.
- the cross-sectional area 4 has a first axis 5 and a second axis 6.
- the cross-sectional area 4 is symmetrical.
- the illustrated cross-sectional area 4 essentially has an elliptical basic shape.
- the rotor yoke 1 is designed as a solid-body profile, ie it has no closed cavities.
- Fig. 3 is the total cross-sectional area of the rotor yoke shown, which is composed of the cross-sectional area 4 of the rotor yoke and the cross-sectional area of the guide element 2.
- the guide element 2 covers in the plane shown the longitudinal groove cross-sectional area 10, so that a closed strand guide recess 12 is formed.
- the surface of the longitudinal groove 11 is partially covered with a sliding plate 8.
- the guide element 2 has two threaded portions 7 for receiving the fastening screws 15.
- the fastening screws 15 are inserted through the rotor yoke 1 in the guide element 2 and connected thereto, while the heads of the fastening screws 15 are substantially received in recesses 9 in the rotor yoke 1.
- the Leksrülen cross-sectional area 10 intersects the first axis 5 and is symmetrical to the second axis 6.
- the longitudinal groove cross-sectional area 10 is the strand material (not shown) in the rotational movement well protected from external influences, such as air currents, in the longitudinal groove.
Description
Die vorliegende Erfindung betrifft einen Rotorbügel für eine Maschine zum Verarbeiten von langgestreckterm Stranggut, wobei der Rotorbügel derart ausgelegt ist, dass er in der Maschine drehbar gelagert werden kann und wobei der Rotorbügel zum Verdrehen des Strangguts dient. Des weiteren betrifft die Erfindung ein Verfahren zum Herstellen eines solchen Rotorbügels.The present invention relates to a rotor yoke for a machine for processing elongated strand material, wherein the rotor yoke is designed such that it can be rotatably mounted in the machine and wherein the rotor yoke is used for twisting the strand material. Furthermore, the invention relates to a method for producing such a rotor yoke.
Maschinen mit einem drehbar gelagerten Rotorbügel zum Verarbeiten von langgestrecktem Stranggut sind aus dem Stand der Technik bekannt. Solche Maschinen werden zum Verarbeiten von Leitern, Adern, Fäden oder Schnüren zu Kabeln oder Seilen verwendet und als Verseil- oder Verlitzmaschinen bezeichnet, grundsätzlich wird zwischen einschtagigen oder doppelschlagigen Maschinen unterschieden. Nachfolgend wird die Erfindung am Beispiel einer Doppelschlagverlitzmaschine beschrieben, es wird aber darauf hingewiesen, dass sich die Erfindung auch auf alle anderen Arten von Maschinen bezieht, in welchen ein Rotorbügel in der beschriebenen Art eingesetzt wird.Machines with a rotatably mounted rotor bar for processing elongated extrudates are known from the prior art. Such machines are used for processing ladders, veins, threads or cords to cables or ropes and referred to as stranding or Verlitzmaschinen, in principle, a distinction is made between einschtagigen or doppelschlagigen machines. In the following, the invention will be described using the example of a Doppelschlagverlitzmaschine, but it should be noted that the invention also relates to all other types of machinery, in which a rotor yoke is used in the manner described.
Alle bekannten Ausführungsfortnen von Doppelschlagverlitzmaschinen stimmen insoweit überein, dass die Führung des langgestreckten Strangguts über einen Rotor- oder Verseilbügel verläuft, dass zwei Verlitzpunkte vorgesehen sind und doppelt so viele Verlitzschläge wie Rotorbügelumdrehungen erzeugt werden. Diesbezüglich wird auf die
Das Funktionsprinzip der beschriebenen Doppelschlagverlitzmaschinen sieht vor, dass der Rotorbügel um eine Achse rotiert. Doppelschlagverlitzmaschinen werden vorwiegend zum Herstellen von Massenware, wie zum Beispiel Elektrokabel für die Automobilindustrie eingesetzt und weisen dementsprechend eine äußerst hohe Verarbeitungsgeschwindigkeit auf. Damit einhergehend ist die Rotationsgeschwindigkeit des Rotorbügels hoch und beträgt zum Teil mehrere tausend Umdrehungen pro Minute.The principle of operation of the double-twist machines described provides that the rotor yoke rotates about an axis. Double weft-stranding machines are mainly used for the production of mass-produced goods, such as electrical cables for the automotive industry, and accordingly have an extremely high processing speed. Along with this, the rotational speed of the rotor yoke is high and sometimes amounts to several thousand revolutions per minute.
Doppelschlagverlitzmaschinen sind häufig in Produktionsstraßen, also in der sogenannten In-Line-Produktion eingebunden. Bei dieser Art der Verarbeitung sind der Doppelschlagverlitzmaschine vor und/oder nachgelagerte Produktionsschritte zum Herstellen des Endproduktes notwendig. Bei der Herstellung eines Elektrokabels ist dem Verlitzen beispielsweise das Isolieren das Kabels nachgelagert. Fällt bei der In-Line-Produktion nur ein Glied der Produktionskette aus, so kommt die gesamte Produktionsstraße zum Stillstand und es entstehen hohe Ausfallkosten. Daher werden an die Funktionssicherheit einer Doppelschlagverlitzmaschine außerordentliche Anforderungen gestellt.Doppelschlagverlitzmaschinen are often involved in production lines, ie in the so-called in-line production. In this type of processing the Doppelschlagverlitzmaschine are before and / or downstream production steps for the production of the final product necessary. In the manufacture of an electric cable, for example, insulating the cable is downstream of the stranding. If only one link in the production chain fails during in-line production, the entire production line comes to a standstill and high downtime costs arise. Therefore, the reliability of a Doppelschlagverlitzmaschine extraordinary requirements.
Bisher werden in Doppelschlagverlitzmaschinen drehbar gelagerte Rotorbügel eingesetzt, welche häufig aus einem hochfesten metallischen Werkstoff bestehen, oder Rotorbügel, welche als sehr aufwändiges Hohlkörperprofil ausgebildet sind, wie dies zum Beispiel in der
Aus der
Ferner ist aus der
Die Aufgabe der Erfindung ist es, einen Rotorbügel für eine Maschine zum Verarbeiten von langgestrecktem Stranggut, wobei der Rotorbügel derart ausgelegt ist, dass er in der Maschine drehbar gelagert werden kann und wobei der Rotorbügel zum Verdrehen des Strangguts dient bereitzustellen, welcher die Funktionssicherheit der Maschine erhöht sowie ein Verfahren zum Herstellen eines erfindungsgemäßen Rotorbügels.The object of the invention is to provide a rotor yoke for a machine for processing elongated extrudates, wherein the rotor yoke is designed such that it can be rotatably mounted in the machine and wherein the rotor yoke is used for twisting the strand, which ensures the functional reliability of the machine increases as well as a method for producing a rotor yoke according to the invention.
Diese Aufgabe wird durch zum Verarbeiten von langgestrecktem Stranggut wobei der Rotorbügel derart ausgelegt ist, dass er in der Maschine drehbar gelagert werden kann und wobei der Rotorbügel zum Verdrehen des Strangguts dient gemäß Anspruch 1 sowie durch ein Verfahren zum Herstellen eines solchen Rotorbügels gemäß Anspruch 10 gelöst. Die Merkmale der Unteransprüche beziehen sich auf zu bevorzugende Weiterbildungen der erfindungsgemäßen Maschine.This object is achieved by the processing of elongate extruded material wherein the rotor yoke is designed such that it can be rotatably mounted in the machine and wherein the rotor yoke for twisting the strand material according to claim 1 and by a method for producing such a rotor yoke according to
Der drehbar gelagerten Rotorbügel dient zum Verdrehen des Strangguts und erstreckt sich ausgehend von einer Querschnittsfläche in Richtung einer Längsachse. Der Rotorbügel verläuft in Richtung dieser Längsachse wenigstens abschnittsweise gebogen. Der Rotorbügel weist in dieser Richtung eine im Wesentlichen zu dieser Querschnittsfläche rechtwinklig verlaufende Längsrille auf.The rotatably mounted rotor yoke serves to twist the strand material and extends starting from a cross-sectional area in the direction of a longitudinal axis. The rotor yoke extends at least partially bent in the direction of this longitudinal axis. The rotor yoke has in this direction a substantially perpendicular to this cross-sectional area extending longitudinal groove.
Diese Längsrille wird wenigstens bereichsweise von wenigstens einem Führungselement überdeckt. In diesem Rotorbügel wird das Stranggut in Richtung der Längsachse beweglich geführt.This longitudinal groove is at least partially covered by at least one guide element. In this rotor yoke, the extruded material is guided movably in the direction of the longitudinal axis.
Der erfindungsgemäße Rotorbügel besteht im Wesentlichen aus Kunststoff mit Faserverstärkung.The rotor yoke according to the invention consists essentially of plastic with fiber reinforcement.
Unter der Querschnittsfläche des Rotorbügels ist eine Fläche zu verstehen, welche im Wesentlichen senkrecht zur Längsachse des Rotorbügels angeordnet ist, und den Querschnitt des Rotorbügels wenigstens abschnittsweise beschreibt. Der Rotorbügel erstreckt sich rechtwinklig zu seiner Querschnittsfläche. Die Querschnittsfläche kann sich entlang der Längsachse des Rotorbügels verändern.The cross-sectional area of the rotor yoke is to be understood as an area which is arranged essentially perpendicular to the longitudinal axis of the rotor yoke and describes the cross section of the rotor yoke at least in sections. The rotor yoke extends at right angles to its cross-sectional area. The cross-sectional area may vary along the longitudinal axis of the rotor yoke.
Unter einem Rotorbügel ist ein langgestrecktes, abschnittsweise gebogenes Bauteil zu verstehen. Die Biegung des Rotorbügels kann durch einzelne Knicke entstehen, wobei der Rotorbügel zwischen zwei aufeinanderfolgenden Knicken gerade oder gebogen verläuft. Unter einem Knick ist dabei eine Biegung mit relativ kleinem Biegeradius, vorzugsweise r < 100 mm, zu verstehen. Der Rotorbügel kann in Richtung der Längsachse eine kontinuierliche Biegung in einem Bereich aufweisen und in einem anderen Bereich ohne Biegung verlaufen, dabei kann der Radius der Biegung variabel sein. Durch die beschriebene Formgebung des Rotorbügels wird das Verdrehen des langgestreckten Strangguts ermöglicht. Der Rotorbügel ist vorzugsweise im Bereich seiner Enden drehbar gelagert und somit insbesondere um eine Rotationsachse drehbar.A rotor yoke is to be understood as meaning an elongated, partially bent component. The bending of the rotor yoke may be caused by individual kinks, wherein the rotor yoke is straight or bent between two consecutive kinks. Under a kink is a bend with a relatively small bending radius, preferably r <100 mm to understand. The rotor yoke can have a continuous bend in one area in the direction of the longitudinal axis and run without bending in another area, in which case the radius of the bend can be variable. By the described shaping of the rotor yoke, the twisting of the elongated strand material is made possible. The rotor yoke is preferably rotatably mounted in the region of its ends and thus in particular rotatable about an axis of rotation.
Unter einer Längsrille ist eine Ausnehmung in diesem Rotorbügel zu verstehen, welche im Wesentlichen in Richtung der Längsachse verläuft. Die Längsrille ist dazu vorgesehen das langgestreckte Stranggut in Richtung der Längsachse des Rotorbügels zu führen.A longitudinal groove is to be understood as meaning a recess in this rotor yoke which runs essentially in the direction of the longitudinal axis. The longitudinal groove is intended to guide the elongated strand material in the direction of the longitudinal axis of the rotor yoke.
Unter einem Führungselement ist ein Bauteil zu verstehen, welches diese Längsrille wenigstens teilweise überdeckt. Ein Führungselement ist dazu vorgesehen, das langgestreckte Stranggut sicher in der Längsrille zu führen.A guide element is to be understood as meaning a component which at least partially covers this longitudinal groove. A guide element is provided to securely guide the elongate strand material in the longitudinal groove.
Unter einem Kunststoff mit Faserverstärkung ist ein Werkstoff zu verstehen, welcher wenigstens einen Anteil Matrixwerkstoff und einen Anteil Verstärkungsfasern aufweist.A plastic with fiber reinforcement is to be understood as meaning a material which has at least one proportion of matrix material and one portion of reinforcing fibers.
Dabei können die Verstärkungsfasern aus anorganischen Werkstoffen wie Basalt, Bor, Glas, Keramik oder Kieselsäure; aus metallischen Werkstoffen wie Stahl, Aluminium oder Titan, sowie aus metallischen Legierungen; aus natürlichen Werkstoffen wie Holz, Flachs, Hanf oder Sisal oder vorzugsweise aus organischen Werkstoffen wie Aramid, Kohlenstoff, Polyester, Nylon, Polyethylen oder Plexiglas bestehen.In this case, the reinforcing fibers of inorganic materials such as basalt, boron, glass, ceramic or silica; made of metallic materials such as steel, aluminum or titanium, as well as of metallic alloys; Made of natural materials such as wood, flax, hemp or sisal or preferably made of organic materials such as aramid, carbon, polyester, nylon, polyethylene or Plexiglas.
Die eingesetzten Verstärkungsfasern können unterschiedliche Faserlängen aufweisen. Vorzugsweise werden Kurzfasern mit einer Faserlänge von 0,1 bis 1 mm eingesetzt, diese Verstärkungsfasern können insbesondere dann vorteilhaft eingesetzt werden, wenn der Rotorbügel in einem Spritzgussverfahren hergestellt wird. Besonders bevorzugt werden, insbesondere in Kombination mit einem duroplastischen Matrixwerkstoff, Langfasern mit einer Länge von 1 mm bis 50 mm eingesetzt. Langfasern führen insbesondere zu einer Erhöhung der Festigkeit und Steifigkeit des Kunststoffs mit Faserverstärkung. Ganz besonders bevorzugt werden Endlosfasern mit einer Länge von über 50 mm eingesetzt. Endlosfasern werden insbesondere in Form von Rovings oder Geweben eingesetzt. Ein Kunststoff mit Faserverstärkung durch Endlosfasern genügt höchsten Ansprüchen insbesondere an die Festigkeit und Steifigkeit.The reinforcing fibers used can have different fiber lengths. Preferably short fibers are used with a fiber length of 0.1 to 1 mm, these reinforcing fibers can be used advantageously in particular when the rotor yoke is produced in an injection molding process. Long fibers with a length of 1 mm to 50 mm are particularly preferably used, in particular in combination with a thermoset matrix material. Long fibers in particular lead to an increase in the strength and rigidity of the plastic with fiber reinforcement. Very particular preference is given to using continuous fibers having a length of more than 50 mm. continuous fibers are used in particular in the form of rovings or fabrics. A plastic with fiber reinforcement by continuous fibers meets the highest demands, in particular on the strength and rigidity.
Durch die Ausrichtung der Verstärkungsfasern im Matrixwerkstoff kann insbesondere das Verformungsverhalten und/oder die Festigkeit des Kunststoffs mit Faserverstärkung beeinflusst werden. Die Verstärkungsfasern werden vorzugsweise regellos, multidirektional im Matrixwerkstoff angeordnet. Somit ergibt sich ein nahezu in alle Raumrichtungen gleichmäßig steifer und/oder fester Kunststoff mit Faserverstärkung. Bevorzugt werden die Verstärkungsfasern entsprechend bekannter Beanspruchungen des Rotorbügels ausgerichtet. Somit ergibt sich insbesondere eine multidirektional gerichtete oder vorzugsweise eine unidirektionale Ausrichtung der Verstärkungsfasern, so dass der Rotorbügel in seine Hauptbeanspruchungsrichtung ein vorgebbares Verformungsverhalten aufweist.By aligning the reinforcing fibers in the matrix material, in particular the deformation behavior and / or the strength of the plastic can be influenced with fiber reinforcement. The reinforcing fibers are preferably arranged randomly, multidirectionally in the matrix material. Thus, an almost uniformly rigid and / or solid plastic with fiber reinforcement results in almost all spatial directions. Preferably, the reinforcing fibers are aligned according to known stresses of the rotor yoke. This results in particular in a multidirectionally directed or preferably unidirectional orientation of the reinforcing fibers, so that the rotor hoop has a predeterminable deformation behavior in its main stress direction.
Der Matrixwerkstoff eines Kunststoffs mit Faserverstärkung weist als einen Bestandteil vorzugsweise einen thermoplastischen Kunststoff wie Polyetheretherketon (PEEK), Polyphenylensulfid (PPS), Polysulfon (PSU), Polyetherimid (PEI) oder Polytetrafluorethen (PTFE) oder bevorzugt einen duroplastischen Kunststoff wie Epoxidharz (EP), ungesättigtes Polyesterharz (UP), Vinylesterharz (VE), Phenol-Formaldehydharz (PF), Diallylphthalatharz (DAP), Methacrylatharz (MMA), Polyurethan (PUR) oder aus Aminoharz.The matrix material of a fiber-reinforced plastic preferably has as a constituent a thermoplastic such as polyether ether ketone (PEEK), polyphenylene sulfide (PPS), polysulfone (PSU), polyether imide (PEI) or polytetrafluoroethene (PTFE) or preferably a thermosetting plastic such as epoxy resin (EP), unsaturated polyester resin (UP), vinyl ester resin (VE), phenol-formaldehyde resin (PF), diallyl phthalate resin (DAP), methacrylate resin (MMA), polyurethane (PUR) or amino resin.
Der Volumenanteil von Verstärkungsfasern zu Matrixwerkstoff wird vorzugsweise an die zu erwartende Beanspruchung und die zulässige Verformung des Rotorbügels angepasst. Insbesondere führt ein hoher Anteil längerer Fasern zu einer Steigerung der Steifigkeit und Festigkeit. Vorzugsweise weist ein Kunststoff mit Faserverstärkung einen Faseranteil von 3 bis 95 Volumen-% auf, bevorzugt von 60 bis 80 Volumen-% und besonders bevorzugt von 65 bis 70 Volumen-%.The volume fraction of reinforcing fibers to matrix material is preferably adapted to the expected stress and the allowable deformation of the rotor yoke. In particular, a high proportion of longer fibers leads to an increase in rigidity and strength. A fiber-reinforced plastic preferably has a fiber content of from 3 to 95% by volume, preferably from 60 to 80% by volume and particularly preferably from 65 to 70% by volume.
Erfindungsgemäß ist der Rotorbügel als Vollkörperprofil ausgebildet, d. h. er weist keine geschlossenen Hohlräume auf.According to the invention the rotor yoke is designed as a solid profile, d. H. he has no closed cavities.
Weiterhin weist die Querschnittsfläche des Rotorbügels erfindungsgemäß eine elliptische Grundform auf.Furthermore, the cross-sectional area of the rotor yoke according to the invention has an elliptical basic shape.
In einer bevorzugten Ausführungsform weist die Querschnittsfläche des Rotorbügels eine erste und eine zweite Achse auf. Vorzugsweise sind diese erste und diese zweite Achse rechtwinklig zueinander. Vorzugsweise ist die Querschnittsfläche im Wesentlichen symmetrisch zu der ersten Achse und/oder zu der zweiten Achse.Ein erfindungsgemäßer Rotorbügel weist aufgrund seiner Querschnittsfläche insbesondere in beide Richtungen rechtwinklig zur Richtung der Längsachse, im Wesentlichen den gleichen Luftwiderstandsbeiwert auf und kann damit insbesondere unabhängig von der Rotationsrichtung eingesetzt werden. Dadurch wird das Risiko von Fehlern beim Einsatz des Rotorbügels gesenkt und damit insbesondere die Funktionssicherheit der Doppelschlagverlitzmaschine gesteigert.In a preferred embodiment, the cross-sectional area of the rotor yoke has a first and a second axis. Preferably, these first and second axes are perpendicular to each other. Preferably, the cross-sectional area is substantially symmetrical with respect to the first axis and / or to the second axis. A rotor bracket according to the invention has essentially the same coefficient of air resistance due to its cross-sectional area, in particular in both directions at right angles to the direction of the longitudinal axis, and thus can be independent of the direction of rotation be used. As a result, the risk of errors when using the rotor yoke is lowered and thus in particular increases the reliability of Doppelschlagverlitzmaschine.
Erfindungsgemäß weist der Rotorbügel eine Längsrille auf. Die Gestalt dieser Längsrille wird teilweise durch eine Längsrillen-Querschnittsfläche bestimmt, welche vorzugsweise mit der Querschnittsfläche des Rotorbügels in einer gemeinsamen Ebene liegt. Ausgehend von dieser Längsrillen-Querschnittsfläche erstreckt sich die Längsrille in Richtung der Längsachse des Rotorbügels. Vorzugsweise schneidet die Längsrillen-Querschnittsfläche die erste Achse der Querschnittsfläche des Rotorbügels und ist insbesondere symmetrisch zur zweiten Achse dieser Querschnittsfläche. Insbesondere durch diese Ausgestaltung wird das langgestreckte Stranggut während der Rotationsbewegung geschützt, so ist es insbesondere äußeren Beanspruchungen, wie zum Beispiel Luftströmungen, nur wenig ausgesetzt. Durch diesen Schutz des Strangguts wird insbesondere die Funktionssicherheit der Doppelschlagverlitzmaschine gesteigert.According to the invention, the rotor yoke has a longitudinal groove. The shape of this longitudinal groove is determined in part by a longitudinal groove cross-sectional area which is preferably in a common plane with the cross-sectional area of the rotor yoke. Starting from this longitudinal groove cross-sectional area, the longitudinal groove extends in the direction of the longitudinal axis of the rotor yoke. Preferably, the longitudinal groove cross-sectional area intersects the first axis of the cross-sectional area of the rotor yoke and in particular is symmetrical with respect to the second axis of this cross-sectional area. In particular, by this embodiment, the elongated extruded material is protected during the rotational movement, it is particularly exposed to external stresses, such as air currents, only slightly. Through this protection of the strand material, in particular the reliability of the Doppelschlagverlitzmaschine is increased.
In einer bevorzugten Ausführungsform weist die Oberfläche dieser Längsrille wenigstens bereichsweise eine Beschichtung auf. Vorzugsweise ist die Längsrille zumindest bereichsweise mit einer verschleißmindernden und/oder reibungserhöhenden Beschichtung versehen. Durch die Reibungserhöhung auf µ > 0,1 an der Längsrillenoberfläche wird insbesondere erreicht, dass auf der Oberfläche der Längsrille ein Gleitwerkstoff verrutschsicher befestigt werden kann. Durch die verrutschsichere Befestigung wird insbesondere die Funktionssicherheit der Doppetschlagverlitzmaschine erhöht. Bevorzugt ist die Oberfläche der Längsrille zumindest bereichsweise mit einer verschleiß- und/oder reibungsmindernden Beschichtung versehen. Durch die reibungsmindernde Beschichtung wird insbesondere erreicht, dass das langgestreckte Stranggut mit einem Reibwert von µ < 0,1 in der Längsrille gleiten kann. Durch diese niedrige Reibungszahl wird die Funktionssicherheit der Doppelschlagverlitzmaschine erhöht.In a preferred embodiment, the surface of this longitudinal groove at least partially on a coating. Preferably, the longitudinal groove is at least partially provided with a wear-reducing and / or friction-increasing coating. By increasing the friction to μ> 0.1 at the longitudinal groove surface is achieved in particular that on the surface of the longitudinal groove a sliding material can be secured against slipping. Due to the anti-slip fastening, in particular the functional reliability of the double-tucked glittering machine is increased. Preferably, the surface of the longitudinal groove is at least partially provided with a wear and / or friction-reducing coating. The friction-reducing coating achieves, in particular, that the elongate extruded material with a coefficient of friction of μ <0.1 can slide in the longitudinal groove. Due to this low coefficient of friction, the reliability of Doppelschlagverlitzmaschine is increased.
In einer weiteren bevorzugten Ausführungsform ist die Oberfläche der Längsrille mit keiner Beschichtung versehen.In a further preferred embodiment, the surface of the longitudinal groove is provided with no coating.
In einer anderen bevorzugten Ausführungsform ist die Oberfläche dieser Längsrille mit einem Gleitblech versehen. Insbesondere besteht das Gleitblech aus einem reibungs- und/oder verschleißmindernden Werkstoff. Vorzugsweise senkt dieses Gleitblech die Reibungszahl zwischen dem langgestreckten Stranggut und dem Gleitblech auf µ < 0,1.In another preferred embodiment, the surface of this longitudinal groove is provided with a sliding plate. In particular, the sliding plate consists of a friction and / or wear-reducing material. Preferably, this sliding plate lowers the coefficient of friction between the elongated extrudate and the sliding plate to μ <0.1.
Vorzugsweise besteht das Gleitblech aus einem metallischen Werkstoff. Durch ein Gleitblech wird insbesondere verhindert, dass ein durch das Gleiten des langgestreckten Wickelguts verursachter Verschleiß die Struktur des Rotorbügels schädigt und damit die Bauteilfestigkeit verringert. Durch ein Gleitblech wird somit insbesondere die Funktionssicherheit der Doppelschlagverlitzmaschine gesteigert.Preferably, the sliding plate is made of a metallic material. By a sliding plate is in particular prevents that caused by the sliding of the elongated winding material wear damages the structure of the rotor yoke and thus reduces the component strength. By a sliding plate thus in particular the reliability of Doppelschlagverlitzmaschine is increased.
In einer bevorzugten Ausführungsform weist eine Doppelschlagverlitzmaschine einen Rotorbügel mit einem Führungselement aus einem verschleiß- und/oder reibungsminderndem Werkstoff auf. Vorzugsweise ist dieses Führungselement aus einem metallischen oder bevorzugt aus einem keramischen Werkstoff hergestellt. Insbesondere weist ein Führungselement wenigstens einen Anteil von Siliciumcarbid vorzugsweise von Aluminiumoxid und besonders bevorzugt von Zirkonoxid auf. Durch eine verschleißarmes und reibungsmindemdes Führungselement wird insbesondere die Funktionssicherheit einer Doppelschlagverlitzmaschine gesteigert, da sich insbesondere das langgestreckte Stranggut beim Gleiten durch das Führungselement nur wenig erwärmt. Ein weiterer Vorteil dieser Ausführungsform gegenüber anderen ist, dass das Stranggut weniger beansprucht und gedehnt wird.In a preferred embodiment, a Doppelschlagverlitzmaschine a rotor bracket with a guide element made of a wear and / or friction-reducing material. Preferably, this guide element is made of a metallic or preferably of a ceramic material. In particular, a guide element has at least a proportion of silicon carbide, preferably of aluminum oxide and particularly preferably of zirconium oxide. By a wear-resistant and friction-reducing guide element in particular the reliability of a Doppelschlagverlitzmaschine is increased because, in particular, the elongated Stranggut only slightly heated when sliding through the guide element. Another advantage of this embodiment over others is that the tow is less stressed and stretched.
In einer bevorzugten Ausführungsform ist ein Führungselement mit einem Befestigungselement auf diesem Rotorbügel lösbar befestigt. Vorzugsweise ist das Führungselement durch einen Stift, bevorzugt durch einen Niet und besonders bevorzugt durch eine Schraube befestigt. Vorzugsweise ist ein Führungselement mit 1 bis 4 Befestigungselementen befestigt, bevorzugt mit 2 bis 3 und besonders bevorzugt mit 2 Befestigungselementen wie beispielsweise einer Schraubverbindung. Durch die lösbare Verbindung zwischen Führungselement und Rotorbügel kann das Führungselement einfach und sicher ausgewechselt werden und somit wird verhindert, dass dieses trotz starkem Verschleiß weiterverwendet wird. Dadurch wird die Funktionssicherheit der Doppelschlagverlitzmaschine erhöht. In einer anderen erfindungsgemäßen Ausgestaltung ist das Führungselement stoffschlüssig mit dem Rotorbügel verbunden.In a preferred embodiment, a guide element with a fastening element on this rotor bracket is releasably attached. Preferably, the guide element is fastened by a pin, preferably by a rivet and more preferably by a screw. Preferably, a guide element is fastened with 1 to 4 fastening elements, preferably with 2 to 3 and particularly preferably with 2 fastening elements such as a screw connection. Due to the detachable connection between the guide element and the rotor yoke, the guide element can be easily and safely replaced and thus prevents this from being used despite heavy wear. As a result, the reliability of Doppelschlagverlitzmaschine is increased. In another embodiment of the invention, the guide element is integrally connected to the rotor yoke.
In einer bevorzugten Ausführungsform überdeckt das Führungselement die Längsrille bereichsweise so, dass in diesem überdecktem Bereich eine Gesamtquerschnittsfläche mit einer im Wesentlichen geschlossenen Stranggutführungs-Ausnehmung entsteht. Durch diese Ausprägung der Stranggutführungs-Ausnehmung kann verhindert werden, dass das Stranggut unplanmäßig aus der Längsrille austritt. Insbesondere durch die sichere Führung des Strangguts in der Längsrille wird die Funktionssicherheit der Doppelschlagverlitzmaschine erhöht.In a preferred embodiment, the guide element partially overlaps the longitudinal groove so that an overall cross-sectional area with a substantially closed strand guide recess arises in this covered area. By this expression of the strand guide recess can be prevented that the strand unscheduled leaking from the longitudinal groove. In particular, by the safe guidance of the strand in the longitudinal groove, the reliability of Doppelschlagverlitzmaschine is increased.
In einer bevorzugten Ausführungsform ragt wenigstens eines der Befestigungsmittel nicht über die Gesamtquerschnittsfläche hinaus. Vorzugsweise wird ein Befestigungsmittel durch das Führungselement in den Rotorbügel eingeführt und ragt nach abgeschlossener Befestigung des Führungselements nicht mehr über dieses hinaus. Vorzugsweise ist das Befestigungselement eine Schraube und das Führungselement weist eine Ausnehmung zur Aufnahme eines Befestigungsmittels auf. Durch die Anordnung der Ausnehmung im Führungselement wird der Rotorbügel weniger geschwächt als bei einer Anordnung der Ausnehmung im Rotorbügel. Der Rotorbügel weist damit eine weniger verminderte Bauteilfestigkeit auf.In a preferred embodiment, at least one of the attachment means does not protrude beyond the overall cross-sectional area. Preferably, a fastening means is introduced by the guide member in the rotor yoke and no longer protrudes beyond the attachment of the guide member beyond this. Preferably, the fastening element is a screw and the guide element has a recess for receiving a fastening means. The arrangement of the recess in the guide element of the rotor yoke is less weakened than in an arrangement of the recess in the rotor yoke. The rotor yoke thus has a less reduced component strength.
Vorzugsweise wird ein Befestigungsmittel durch den Rotorbügel in das Führungselement eingeführt und ragt nach abgeschlossener Befestigung des Führungselements nicht mehr über den Rotorbügel hinaus. In einer bevorzugten Ausführungsform ist das Befestigungsmittel eine Schraube und der Rotorbügel weist eine Ausnehmung zum Aufnehmen des Schraubenkopfes und das Führungselement einen Gewindeabschnitt auf. Insbesondere durch die hohe Festigkeit des Führungselements entsteht so eine besonderes tragfähige Schraubenverbindung und die Funktionssicherheit der Doppelschlagverlitzmaschine wird erhöht.Preferably, a fastening means is inserted through the rotor bracket into the guide element and, after the fastening of the guide element has been completed, no longer projects beyond the rotor bracket. In a preferred embodiment, the fastening means is a screw and the rotor bracket has a recess for receiving the screw head and the guide element has a threaded portion. In particular, by the high strength of the guide element so creates a special viable screw connection and the reliability of Doppelschlagverlitzmaschine is increased.
In einer weiteren bevorzugten Ausführungsform sind die Führungselemente so positioniert, dass das Stranggut wenigstens an zwei aufeinanderfolgenden Führungselementen um den gleichen Winkel abgelenkt wird, um insbesondere dem Verlauf der Längsrille zu folgen. Vorzugsweise werden durch diese Art der Anbringung der Führungselemente mehrere aber wenigstens zwei Führungselemente im Wesentlichen gleich beansprucht. Vorzugsweise verursacht die gleiche Beanspruchung an baugleichen Führungselementen einen ähnlichen Verschleiß, so dass durch die Kontrolle eines Führungselements auf den Verschleißzustand mehrerer Führungselemente gefolgert und damit deren Austausch vereinfacht werden kann. Insbesondere durch den vereinfachten Austausch der Führungselemente wird die Funktionssicherheit der Doppelschlagverlitzmaschine erhöht. Durch diese Art der Positionierung der Führungselemente ist es möglich weniger Führungselemente einzusetzen, dadurch wird zum einen die Anzahl an verschleißenden Teilen reduziert, zum anderen verlängert sich die freie, nicht überdeckte Strecke zwischen den Führungselementen. Beim Gleiten des langgestreckten Strangguts durch die Längsrille und/oder durch ein Führungselement können sich Partikel vom Stranggut und/oder von den Gleitflächen lösen und am Rotorbügel ablagern, insbesondere lagert sich Kupfer- oder Zinnstaub am Rotorbügel ab. Der durch die Rotationsbewegung entstehende Luftstrom kann in vorteilhafter Weise auf den freien nicht überdeckten Strecken des Rotorbügels diese Partikel entfernen. Somit wird durch die beschriebene Art der Positionierung der Führungselemente die Funktionssicherheit der Doppelschlagverlitzmaschine erhöht.In a further preferred embodiment, the guide elements are positioned so that the strand is deflected at least on two successive guide elements by the same angle, in particular to follow the course of the longitudinal groove. Preferably, a plurality of but at least two guide elements are claimed substantially equal by this type of attachment of the guide elements. Preferably, the same stress on identical guide elements causes a similar wear, so that inferred by the control of a guide element on the state of wear of several guide elements and thus their replacement can be simplified. In particular, by the simplified replacement of the guide elements, the reliability of Doppelschlagverlitzmaschine is increased. By this type of positioning of the guide elements, it is possible to use fewer guide elements, thereby reducing the number of wear parts on the one hand, on the other hand extends the free, not covered route between the guide elements. When the elongated strand material slides through the longitudinal groove and / or through a guide element, particles can detach from the extruded material and / or from the sliding surfaces and deposit on the rotor yoke, in particular copper or tin dust deposits on the rotor yoke. The air flow generated by the rotational movement can in advantageously remove these particles on the free uncovered sections of the rotor yoke. Thus, the functional reliability of the Doppelschlagverlitzmaschine is increased by the described type of positioning of the guide elements.
In einem erfindungsgemäßen Verfahren zum Herstellen eines Rotorbügels insbesondere zum Einsatz in einer Doppelschlagverlitzmaschine wird zunächst ein erfindungsgemäßer Rotorbügel aus einem Kunststoff, insbesondere mit Faserverstärlung hergestellt, auf diesem wird anschließend ein Führungselement angebracht.In a method according to the invention for producing a rotor yoke, in particular for use in a double-twist extruder, a rotor yoke according to the invention is first produced from a plastic, in particular with fiber reinforcement, on which a guide element is subsequently attached.
In einer bevorzugten Ausführungsform des Herstellverfahrens weist dieses insbesondere die Schritte Urformen und Aushärten beziehungsweise Abkühlen dieses Rotorbügels auf. Insbesondere ist unter Urformen das Einbringen von Kunststoff mit Faserverstärkung in eine Form, welche vorzugsweise im Wesentlichen eine Negativform des Rotorbügels darstellt, zu verstehen. Vorzugsweise werden der Matrixwerkstoff und die Verstärkungsfasern gemeinsam, insbesondere durch Spritzgießen, in die Negativform eingebracht. Bevorzugt werden der Matrixwerkstoff und die Verstärkungsfasern getrennt voneinander in die Negativform eingebracht.In a preferred embodiment of the production method, this has in particular the steps of prototyping and curing or cooling of this rotor yoke. In particular, under prototypes is the introduction of plastic with fiber reinforcement in a mold, which is preferably substantially a negative form of the rotor yoke to understand. Preferably, the matrix material and the reinforcing fibers are introduced together, in particular by injection molding, in the negative mold. The matrix material and the reinforcing fibers are preferably introduced into the negative mold separately from one another.
Unter Aushärten beziehungsweise Abkühlen ist zu verstehen, dass der Rotorbügel insbesondere nach Abschluss dieses Vorgangs im Wesentlichen die gewünschten mechanischen Eigenschaften, insbesondere in Bezug auf seine Steifigkeit und Festigkeit besitzt.By hardening or cooling, it is to be understood that the rotor yoke has substantially the desired mechanical properties, in particular with regard to its rigidity and strength, especially after completion of this process.
Unter dem Befestigen eines Führungselements ist zu verstehen, dass dieses formschlüssig mit dem Rotorbügel, zum Beispiel durch ein Befestigungselement verbunden wird oder, dass dieses stoffschlüssig mit dem Rotorbügel verbunden wird. Vorzugsweise ist unter einem Befestigungselement ein Niet oder eine Schraube zu verstehen. Vorzugsweise wird ein Führungselement mit zwei Befestigungselementen am Rotorbügel befestigt, besonders bevorzugt mit zwei Schrauben.By attaching a guide element is to be understood that this is positively connected to the rotor bracket, for example by a fastener or that this is materially connected to the rotor yoke. Preferably, a fastener is a rivet or a screw to understand. Preferably, a guide element is fastened with two fastening elements on the rotor yoke, particularly preferably with two screws.
Weitere Vorteile, Merkmale und Anwendungsmöglichkeiten der vorliegenden Erfindung ergeben sich aus der nachfolgenden Beschreibung in Zusammenhang mit den Figuren. Es zeigt:
- Fig. 1
- einen Rotorbügel 1 zum Einsatz in einer Doppelschlag-Verlitzmaschine, wobei dieser einige Führungselemente 2 aufweist,
- Fig. 2
- die
Querschnittsfläche 4 eines Rotorbügels 1 mit einer ersten Achse 5 und einer zweiten Achse 6, - Fig. 3
- die
Gesamtquerschnittsfläche 4 mit einer Stranggutführungs-Ausnehmung 6, wobei der Längsrillen-Querschnitt 10 ein Teil dieser ist und zwei Befestigungselemente 15.
- Fig. 1
- a rotor yoke 1 for use in a double-stroke Verlitzmaschine, wherein this has some
guide elements 2, - Fig. 2
- the
cross-sectional area 4 of a rotor yoke 1 with afirst axis 5 and asecond axis 6, - Fig. 3
- the total
cross-sectional area 4 with astrand guide recess 6, wherein thelongitudinal groove cross-section 10 is a part of this and two fastening elements 15th
In
In
In
Claims (11)
- A rotor bow (1) for a machine for processing elongate strand stock,
wherein the rotor bow (1) is constructed such that it can be rotatably mounted in the machine, and wherein rotor bow (1) serves to twist the strand stock, with:an extension substantially along a longitudinal axis (3), at least sections of which are curved;a cross-section described by a cross-sectional area (4) and extending substantially right-angled to the longitudinal axis (3);a longitudinal groove extending substantially parallel to the longitudinal axis (3) and having its cross-section described by a longitudinal groove cross-sectional area (10), wherein the strand stock can be movably guided in the direction of the longitudinal axis (3) in said longitudinal groove of the rotor bow (1);wherein the rotor bow (1) consists of plastic reinforced with fibers and is formed as a solid body profile, characterized in that at least one guide element (2) is provided which covers at least portions of said longitudinal groove and which is adapted for guiding the strand stock;
and that said cross-sectional area (4) has an elliptical basic form. - The rotor bow (1) according to claim 1, characterized in that portions of the longitudinal groove cross-sectional area (10) are intersected by a first semi-axis (5) of the elliptical basic form and is in particular symmetrical to a second semi-axis (6) of the elliptical basic form.
- The rotor bow (1) according to one of the preceding claims, characterized in that at least portions of the surface (11) of the longitudinal groove are provided with a coating, wherein said coating is composed of a wear-reducing and/or friction-reducing material.
- The rotor bow (1) according to claim 1 or 2, characterized in that at least portions of the surface (11) of the longitudinal groove are provided with a slide plate (8), wherein at least sections of same consist of a wear-reducing and/or friction-reducing material.
- The rotor bow (1) according to one of the preceding claims, characterized in that at least sections of the at least one guide element (2) consists of a wear-reducing and/or friction-reducing material, particularly a ceramic material.
- The rotor bow (1) according to one of the preceding claims, characterized in that the at least one guide element (2) is detachably affixed on the rotor bow (1) by means of at least one fixing element (15).
- The rotor bow (1) according to claim 6, characterized in that a total cross-sectional area having a circumferentially closed strand stock guiding recess (12) is formed in the covered area.
- The rotor bow (1) according to claim 6 or 7, characterized in that the at least one fixing element (15) is substantially disposed within the total cross-sectional area.
- The rotor bow (1) according to one of the preceding claims, characterized in that the rotor bow (1) has at least two guide elements (2) which are positioned such that the angle of deflection by which the strand stock is deflected at a guide element (2), particularly in order to follow the path of the longitudinal groove, is the same at two consecutive guide elements (2).
- A method of manufacturing a rotor bow (1) according to one of claims 1 to 9 for a rotatably mounting in a machine for processing elongate strand stock, wherein
the rotor bow (1), which serves to twist the strand stock, comprises:an extension substantially along a longitudinal axis (3), at least sections of which are curved;a cross-section described by a cross-sectional area (4) and extending substantially right-angled to the longitudinal axis (3);a longitudinal groove extending substantially parallel to the longitudinal axis (3) and having its cross-section described by a longitudinal groove cross-sectional area (10), wherein the strand stock can be movably guided in the direction of the longitudinal axis (3) in said longitudinal groove of the rotor bow (1);at least one guide element (2) which covers at least portions of said longitudinal groove and which is adapted for guiding the strand stock;wherein the rotor bow (1) with the longitudinal groove is manufactured from plastic reinforced with fibers as a solid body profile, wherein the cross-sectional area (4) has an elliptical basic form, and wherein the at least one guiding element (2) is connected to the rotor bow (1). - A machine for processing elongate strand stock comprising a rotor bow (1) according to at least one of the claims 1 to 9.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL11701763T PL2556518T3 (en) | 2010-04-09 | 2011-01-27 | Flyer bow and method for the production thereof |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102010014356A DE102010014356A1 (en) | 2010-04-09 | 2010-04-09 | Machine for processing elongated extrudates |
PCT/EP2011/000374 WO2011124291A1 (en) | 2010-04-09 | 2011-01-27 | Machine for processing elongate strand-form material |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2556518A1 EP2556518A1 (en) | 2013-02-13 |
EP2556518B1 true EP2556518B1 (en) | 2015-03-11 |
Family
ID=44462038
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11701763.2A Active EP2556518B1 (en) | 2010-04-09 | 2011-01-27 | Flyer bow and method for the production thereof |
Country Status (12)
Country | Link |
---|---|
US (1) | US8893464B2 (en) |
EP (1) | EP2556518B1 (en) |
JP (1) | JP5685640B2 (en) |
CN (1) | CN103125000B (en) |
BR (1) | BR112012025810B1 (en) |
DE (2) | DE102010014356A1 (en) |
ES (1) | ES2539242T3 (en) |
HU (1) | HUE026177T2 (en) |
MX (1) | MX2012011580A (en) |
PL (1) | PL2556518T3 (en) |
RU (1) | RU2569255C2 (en) |
WO (1) | WO2011124291A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
TR201818824T4 (en) | 2014-07-21 | 2019-01-21 | Keir Mfg Inc | Aerodynamic twist circle. |
DE102014011772A1 (en) | 2014-08-08 | 2016-02-11 | Maschinenfabrik Niehoff Gmbh & Co. Kg | Rotor yoke with tubular guide element, in particular for a machine for processing elongate extrudates |
JP7018750B2 (en) * | 2017-12-06 | 2022-02-14 | 京セラ株式会社 | Twisting machine |
KR102339150B1 (en) * | 2019-11-29 | 2021-12-14 | 재단법인 한국탄소산업진흥원 | Flyer bow and double twist bunching machine having the same |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3793819A (en) * | 1973-02-16 | 1974-02-26 | Anaconda Co | Quiet strander |
JPS5921998B2 (en) | 1976-08-26 | 1984-05-23 | 住友電気工業株式会社 | Double stranding machine |
DE69208964T2 (en) * | 1991-07-23 | 1996-08-14 | Bekaert Sa Nv | Guide bow |
GB9315907D0 (en) | 1993-07-31 | 1993-09-15 | Northampton Machinery Co | Apparatus for and a method of applying an elongate element in a double twist stranding machine or buncher |
US5809763A (en) * | 1996-10-16 | 1998-09-22 | Kamatics Corporation | Flyer bow having an airfoil shape in cross section |
CA2201849A1 (en) * | 1997-04-04 | 1998-10-04 | Michel Brazeau | Apparatus for making twisted wire |
JP3180077B2 (en) * | 1998-03-09 | 2001-06-25 | リグナイト株式会社 | Bow guide plate for stranded wire machine and method of manufacturing the same |
US6223513B1 (en) * | 1999-11-24 | 2001-05-01 | Kamatics Corporation | Flyer bow with integral enclosed wire guide |
US6289661B1 (en) * | 1999-12-07 | 2001-09-18 | Kamatics Corporation | Wire guide holder |
JP2002242086A (en) * | 2001-02-16 | 2002-08-28 | Sumitomo Wiring Syst Ltd | Bow for buncher |
EP1525147A4 (en) * | 2002-07-29 | 2006-08-23 | Bartell Mach Sys Llc | Flyer bow apparatus with travelling carrier strip |
EP1441063A1 (en) | 2003-01-24 | 2004-07-28 | Officine Meccaniche di Lesmo S.p.A. | Double-twist stranding machine |
US6865875B2 (en) * | 2003-03-06 | 2005-03-15 | Keir Manufacturing Inc. | Replaceable components for a flyer bow |
EP1612325B1 (en) * | 2004-06-29 | 2010-10-13 | SGL Carbon SE | Flyer bow for a wire stranding or cabling machine |
US7165387B2 (en) | 2005-03-02 | 2007-01-23 | Kamatics Corporation | Flyer bow with semi-enclosed wire guides |
JP5324887B2 (en) * | 2008-10-30 | 2013-10-23 | 矢崎総業株式会社 | Bow-shaped member of stranded wire device, stranded wire device, and stranded wire manufacturing method |
-
2010
- 2010-04-09 DE DE102010014356A patent/DE102010014356A1/en active Pending
-
2011
- 2011-01-27 CN CN201180018335.0A patent/CN103125000B/en active Active
- 2011-01-27 BR BR112012025810-9A patent/BR112012025810B1/en active IP Right Grant
- 2011-01-27 RU RU2012147586/12A patent/RU2569255C2/en active
- 2011-01-27 WO PCT/EP2011/000374 patent/WO2011124291A1/en active Application Filing
- 2011-01-27 US US13/639,947 patent/US8893464B2/en active Active
- 2011-01-27 EP EP11701763.2A patent/EP2556518B1/en active Active
- 2011-01-27 HU HUE11701763A patent/HUE026177T2/en unknown
- 2011-01-27 JP JP2013503018A patent/JP5685640B2/en active Active
- 2011-01-27 PL PL11701763T patent/PL2556518T3/en unknown
- 2011-01-27 MX MX2012011580A patent/MX2012011580A/en active IP Right Grant
- 2011-01-27 DE DE202011110557.5U patent/DE202011110557U1/en not_active Expired - Lifetime
- 2011-01-27 ES ES11701763.2T patent/ES2539242T3/en active Active
Also Published As
Publication number | Publication date |
---|---|
US8893464B2 (en) | 2014-11-25 |
US20130133304A1 (en) | 2013-05-30 |
EP2556518A1 (en) | 2013-02-13 |
ES2539242T3 (en) | 2015-06-29 |
WO2011124291A1 (en) | 2011-10-13 |
DE202011110557U1 (en) | 2014-08-22 |
MX2012011580A (en) | 2012-11-23 |
BR112012025810A2 (en) | 2016-06-28 |
PL2556518T3 (en) | 2015-08-31 |
BR112012025810B1 (en) | 2020-12-01 |
RU2569255C2 (en) | 2015-11-20 |
DE102010014356A1 (en) | 2011-10-13 |
CN103125000B (en) | 2016-12-21 |
JP2013527330A (en) | 2013-06-27 |
CN103125000A (en) | 2013-05-29 |
RU2012147586A (en) | 2014-05-20 |
JP5685640B2 (en) | 2015-03-18 |
WO2011124291A4 (en) | 2011-12-29 |
HUE026177T2 (en) | 2016-05-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1908863B1 (en) | Heddle for Jacquard loom | |
EP0402309B1 (en) | Profiled rod made from compact composite and method for producing same | |
DE19911073C2 (en) | Rope window for winches | |
EP2556518B1 (en) | Flyer bow and method for the production thereof | |
DE102016221309A1 (en) | A support structure for a power transmission element, aircraft reaction connection, flight control surface drive unit, method for attaching a power transmission element and method for producing an aircraft reaction connection | |
AT505512A1 (en) | ARRANGEMENT FOR CONNECTING A PERMANENT ELEMENT WITH ANOTHER COMPONENT | |
EP3079927B1 (en) | Assembly comprising a frame element and a connecting element, and method for securing a connecting element to a frame element | |
DE102019006280A1 (en) | Process for the production of a positive load introduction for rod-shaped fiber bundle structures and their design | |
DE102009003146A1 (en) | Electrically driven liquid pump with a multi-part rotor and manufacturing method for such a rotor | |
EP3463824A1 (en) | Method for producing an at least partially contoured, fibre reinforced plastic profile, a contoured, fibre reinforced plastic profile and its use | |
EP2953775B1 (en) | Method for producing a pvc long fibre thermoplastic | |
DE102006047412B4 (en) | Bar-shaped fiber composite structure with load introduction elements and method for the production | |
DE102014015870B4 (en) | Chassis component for a motor vehicle made from a short fiber reinforced plastic | |
EP2818594A2 (en) | Wire rope and method of manufacturing the same | |
WO2009027226A2 (en) | Method for the production of a rope-type semifinished spring element and a helical spring element, tool for machining a rope-type semifinished spring element, shaping member for shaping a rope-type semifinished spring element, and helical spring element | |
DE102010039384A1 (en) | Electrical power steering for motor car, has push rod comprising base body on which toothing and/or screw thread are arranged, where body is made from plastic and toothing and/or screw thread are formed as inserts made of metallic material | |
EP0564954B1 (en) | Chain link plate and method of manufacturing the same | |
DE102017116792B4 (en) | Switching axis shift fork-adhesive bond | |
EP3177766B1 (en) | Flyer bow comprising a tubular guiding element, especially for a machine for processing elongate strand-type material | |
WO2020048625A1 (en) | Method and strand-drawing device for producing leaf springs in fiber composite construction | |
DE102014114324B4 (en) | Unwinding device for fiber rovings | |
DE102016203805A1 (en) | Connecting arrangement with a connecting element of a fiber-matrix molding compound | |
CH681793A5 (en) | Heavy duty fibre reinforced thermoplastic component - includes load-bearing core contg. endless fibres | |
DE102011055187B4 (en) | metering rod | |
DE102014218637A1 (en) | Handrail system for passenger transport vehicles |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20121105 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
DAX | Request for extension of the european patent (deleted) | ||
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
INTG | Intention to grant announced |
Effective date: 20140922 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
INTG | Intention to grant announced |
Effective date: 20141114 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 715714 Country of ref document: AT Kind code of ref document: T Effective date: 20150415 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502011006193 Country of ref document: DE Effective date: 20150423 |
|
REG | Reference to a national code |
Ref country code: RO Ref legal event code: EPE |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: AMMANN PATENTANWAELTE AG BERN, CH |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2539242 Country of ref document: ES Kind code of ref document: T3 Effective date: 20150629 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: VDEP Effective date: 20150311 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: VDEP Effective date: 20150311 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150611 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150612 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
REG | Reference to a national code |
Ref country code: PL Ref legal event code: T3 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150713 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150711 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502011006193 Country of ref document: DE |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 6 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
26N | No opposition filed |
Effective date: 20151214 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
REG | Reference to a national code |
Ref country code: HU Ref legal event code: AG4A Ref document number: E026177 Country of ref document: HU |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20160131 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160127 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20160127 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20160127 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 7 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20160127 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 8 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150311 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: RO Payment date: 20230125 Year of fee payment: 13 Ref country code: FR Payment date: 20230123 Year of fee payment: 13 Ref country code: ES Payment date: 20230216 Year of fee payment: 13 Ref country code: CZ Payment date: 20230113 Year of fee payment: 13 Ref country code: CH Payment date: 20230130 Year of fee payment: 13 Ref country code: AT Payment date: 20230118 Year of fee payment: 13 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: TR Payment date: 20230125 Year of fee payment: 13 Ref country code: PL Payment date: 20230118 Year of fee payment: 13 Ref country code: IT Payment date: 20230131 Year of fee payment: 13 Ref country code: HU Payment date: 20230123 Year of fee payment: 13 Ref country code: DE Payment date: 20230119 Year of fee payment: 13 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230510 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20240216 Year of fee payment: 14 |