EP2715744B1 - Verfahren zur herstellung eines hohlkörpers für elektrische verbundisolatoren und nach diesem verfahren hergestellter hohlkörper - Google Patents

Verfahren zur herstellung eines hohlkörpers für elektrische verbundisolatoren und nach diesem verfahren hergestellter hohlkörper Download PDF

Info

Publication number
EP2715744B1
EP2715744B1 EP12731082.9A EP12731082A EP2715744B1 EP 2715744 B1 EP2715744 B1 EP 2715744B1 EP 12731082 A EP12731082 A EP 12731082A EP 2715744 B1 EP2715744 B1 EP 2715744B1
Authority
EP
European Patent Office
Prior art keywords
hollow body
mandrel
winding
bell
central region
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.)
Not-in-force
Application number
EP12731082.9A
Other languages
English (en)
French (fr)
Other versions
EP2715744A1 (de
Inventor
Michaël FRITSCH
Cyril LESTARQUIT
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.)
Reinhausen France SAS
Original Assignee
MacLean Power France SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MacLean Power France SAS filed Critical MacLean Power France SAS
Priority to PL12731082T priority Critical patent/PL2715744T3/pl
Publication of EP2715744A1 publication Critical patent/EP2715744A1/de
Application granted granted Critical
Publication of EP2715744B1 publication Critical patent/EP2715744B1/de
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B17/00Insulators or insulating bodies characterised by their form
    • H01B17/56Insulating bodies
    • H01B17/60Composite insulating bodies
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B19/00Apparatus or processes specially adapted for manufacturing insulators or insulating bodies
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B17/00Insulators or insulating bodies characterised by their form
    • H01B17/36Insulators having evacuated or gas-filled spaces

Definitions

  • the invention generally relates to a method for manufacturing hollow bodies for composite electrical insulators, during which a first helical winding is performed on a mandrel with a longitudinal axis of at least one strip material.
  • the invention also relates to a hollow body for composite electrical insulator for very high, high and medium voltage, obtained by such a method.
  • composite electrical insulators for very high, medium and high voltage comprise a hollow body that can have a cylindrical, frustoconical, bi-frustoconical shape, a barrel shape or any other adapted form of revolution.
  • Metal reinforcements are provided at the ends of the hollow body and an elastomeric insulating envelope surrounds the hollow body forming fins.
  • These hollow bodies are used more particularly envelopes for electrical equipment, such as a capacitor or an oil-insulated transformer or a gas-insulated circuit breaker under a pressure of a few bars.
  • the hollow body of such a composite electrical insulator is generally made by helical winding of fibers or inorganic or organic son, such as glass fibers agglomerated with a synthetic resin capable of curing, for example epoxy resin.
  • the publication US 4,495,381 discloses a hollow composite electrical insulator obtained by helically winding, on a rotating mandrel, a fiber web having passed through a bath of liquid resin.
  • the helical winding is made in a first direction to obtain a first layer of fibers and, once the first end of the mandrel is reached, in a second opposite direction to obtain a second layer of fibers, inverted, wound on the first layer.
  • a third layer is made and so on until that the thickness of the desired wall is reached.
  • the resin is then cured to obtain the finished hollow body.
  • a composite electrical insulator hollow body thus delimits a gas chamber, generally a pressurized gas comprising for example SF6 gas.
  • the composite electrical insulator hollow body must therefore withstand the almost constant pressure of this gas but also any overpressure related to a malfunction, for example a fault on the terminals, inducing a point overpressure generating a shock wave.
  • the known composite electrical insulators are usually made of fiberglass composite materials coated with epoxy resin, a material known to be rather brittle. Attempts to manufacture a reliable epoxy resin insulation have led to relatively thick walls and thus to heavy insulators, difficult to handle during their manufacture, maintenance or repair. In addition, SF6 gas decomposition products can occur as a result of electric arcs generated during the power failure.
  • the document WO 2011/026 519 describes a composite insulator whose hollow body is made by helical winding to resist this type of mechanical and chemical stresses.
  • This hollow body comprises an undercoat obtained by helical winding of a polyester-based fabric provided under the helical winding layers of fiber web. This underlayer allows the insulator to better resist decomposition products and shock waves.
  • the object of the invention is to overcome these disadvantages by providing a hollow body manufacturing method for composite electrical insulators generating less waste than known methods, easy to implement, compatible with the presence of an undercoat resistant to gas, allowing the manufacture of several hollow bodies for composite electrical insulators on the same mandrel and limiting the need to use intermediate flanges to seal the enclosure defined by the hollow body of the composite electrical insulator.
  • the subject of the invention is a method for manufacturing hollow bodies for composite electrical insulators, during which a first helical winding is carried out on a longitudinal axis mandrel of at least one strip material, characterized in that that a mandrel comprising at least one at least partly spherical end shaped to produce a hollow body for a composite electrical isolator of "bell" type and at least one peripheral circular groove dividing in at least two parts the central zone separating the ends of the mandrel, this central zone being a cylinder of revolution, in that said first helical winding is carried out so as to constitute at least one hollow body for a composite electrical insulator of the "bell” type, and in that one cutting said first helical winding transversely to the longitudinal axis, following the peripheral groove to form at least two horns hollow ps for composite electrical insulators, at least one of which is of the "bell” type, and in that these two hollow bodies are axially spaced from one another to separate them from
  • helical winding any multi-turn helical winding comprising one or more layers, the layers being obtained by reversing the longitudinal displacement during the winding, in particular when the ends of the mandrel are reached.
  • bell-type insulator is understood to mean any insulator having a "bell-like” shape, this "bell-like” shape being conventional with inversion of curvature and flared edge, or comprising a spherical portion extended by a cylindrical portion. , or any other suitable form.
  • the method according to the invention thus makes it possible to simultaneously manufacture at least two insulators by limiting the amount of waste.
  • the method according to the invention makes it possible to obtain isolators whose shape makes it possible to overcome the need to use an intermediate piece to ensure the tightness of the enclosure delimited by the hollow body of the insulator. .
  • a rotary mandrel is advantageously used.
  • a first helical winding of contiguous turns around said median zone separating the ends of said mandrel and around said end is made, at least partially covering said first helical winding.
  • non-contiguous turns are meant turns that do not tangent, which are spaced a few millimeters to several centimeters apart. Non-joined turns can also intersect. Joining turns are understood to mean turns which tangent or even overlap.
  • a second embodiment of the method according to the invention at least partly covers said end and the adjacent end of said median zone separating the ends of said mandrel by means of at least one envelope distinct from said strip, and thereafter, at least the edges of said envelope covering said adjacent end of said area are covered median by means of said helical winding for bonding said helical winding to said casing.
  • said end "tick” has a shape at least partly spherical extended towards said longitudinal axis by a substantially flat portion and substantially perpendicular to said longitudinal axis.
  • the invention also relates to a hollow body for composite electrical insulator, characterized in that it has a bell-like shape to constitute a composite electrical insulator of "bell" type, the top of said bell-like shape being traversed by an orifice, said bell-like shape comprising at least a substantially cylindrical "bell” portion of longitudinal axis revolution extended by a prolonged substantially spherical "bell” portion, at least within said shape of "bell” type, by a substantially flat portion of "bell” substantially perpendicular to said longitudinal axis and surrounding said orifice, said portion of substantially flat "bell” being adapted to receive the support of an elastic seal surrounding said orifice.
  • the hollow body for isolator according to the invention thus makes it possible to dispense with an intermediate flange to ensure the tightness of the enclosure delimited by the hollow body.
  • Said substantially flat "bell" portion preferably has a surface state having a roughness Ra of less than 3.2 ⁇ m and preferably less than 0.8 ⁇ m.
  • the hollow body 2 for composite electrical insulators 1 obtained with the method according to the invention is said bell-shaped body type, the base of the "bell” being provided with a fastener 3 serving as a reinforcement for the anchoring of the hollow body 2.
  • the hollow body 2 is provided at its semi-spherical apex with a through hole 20.
  • the bell-like shape comprises a substantially cylindrical "bell" portion 21 of longitudinal axis Y extended by a portion of "bell" substantially spherical 22, flattened at the top, that is to say that the orifice 20 is located in a substantially flat "bell” portion 23 surrounding the orifice 20.
  • the orifice 20 has for example a diameter D0 about 140 mm. It is understood that this dimensional value as well as the following values are given for information only.
  • the substantially cylindrical "bell” portion 21 may have an outside diameter D1 of about 380 mm, an internal diameter D2 of about 340 mm and therefore a substantially constant thickness E1 of about 20 mm, and a length L1 of about 330 mm.
  • the substantially spherical "bell” portion 22 has, for example, an inner radius of curvature R1 of about 100 mm while maintaining the substantially constant thickness of 20 mm.
  • the substantially flat "bell" portion 21 is substantially perpendicular to the longitudinal axis Y and extends over a width L2 of about 25 mm to the orifice 20. This substantially flat "bell” portion 21 has a surface condition having a roughness Ra of less than 3.2 ⁇ m and preferably less than 0.8 ⁇ m.
  • this substantially flat "bell" portion 21 is adapted to receive, directly, the support of an elastic seal (not shown) surrounding the orifice 20 for sealingly closing the enclosure delimited by the inner surface of the hollow body 2 of the composite electrical insulator 1.
  • this composite electrical insulator 1 does not require an intermediate flange as is the case for composite electrical insulators substantially cylindrical or frustoconical known.
  • the hollow body 2 is made of glass fibers impregnated with epoxy resin, the internal face of the bell-like shape being able to be covered by a film 24, for example made of polyester, reinforcing the mechanical and chemical characteristics of the electrical insulator. composite 1 and thus allowing it to better withstand any operating shock wave and to form a barrier to any decomposition products of the gas, for example SF6 gas, which may be contained in the composite electrical insulator 1.
  • a film 24 for example made of polyester
  • the manufacturing method according to the invention described below makes it possible to produce any hollow body 2 for a composite electrical insulator 1 of the "bell" type comprising or not comprising, in an inner layer, a film 24 of polyester or any other suitable material. to strengthen the protection of the body hollow 2.
  • the fastener 3 is in the form of a substantially circular ring of a height H1 of about 75 mm, outer diameter D3 of about 465 mm and inner diameter D4 of about 340 mm.
  • This fastener 3 comprises a bore 30 with a peripheral inner boss 31 having a diameter D5 of about 380 mm, into which the cylindrical base of the hollow body 2 bears against the peripheral inner boss 31.
  • the workpiece fixing device 3 comprises an annular flange provided with fixing orifices 32 distributed on its periphery, opening into bosses 33 and able to receive the passage for example of screws (not shown) for fixing the attachment part 3 on a support ( not shown).
  • the fastener 3 further comprises three notches 34 opening radially, regularly distributed angularly on its periphery and can be used for the angular positioning of the fastener 3, and thus the hollow body 2, relative to the support.
  • the fastener 3 is for example made of aluminum.
  • a mandrel 4 of longitudinal axis X is used, driven in rotation by any suitable means, for example motorized pins (not shown).
  • the mandrel 4 is rotated in a single direction. It is understood that the mandrel 4 can also be rotated in both directions of rotation.
  • the mandrel 4 has a substantially cylindrical central zone 40 of revolution, with a longitudinal axis X, on which is provided a circular peripheral groove 41 which divides the winding surface of the central zone 40 into two distinct cylindrical portions of revolution. In this example, these two cylindrical portions of revolution are substantially of the same length along the longitudinal axis X.
  • This peripheral circular groove 41 has example a width of 12 mm and a depth of 35 mm.
  • the mandrel 4 is also provided, at the ends of its central zone 40, with two ends 42 of "bell" type 42.
  • the ends 42 have a flattened axial end 43 (visible on the Figures 3 to 7 , 8 and 9 ) which defines a flat surface substantially perpendicular to the longitudinal axis X.
  • a first band 5 is wound to form helical turns.
  • the ends 42 are covered by the turns of the first band 5 which thus defines a covering piece.
  • the supply of the first band 5, not shown, is provided for example by a reel, motorized or not, coupled to voltage regulation means and means for guiding and aligning the first band 5. These means being known to those skilled in the art, they are not detailed.
  • a fixed mandrel is used around which the guide and / or regulating means and or the reel is moved so as to obtain the helical winding.
  • a first layer of the first helical coil 50 is obtained by the combination of the rotation of the mandrel 4 and the first web supply 5.
  • a second and subsequent layers of the first helical coil 50 are similarly obtained by changing the direction axial displacement of the guide means once the end of the mandrel 4 reached.
  • the rotation and feeding are adjusted so as to obtain, on the median zone 40, a first helical winding 50 of contiguous turns.
  • the free end of the first band 5 can be fixed to the axis of the mandrel 4, for example by means of a node (not shown). This node can be undone after the laying of a few windings of helical winding. This avoids any extra thickness related to this node and any effect of white veil.
  • a second helical winding 60 of non-contiguous turns is made.
  • the second helical winding 60 may comprise several layers of superimposed turns. This second helical winding 60 is obtained for example with adjustments relating to the pitch between turns, to the speed of axial displacement of the guide means, and to the return movements of a second strip 6 between the ends 42.
  • the figure 5 illustrates only part of the second helical winding 60 which covers the first helical winding 50 including the ends 42.
  • a third helical winding 70 with contiguous turns is formed with a band 7, which is substantially similar to the first helical winding 50, and is only partially represented on the helical winding. figure 6 .
  • the strips 5, 6, 7 of fibers used may be coated with resin before or after each helical winding, this resin being cured before or after any new helical winding.
  • the complex obtained is cut off, for example by combining a rotation of the mandrel 4 and the lateral advance of a cutting tool (not shown) towards the longitudinal axis X, following the peripheral circular groove 41.
  • the latter is deep enough to allow the passage of the cutting tool.
  • Two identical insulator hollow bodies 1 in the form of a "bell" shape are thus obtained which can be moved apart from each other along the X axis according to the arrows F to separate them from the mandrel 4. This separation can be facilitated by the use of specific tools (not shown), for example a crown of motorized traction. According to another embodiment not shown, it is possible to obtain two different insulator hollow bodies, either by using ends having different shapes, or by using a mandrel having a peripheral circular groove 41 not centered in the width of its median area 40.
  • each end 42 is covered with envelopes 8, 8 '.
  • the envelopes 8, 8 'thus define covering pieces.
  • Each envelope 8, 8 ' is formed of a sheet of a flexible material such as a polyester film, or a composite film of fibers coated or not with liquid resin.
  • each envelope may be made in a sheet of a preformed rigid material.
  • each envelope 8, 8 ' has a flower petal shape.
  • each flower petal shape is crossed by an orifice 80, 80 'adapted to receive the passage of the axis of the mandrel 4.
  • the periphery of the flower petal shape comprises petals 81, 81', for example six, designed so that when the envelope 8, 8 'is placed on the end 42, it matches the shape of the end 42 largely covering its surface.
  • the flower petal shape is designed to overlap the ends of the petals 81, 81 'with the adjacent end of the central zone 40 covered by the first winding 50.
  • the envelopes 8, 8' may comprise a radial cutout (not shown) for opening them to insert them laterally on the axis of the mandrel 4.
  • a radial cutout (not shown) for opening them to insert them laterally on the axis of the mandrel 4.
  • it is possible to use more superimposed envelopes such as at least three superposed envelopes.
  • the envelopes 8, 8 ' are bonded to each other and to the first winding by means of a binder known to those skilled in the art.
  • a second helical winding 70 is made with contiguous turns using a second strip 7.
  • This second helical winding 70 is substantially similar to the first helical winding 50, and represented on the figure 12 .
  • the second helical winding 70 can be made in the same direction, or in a direction opposite to the first helical winding 50.
  • This second helical winding 70 is made to overlap the ends of the petals 81, 81 'straddling the first winding 50.
  • the first and second strips 5, 7 may be coated with resin before or after each helical winding, this resin being cured before or after any new helical winding.
  • the resulting complex is cut along the peripheral circular groove 41 in a manner similar to the first embodiment.
  • the second embodiment it is possible to place one or more first envelopes before making the first helical winding and, after making the first helical winding, it is possible to lay even further envelopes superimposed on the first envelopes before making the second helical winding.
  • the first and second helical windings are produced by means of non-contiguous turns intersecting each other.
  • the strips 5, 6, 7 used in these processes may be strips of film, polyester yarns or fibers and / or strips of fibers or sheets of fibers, for example glass fibers and / or any other suitable strip. These strips 5, 6, 7 have for example a width of about 50 mm.
  • the layers of fibers individually have, for example, a width of approximately 3 to 4 mm.
  • Each winding can also be obtained with widths of strips 5, 6, 7 different, for example about 25 mm to cover the ends 42 and about 50 mm for the central zone 40.
  • the bands 5, 6, 7 are made of fibers and are in the form of strands, independent of each other, parallel to each other, the alignment of the strands can be provided by a comb.
  • the binder used to bind the strips 5, 6, 7 together and possibly the strips to the envelopes 8, 8 ' is a conventional binder known to those skilled in the art.
  • the steps of the method according to the invention described above can be implemented to produce a resistant underlayer, for example polyester and repeated in order to achieve the layer of composite material itself.
  • a mandrel having a single end provided with a "bell” type end the other end of the mandrel being conventional per se, insofar as a single "bell” type body must be manufactured on the mandrel.
  • a mandrel comprising a plurality of peripheral circular grooves, for example two or more, axially spaced from one another along the longitudinal axis X to manufacture simultaneously, on the same mandrel, two hollow bodies of the " bell “and one or more, tubular hollow body type cylindrical or frustoconical.

Landscapes

  • Insulating Bodies (AREA)
  • Moulding By Coating Moulds (AREA)

Claims (8)

  1. Verfahren zum Herstellen von Hohlkörpern (2) für elektrische Verbundisolatoren (1), bei dem eine erste schraubenförmige Wicklung (50, 60, 70) auf einem Dorn (4) mit Längsachse (X) aus zumindest einem Streifenmaterial (5, 6, 7) erzeugt wird,
    dadurch gekennzeichnet,
    dass ein Dorn (4), umfassend wenigstens ein zumindest teilweise sphärisches, zum Erzeugen eines Hohlkörpers (2) für elektische Verbundisolatoren (1) der Bauart "Glocke" ausgebildetes Ende (42) und wenigstens einen kreisförmig umlaufenden Hals (41), der den die Enden (42) des Dorns (4) trennenden mittleren Bereich (40) in zumindest zwei Teile teilt, eingesetzt wird, wobei der mittlere Bereich (40) ein Drehzylinder ist,
    dass die erste schraubenförmige Wicklung (50, 60, 70) derart erzeugt wird, dass zumindest ein Hohlkörper (2) für elektische Verbundisolatoren (1) der Bauart "Glocke" gebildet wird, und
    dass die erste schraubenförmige Wicklung (50, 60, 70) quer zu der Längsachse (X) und entlang des umlaufenden Halses (41) zur Bildung von wenigsstens zwei Hohlkörpern (2) für elektische Verbundisolatoren (1) zerteilt wird, von denen zumindest einer der Bauart "Glocke" ist, und
    dass die beiden Hohlkörper (2) axial voneinander entfernt werden, um sie von dem Dorn (4) abzulösen.
  2. Verfahren zum Herstellen von Hohlkörpern (2) nach Anspruch 1, dadurch gekennzeichnet, dass ein drehbarer Dorn (4) eingesetzt wird.
  3. Verfahren zum Herstellen von Hohlkörpern (2) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass eine erste schraubenförmige Wicklung (50) aus fugendichten Windungen um den die Enden (42) des Dorns (4) trennenden mittleren Bereich (40) und um das Ende (42) erzeugt wird, die erste schraubenförmige Wicklung (50) wenigstens teilweise von einer zweiten schraubenförmigen Wicklung (60) aus sich kreuzenden, nicht fugendichten Windungen bedeckt wird, und die zweite schraubenförmige Wicklung (60) wenigstens teilweise von einer dritten schraubenförmigen Wicklung (70) aus fugendichten Windungen bedeckt wird
  4. Verfahren zum Herstellen von Hohlkörpern (2) nach Anspruch 1, dadurch gekennzeichnet, dass das Ende (42) und das dem die Enden (42) des Dorns (4) trennenden mittleren Bereich (40) benachbarte Ende mittels wenigstens einer von dem Streifen (5, 6, 7) verschiedenen Hülle (8, 8') wenigstens teilweise bedeckt werden, und dass anschließend wenigstens die Ränder der das dem mittleren Bereich (40) benachbarten Ende bedeckenden Hülle (8, 8') mittels der schraubenförmigen Wicklung (50, 60, 70) zum Binden der schraubenförmigen Wicklung (50, 60, 70) an die Hülle (8, 8') bedeckt werden.
  5. Verfahren zum Herstellen von Hohlkörpern (2) nach Anspruch 4, dadurch gekennzeichnet, dass wenigstens eine Hülle (8, 8') mit einer Blumenblütenblatt Anordnung eingesetzt wird, deren Zentrum mit einer Öffnung (80, 80') versehen ist, die in der Lage ist, die Achse des Dorns (4) aufzunehmen, und deren Rand mit Blütenblättern (81, 81') versehen ist, die in der Lage sind, sich an das Ende (42) und an das dem mittleren Bereich (40) benachbarte Ende anzupassen.
  6. Verfahren zum Herstellen von Hohlkörpern (2) nach Anspruch 4, dadurch gekennzeichnet, dass wenigstens eine erste schraubenförmige Wicklung (50) aus wenigstens einem ersten Streifen (5) um den mittleren Bereich (40) erzeugt wird, bevor das Ende (42) mittels der Hülle (8, 8') bedeckt und wenigstens eine zweite schraubenförmige Wicklung (70) mittels eines zweiten Streifens (7) auf die erste schraubenförmige Wicklung (50) und die Ränder der Hülle (8, 8') erzeugt wird.
  7. Verfahren zum Herstellen von Hohlkörpern (2) nach Anspruch 4, dadurch gekennzeichnet, dass mehrere Hüllen (8, 8') eingesetzt werden, die gegenseitig überdeckt und um die Längsachse (X) gegenseitig im Winkel versetzt werden.
  8. Verfahren zum Herstellen von Hohlkörpern (2) nach Anspruch 1, dadurch gekennzeichnet, dass ein Dorn (4) eingesetzt wird, dessen Ende (42) eine wenigstens teilweise sphärische Gestalt aufweist, die zu der Längsachse (X) durch einen im Wesentlichen planen und im Wesentlichen quer zu der Längsachse (X) verlaufenden Abschnitt verlängert ist.
EP12731082.9A 2011-05-27 2012-05-29 Verfahren zur herstellung eines hohlkörpers für elektrische verbundisolatoren und nach diesem verfahren hergestellter hohlkörper Not-in-force EP2715744B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL12731082T PL2715744T3 (pl) 2011-05-27 2012-05-29 Sposób wytwarzania pustego korpusu dla kompozytowych izolatorów elektrycznych i pusty korpus wytwarzany tym sposobem

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1154630A FR2975814B1 (fr) 2011-05-27 2011-05-27 Procede de fabrication de corps creux pour isolateurs electriques composites et corps creux obtenu avec un tel procede
PCT/FR2012/051197 WO2012164215A1 (fr) 2011-05-27 2012-05-29 Procédé de fabrication de corps creux pour isolateurs électriques composites et corps creux obtenu avec un tel procédé

Publications (2)

Publication Number Publication Date
EP2715744A1 EP2715744A1 (de) 2014-04-09
EP2715744B1 true EP2715744B1 (de) 2015-07-08

Family

ID=46420398

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12731082.9A Not-in-force EP2715744B1 (de) 2011-05-27 2012-05-29 Verfahren zur herstellung eines hohlkörpers für elektrische verbundisolatoren und nach diesem verfahren hergestellter hohlkörper

Country Status (4)

Country Link
EP (1) EP2715744B1 (de)
FR (1) FR2975814B1 (de)
PL (1) PL2715744T3 (de)
WO (1) WO2012164215A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102019117501A1 (de) 2019-06-28 2020-12-31 Maschinenfabrik Reinhausen Gmbh Verfahren zur Herstellung eines elektrischen Hohlisolators, elektrischer Hohlisolator und Verwendung eines elektrischen Hohlisolators

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2079896A5 (de) * 1970-02-16 1971-11-12 Merlin Gerin
CH538186A (de) * 1972-09-21 1973-06-15 Sprecher & Schuh Ag Verfahren zur Herstellung eines aus gegossenem, elektrisch isolierendem, härtbarem Kunststoff bestehenden Gehäuses für Hochspannungs-Leistungsschalter und nach dem Verfahren hergestelltes Gehäuse
FR2428905A1 (fr) * 1978-06-12 1980-01-11 Merlin Gerin Enveloppe isolante a filet de protection incorpore pour appareillage electrique a isolement gazeux
US4495381A (en) 1982-09-30 1985-01-22 General Electric Company Dynamic load bearing transmission line support member
DE19653527C1 (de) * 1996-12-20 1998-08-13 Hsp Hochspannungsgeraete Porz Durchführung, insbesondere für einen Hochspannungstransformator, und Verfahren zur Herstellung einer Durchführung
US7799160B2 (en) * 2007-07-13 2010-09-21 Chung Shan Institute Of Science And Technology, Armaments Bureau, M.N.D. Method for manufacturing composite container with different opening sizes
WO2011026519A1 (en) * 2009-09-03 2011-03-10 Abb Research Ltd Hollow electric insulator and manufacturing thereof

Also Published As

Publication number Publication date
FR2975814A1 (fr) 2012-11-30
PL2715744T3 (pl) 2015-12-31
EP2715744A1 (de) 2014-04-09
WO2012164215A1 (fr) 2012-12-06
FR2975814B1 (fr) 2014-02-21

Similar Documents

Publication Publication Date Title
EP1977497B1 (de) Verfahren zur herstellung der spule eines stators einer elektrischen rotationsmaschine und auf diese weise hergestellter stator
EP2601429B2 (de) Rohrförmige kunststoffverbindungsmuffe für ein rohr mit innenauskleidung
EP3458767A1 (de) Aus verbundwerkstoff gefertigter behälter zur aufnahme eines druckfluids
WO2022200717A1 (fr) Pneumatique comprenant une structure de rigidification endurante
FR3001656A1 (fr) Procede de fabrication ameliore d'un arbre de transmission, de preference pour systeme de boite d'accessoires de turbomachine d'aeronef
FR3053623A1 (fr) Procede de fabrication d’une preforme pour materiaux composites
EP3110618B1 (de) Flugzeugreifen mit einem gürtel
EP0270412B1 (de) Herstellungsweise für den Brennkammerkörper eines Feststofftreibsatzes
EP2715744B1 (de) Verfahren zur herstellung eines hohlkörpers für elektrische verbundisolatoren und nach diesem verfahren hergestellter hohlkörper
EP0310499A1 (de) Verfahren und Vorrichtung zur Herstellung eines Faserschichtkörpers, verwendbar als Verstärkungsstruktur für ein aus mehreren Bestandteilen zusammengesetztes
EP4136382A1 (de) Verstärkter druckflüssigkeitsspeichertank
EP3277867B1 (de) Methode zur herstellung einer verstärkungsstruktur von fahrzeugreifen
EP0025971B1 (de) Vorrichtung zur kontinuierlichen Herstellung von Kunststoffrohren durch schraubenlinienförmiges Wickeln
WO2013092326A1 (fr) Pneumatique et procede de fabrication d'une ceinture de triangulation de pneumatique
EP3532313A1 (de) Gürtelverstärkung für flugzeugreifen
EP3126157B1 (de) Flugzeugreifengürtel
EP4313628B1 (de) Reifen mit umfangsausschnitt und dauerhafter versteifungsstruktur und optimierter laufflächenabflachung
FR3156185A1 (fr) Réservoir pour gaz sous pression
EP0225202A1 (de) Betonrohr mit einer aus Kunststoff bestehenden Innenauskleidung und Verfahren zu dessen Herstellung
EP4136381B1 (de) Verfahren zur herstellung eines verbundspeichertanks
FR2893111A1 (fr) Boitier pour joints, de preference pour joints radiaux d'arbres, et procede pour sa fabrication
EP2520699A1 (de) Roller zur Abdichtung eines Einlasses und Herstellungsverfahren
EP0202983A1 (de) Verfahren und Apparat zur Herstellung einer thermischen mehrschichtigen Isolierung rundum und entlang einer festen Durchfuhr und dazugehöriger Kryogenbehälter
EP4552817A1 (de) Verfahren zur herstellung eines dichten behälters zur aufnahme eines gases und/oder eines fluids
FR3153018A1 (fr) Procédé de fabrication d’un réservoir en matériau composite compartimenté

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: 20140102

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)
REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 602012008668

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: H01B0017600000

Ipc: H01B0019000000

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

RIC1 Information provided on ipc code assigned before grant

Ipc: H01B 19/00 20060101AFI20150227BHEP

Ipc: H01B 17/36 20060101ALN20150227BHEP

Ipc: H01B 17/60 20060101ALI20150227BHEP

INTG Intention to grant announced

Effective date: 20150316

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: AT

Ref legal event code: REF

Ref document number: 735944

Country of ref document: AT

Kind code of ref document: T

Effective date: 20150715

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: FRENCH

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602012008668

Country of ref document: DE

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: SPIERENBURG AND PARTNER AG, PATENT- UND MARKEN, CH

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 735944

Country of ref document: AT

Kind code of ref document: T

Effective date: 20150708

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20150708

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

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: 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: 20151009

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: 20150708

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: 20150708

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: 20150708

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: 20151008

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

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: 20151109

Ref country code: AT

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: 20150708

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: 20151108

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: 20150708

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: 20150708

Ref country code: ES

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: 20150708

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602012008668

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

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: 20150708

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: 20150708

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: 20150708

Ref country code: CZ

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: 20150708

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: 5

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

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: 20150708

26N No opposition filed

Effective date: 20160411

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: 20150708

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20160531

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: 20160529

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20160529

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: 6

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: 20160529

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20160529

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: 20150708

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20170519

Year of fee payment: 6

Ref country code: FR

Payment date: 20170516

Year of fee payment: 6

Ref country code: DE

Payment date: 20170523

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20170519

Year of fee payment: 6

Ref country code: PL

Payment date: 20170421

Year of fee payment: 6

Ref country code: IT

Payment date: 20170526

Year of fee payment: 6

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: 20150708

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20120529

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: 20150708

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: 20150708

Ref country code: TR

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: 20150708

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: 20150708

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: 20150708

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: 20150708

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: 20150708

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602012008668

Country of ref document: DE

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180530

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180531

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180531

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180529

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181201

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180531

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180529