EP2266170B1 - Procédé de sertissage de borne électrique et ensemble obtenu - Google Patents

Procédé de sertissage de borne électrique et ensemble obtenu Download PDF

Info

Publication number
EP2266170B1
EP2266170B1 EP08806907.5A EP08806907A EP2266170B1 EP 2266170 B1 EP2266170 B1 EP 2266170B1 EP 08806907 A EP08806907 A EP 08806907A EP 2266170 B1 EP2266170 B1 EP 2266170B1
Authority
EP
European Patent Office
Prior art keywords
wing portions
crimping
pair
subsequent
initial
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
EP08806907.5A
Other languages
German (de)
English (en)
Other versions
EP2266170A1 (fr
Inventor
Ilias Jossifidis
Andreas Bauer
El Mostafa Zindine
Flavio Fantini
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.)
Delphi International Operations Luxembourg SARL
Original Assignee
Delphi International Operations Luxembourg SARL
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 Delphi International Operations Luxembourg SARL filed Critical Delphi International Operations Luxembourg SARL
Publication of EP2266170A1 publication Critical patent/EP2266170A1/fr
Application granted granted Critical
Publication of EP2266170B1 publication Critical patent/EP2266170B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R43/00—Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors
    • H01R43/04—Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors for forming connections by deformation, e.g. crimping tool
    • H01R43/048—Crimping apparatus or processes
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R4/00—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
    • H01R4/10—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation
    • H01R4/18—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation by crimping
    • H01R4/183—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation by crimping for cylindrical elongated bodies, e.g. cables having circular cross-section
    • H01R4/184—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation by crimping for cylindrical elongated bodies, e.g. cables having circular cross-section comprising a U-shaped wire-receiving portion
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R4/00—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
    • H01R4/10—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation
    • H01R4/18—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation by crimping
    • H01R4/20—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation by crimping using a crimping sleeve
    • H01R4/203—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation by crimping using a crimping sleeve having an uneven wire-receiving surface to improve the contact
    • H01R4/206—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation effected solely by twisting, wrapping, bending, crimping, or other permanent deformation by crimping using a crimping sleeve having an uneven wire-receiving surface to improve the contact with transversal grooves or threads

Definitions

  • the present invention relates to an electric terminal crimping method and the assembly obtained by this method.
  • US patent 5,561,267 discloses a terminal to be crimped comprising wings of different size allowing covering one crimping wing onto another and a crimping method with a specifically designed stamp-anvil tool.
  • the crimped terminals encounter problems of reliability in low current and low voltage applications and more particularly, microcracks appear over time. It has been shown that crimping can lose its efficiency due to an elastic spring back phenomenon of the crimping wings which causes a reduction of the terminal pressure between the wings and the strands of crimped wire and can lead to terminal resistance increase or instabilities, or even losses of electrical contact and continuity.
  • DE102006013347 and JP2005050736 and US2007/054565 A1 disclose methods for crimping terminals.
  • the present invention relates to a method according to claim 1.
  • initial part and subsequent part of the crimping section are not necessary different parts, in particular the subsequent part may correspond to at least a portion of the initial part.
  • the invention also relates to an assembly according to claim 9.
  • a crimping process is conducted on electric terminals with an open barrel.
  • Such terminals comprise:
  • terminal element 1 has a terminal section 31 forming a force-absorbing or stress-release zone provided with wings 10, 11 designed to be closed on the insulating sheath 13 of the wire 2.
  • Front part A of the terminal element can be of any type and can possibly even be made of a second crimping section in order to create a splice, for example.
  • Such terminal elements are made by cutting and folding a metal strip of small thickness of the order of 0.2 mm to several millimetres thick.
  • this elastic spring back effect exists at the level of wings 4, 5 for crimping and even if the variations in dimensions are only of the order of several microns, this elastic spring back effect can cause intermittent loss of contact between the strands and the terminal element, particularly in low-current and low-voltage applications such as self-diagnostic procedures for elements mounted on automobiles.
  • the wire generally copper-based, has a small elastic spring back capacity which is notably smaller than that of alloys such as a copper-beryllium alloy often employed for terminal elements.
  • the invention intends to modify the mechanical crimping behaviour in order to utilize the physical phenomenon of elastic spring back in a favourable sense over a particular terminal zone.
  • a method of crimping a crimping section of an electric terminal element 1 on an electric wire 2 comprises a first crimping step for crimping the crimping section 30 on the stripped part 12 of the wire by folding wings 4, 5 on the wire 2 by means of a crimping tool comprising a stamping element 6 and an anvil 7 (See Fig.1 ).
  • a stamping element 6 made up of three parts 6a, 6b, 6c according to the example, is applied advantageously with its three parts over the whole length of the wings 4 and 5 and the anvil is applied under the barrel 3, wings 4 and 5 being continuous wings, i.e. single sections.
  • the crimping section is obtained as a function of the dimensions of the terminal and of the wire by classical crimping, a minimal amount of compression being obtained so as to close the wings onto and into the wire.
  • This first crimping step is carried out over a major part of the surface of wings 4, 5 or even the whole length of these wings by stamping element 6 over a major part or even the whole length of barrel 3 with the anvil 7.
  • the residual void obtained within the strands under the wings 4, 5 after completion of the first crimping step is of the order of about 5-10%.
  • the method comprises a second step or crimping operation, this operation being conducted in a localized zone of the wings.
  • This step is advantageously conducted in such a way that a greater amount of compression is obtained under the crimping tool than the amount of compression exerted during the first crimping step.
  • This second step is shown schematically in Figures 4 and 5b representing a first embodiment for which only parts 6a, 6c of the stamping element 6 are applied on ends 4a, 4c, 5a, 5c of the wings (See Fig.3a ), the central part 6b being advantageously slightly maintained in a set-back position in such a way that the pressure of part 6b on the wings becomes zero or about zero.
  • a second embodiment shown on Figure 5a only the stamping part element 6b is pressed on parts 4b and 5b of the wings, stamping parts 6a and 6c being advantageously slightly maintained in a set back position.
  • the second crimping step is carried out over a part of the wing surface that has undergone the first crimping step.
  • the crimped terminal has three successive zones for squeezing the wings onto the wire, two of the three zones having been subjected to the second crimping step so that subsequently the wire exerts some force on the wings at the level of the third zone.
  • the crimped terminal has three successive zones for squeezing the wings onto the wire, one of the three zones having been subjected to the second crimping step so that subsequently the wire exerts some force on the wings at the level of the other two zones.
  • the double crimping reverses the elastic spring back to make it play a positive role, i.e., to create a contact pressure between the barrel (i.e. the barrel wings) and the wire strands.
  • some portion of strand material is displaced from zones 20a and 20c to zone 20b, whereby the wire strands locally expand in zone 20b between the two tool parts 6a and 6c creating the positive effect of second crimping step.
  • the elastic spring back of the wings remains greater than that of the wire strands, in intermediate zone 20b, the wire strands press and deform the wing by expanding effect.
  • the strands under the intermediate zone 20b expand during the second crimping operation.
  • the expanding strands deform the intermediate zone 20b away from its rest position obtained after the first crimping operation.
  • the elasticity of the wings thus has a positive effect in the intermediate part 20b since it tends to compress the wire, which involves a mechanical contact pressure, and therefore a better and more reliable electrical conduction, even under mechanical or thermal stress.
  • the crimping tool shown in Figure 1 and designed for the method according to the invention comprises a common anvil 7 and separable stamping element parts 6a, 6b, 6c.
  • Such a tool can function in an automatic press traditionally used by means of a separate control for the stamping element parts 6a, 6b.
  • stamping element 6 is divided into mobile stamping element parts that can be activated separately allows conserving a perfect alignment of the terminal element with the stamping element parts and successively conducting the two operations on the same press.
  • the purpose of the common anvil is that barrel 3 is deformed during the first crimping step and keeps its form during the second crimping step.
  • the barrel thus keeps a good mechanical rigidity and a good resistance to mechanical stress in cases of traction on the wire.
  • Such a method is applicable to terminals to be crimped with an open barrel for cut-out and folded electric terminals, but also to closed-barrel terminals such as cut-out and rolled terminals made from a metal sheet.
  • the first crimping step can be executed by means of only the stamping element part 6b (for a final result, after the second crimping operation, of the type shown on Figure 3a ) or by means of only parts 6a and 6c of this stamping element (for a final result, after the second crimping operation, of the type shown in Figure 3b ), this means that parts 6a and 6c, and respectively, part 6b, remain(s) in a high position during this first crimping step without coming to be hard pressed onto wings 4 and 5 of the barrel positioned on the anvil.
  • the wings 4 and 5 nevertheless will undergo a more-or-less marked folding/crimping operation over all or a very significant part of their length beyond the sole zone(s) of the wing(s) onto which part 6b, or respectively, parts 6a/6c of the stamping element come to be applied during the second crimping step.
  • the first crimping step is applied on the central zone of the wings, or on the end zones of the wings, respectively.
  • the second crimping step which follows the first step is thus conducted by means of parts 6a, 6c, or, respectively, part 6b, according to the invention, the stamping element part 6b, or, respectively, parts 6a and 6c of this stamping part, remaining in an end-of-course position in the first step to keep the barrel in the form resulting from the first step.
  • the first crimping step crimps at least one first zone of each wing 4 and 5 of the barrel, by folding the wings in a more-or-less marked manner over a surface extending beyond said at least one first zone, and the second crimping step crimps at a advantageously second crimping height in at least one second zone of each wing 4 and 5, called the localized region of the crimping section, complementary to said at least one first zone.
  • Figure 7a shows in perspective a part of a metal sheet strip 8 which comprises a plurality (only one being shown on Figure 7 ) of blanks 9 which are to be formed into the terminal element 1.
  • the blank 9 comprises a terminal portion 14 to be formed into a terminal section to crimp the insulation sheet of an electric wire.
  • the blank 9 further comprises a crimping portion 15 to be formed into the crimping section, for crimping onto the stripped part of the electrical wire.
  • the blank further comprises a mating portion 16 for forming a front part for coupling to a complementary terminal.
  • Figure 8a shows a crimping section 30 obtained from the blank of Figure 7a , according to another embodiment of the invention, placed on the anvil 7.
  • the crimping portion is shown on Figure 7b before being formed as the crimping section 30.
  • the crimping section 30 comprises the barrel 3 receiving the stripped part 12 of the wire which comprises a plurality of parallel extending strands 17.
  • the barrel 3 comprises, on its internal face 3a, a plurality of transverse recesses 18 designed for easing the deformation of the terminal element upon crimping.
  • Wings 4 and 5 extend from the barrel 3 symmetrically with respect to the wire longitudinal axis X.
  • the central zone 4b, 5b of the wings is longer than the surrounding end zones 4a, 4c, 5a, 5c.
  • This length is measured for example, from a connection end of the wings, at which the wings are connected to the barrel 3, and which is exemplified on Fig. 8a by dotted line 19, to the opposite free end of the wing portion.
  • the dotted line 19 is a straight line running parallel to the longitudinal axis X, and the length is measured in a plane transverse to that axis.
  • the exact location of the connection end of the wings does not itself need being precisely defined. It is sufficient that the location of the connection end be the same for all the wings, so as to define a common reference for measuring the length of the wings.
  • slots 21 are performed between neighbouring wing portions 4a and 4b, 4b and 4c, 5a and 5b, 5b and 5c. These slots are performed so that, in the slot portion formed between two adjacent wing portions, the length between the connection end and the free end is lower than the length of the neighbouring wing portions.
  • the slots 21 are for example performed by a cut-out in the wings during the forming step.
  • Figure 8b shows a sectional planar view taken along line B-B of Figure 8a of one of the wing end portions 4a, 5a.
  • Figure 8c shows a similar view taken along line C-C of Figure 8a at the level of portions 4b, 5b.
  • Figure 8d is a lateral view taken along line D-D of Figure 8a showing the three stamping elements 6a, 6b, 6c before applying the crimping method.
  • the stamping elements 6a and 6c have a stamping surface.
  • At least one 6b of the stamping elements has a stamping surface that is not at the same level as the stamping surfaces of the other stamping elements 6a and 6c, relatively to the stamping movement direction.
  • the stamping elements 6a and 6c have a stamping surface located forward of the stamping elements 6b by about 0.5 mm.
  • an initial crimping step is performed for example by moving simultaneously and by a same displacement, the stamping elements 6a, 6b, 6c downward.
  • the free ends of the wings penetrate in between the strands 17 of the stripped part 12 of the wire.
  • the stamping elements 6a and 6c, in the position in which they are stopped are still located forward with respect to the intermediate stamping part 6b, for example by 0.5 mm.
  • the parts 4a, 4c, 5a and 5c of the wings will spring back from their position at the end of the initial crimping step, due to the natural elasticity of their material, to a rest position.
  • This spring back effect which might be only of few microns, and could therefore not be represented, may release the contact between the wings and the strands at the end portions 4a, 4c, 5a, and 5c.
  • a subsequent crimping step is applied, as illustrated on Figures 10a-10d .
  • the central portion 6b alone is submitted to a continuous forward movement, so as to further crimp the corresponding wing portions 4b and 5b to the strands.
  • the compression of the strands 17 in zone 20b during the subsequent crimping step will cause a displacement of strand material to the two neighbouring zones 20a and 20c.
  • This displacement will cause an expansion of the strands in zones 20a and 20c.
  • this expansion will elastically deform, in zones 20a and 20c, the wing portions 4a, 4c, 5a, 5c away from their rest position.
  • the spring back effect in zones 20a and 20c tends to bring the wing portions 4a, 4c, 5a and 5c back to their rest position, thereby tending to compress the strands 17 in this zone. Electrical connectivity is thereby improved by way of the positive spring back effect in these zones.
  • the residual void measured in zone 20b has shown to be well below 1%, even below 0.1%, and has often been observed in the range 0.05-0.01%.
  • the residual void in zones 20a and 20c remains at about 5%-10%.
  • the subsequent crimping step is performed, for example, so that the stamping elements 6a and 6c still lie forward of the central stamping element 6b at the end of the subsequent crimping step, for example by 0.03 mm.
  • the height e 2 in zones 20a and 20c is lower than the height e 1 in zone 20b such as in the embodiment of Figure 3a .
  • the subsequent crimping step is performed until the central stamping element 6b lies level with, or forward of, the end stamping elements 6a and 6c.
  • the height e 1 in the end zones 20a and 20c will be greater than the height e 2 in the central zone 20b such as in the embodiment of Figure 3b .
  • slots 21 are used between neighbouring wing portions, so that independent wing portions correspond to independently activated stamping elements.
  • a stamping element when activated, has a limited influence on the wing portions other than the wing portion directly below it.
  • the stamping force applied to each stamping element can be better controlled, is more uniform, and the process reproducibility is improved.
  • Such slots 21 could be used for any barrel geometry, whatever the lengths of the wing portions are (for example in an embodiment having all its wing portions 4a-5c of identical length). In other embodiments, it is possible not to use any slots in between the wing portions, in particular when the wing portions are of different length.
  • FIG. 11a Another embodiment differing from the previous one by the crimping portion 15 of its blank is shown on Figure 11a .
  • the lateral edge 22 of the central wing portions 4b, 5b is angled by an angle ⁇ 1 with respect to the transverse axis Y orthogonal to the longitudinal axis X.
  • the central wing portions 4b, 5b are thus bevelled so that their widths measured along the longitudinal axis X at their free end is lower than their width at their connection end.
  • This bevel is performed, for example, both for the central wing portion 4b and the central wing portion 5b, and for both their lateral edges 22.
  • the blank partly shown on Figure 11a could be formed and crimped onto an electric wire by any of the above embodiments, such as for example, by the method described above in relation to Figures 8a to 10d .
  • Figure 11b shows a blank 9 of a terminal element according to another embodiment.
  • the lateral edge 23 of the wing end portions 4a, 4c, 5a, 5c which neighbours the lateral edge 22 of the central wing portion 4b, 5b, respectively, which is angled relative to the transverse direction Y by an angle ⁇ 2 .
  • the lateral edge 23 of an end wing portion and the neighbour lateral edge 22 of a central wing portion are connected by a partly circular portion 24 so as to further minimize the stresses encountered there during the crimping process.
  • the terminal element as obtained from the blank of Figure 11b could be submitted to any of the above-described crimping methods, for example such as the one described in reference to Figure 8a to 10d .
  • the crimping portion 15 is made of only two wing portions 4a, 4b, 5a, 5b on each side.
  • the geometry of the terminal element of this embodiment is, for example, similar to the one of Figure 7b , from which the wing portions 4c, 5c have been removed.
  • Such a terminal element could be crimped onto the stripped part of an electric wire according to any of the above described embodiments, adapted to the geometry of Figure 11c .
  • a crimping tool having only two crimping elements 6a and 6b, and the method as described in relation Figures 8a to 10d is applied.
  • the resulting assembly is for example partially shown on Figure 12b (on which the terminal section is not shown).
  • the subsequent crimping step could be performed down to a height lower than the height resulting from of the initial crimping step (i.e. the first crimping operation), to provide with an assembly partially shown on Figure 12a .
  • the blank of which is partially shown on Figure 11d , it is the other short wing portions 4a, 5a of the fifth embodiment which are removed.
  • Above described crimping methods can also be applied to this embodiment.
  • transition portion between adjacent wing portions of the embodiments of Figures 11c and 11d could have any suitable shape, such as the shapes shown on Figures 7b , 11a or 11b , for example.
  • the crimping portion comprises four or more wing portions on each side, at least one of which being longer than at least one of the others.
  • One of the basic concepts of the invention comprises a first conventional crimping in a first zone. First spring-back effect then occurs after this first crimping. Then, a second crimping is performed in a nearby second zone. The exerted pressure and deformation from this second crimping pushes some amount of the strand material from the second zone into the first zone. Therefore, in the first zone some "reversed” crimping occurs, i.e. the soft material (wire) pushes on the harder material (the terminal sheet-metal). Then, a second spring-back occurs or might occur, but in the reverse and favourable direction. The more elastic sheet metal pressing on the softer wire.
  • the invention provides various improvements.
  • the crimping wings can have divided end portions, in such a way the deformations of first and second steps are easier and independent from each other. Further, the pressure along each zone is then more uniform.
  • the wings can have, before crimping, different length or highness. In this way it is possible to separately adjust the compression/compactness in each zone.
  • Concerning compactness a gauge is to give the residual void mainly within the bundle between the individual strands. With use of the invention, as can be measured under a microscope, compactness can comprise:

Claims (9)

  1. Procédé pour sertir une borne électrique (1) sur un fil (2), comprenant :
    - la fourniture d'un assemblage comprenant :
    - un fil (2) s'étendant le long d'une direction longitudinale et ayant une partie dénudée (12) comprenant une pluralité de brins (17),
    - une borne électrique (1) comprenant une section de sertissage (30) qui comprend un cylindre (3) adapté à recevoir ladite partie dénudée (12) et une pluralité de paires de portions en ailettes individuelles (4a, 5a, 4b, 5b, 4c, 5c) s'étendant depuis le cylindre (3), dans lequel des fentes (21) sont ménagées entre des portions en ailettes voisines (4a, 5a, 4b, 5b, 4c, 5c), chaque paire de portions en ailettes (4a, 5a, 4b, 5b, 4c, 5c) comprenant deux portions en ailettes (4a, 5a, 4b, 5b, 4c, 5c) qui se font mutuellement face, chaque portion en ailette (4a, 5a, 4b, 5b, 4c, 5c) ayant une extrémité de connexion connectée au cylindre (3), et une extrémité libre opposée à l'extrémité de connexion, et ayant une longueur, mesurée lors de l'étape de fourniture de l'assemblage, entre l'extrémité de connexion électrique et l'extrémité libre,
    ladite partie dénudée (12) s'étendant jusque dans ledit cylindre (3) entre les portions en ailettes (4a, 5a, 4b, 5b, 4c, 5c) de chaque paire de portions en ailettes (4a, 5a, 4b, 5b, 4c, 5c),
    - appliquer une étape de sertissage initiale, en repliant une partie initiale de la section de sertissage (30), comprenant au moins une paire de portions en ailettes (4a, 5a, 4b, 5b, 4c, 5c), par-dessus la partie dénudée (12) du fil (2),
    - appliquer une étape de sertissage successive, en repliant une partie successive de la section de sertissage (30), comprenant au moins une autre paire de portions en ailettes (4a, 5a, 4b, 5b, 4c, 5c), par-dessus la partie dénudée (12) du fil (2), de manière à comprimer les brins (17) sous la partie successive,
    dans lequel la longueur des portions en ailettes (4b, 5b) d'une paire de portions en ailettes (4b, 5b) est plus grande que celle des portions en ailettes (4a, 5a, 4c, 5c) d'une autre paire de portions en ailettes (4a, 5a, 4c, 5c),
    dans lequel les portions en ailettes (4b, 5b) avec une plus grande longueur sont soumises à l'étape de sertissage successive en provoquant un déplacement du matériau des brins vers des zones voisines, le déplacement provoquant l'expansion des brins (17) dans les zones voisines, et l'expansion déformant élastiquement les portions en ailettes voisines (4a, 5a, 4c, 5c) en éloignement d'une position de repos.
  2. Procédé selon la revendication 1, dans lequel avant ou pendant l'étape de sertissage successive, la partie initiale de la section de sertissage (30) est au moins partiellement relâchée de sorte qu'elle retourne par effet ressort à une position de repos en raison de son élasticité naturelle.
  3. Procédé selon la revendication 1 ou 2, dans lequel la partie initiale de la section de sertissage (30) comprend au moins ladite paire de portions en ailettes (4a, 5a), et dans lequel la partie successive de la section de sertissage (30) comprend au moins ladite autre paire de portions en ailettes avec une plus grande longueur (4b, 5b).
  4. Procédé selon la revendication 3, dans lequel la partie initiale de la section de sertissage (30) comprend au moins une autre paire de portions en ailettes (4c, 5c) et ladite autre paire avec une plus grande longueur (4b, 5b) est située entre ladite paire (4a, 5a) et ladite autre paire (4c, 5c) le long de la direction longitudinale du fil.
  5. Procédé selon l'une quelconque des revendications précédentes, dans lequel il est prévu un outil de sertissage comprenant une enclume commune (7) et des parties d'éléments de matriçage séparables (6a, 6b, 6c) juxtaposées le long de la direction longitudinale,
    dans lequel la borne électrique (1) est prévue avec sa partie initiale de la section de sertissage (30) en face d'au moins une partie initiale de l'élément de matriçage (6a, 6c), et sa partie successive de la section de sertissage (30) en face d'au moins une partie de matriçage successive, dans lequel l'étape de sertissage initiale comprend de déplacer la partie initiale de l'élément de matriçage (6a, 6c) vers l'enclume jusqu'à une position de matriçage initiale,
    dans lequel l'étape de sertissage successive comprend de déplacer la partie successive de l'élément de matriçage vers l'enclume jusqu'à une position de matriçage successive.
  6. Procédé selon la revendication 5, dans lequel la partie successive de l'élément de matriçage (6b) est prévue plus éloignée de l'enclume (7) que la partie initiale de l'élément de matriçage (6a, 6c), et dans lequel l'étape de sertissage initiale comprend de déplacer à la fois la partie initiale de l'élément de matriçage (6a, 6c) et la partie successive de l'élément de matriçage (6b) vers l'enclume (7) par le même déplacement.
  7. Procédé selon l'une quelconque des revendications précédentes, dans lequel l'une au moins desdites étapes d'application inclut d'introduire l'extrémité libre des portions en ailettes respectives (4a, 5a, 4b, 5b, 4c, 5c) entre les brins.
  8. Assemblage composé d'un fil (2) et d'une borne électrique (1) sertie sur ledit fil (2), l'assemblage comprenant :
    - un fil (2) s'étendant le long d'une direction longitudinale et ayant une partie dénudée (12) comprenant une pluralité de brins (17),
    - une borne électrique (1) comprenant une section de sertissage (30) qui comprend un cylindre (3) adapté à recevoir ladite partie dénudée (12) et une pluralité de paires de portions en ailettes individuelles (4a, 5a, 4b, 5b, 4c, 5c) s'étendant depuis le cylindre (3), dans lequel des fentes (21) sont ménagées entre des portions en ailettes voisines (4a, 5a, 4b, 5b, 4c, 5c), chaque paire de portions en ailettes (4a, 5a, 4b, 5b, 4c, 5c) comprenant deux portions en ailettes (4a, 5a, 4b, 5b, 4c, 5c) qui se font mutuellement face,
    dans lequel chaque portion en ailette (4a, 5a, 4b, 5b, 4c, 5c) comporte une extrémité de connexion connectée au cylindre (3) et une extrémité libre opposée à l'extrémité de connexion, et a une longueur mesurée entre l'extrémité de connexion et l'extrémité libre,
    ladite partie dénudée (12) s'étendant jusque dans ledit cylindre (3) entre les portions en ailettes (4a, 5a, 4b, 5b, 4c, 5c) de chaque paire de portions en ailettes (4a, 5a, 4b, 5b, 4c, 5c),
    dans lequel une partie initiale de la section de sertissage (30) est repliée par-dessus la partie dénudée (12) du fil (2),
    dans lequel une partie successive de la section de sertissage (30) est repliée par-dessus la partie dénudée (12) du fil (2),
    dans lequel la longueur des portions en ailettes (4b, 5b) d'une paire de portions en ailettes (4b, 5b) est plus grande que celle des portions en ailettes (4a, 5a, 4c, 5c) d'une autre paire de portions en ailettes (4a, 5a, 4c, 5c),
    dans lequel les portions en ailettes (4b, 5b) avec une plus grande longueur sont soumises à une étape de sertissage successive en provoquant un déplacement du matériau des brins vers des zones voisines, le déplacement provoquant une expansion de la pluralité de brins (17) dans des zones voisines, et l'expansion déformant élastiquement une portion en ailette voisine (4a, 5a, 4c, 5c) en éloignement d'une position de repos.
  9. Assemblage selon la revendication 8, dans lequel la partie initiale de la section de sertissage (30) comprend au moins ladite paire de portions en ailettes (4a, 5a, 4c, 5c), dans lequel la partie successive de la section de sertissage (30) comprend au moins ladite autre paire de portions en ailettes (4b, 5b), dans lequel la partie initiale de la section de sertissage (30) comprend au moins une autre paire de portions en ailettes (4c, 5c), et dans lequel ladite autre paire (4b, 5b) est située entre ladite paire (4a, 5a) et ladite autre paire (4c, 5c) le long de la direction longitudinale du fil.
EP08806907.5A 2008-03-20 2008-03-20 Procédé de sertissage de borne électrique et ensemble obtenu Active EP2266170B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IB2008/002191 WO2009115860A1 (fr) 2008-03-20 2008-03-20 Procédé de sertissage de borne électrique et ensemble obtenu

Publications (2)

Publication Number Publication Date
EP2266170A1 EP2266170A1 (fr) 2010-12-29
EP2266170B1 true EP2266170B1 (fr) 2016-11-16

Family

ID=40015978

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08806907.5A Active EP2266170B1 (fr) 2008-03-20 2008-03-20 Procédé de sertissage de borne électrique et ensemble obtenu

Country Status (3)

Country Link
EP (1) EP2266170B1 (fr)
CN (1) CN102037622B (fr)
WO (1) WO2009115860A1 (fr)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010118238A (ja) * 2008-11-12 2010-05-27 Sumitomo Wiring Syst Ltd 端子金具と電線の接続構造
DE102009047701A1 (de) * 2009-12-09 2011-06-16 Robert Bosch Gmbh Crimpverbindung mit unterschiedlichen Crimphöhen
US8454186B2 (en) 2010-09-23 2013-06-04 Willis Electric Co., Ltd. Modular lighted tree with trunk electical connectors
JP5622314B2 (ja) 2010-10-12 2014-11-12 矢崎総業株式会社 コネクタ端子の電線接続構造
US8298633B1 (en) 2011-05-20 2012-10-30 Willis Electric Co., Ltd. Multi-positional, locking artificial tree trunk
US8920002B2 (en) 2011-06-21 2014-12-30 Willis Electric Co., Ltd. Wire-clasping light-emitting diode lights
US8469750B2 (en) 2011-09-22 2013-06-25 Willis Electric Co., Ltd. LED lamp assembly and light strings including a lamp assembly
US8569960B2 (en) 2011-11-14 2013-10-29 Willis Electric Co., Ltd Conformal power adapter for lighted artificial tree
US9157587B2 (en) 2011-11-14 2015-10-13 Willis Electric Co., Ltd. Conformal power adapter for lighted artificial tree
US8876321B2 (en) 2011-12-09 2014-11-04 Willis Electric Co., Ltd. Modular lighted artificial tree
WO2013110503A1 (fr) 2012-01-26 2013-08-01 Delphi Connection Systems Holding France Borne de contact électrique comprenant une section de sertissage
US9044056B2 (en) 2012-05-08 2015-06-02 Willis Electric Co., Ltd. Modular tree with electrical connector
US9179793B2 (en) 2012-05-08 2015-11-10 Willis Electric Co., Ltd. Modular tree with rotation-lock electrical connectors
US10206530B2 (en) 2012-05-08 2019-02-19 Willis Electric Co., Ltd. Modular tree with locking trunk
US9572446B2 (en) 2012-05-08 2017-02-21 Willis Electric Co., Ltd. Modular tree with locking trunk and locking electrical connectors
ITPD20120215A1 (it) * 2012-07-05 2014-01-06 Co Plast S R L Fa Capocorda per cavi di sigillatura per teloni di copertura per container a cielo aperto, di camion, tir e simili
JP5422713B1 (ja) 2012-08-24 2014-02-19 昭和電線デバイステクノロジー株式会社 リッツ線の端子接続方法及び端子金具付きリッツ線
DE102012216780B4 (de) * 2012-09-19 2015-03-26 Lisa Dräxlmaier GmbH Alterungsbeständige Crimpverbindung
US9343820B2 (en) * 2013-01-11 2016-05-17 Tyco Electronics Corporation Crimp contact and cable assembly including the same
US9439528B2 (en) 2013-03-13 2016-09-13 Willis Electric Co., Ltd. Modular tree with locking trunk and locking electrical connectors
US9671074B2 (en) 2013-03-13 2017-06-06 Willis Electric Co., Ltd. Modular tree with trunk connectors
JP5881067B2 (ja) * 2013-03-15 2016-03-09 株式会社ビスキャス 電力ケーブルの接続方法
EP2790278B1 (fr) * 2013-04-11 2017-09-27 Delphi International Operations Luxembourg S.à r.l. Matrice de sertissage
US9894949B1 (en) 2013-11-27 2018-02-20 Willis Electric Co., Ltd. Lighted artificial tree with improved electrical connections
US8870404B1 (en) 2013-12-03 2014-10-28 Willis Electric Co., Ltd. Dual-voltage lighted artificial tree
JP6297717B2 (ja) * 2014-04-24 2018-03-20 モレックス エルエルシー 端子金具
US9883566B1 (en) 2014-05-01 2018-01-30 Willis Electric Co., Ltd. Control of modular lighted artificial trees
US9800008B2 (en) * 2014-06-20 2017-10-24 Te Connectivity Corporation Terminal crimping machine having a wire clamp
JP6147232B2 (ja) 2014-08-25 2017-06-14 古河電気工業株式会社 端子付き電線の製造方法
FR3033450B1 (fr) * 2015-03-06 2017-02-17 Delphi Int Operations Luxembourg Sarl Procede de sertissage d'un contact electrique sur un cable et outil pour la mise en oeuvre de ce procede
CN105665543B (zh) * 2016-02-26 2017-07-28 宁波拓普电器有限公司 线束钣金铆压设备及使用控制方法
CN105710229B (zh) * 2016-02-26 2017-06-23 宁波拓普电器有限公司 线束钣金铆压装置及异常检测与使用控制方法
CN107317207A (zh) * 2017-07-10 2017-11-03 中车株洲电机有限公司 一种电缆线与电缆接头的连接方法
US10683974B1 (en) 2017-12-11 2020-06-16 Willis Electric Co., Ltd. Decorative lighting control
JP7185417B2 (ja) * 2018-04-05 2022-12-07 矢崎総業株式会社 端子付き電線
WO2020222706A1 (fr) 2019-04-29 2020-11-05 Bi̇med Tekni̇k Aletler Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇ Appareil d'interconnexion
EP3989363A1 (fr) 2020-10-26 2022-04-27 Aptiv Technologies Limited Terminal de sertissage électrique

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005050736A (ja) * 2003-07-30 2005-02-24 Furukawa Electric Co Ltd:The アルミ電線への端子圧着構造及び端子付アルミ電線の製造方法
US20070054565A1 (en) * 2003-08-19 2007-03-08 Thierry Courtin Electric contract crimping method and contact obtained according to said method
DE102006013347A1 (de) * 2006-03-23 2007-09-27 Kostal Kontakt Systeme Gmbh Steckverbinder mit einem durch Crimpen befestigten Leiter

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11297375A (ja) * 1998-04-15 1999-10-29 Yazaki Corp 圧着端子
DE20008544U1 (de) * 2000-05-12 2000-07-27 Viessmann Werke Kg Leiterendhülse
EP2472675B1 (fr) * 2003-07-30 2020-09-30 The Furukawa Electric Co., Ltd. Structure de sertissage de borne et procédé de sertissage de borne sur un fil électrique en aluminium
WO2007043345A1 (fr) * 2005-09-30 2007-04-19 Autonetworks Technologies, Ltd. Procédé de fabrication d'un fil électrique avec des bornes, fil électrique avec des bornes et dispositif de sertissage de bornes

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005050736A (ja) * 2003-07-30 2005-02-24 Furukawa Electric Co Ltd:The アルミ電線への端子圧着構造及び端子付アルミ電線の製造方法
US20070054565A1 (en) * 2003-08-19 2007-03-08 Thierry Courtin Electric contract crimping method and contact obtained according to said method
DE102006013347A1 (de) * 2006-03-23 2007-09-27 Kostal Kontakt Systeme Gmbh Steckverbinder mit einem durch Crimpen befestigten Leiter

Also Published As

Publication number Publication date
CN102037622B (zh) 2015-04-08
CN102037622A (zh) 2011-04-27
WO2009115860A1 (fr) 2009-09-24
EP2266170A1 (fr) 2010-12-29

Similar Documents

Publication Publication Date Title
EP2266170B1 (fr) Procédé de sertissage de borne électrique et ensemble obtenu
KR101103114B1 (ko) 압착 단자 피팅, 압착 단자 피팅의 제조 방법 및 단자 피팅을 구비한 전선
US8726500B2 (en) Method for manufacturing electric wire with terminal
EP0552741A2 (fr) Contact électrique, ainsi que matériel et procédé pour sa fabrication
CA2534403C (fr) Procede de sertissage de contact electrique et contact obtenu par ce procede
CN110034419B (zh) 用于连接导线的压接件
EP2609654B1 (fr) Cosse de connexion électrique ainsi que procédé et dispositif de production d'une cosse de connexion électrique
CN110718772B (zh) 具有双向锯齿部的电端子及其制造方法
US11831116B2 (en) Seam self locking crimp
CN109565140B (zh) 压接工具和使用该压接工具获得的端子

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: 20101020

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: FCI AUTOMOTIVE HOLDING

DAX Request for extension of the european patent (deleted)
17Q First examination report despatched

Effective date: 20121105

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: DELPHI INTERNATIONAL OPERATIONS LUXEMBOURG S.A R.L

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: H01R 43/048 20060101AFI20160530BHEP

Ipc: H01R 4/20 20060101ALI20160530BHEP

Ipc: H01R 4/18 20060101ALI20160530BHEP

INTG Intention to grant announced

Effective date: 20160704

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): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

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

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 846718

Country of ref document: AT

Kind code of ref document: T

Effective date: 20161215

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602008047431

Country of ref document: DE

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

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: 20161116

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20161116

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 846718

Country of ref document: AT

Kind code of ref document: T

Effective date: 20161116

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: 20170217

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: 20161116

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: 20161116

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: 20170216

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: 20161116

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

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: 20161116

Ref country code: PL

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: 20161116

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: 20170316

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: 20161116

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: 20161116

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: 20161116

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

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: 20161116

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: 20161116

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: 20161116

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: 20161116

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: 20161116

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602008047431

Country of ref document: DE

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161116

Ref country code: IT

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: 20161116

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: 20170216

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

26N No opposition filed

Effective date: 20170817

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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: 20161116

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: 20161116

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

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 NON-PAYMENT OF DUE FEES

Effective date: 20170320

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

Ref country code: CH

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

Effective date: 20170331

Ref country code: LI

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

Effective date: 20170331

Ref country code: IE

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

Effective date: 20170320

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

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 NON-PAYMENT OF DUE FEES

Effective date: 20170320

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 602008047431

Country of ref document: DE

Owner name: APTIV TECHNOLOGIES LIMITED, BB

Free format text: FORMER OWNER: DELPHI INTERNATIONAL OPERATIONS LUXEMBOURG S.A R.L., BASCHARAGE, LU

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

Free format text: REGISTERED BETWEEN 20181213 AND 20181219

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

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: 20080320

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 NON-PAYMENT OF DUE FEES

Effective date: 20161116

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

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: 20161116

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: 20170316

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

Ref country code: FR

Payment date: 20230325

Year of fee payment: 16

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230425

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

Ref country code: DE

Payment date: 20240322

Year of fee payment: 17

Ref country code: GB

Payment date: 20240319

Year of fee payment: 17