EP3381580B1 - Method and apparatus for the assemly of sail eyelets - Google Patents

Method and apparatus for the assemly of sail eyelets Download PDF

Info

Publication number
EP3381580B1
EP3381580B1 EP18164754.6A EP18164754A EP3381580B1 EP 3381580 B1 EP3381580 B1 EP 3381580B1 EP 18164754 A EP18164754 A EP 18164754A EP 3381580 B1 EP3381580 B1 EP 3381580B1
Authority
EP
European Patent Office
Prior art keywords
mold part
eyelet
abutment element
primary mold
front plate
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
EP18164754.6A
Other languages
German (de)
French (fr)
Other versions
EP3381580A1 (en
Inventor
Giuseppe PARIS
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.)
Metal P Di Paris G & C Srl
Original Assignee
Metal P Di Paris G & C Srl
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 Metal P Di Paris G & C Srl filed Critical Metal P Di Paris G & C Srl
Publication of EP3381580A1 publication Critical patent/EP3381580A1/en
Application granted granted Critical
Publication of EP3381580B1 publication Critical patent/EP3381580B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00Riveting
    • B21J15/02Riveting procedures
    • B21J15/04Riveting hollow rivets mechanically
    • B21J15/046Riveting hollow rivets mechanically by edge-curling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/06Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
    • B21J5/08Upsetting

Definitions

  • the present invention relates to a method and a corresponding apparatus for the assembly of sail eyelets.
  • Sail eyelets are generally known and widely used in fields such as maritime (where they were invented), clothing and clothing accessories, in the leather goods sector and the like.
  • sail eyelets are made up of an eyelet part and a washer, both perforated, which are applied at a perforated seat provided on a flap of a flexible material (e.g. fabric, leather, plastic and the like), so as to cover the edges of the perforated seat and reinforce them.
  • a flexible material e.g. fabric, leather, plastic and the like
  • Sail eyelets are usually made of brass for its good malleability.
  • the eyelet part has a deep-drawn portion (which extends axially) over which the perforated seat of the flap is first fitted and then the washer, so that the flap is interposed between the eyelet and the washer, with the holes of these two parts and the perforated seat substantially mutually concentric.
  • a press usually a special eyelet press
  • the axial length (or extension) of the deep-drawn portion of the eyelet is particularly important for two separate reasons: firstly it determines the stability of the anchoring, because it affects the length of the fold that constitutes the undercut through which the washer and eyelet are anchored; secondly, and perhaps more importantly, during assembly in the press, the deep-drawn portion of the eyelet is inserted into the perforated seat of the flap and retains it radially in position, ensuring that the sail eyelet is correctly applied.
  • the deep-drawn portion of the eyelet plays a critical role both at the manufacturing stage and in the assembled sail eyelet; in particular the axial length of the deep-drawn portion is a determining factor, since in fact below a certain length (variable as a function of the size of the eyelet proper and of the type and thickness of the flap) the effects of the deep-drawn portion would be canceled out.
  • EP 0 009 863 on which the preamble of claims 1 and 5 is based, and DE 32 27 686 disclose a method for the assembly of a sail eyelet on a flap of flexible material at a perforated seat.
  • the aim of the present invention consists of providing a method and a corresponding apparatus for the assembly of sail eyelets that solve the above technical problem, eliminate the drawbacks and overcome the limitations of the known art while also making it possible to use materials other than brass, while not compromising the manufacturing or the strength of the sail eyelets proper.
  • an object of the present invention is to provide a method and a corresponding apparatus for the assembly of sail eyelets that make it possible, if brass is used as the material for the eyelet, to save on the brass by reducing the quantity thereof necessary per individual sail eyelet.
  • Another object of the invention consists of providing an improved sail eyelet that is low cost, easily sourced and can substitute brass without compromising the characteristics required to sail eyelets.
  • Another object of the invention consists of providing an improved sail eyelet that is easy to implement and economically competitive when compared to the known art.
  • Another object of the invention is to provide an apparatus for the assembly of sail eyelets according to the corresponding enclosed independent claim 5.
  • another object of the invention is furthermore to provide an improved sail eyelet according to the corresponding enclosed independent claim.
  • the method of the invention relates to the assembly of a sail eyelet 1, 1A on a flap of flexible material 2 at a perforated seat 8 which is provided in said material.
  • the sail eyelet can be of the first type, designated with the reference numeral 1 or of a second type, designated with the reference numeral 1A; in general for the latter the same parts as in the former are designated with the same reference numerals followed by the letter "A".
  • the sail eyelet comprises an eyelet 3, 3A which is provided with a first hole and a washer 4, 4A which is provided with a second hole.
  • the sail eyelet 1, 1A is assembled on the flap 2
  • the first hole, the second hole and the perforated seat are substantially concentric, with the flexible material 2 interposed at least partially between the eyelet 3, 3A and the washer 4, 4A.
  • the method of assembly is carried out by way of an apparatus that comprises a press 10', 10" which is adapted to cause a plastic deformation at least of part of the eyelet 3, 3A in order to result in its anchoring on the washer 4, 4A.
  • the method for assembly the invention comprises a step of retention of the flap of flexible material 2 in position, which is obtained by temporarily inserting an abutment element 11', 11" of the press 10', 10" into the perforated seat 8 in the condition in which the eyelet 3, 3A is not anchored to the washer 4, 4A.
  • the abutment element of the press can be free, as in the case of the element 11 of the press 10, which is not stably coupled to the parts of the press 10 proper, in the manner of an insert; or the abutment element of the press can be coupled to at least one part of the press, as in the case of the element 11', 11" of the press 10', 10".
  • the abutment element 11, 11', 11" acts as a retaining shoulder, being inserted into the perforated seat 8 of the flap 2 so as to retain the latter in position; this makes it possible to avoid the use of eyelets that have a long deep-drawn part, while on the contrary making it possible to reduce the axial length of the deep-drawn part of the eyelet 3, 3A.
  • the retention function that was originally performed by the deep-drawn part of a traditional eyelet is performed by the abutment element 11, 11', 11", which is then removed when the sail eyelet 1, 1A has by that time been applied to the flap.
  • the abutment element 11', 11" also acts as a guide for the plastic deformation of the eyelet 3.
  • the abutment element 11', 11" comprises an axial extension 111', 111" which is designed to perform a function of engaging with the eyelet 3, 3A, so as to enable a simplified step of positioning of the latter: the eyelet 3, 3A is in fact fitted over the axial extension 111', 111" instead of being associated with the complementary mold part.
  • the retention of the flap of flexible material 2 in position by way of the abutment element 11, 11', 11" is a retention on a plane that is perpendicular with respect to a direction Y of approach/distancing of a primary mold part 15, 15', 15" and a complementary mold part 16, 16', 16" of the press 10, 10', 10".
  • the retention of the flap of flexible material 2 in position by way of the abutment element 11, 11', 11" is preferably maintained at least during all of the step of plastic deformation at least of part of the eyelet.
  • the step of retention of the flap of flexible material 2 in position is preceded by a step of positioning either the eyelet 3, 3A or the washer 4, 4A on the primary mold part 15, 15', 15"; after such step the abutment element 11, 11', 11" is arranged inside the hole of the eyelet 3, 3A (or of the washer 4, 4A) and remains in such position during the positioning of the flap 2 which is fitted over with the perforated seat 8 so as to surround the abutment element 11, 11', 11".
  • the sail eyelet 1 and 1A of both embodiments is preferably made of zamak, even more preferably by way of a die casting technique, so as to be relatively economic and simple to provide.
  • the principal difference between the sail eyelet 1 and the sail eyelet 1A lies in the shape structure of the parts that are subjected to plastic deformation, which make it possible to anchor the eyelet 3, 3A and the washer 4, 4A.
  • the eyelet 3 has a body part 30 (extending radially) and an edge 31 (extending axially) which are mutually connected; the edge 31 extends around the first hole and is intended to be plastically deformed during the manufacturing in order to carry out the anchoring with the washer 4.
  • the eyelet 3A comprises, in addition to the body part 30A and to the edge 31A which are arranged similarly to as described above, fixing pins 32A which extend axially (substantially parallel to the edge 31A); the washer 4A comprises passage holes into which (in the mounted condition) the pins 32A extend.
  • the anchoring between the eyelet 3A and the washer 4A occurs by virtue of the plastic deformation of the free ends of the pins 32A, which generate the necessary undercut to anchor the eyelet and the washer.
  • the presses 10, 10', 10" comprise a primary mold part 15, 15', 15" and a complementary mold part 16, 16', 16", at least one of which can move in order to allow a mutual approach/distancing in the direction Y, which is useful to causing the plastic deformation of a part of the eyelet (the edge 31 or the pins 32A) in order to thus provide the anchoring with the washer 4, 4A.
  • the primary mold part 15, 15', 15" and the complementary mold part 16, 16', 16" move toward/away from each other following a straight path Y which is vertical, the primary mold part 15, 15', 15" being positioned below the respective complementary mold part 16, 16', 16".
  • the primary mold part 15, 15', 15" has a lower accommodation seat 17, 17', 17" defined in the primary mold part 15 proper, in which the abutment element 11, 11', 11" is accommodated.
  • the main difference between the example 15 and the embodiments 15' or 15" lies in the fact that, in the former, the abutment element 11 is free and can move.
  • the abutment element 11 is inserted (for example manually) into the lower accommodation seat 17 before the eyelet and washer are anchored, and then removed when the anchoring is achieved.
  • this has shapes and dimensions that are such as to determine the plastic deformation of the edge 31 of the eyelet 3 if it is desired to assemble a sail eyelet of the type 1 described above.
  • the abutment element 11 has, in its longitudinal extension (along its height), a substantially frustum-shaped section which is useful to deform the edge 31 and create the coupling with the washer, as shown in Figures 1-3 .
  • the plan dimensions of the lower portion of the abutment element 11 are such as to allow its passage in the first hole of the eyelet 3, the dimensions being slightly smaller than the latter.
  • plan dimensions of the upper portion of the abutment element 11 on the other hand are slightly smaller than the hole of the washer 4 in order to allow the correct insertion.
  • the abutment element 11 in this example has a diameter of its top portion greater than the diameter of its lower portion, as can clearly be seen from Figures 1-3 .
  • the abutment element 11 does not necessarily have the same shape as the corresponding element in Figures 1-3 , in view of the fact that the deformation that produces the engagement between the eyelet and the washer does not occur on the rim 31, but at the pins 32A; for example while the abutment element 11 in Figures 1-3 has a substantially frustum-shaped section, the abutment element 11 in Figures 4-6 is substantially provided by joining two cylinders of different sizes, which thus identify a transverse step or notch that acts as the seat of the edge 31A of the eyelet 3A, which remains unaltered and not deformed ( Figure 6 ).
  • both the primary mold part 15, 15', 15" and the complementary mold part 16, 16', 16" have seats for accommodating the eyelet or the washer; on this point note that, irrespective of the type of sail eyelet 1 or 1A, the washer 4 or 4A in the press 10 is associated with the complementary mold part 16 which has a corresponding seat.
  • the difference between the press 10' and the press 10" lies mainly in the plate 20', 20" which is movable in the first case (press 10') and is fixed in the second case (press 10").
  • the front plate 20', 20" is interposed between the primary mold part 15', 15" and the complementary mold part 16', 16" and is provided with a passage opening in which the abutment element 11', 11", which is fixed so that it can move to the primary mold part 15', 15", slides; the abutment element 11', 11" is coupled to the primary mold part 15', 15" so that it can move elastically between an extended position and a compressed position.
  • first elastic element 21', 21" for example a spring, interposed between a base of the abutment element 11', 11" and the primary mold part 15', 15".
  • the abutment element 11', 11" can move in the direction Y of approach/distancing of the primary mold part 15', 15" and the complementary mold part 16', 16", so that it can be moved at least between an extended position, in which it protrudes from the front plate 20', 20" toward the complementary mold part 16', 16", and a compressed position, in which substantially it does not protrude from the front plate 20', 20", remaining flush with the latter.
  • the complementary mold part 16', 16" is preferably lacking the upper seat 18.
  • the eyelet 3, 3A before the coupling with the washer 4, 4A is associated with the seat provided in the complementary mold part 16', 16", so that prior to the formation of the sail eyelet 1, 1A proper, it is supported by the complementary mold part 16', 16"; in this case preferably the axial extension 111', 111" is absent and the abutment element 11', 11" has a sufficient length to retain the flap 2, but not to retain the eyelet 3, 3A in position; in this embodiment the upper complementary mold part 16', 16", at the abutment element 11', 11", is substantially flat and lacking dedicated seats.
  • the abutment element 11', 11" comprises an axial extension 111', 111" which is designed to engage the eyelet 3, 3A, when it is not yet coupled to the washer 4, 4A.
  • the axial extension 111', 111 in order to accommodate (in the closed condition on the primary mold part 15', 15") the axial extension 111', 111", has, according to the invention, a dedicated concave seat 18', 18", which overall is similar to the seat 18 in Figures 1-6 .
  • the axial extension 111', 111" can be provided in the manner of an insert and mounted on the lower portion of the abutment element 11', 11" (as in the embodiment shown) or be monolithic with it.
  • the front plate 20 is integral with the primary mold part 15", thus providing a simpler configuration.
  • the abutment element 11 has a diameter of the upper portion greater than the diameter of its lower portion.
  • the axial extension 111', 111" of the abutment element 11', 11" has a smaller diameter than the diameter of the abutment element 11', 11".
  • the front plate 20', 20" is provided with a notch 50', 50" at the edge of the front plate 20', 20" which is adjacent to the abutment element 11', 11".
  • notch enables respectively the folding of the edge 31, 32A.
  • sail eyelets preferably made of zamak
  • any shape including non-circular (in plan view), for example sail eyelets with an oval shape in plan view, or elliptical, square, polygonal and the like.
  • Another advantage of the invention consists in that it entails a solution consisting of a method of assembly and pressing that is simple overall, in which the flap is held in position correctly and stably during assembly.

Description

  • The present invention relates to a method and a corresponding apparatus for the assembly of sail eyelets.
  • Sail eyelets are generally known and widely used in fields such as maritime (where they were invented), clothing and clothing accessories, in the leather goods sector and the like.
  • Very generally, sail eyelets are made up of an eyelet part and a washer, both perforated, which are applied at a perforated seat provided on a flap of a flexible material (e.g. fabric, leather, plastic and the like), so as to cover the edges of the perforated seat and reinforce them.
  • Sail eyelets are usually made of brass for its good malleability.
  • In the manufacturing process, in fact, the eyelet part has a deep-drawn portion (which extends axially) over which the perforated seat of the flap is first fitted and then the washer, so that the flap is interposed between the eyelet and the washer, with the holes of these two parts and the perforated seat substantially mutually concentric. Then, at the assembly stage, a press (usually a special eyelet press) generates a plastic deformation of the deep-drawn portion which is folded around the washer, thus rendering the two mutually integral and stably retaining the flap of flexible material in position.
  • The axial length (or extension) of the deep-drawn portion of the eyelet is particularly important for two separate reasons: firstly it determines the stability of the anchoring, because it affects the length of the fold that constitutes the undercut through which the washer and eyelet are anchored; secondly, and perhaps more importantly, during assembly in the press, the deep-drawn portion of the eyelet is inserted into the perforated seat of the flap and retains it radially in position, ensuring that the sail eyelet is correctly applied.
  • It can thus be seen that the deep-drawn portion of the eyelet plays a critical role both at the manufacturing stage and in the assembled sail eyelet; in particular the axial length of the deep-drawn portion is a determining factor, since in fact below a certain length (variable as a function of the size of the eyelet proper and of the type and thickness of the flap) the effects of the deep-drawn portion would be canceled out.
  • Over time, this has prevented the use of materials other than brass to provide the eyelet and the washer: although different materials have in fact been tried as a substitute for it, their poor malleability has prevented their adoption; the deep-drawn portion would have had, in these cases, reduced axial extension in order to permit its plastic deformation without breaking, but this would have entailed problems both at the manufacturing stage and over the life of the sail eyelet.
  • Besides, even brass is not without its drawbacks, in the sense that apart from a relatively high cost, it has drawbacks associated with its ready availability and with the resulting productivity limitations if demand is high, especially when sail eyelets are required in high volumes and with particular characteristics (e.g. glossy and shiny surface finish).
  • EP 0 009 863 , on which the preamble of claims 1 and 5 is based, and DE 32 27 686 disclose a method for the assembly of a sail eyelet on a flap of flexible material at a perforated seat.
  • The aim of the present invention consists of providing a method and a corresponding apparatus for the assembly of sail eyelets that solve the above technical problem, eliminate the drawbacks and overcome the limitations of the known art while also making it possible to use materials other than brass, while not compromising the manufacturing or the strength of the sail eyelets proper.
  • Within this aim, an object of the present invention is to provide a method and a corresponding apparatus for the assembly of sail eyelets that make it possible, if brass is used as the material for the eyelet, to save on the brass by reducing the quantity thereof necessary per individual sail eyelet.
  • Another object of the invention consists of providing an improved sail eyelet that is low cost, easily sourced and can substitute brass without compromising the characteristics required to sail eyelets.
  • Another object of the invention consists of providing an improved sail eyelet that is easy to implement and economically competitive when compared to the known art.
  • This aim and these and other objects which will become better apparent hereinafter are achieved by a method for the assembly of an eyelet, as defined in claim 1.
  • As a consequence, another object of the invention is to provide an apparatus for the assembly of sail eyelets according to the corresponding enclosed independent claim 5.
  • In a related aspect, another object of the invention is furthermore to provide an improved sail eyelet according to the corresponding enclosed independent claim.
  • The dependent claims refer to optional characteristics of the invention and are understood to be an integral part of the present description.
  • Further characteristics and advantages of the invention will become better apparent from the description of some preferred, but not exclusive, embodiments of the invention which are illustrated by way of non-limiting example with the aid of the accompanying drawings wherein:
    • Figures 1-3 are cross-sectional schematic views at different times and a view of a detail of part of an example of an apparatus for the assembly of a first type of sail eyelet, not part of the present invention;
    • Figures 4-6 are cross-sectional schematic views at different times and a view of a detail of part of an example of an apparatus for the assembly of a second type of sail eyelet, not part of the present invention;
    • Figures 7-9 are cross-sectional schematic views at different times and a view of a detail of part of a first embodiment of an apparatus for the assembly of a first type of sail eyelet;
    • Figures 10-12 are cross-sectional schematic views at different times and a view of a detail of part of a second embodiment of an apparatus for the assembly of a second type of sail eyelet;
    • Figures 13-15 are cross-sectional schematic views at different times and a view of a detail of part of a third embodiment of an apparatus for the assembly of a second type of sail eyelet;
    • Figures 16-18 are cross-sectional schematic views at different times and a view of a detail of part of a third embodiment of an apparatus for the assembly of a first type of sail eyelet.
  • With reference to the figures, first the method of assembly will be described in terms of its characteristics that are common to all the embodiments of the apparatus and/or sail eyelet that will be presented.
  • In broad terms the method of the invention relates to the assembly of a sail eyelet 1, 1A on a flap of flexible material 2 at a perforated seat 8 which is provided in said material.
  • The sail eyelet can be of the first type, designated with the reference numeral 1 or of a second type, designated with the reference numeral 1A; in general for the latter the same parts as in the former are designated with the same reference numerals followed by the letter "A".
  • In both types 1 and 1A, the sail eyelet comprises an eyelet 3, 3A which is provided with a first hole and a washer 4, 4A which is provided with a second hole.
  • We will return later to the details and differences of the embodiments 3, 3A of the eyelet and 4, 4A of the washer; for now it is sufficient to note that, on principle, the mutual anchoring is provided by the plastic deformation of part of the eyelet 3, 3A with consequent engagement and retention of the washer 4, 4A.
  • Once the sail eyelet 1, 1A is assembled on the flap 2, the first hole, the second hole and the perforated seat are substantially concentric, with the flexible material 2 interposed at least partially between the eyelet 3, 3A and the washer 4, 4A.
  • The method of assembly is carried out by way of an apparatus that comprises a press 10', 10" which is adapted to cause a plastic deformation at least of part of the eyelet 3, 3A in order to result in its anchoring on the washer 4, 4A.
  • In this case too, we will return to the differences between the two embodiments 10', 10" of the press and the example of the press 10 that can be used; similarly, the same parts of the press 10 are designated with the same reference numerals followed by the primes ' or " respectively for the embodiments of the press 10', 10".
  • The method for assembly the invention comprises a step of retention of the flap of flexible material 2 in position, which is obtained by temporarily inserting an abutment element 11', 11" of the press 10', 10" into the perforated seat 8 in the condition in which the eyelet 3, 3A is not anchored to the washer 4, 4A.
  • In particular, the abutment element of the press can be free, as in the case of the element 11 of the press 10, which is not stably coupled to the parts of the press 10 proper, in the manner of an insert; or the abutment element of the press can be coupled to at least one part of the press, as in the case of the element 11', 11" of the press 10', 10".
  • In any case, the abutment element 11, 11', 11" acts as a retaining shoulder, being inserted into the perforated seat 8 of the flap 2 so as to retain the latter in position; this makes it possible to avoid the use of eyelets that have a long deep-drawn part, while on the contrary making it possible to reduce the axial length of the deep-drawn part of the eyelet 3, 3A. During the manufacturing, in fact, the retention function that was originally performed by the deep-drawn part of a traditional eyelet is performed by the abutment element 11, 11', 11", which is then removed when the sail eyelet 1, 1A has by that time been applied to the flap.
  • In some embodiments the abutment element 11', 11" also acts as a guide for the plastic deformation of the eyelet 3.
  • According to the invention, the abutment element 11', 11" comprises an axial extension 111', 111" which is designed to perform a function of engaging with the eyelet 3, 3A, so as to enable a simplified step of positioning of the latter: the eyelet 3, 3A is in fact fitted over the axial extension 111', 111" instead of being associated with the complementary mold part.
  • This makes it possible to use materials other than brass in order to provide the sail eyelet 1, 1A, for example materials with lower malleability, the use of which entails a reduced length of the deep-drawn part of the eyelet 3, 3A; on the other hand, if it is desired to use brass in any case, then the method of the invention enables a saving of such material.
  • Returning to the method, in its characteristics in common with all the embodiments, it entails that the retention of the flap of flexible material 2 in position by way of the abutment element 11, 11', 11" is a retention on a plane that is perpendicular with respect to a direction Y of approach/distancing of a primary mold part 15, 15', 15" and a complementary mold part 16, 16', 16" of the press 10, 10', 10".
  • Furthermore, the retention of the flap of flexible material 2 in position by way of the abutment element 11, 11', 11" is preferably maintained at least during all of the step of plastic deformation at least of part of the eyelet.
  • The step of retention of the flap of flexible material 2 in position, mentioned previously, is preceded by a step of positioning either the eyelet 3, 3A or the washer 4, 4A on the primary mold part 15, 15', 15"; after such step the abutment element 11, 11', 11" is arranged inside the hole of the eyelet 3, 3A (or of the washer 4, 4A) and remains in such position during the positioning of the flap 2 which is fitted over with the perforated seat 8 so as to surround the abutment element 11, 11', 11".
  • Now we will describe first the two different types of sail eyelet 1 and 1A and then the manufacturing apparatus with the associated presses 10, 10', 10".
  • The sail eyelet 1 and 1A of both embodiments is preferably made of zamak, even more preferably by way of a die casting technique, so as to be relatively economic and simple to provide.
  • The principal difference between the sail eyelet 1 and the sail eyelet 1A lies in the shape structure of the parts that are subjected to plastic deformation, which make it possible to anchor the eyelet 3, 3A and the washer 4, 4A.
  • In the first embodiment 1, the eyelet 3 has a body part 30 (extending radially) and an edge 31 (extending axially) which are mutually connected; the edge 31 extends around the first hole and is intended to be plastically deformed during the manufacturing in order to carry out the anchoring with the washer 4.
  • In the second embodiment 1A, instead, the eyelet 3A comprises, in addition to the body part 30A and to the edge 31A which are arranged similarly to as described above, fixing pins 32A which extend axially (substantially parallel to the edge 31A); the washer 4A comprises passage holes into which (in the mounted condition) the pins 32A extend. In this second embodiment, in fact, the anchoring between the eyelet 3A and the washer 4A occurs by virtue of the plastic deformation of the free ends of the pins 32A, which generate the necessary undercut to anchor the eyelet and the washer.
  • These solutions, in particular the embodiment of the sail eyelet 1A, are found to be particularly useful when the material used is zamak, which has a lower malleability than that of brass and in which, therefore, the plastic deformations must be contained and localized in order to not generate fractures or cracks.
  • Turning now to describe the various embodiments of the manufacturing apparatuses, which are also the subject of the invention, the accompanying figures show, by way of non-limiting example, two different embodiments of parts of the presses 10', 10" and an example of parts of a press 10 not forming part of the invention.
  • In all the embodiments and example, the presses 10, 10', 10" comprise a primary mold part 15, 15', 15" and a complementary mold part 16, 16', 16", at least one of which can move in order to allow a mutual approach/distancing in the direction Y, which is useful to causing the plastic deformation of a part of the eyelet (the edge 31 or the pins 32A) in order to thus provide the anchoring with the washer 4, 4A.
  • Preferably the primary mold part 15, 15', 15" and the complementary mold part 16, 16', 16" move toward/away from each other following a straight path Y which is vertical, the primary mold part 15, 15', 15" being positioned below the respective complementary mold part 16, 16', 16".
  • Preferably, in all the embodiments and example, the primary mold part 15, 15', 15" has a lower accommodation seat 17, 17', 17" defined in the primary mold part 15 proper, in which the abutment element 11, 11', 11" is accommodated.
  • The main difference between the example 15 and the embodiments 15' or 15" lies in the fact that, in the former, the abutment element 11 is free and can move.
  • The abutment element 11 is inserted (for example manually) into the lower accommodation seat 17 before the eyelet and washer are anchored, and then removed when the anchoring is achieved.
  • To this end there is preferably an upper accommodation seat 18 defined in the complementary mold part 16: when the primary mold part 15 and the complementary mold part 16 are closed, the abutment element 11 is fully contained within them, in the seats 17 and 18; this makes it possible to use an abutment element 11 that extends considerably from the seat 17 and makes it possible to easily fit the flap 2 over it.
  • Considering the abutment element 11, this has shapes and dimensions that are such as to determine the plastic deformation of the edge 31 of the eyelet 3 if it is desired to assemble a sail eyelet of the type 1 described above.
  • In this case the abutment element 11 has, in its longitudinal extension (along its height), a substantially frustum-shaped section which is useful to deform the edge 31 and create the coupling with the washer, as shown in Figures 1-3. Preferably, the plan dimensions of the lower portion of the abutment element 11 are such as to allow its passage in the first hole of the eyelet 3, the dimensions being slightly smaller than the latter.
  • The plan dimensions of the upper portion of the abutment element 11 on the other hand are slightly smaller than the hole of the washer 4 in order to allow the correct insertion.
  • In substance, the abutment element 11 in this example has a diameter of its top portion greater than the diameter of its lower portion, as can clearly be seen from Figures 1-3.
  • Turning now to examine the example shown in Figures 4-6, the abutment element 11 does not necessarily have the same shape as the corresponding element in Figures 1-3, in view of the fact that the deformation that produces the engagement between the eyelet and the washer does not occur on the rim 31, but at the pins 32A; for example while the abutment element 11 in Figures 1-3 has a substantially frustum-shaped section, the abutment element 11 in Figures 4-6 is substantially provided by joining two cylinders of different sizes, which thus identify a transverse step or notch that acts as the seat of the edge 31A of the eyelet 3A, which remains unaltered and not deformed (Figure 6).
  • Obviously, in both embodiments and example, both the primary mold part 15, 15', 15" and the complementary mold part 16, 16', 16" have seats for accommodating the eyelet or the washer; on this point note that, irrespective of the type of sail eyelet 1 or 1A, the washer 4 or 4A in the press 10 is associated with the complementary mold part 16 which has a corresponding seat.
  • Turning now to describe the press 10', 10" in the remaining figures, note that in them the abutment element 11', 11" is not free, but is fixed so that it can move to the primary mold part 15', 15".
  • According to the invention, on the primary mold part 15', 15" there is also a front plate 20', 20".
  • The difference between the press 10' and the press 10" lies mainly in the plate 20', 20" which is movable in the first case (press 10') and is fixed in the second case (press 10").
  • According to the invention, the front plate 20', 20" is interposed between the primary mold part 15', 15" and the complementary mold part 16', 16" and is provided with a passage opening in which the abutment element 11', 11", which is fixed so that it can move to the primary mold part 15', 15", slides; the abutment element 11', 11" is coupled to the primary mold part 15', 15" so that it can move elastically between an extended position and a compressed position.
  • According to the invention, there is a first elastic element 21', 21", for example a spring, interposed between a base of the abutment element 11', 11" and the primary mold part 15', 15".
  • The abutment element 11', 11" can move in the direction Y of approach/distancing of the primary mold part 15', 15" and the complementary mold part 16', 16", so that it can be moved at least between an extended position, in which it protrudes from the front plate 20', 20" toward the complementary mold part 16', 16", and a compressed position, in which substantially it does not protrude from the front plate 20', 20", remaining flush with the latter.
  • When the primary mold part 15', 15" and the complementary mold part 16', 16" move toward each other in order to achieve the plastic deformation and fix the eyelet 3, 3A and the washer 4, 4A, the abutment element 11', 11" returns toward the primary mold part 15', 15", contrasting the action of the spring 21', 21".
  • In these embodiments the complementary mold part 16', 16" is preferably lacking the upper seat 18.
  • In this manner the operation of fixing of the flap 2 is facilitated, since when the primary mold part 15', 15" and the complementary mold part 16', 16" are separated, the element 11', 11" protrudes, pushed by the spring 21', 21".
  • In a basic embodiment (not shown), the eyelet 3, 3A before the coupling with the washer 4, 4A is associated with the seat provided in the complementary mold part 16', 16", so that prior to the formation of the sail eyelet 1, 1A proper, it is supported by the complementary mold part 16', 16"; in this case preferably the axial extension 111', 111" is absent and the abutment element 11', 11" has a sufficient length to retain the flap 2, but not to retain the eyelet 3, 3A in position; in this embodiment the upper complementary mold part 16', 16", at the abutment element 11', 11", is substantially flat and lacking dedicated seats.
  • According to the invention, on the other hand, the abutment element 11', 11" comprises an axial extension 111', 111" which is designed to engage the eyelet 3, 3A, when it is not yet coupled to the washer 4, 4A.
  • In this way a simplified step of positioning the eyelet 3, 3A is possible, since this is fitted over the axial extension 111', 111" instead of being coupled to the complementary mold part 16', 16".
  • The latter, in order to accommodate (in the closed condition on the primary mold part 15', 15") the axial extension 111', 111", has, according to the invention, a dedicated concave seat 18', 18", which overall is similar to the seat 18 in Figures 1-6. The axial extension 111', 111" can be provided in the manner of an insert and mounted on the lower portion of the abutment element 11', 11" (as in the embodiment shown) or be monolithic with it.
  • Turning to the front plate 20', this can move elastically with respect to the primary mold part 15' in the direction Y (already described), there being to this end a second elastic element 25' acting between the front plate 20' and the primary mold part 15'.
  • This helps to retain the flap 2 in position in the step of closing the press 10'.
  • By contrast, in the press 10" the front plate 20" is integral with the primary mold part 15", thus providing a simpler configuration.
  • In the example in Figures 4-6, the abutment element 11 has a diameter of the upper portion greater than the diameter of its lower portion. By contrast, in the embodiments in Figures 7-18, and according to the invention, the axial extension 111', 111" of the abutment element 11', 11" has a smaller diameter than the diameter of the abutment element 11', 11".
  • Furthermore, in the embodiments in Figures 7-9 and 16-18 the front plate 20', 20" is provided with a notch 50', 50" at the edge of the front plate 20', 20" which is adjacent to the abutment element 11', 11". Such notch enables respectively the folding of the edge 31, 32A.
  • Advantageously, by way of the present invention, sail eyelets, preferably made of zamak, can be provided and applied in any shape, including non-circular (in plan view), for example sail eyelets with an oval shape in plan view, or elliptical, square, polygonal and the like.
  • By way of the invention, in fact, it is possible to break the edge at several points and so bypass the problem of the corners.
  • In practice it has been found that the method and the apparatus according to the invention achieve the intended aim and objects, since they make it possible to provide a sail eyelet made of a material also other than brass, without this entailing a bad fixing of the flap of flexible material to which the sail eyelet is applied.
  • Another advantage of the invention consists in that it entails a solution consisting of a method of assembly and pressing that is simple overall, in which the flap is held in position correctly and stably during assembly.
  • The invention, thus conceived, is susceptible of numerous modifications and variations, all of which are within the scope of the appended claims.
  • Where technical features mentioned in any claim are followed by reference signs, those reference signs have been included for the sole purpose of increasing the intelligibility of the claims and accordingly, such reference signs do not have any limiting effect on the interpretation of each element identified by way of example by such reference signs.

Claims (8)

  1. A method for the assembly of a sail eyelet (1, 1A) on a flap of flexible material (2) at a perforated seat (8) provided in said material, wherein the sail eyelet (1, 1A) comprises an eyelet (3, 3A) provided with a first hole and a washer (4, 4A) provided with a second hole, the first hole, the second hole and the perforated seat being, in the condition in which the sail eyelet (1, 1A) is assembled on the flap (2), substantially concentric, with the flexible material (2) interposed at least partly between the eyelet (3, 3A) and the washer (4, 4A), and wherein assembly is carried out by means of a press (10', 10"), comprising a primary mold part (15', 15") and a complementary mold part (16', 16"), said press causing a plastic deformation at least of part of the eyelet (3, 3A) in order to result in the anchoring thereof on the washer (4, 4A),
    the assembly method comprising a step of retention of the flap of flexible material (2) in position, which is obtained by temporarily inserting an abutment element ( 11', 11") of the press ( 10', 10") into the perforated seat (8), at least in the condition in which the eyelet (3, 3A) is not anchored to the washer (4, 4A), characterized in that said abutment element (11', 11") comprises an axial extension (111', 111") having a diameter that is smaller than the diameter of said abutment element (11', 11"), wherein the complementary mold part (16', 16") comprises a dedicated concave seat (18', 18") configured to accommodate the axial extension (111', 111") in a closed condition on the primary mold part (15', 15"), wherein a front plate (20', 20") is provided on the primary mold part (15', 15"), said front plate (20', 20") being interposed between said primary mold part (15', 15") and said complementary mold part (16', 16"), wherein said front plate (20', 20") has a passage opening in which said abutment element (11', 11") slides, said abutment element (11', 11") being fixed in an elastically movable manner to the primary mold part (15', 15"), and wherein a first elastic element (21', 21") is interposed between a base of the abutment element (11', 11") and the primary mold part (15', 15").
  2. The method according to claim 1, characterized in that the retention of the flap of flexible material (2) in position by way of the abutment element ( 11', 11") is a retention on a plane that is perpendicular with respect to a direction (Y) of approach/distancing of a primary mold part ( 15', 15") and a complementary mold part (16', 16") of the press ( 10', 10").
  3. The method according to claim 1 or 2, characterized in that the retention of the flap of flexible material (2) in position by way of the abutment element ( 11', 11") is maintained during said step of plastic deformation at least of part of the eyelet (3, 3A).
  4. The method according to claim 1, 2 or 3, characterized in that said plastic deformation is achieved at at least one of: an edge (31) of the eyelet (3) and/or a fixing pin (32A) provided on a body of the eyelet (3A).
  5. An apparatus for the assembly of a sail eyelet (1, 1A) on a flap of flexible material (2), which comprises a press ( 10', 10") provided with a primary mold part ( 15', 15") and a complementary mold part ( 16', 16"), at least one of which can move in order to allow a mutual approach/distancing along a direction (Y),
    the primary mold part ( 15', 15") being provided with a lower accommodation seat ( 17", 17"),
    and the press ( 10', 10") comprises an abutment element ( 11', 11") which can be inserted at least into the lower accommodation seat ( 17', 17"), so as to protrude from the primary mold part ( 15', 15") toward the complementary mold part ( 16', 16") in at least one condition of operation, characterized in that said abutment element (11', 11") comprises an axial extension (111', 111") having a diameter that is smaller than said abutment element (11', 11"), wherein the complementary mold part (16', 16") comprises a dedicated concave seat (18', 18") configured to accommodate the axial extension (111', 111") in a closed condition on the primary mold part (15', 15"), wherein a front plate (20', 20") is provided on the primary mold part (15', 15"), said front plate (20', 20") being interposed between said primary mold part (15', 15") and said complementary mold part (16', 16"), wherein said front plate (20', 20") has a passage opening in which said abutment element (11', 11") can slide, said abutment element (11', 11") being fixed in an elastically movable manner to the primary mold part (15', 15"), and wherein a first elastic element (21', 21") is interposed between a base of the abutment element (11', 11") and the primary mold part (15', 15").
  6. The apparatus according to claim 5, characterized in that the abutment element (11') has, in its longitudinal extension, a substantially frustum-shaped portion in order to deform an edge (31) of an eyelet (3) and create an engagement with a washer (4).
  7. The apparatus according to claim 5, characterized in that the abutment element (11', 11") can be moved between at least one extended position, in which it protrudes from the front plate (20', 20") toward the complementary mold part ( 16', 16"), and a compressed position, in which substantially it does not protrude from the front plate (20', 20").
  8. The apparatus according to claim 7, characterized in that the front plate (20', 20") is alternately elastically movable with respect to the primary mold part (15') or fixed with respect to the primary mold part (15").
EP18164754.6A 2017-03-30 2018-03-28 Method and apparatus for the assemly of sail eyelets Active EP3381580B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT102017000034811A IT201700034811A1 (en) 2017-03-30 2017-03-30 Process and assembly apparatus of perfected eyelets and sail eyelet.

Publications (2)

Publication Number Publication Date
EP3381580A1 EP3381580A1 (en) 2018-10-03
EP3381580B1 true EP3381580B1 (en) 2021-08-11

Family

ID=59683763

Family Applications (1)

Application Number Title Priority Date Filing Date
EP18164754.6A Active EP3381580B1 (en) 2017-03-30 2018-03-28 Method and apparatus for the assemly of sail eyelets

Country Status (3)

Country Link
EP (1) EP3381580B1 (en)
ES (1) ES2898404T3 (en)
IT (1) IT201700034811A1 (en)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB190414524A (en) * 1904-06-28 1905-04-13 Edwin John Davey Improvements in Metallic Eyelets or Gromets for Sails, Tents Waterproof Sheets and other like Articles.
DE7042423U (en) * 1970-11-17 1971-04-08 William Prym Werke Kg Eyelet for edging an opening in girders, in particular in tarpaulins
EP0009863A1 (en) * 1978-08-09 1980-04-16 Bennet-Bowler (Sp) Limited Method and apparatus for the attachment of reinforcing elements or fitments to thin sheet materials
DE3227686A1 (en) * 1982-07-24 1984-01-26 Omikron GmbH, 3300 Braunschweig Eyelet
US5191689A (en) * 1992-05-01 1993-03-09 Mcdonnell Douglas Corporation Grommet installation device

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
ES2898404T3 (en) 2022-03-07
EP3381580A1 (en) 2018-10-03
IT201700034811A1 (en) 2018-09-30

Similar Documents

Publication Publication Date Title
US8844335B2 (en) Low profile pilot assembly and method for metal forming dies
CN103502548B (en) The installation constitution of handle base
CN101421524A (en) Article fixture
CN101254041A (en) Slide fastener engaging element and slide fastener
EP3381580B1 (en) Method and apparatus for the assemly of sail eyelets
US20100158632A1 (en) Fastener
WO2005070247A2 (en) Swivel tack button, particularly for items of clothing such as jeans or the like, with very simple assembly and application
KR100766620B1 (en) A fastening plate to fasten a hinge arm of a furniture hinge
US20230364665A1 (en) Tapered transition pilot
EP3360436B1 (en) Device and method for applying inserts on sheet supports and kit for use with said device
US20210262510A1 (en) Fastening device for attaching two planar elements
CN206482518U (en) A kind of Quick Release quick fixation structure of toilet seat
EP0270847B1 (en) Open-faced buttons
US6839916B1 (en) Belt for casual wear
CN113969928B (en) Fastener blank and pre-assembly structure and assembly structure thereof
EP2006196A1 (en) Safety release for fender
US20050002759A1 (en) Rivet for the fastening of pieces to the bodywork of a vehicle
US2631359A (en) Method of making spring clips
US10892586B2 (en) Cage assembly and method of manufacturing the same
CN209305400U (en) A kind of adjustable slideway connecting bracket
CN209183472U (en) A kind of movable contact spring component and relay
US9346581B2 (en) Method of manufacturing and fixing metal label
KR100190390B1 (en) Jig for leather strip insertion in a car
CN211648714U (en) Integrated fixing rivet
CN212704015U (en) Gas valve casing stamping die

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

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

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

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20190326

RBV Designated contracting states (corrected)

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

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20191105

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20210301

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

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: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602018021467

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Ref country code: AT

Ref legal event code: REF

Ref document number: 1418861

Country of ref document: AT

Kind code of ref document: T

Effective date: 20210915

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20210811

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1418861

Country of ref document: AT

Kind code of ref document: T

Effective date: 20210811

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

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: 20210811

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: 20210811

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: 20210811

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: 20210811

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: 20211111

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: 20211213

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: 20210811

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: 20211111

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: 20210811

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

Effective date: 20210811

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: 20210811

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: 20211112

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2898404

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20220307

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: 20210811

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

Ref country code: DK

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

Effective date: 20210811

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602018021467

Country of ref document: DE

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

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: 20210811

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: 20210811

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: 20210811

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: 20210811

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: 20210811

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: 20210811

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: 20220512

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: 20210811

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: 20210811

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20220331

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: 20220328

Ref country code: LI

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

Effective date: 20220331

Ref country code: CH

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

Effective date: 20220331

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

Ref country code: BE

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

Effective date: 20220331

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

Ref country code: FR

Payment date: 20230316

Year of fee payment: 6

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

Ref country code: IT

Payment date: 20230310

Year of fee payment: 6

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

Effective date: 20230528

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

Ref country code: IE

Payment date: 20230621

Year of fee payment: 6

Ref country code: ES

Payment date: 20230414

Year of fee payment: 6

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: 20180328

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

Ref country code: MK

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

Effective date: 20210811

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: 20210811

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

Ref country code: DE

Payment date: 20240321

Year of fee payment: 7

Ref country code: GB

Payment date: 20240318

Year of fee payment: 7