EP2714986B1 - Drahtführung und fliegerbügel mit dieser drahtführung - Google Patents

Drahtführung und fliegerbügel mit dieser drahtführung Download PDF

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Publication number
EP2714986B1
EP2714986B1 EP12728769.6A EP12728769A EP2714986B1 EP 2714986 B1 EP2714986 B1 EP 2714986B1 EP 12728769 A EP12728769 A EP 12728769A EP 2714986 B1 EP2714986 B1 EP 2714986B1
Authority
EP
European Patent Office
Prior art keywords
cable
lyre
flyer bow
micro
guide
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
Application number
EP12728769.6A
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English (en)
French (fr)
Other versions
EP2714986A1 (de
Inventor
Mostafa BOUJAADA
Denis GIANONCELLI
Sophie RONDEPIERRE
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SETIC Sas
Original Assignee
SETIC Sas
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Publication date
Application filed by SETIC Sas filed Critical SETIC Sas
Priority to SI201231707T priority Critical patent/SI2714986T1/sl
Priority to PL12728769T priority patent/PL2714986T3/pl
Priority to RS20191587A priority patent/RS59792B1/sr
Publication of EP2714986A1 publication Critical patent/EP2714986A1/de
Application granted granted Critical
Publication of EP2714986B1 publication Critical patent/EP2714986B1/de
Priority to HRP20192251TT priority patent/HRP20192251T1/hr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • D07B7/021—Guiding means for filaments, strands, ropes or cables
    • 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
    • D07B2501/00—Application field
    • D07B2501/40—Application field related to rope or cable making machines
    • D07B2501/406—Application field related to rope or cable making machines for making electrically conductive cables

Definitions

  • the invention relates to the technical sector of "rotating machines” to lyre for the assembly of cables, and twisting son, strands, including those for performing double or triple torsions (so-called operations "stranding").
  • the present invention essentially relates to a guide means of the "cable” (or wire, strand, etc ..., all "cable” for simplicity).
  • Devices having lyres made of composite fibers (carbon and fiberglass, mainly), wood or steel.
  • the aerodynamics of the assembly lyre, guiding elements of the cable, cable is absolutely not optimal and, at the high speeds of rotation of the lyre considered, the resistance of the ambient air is very important, and creates a significant drag that can be disturbed, with potentially very dangerous mechanical effects. This will also have the consequence that the motor of the lyre will consume more energy.
  • Another disadvantage is that the repeated shocks on the cables as well as the "uncovered" passage of the cable in the air flow will generate dangerous vibrations in themselves and, moreover, by a pressure effect, a level of noise too important for the operator.
  • the cable passing through the lyre the air no longer causes friction and the aerodynamic shape of the lyre allows good penetration into the air and therefore a reduction in engine power.
  • the prior art includes an old patent USP 3, 570, 234 which concerns a flexible lyre constituted by a spring and which contains at least one, preferably two, springs. These elements are all flexible and aim - at the time - to ensure a precise point of entry and exit of the cable.
  • the Kamatics patent is also known WO 2006/09 40 99 PCT US / 2006/007369 which discloses a cable guide integrated into a profiled structure in "aircraft wing", for discharging wear debris through an orifice 91 formed in the guide and which is held in coincidence with the debris outlet port 82 of the lyre in that the guide is not circular on its outer surface and therefore, once set up correctly, can not rotate in the lyre.
  • openings 108, 110 through which the compression effect of the air can escape, which creates in the cable passage 106 a "fluid flow”"of a a zone of high pressure towards the orifices ", flow” without which the debris would accumulate in the passage 106 "(approximate summary of the bottom of column 2).
  • the guide 112 is described as a worn wire guide spring 112, which can easily be removed from the longitudinal bore and replaced by another because, of course, it is subject to heavy wear.
  • this guide element In order to maintain this guide element in position, it is fixed at the ends, by any known means, in particular by a screw fixing element.
  • the internal diameters of the inner tube, outside of the guide element, and outside of the "cable” will obviously be optimized so that the guide element is held slightly in position in the inner tube and so that the "cable” only has minimum vibratory spacing.
  • the invention therefore relates to a lyre of the type described above, and whose essential characteristic lies in a guide element which is a metal element preferably of spring type with "closed” turns, that is to say without space between they. The turns are therefore adjacent. This is exactly the opposite of the "open” coil solution of the Kamatics USP patent 513.
  • the present invention does not necessarily use orifices 108/110 or differential pressure 102/104, unlike the aforementioned Kamatics patent.
  • the present invention has thus overcome the prejudices of the prior art.
  • the cable will be inserted at one end of the lyre and will pass to the center of the spirals in the guide element.
  • This guide element will be made removable by sliding out of the tunnel to facilitate its replacement or simply to clean the debris and other dust.
  • the cable guide element greatly attenuated the wear of the cable (despite the increase in the area of contact with the turns, compared to that of USP '513, surprisingly) because the adjacent turns form a succession of "small bumps" and "small hollows” which unexpectedly, and according to the Applicant's non-limiting theory, attenuate the rebound effect of the cable against the walls of the elements traditional guidance while generating spot contacts of the cable rather than a continuous friction and therefore much less wear, and therefore much less debris.
  • the invention is based on a guide (or generally called “guide element") "cable” whose inner surface is formed by “micro-bumps” alternating with “micro-hollow”.
  • a closed or “adjacent” coil spring has been described above as the best embodiment so far, but any internal guide tube, which may not be a spring, will be considered provided that its inner surface is formed. micro-hump alternating with adjacent microwells.
  • the invention therefore relates to a lyre according to claim 1.
  • the guide element (EG) completely envelops the "cable”.
  • micro-bumps MB
  • micro-hollow MC
  • An order of magnitude of the amplitude (in height) of the micro-hollows and bumps is from 0.1 to 1 mm, preferably from 0.1 to 0.3 mm.
  • Said “element” is in fact of the spring type with "closed” turns, that is to say without space between them, the turns being therefore "adjacent”.
  • micro-deposition (MD) of copper debris can accumulate in the microwells (MC). Surprisingly, these micro-deposits, probably because of their tiny volume, do not disturb the advantages mentioned above; it was also noted that they were dislodged by the running of the cable and that their very small mass was that even their evacuation did not disturb the system.
  • these micro-deposits even have a "smoothing" effect on the inner surface (SI) of the guide, which further limits the bouncing of the cable.
  • the lyre will be made of carbon fiber / epoxy.
  • the guide element will preferably be made of steel.
  • the applicant has noticed a sharp reduction in the electric consumption of the lyre engine of up to 35%, directly related to the reduction of the aerodynamic drag.
  • ovoid and symmetrical profiles according to the invention have the particularity very useful in practice to allow the use of the machine in a clockwise or anti-clockwise manner without it being disassembled.
  • a noise reduction caused by said drag reduction can reach --2.5dB at high speed. (see Table 1). ⁇ u> Table 1 ⁇ / u> Lyre speed% 80% 100% Lyre according to this mention 75.8 81.3 Standard Lyre 77.7 83.8
  • Said protection element (EP) is preferably a carbon tube, put during the manufacture of the lyre.
  • any generally ovoid and symmetrical shape is suitable and is preferred, although in certain cases it may be satisfied with an "airfoil" section or aircraft wing, or any other shape that favors the entry of the lyre into the airfoil. the air at high speed of rotation.
  • the preferred embodiment of the invention is shown, where the cable guide (or wire, strand, etc.), here the preferred mode which is a spring with adjacent turns (RS), is arranged adjacent to a protective tube (EP) itself housed precisely to the assembly in the tubular orifice (O) formed throughout the length of the lyre.
  • the cable guide or wire, strand, etc.
  • the preferred mode which is a spring with adjacent turns (RS)
  • EP protective tube
  • PF is naturally determined by Di, itself adapted according to the outside diameter of the "cable", which is very slightly less than Di, in a manner that is known to reduce friction between the "cable” and (RS) and also for allow only a very small float of the "cable".
  • MD micro-deposits
  • the invention also covers all the embodiments and all the applications which will be directly accessible to the person skilled in the art upon reading the present application, and of his own knowledge.

Landscapes

  • Flexible Shafts (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Processes Specially Adapted For Manufacturing Cables (AREA)
  • Ropes Or Cables (AREA)
  • Fishing Rods (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Insulated Conductors (AREA)
  • Guides For Winding Or Rewinding, Or Guides For Filamentary Materials (AREA)

Claims (7)

  1. Schlagbügel zum Zusammenfügen/Verdrillen/Verlitzen von Kabeln, wobei dieser Schlagbügel umfasst:
    - einen Körper (C) mit einer Längsöffnung (0), ausgespart in der Masse dieses Körpers (C) über die gesamte Länge dieses Schlagbügels, und
    - ein Kabelführungselement (EG), untergebracht in dieser Öffnung (0) um das Durchlaufen in Längsrichtung des Kabels zu führen, dieses Kabelführungselement (EG) weist eine Innenfläche (SI) auf, die das Durchlaufen des Kabels (PF) begrenzt,
    dadurch gekennzeichnet, dass diese Innenfläche (SI) von einer Feder (RS) gebildet wird, die enge Windungen aufweist, die genannten Windungen dieser Feder (RS) bilden Mikro-Beulen (MB) und Mikrovertiefungen (MC), deren Amplitude in der Höhe zwischen 0,1 und 1 mm liegt.
  2. Schlagbügel nach Anspruch 1, dadurch gekennzeichnet, dass er ein rohrförmiges Schutzelement (EP) enthält, das zwischen einer Innenwand dieser Längsöffnung (0) und einer Außenfläche dieser Feder (RS) angeordnet ist.
  3. Schlagbügel nach Anspruch 2, dadurch gekennzeichnet, dass dieses Schutzrohr (EP) aus Karbon besteht.
  4. Schlagbügel nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass diese Mikro-Beulen (MB) und Mikrovertiefungen eine Amplitude mit einer Höhe zwischen 0,1 und 0,3 mm aufweisen.
  5. Schlagbügel nach einem der Ansprüche 1 bis 4,-dadurch gekennzeichnet, dass er aus Karbon-/Epoxy-Fasern hergestellt ist.
  6. Schlagbügel gemäß einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass r ein ovales, symmetrisches Strömungsprofil aufweist.
  7. Schlagbügel nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass er 2 bis 4 symmetrische, seitliche Aussparungen (a, b, c, d) aufweist.
EP12728769.6A 2011-05-27 2012-05-25 Drahtführung und fliegerbügel mit dieser drahtführung Active EP2714986B1 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
SI201231707T SI2714986T1 (sl) 2011-05-27 2012-05-25 Vodilo žice in lok s tem vodilom žice
PL12728769T PL2714986T3 (pl) 2011-05-27 2012-05-25 Prowadnica drutu oraz prowadnik pałąkowy zawierający prowadnicę drutu
RS20191587A RS59792B1 (sr) 2011-05-27 2012-05-25 Element za vođenje niti i leteći luk sa ovim elementom za vođenje niti
HRP20192251TT HRP20192251T1 (hr) 2011-05-27 2019-12-13 Element za vođenje niti i leteći luk s tim elementom za vođenje niti

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1101643A FR2975711B1 (fr) 2011-05-27 2011-05-27 Nouveau guide de fil, toron ou cable pour lyre tournante pour assemblage/tordage/toronnage de cables et/ou tordage de fils, et torons, et lyre correspondante
PCT/IB2012/001023 WO2012164367A1 (fr) 2011-05-27 2012-05-25 Guide de fil et lyre avec ce guide de fil

Publications (2)

Publication Number Publication Date
EP2714986A1 EP2714986A1 (de) 2014-04-09
EP2714986B1 true EP2714986B1 (de) 2019-09-18

Family

ID=46321166

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12728769.6A Active EP2714986B1 (de) 2011-05-27 2012-05-25 Drahtführung und fliegerbügel mit dieser drahtführung

Country Status (14)

Country Link
US (1) US9340926B2 (de)
EP (1) EP2714986B1 (de)
CY (1) CY1122502T1 (de)
DK (1) DK2714986T3 (de)
ES (1) ES2761851T3 (de)
FR (1) FR2975711B1 (de)
HR (1) HRP20192251T1 (de)
HU (1) HUE047533T2 (de)
LT (1) LT2714986T (de)
PL (1) PL2714986T3 (de)
PT (1) PT2714986T (de)
RS (1) RS59792B1 (de)
SI (1) SI2714986T1 (de)
WO (1) WO2012164367A1 (de)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3172377B1 (de) 2014-07-21 2018-09-12 KEIR Manufacturing, Inc. Aerodynamischer schlagbügel
DE102014011772A1 (de) 2014-08-08 2016-02-11 Maschinenfabrik Niehoff Gmbh & Co. Kg Rotorbügel mit rohrförmigem Führungselement, insbesondere für eine Maschine zum Verarbeiten von langgestrecktem Stranggut
US10407826B2 (en) 2015-11-16 2019-09-10 Roy R. R. Rymer Detachable flyer bow system, apparatus and methods of using same

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4378712A (en) * 1979-02-27 1983-04-05 Nippon Cable System, Inc. Control cable
EP0415333A2 (de) * 1989-08-30 1991-03-06 Nippon Cable System Inc. Steuerseil
US20050213859A1 (en) * 2004-03-12 2005-09-29 Daido Metal Company Ltd. Sliding bearing

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3570234A (en) * 1969-01-08 1971-03-16 Bell Telephone Labor Inc Pair flyer twisting using flexible bow
CH618486A5 (en) * 1977-06-20 1980-07-31 Maillefer Sa Double-twist cable-making machine
US4389266A (en) 1981-02-10 1983-06-21 Brockway Glass Co., Inc. Preparation of glass container for thermoplastic closure
JPS58125641U (ja) * 1982-02-19 1983-08-26 金井　宏之 バンチヤ−撚線機のフライヤガイド
JPS63183297A (ja) 1987-01-23 1988-07-28 Mitsubishi Electric Corp タ−ボ分子ポンプ
JPH0111759Y2 (de) * 1987-05-16 1989-04-06
US5809763A (en) 1996-10-16 1998-09-22 Kamatics Corporation Flyer bow having an airfoil shape in cross section
US6223513B1 (en) * 1999-11-24 2001-05-01 Kamatics Corporation Flyer bow with integral enclosed wire guide
ATE484624T1 (de) 2004-06-29 2010-10-15 Sgl Carbon Se Rotorbügel für drahtverlitzungs- oder drahtverseilmaschinen
US7165387B2 (en) 2005-03-02 2007-01-23 Kamatics Corporation Flyer bow with semi-enclosed wire guides

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4378712A (en) * 1979-02-27 1983-04-05 Nippon Cable System, Inc. Control cable
EP0415333A2 (de) * 1989-08-30 1991-03-06 Nippon Cable System Inc. Steuerseil
US20050213859A1 (en) * 2004-03-12 2005-09-29 Daido Metal Company Ltd. Sliding bearing

Also Published As

Publication number Publication date
WO2012164367A1 (fr) 2012-12-06
RS59792B1 (sr) 2020-02-28
SI2714986T1 (sl) 2020-07-31
DK2714986T3 (da) 2019-12-16
ES2761851T3 (es) 2020-05-21
FR2975711B1 (fr) 2013-05-24
PL2714986T3 (pl) 2020-05-18
PT2714986T (pt) 2019-12-19
HRP20192251T1 (hr) 2020-03-20
US20140196431A1 (en) 2014-07-17
LT2714986T (lt) 2020-01-27
FR2975711A1 (fr) 2012-11-30
US9340926B2 (en) 2016-05-17
EP2714986A1 (de) 2014-04-09
HUE047533T2 (hu) 2020-04-28
CY1122502T1 (el) 2021-01-27

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