WO2015177440A1 - Method for attaching a hinge to a page and method for producing a passport - Google Patents

Method for attaching a hinge to a page and method for producing a passport Download PDF

Info

Publication number
WO2015177440A1
WO2015177440A1 PCT/FR2015/051263 FR2015051263W WO2015177440A1 WO 2015177440 A1 WO2015177440 A1 WO 2015177440A1 FR 2015051263 W FR2015051263 W FR 2015051263W WO 2015177440 A1 WO2015177440 A1 WO 2015177440A1
Authority
WO
WIPO (PCT)
Prior art keywords
hinge
patterns
page
fixing
elementary
Prior art date
Application number
PCT/FR2015/051263
Other languages
French (fr)
Inventor
Aurélie BARBOTIN
Franck GEFFRAY
Original Assignee
Oberthur Technologies
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 Oberthur Technologies filed Critical Oberthur Technologies
Publication of WO2015177440A1 publication Critical patent/WO2015177440A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B42BOOKBINDING; ALBUMS; FILES; SPECIAL PRINTED MATTER
    • B42DBOOKS; BOOK COVERS; LOOSE LEAVES; PRINTED MATTER CHARACTERISED BY IDENTIFICATION OR SECURITY FEATURES; PRINTED MATTER OF SPECIAL FORMAT OR STYLE NOT OTHERWISE PROVIDED FOR; DEVICES FOR USE THEREWITH AND NOT OTHERWISE PROVIDED FOR; MOVABLE-STRIP WRITING OR READING APPARATUS
    • B42D25/00Information-bearing cards or sheet-like structures characterised by identification or security features; Manufacture thereof
    • B42D25/20Information-bearing cards or sheet-like structures characterised by identification or security features; Manufacture thereof characterised by a particular use or purpose
    • B42D25/24Passports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/08Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112Single lapped joints
    • B29C66/1122Single lap to lap joints, i.e. overlap joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/20Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/21Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/20Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/23Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being multiple and parallel or being in the form of tessellations
    • B29C66/232Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being multiple and parallel or being in the form of tessellations said joint lines being multiple and parallel, i.e. the joint being formed by several parallel joint lines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/40General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/47Joining single elements to sheets, plates or other substantially flat surfaces
    • B29C66/472Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially flat
    • B29C66/4722Fixing strips to surfaces other than edge faces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/81General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/814General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
    • B29C66/8141General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined
    • B29C66/81433General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined being toothed, i.e. comprising several teeth or pins, or being patterned
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/83General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
    • B29C66/832Reciprocating joining or pressing tools
    • B29C66/8322Joining or pressing tools reciprocating along one axis
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B31MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER; WORKING PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER
    • B31FMECHANICAL WORKING OR DEFORMATION OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER
    • B31F5/00Attaching together sheets, strips or webs; Reinforcing edges
    • B31F5/008Attaching together sheets, strips or webs; Reinforcing edges by friction, e.g. obtained ultrasonic vibrations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B42BOOKBINDING; ALBUMS; FILES; SPECIAL PRINTED MATTER
    • B42CBOOKBINDING
    • B42C11/00Casing-in
    • B42C11/06Machines or equipment for casing-in by welding plastic materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B42BOOKBINDING; ALBUMS; FILES; SPECIAL PRINTED MATTER
    • B42CBOOKBINDING
    • B42C9/00Applying glue or adhesive peculiar to bookbinding
    • B42C9/0093Applying glue or adhesive peculiar to bookbinding by fusing, welding sheets together
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • B29C66/712General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined the composition of one of the parts to be joined being different from the composition of the other part
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/731General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the intensive physical properties of the material of the parts to be joined
    • B29C66/7311Thermal properties
    • B29C66/73115Melting point
    • B29C66/73116Melting point of different melting point, i.e. the melting point of one of the parts to be joined being different from the melting point of the other part
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2017/00Carriers for sound or information
    • B29L2017/001Carriers of records containing fine grooves or impressions, e.g. disc records for needle playback, cylinder records

Definitions

  • the present invention relates to documents of the type books, such as a passport and methods of manufacturing such passports.
  • passports comprising a data page, consisting, for example, of a plastic material and intended to be inserted in a booklet of sheets constituting the visa pages and the cover pages of the passport.
  • data pages include information about the holder of the passport, called personalization data. This data can be printed on the page and / or contained in a microcircuit integrated in the data page.
  • the data pages usually include security data of the document, which data can be accessed directly visually or via appropriate equipment, so that the authenticity or possible falsification of the passport can be easily detected.
  • These data pages are intended to be attached to the passbook of the passport by means of a hinge.
  • the data page is inserted between a cover page of the booklet and a visa page of the latter. It is attached by means of a hinge.
  • the hinge is fixed on the one hand to the data page by means which are the subject of the present invention and on the other hand to the leaflet by a seam made in a median plane of the leaves of the booklet.
  • WO2014 023 482 discloses a method for fixing a polycarbonate page by means of a hinge made of a textile material. The method consists of performing an ultrasonic welding, performed at regular intervals.
  • the present invention provides a method of fixing a hinge consisting of a first material, on a page made of a second material, the first and second materials having substantially melting temperatures.
  • the hinge partially covering the page and defining a fastening zone extending laterally and longitudinally, the hinge being fixed to the page by ultrasonic welding, the welding being performed by a set of elementary solder patterns spaced apart from each other; other and arranged in the fastening zone so that the weld has several rows of elementary patterns, the rows extending substantially parallel to each other in the lateral direction of the fastening zone between two ends and having at least a first row according to first sequence of elementary patterns in which the solder goes out nd over 30% to 60% of the width of the fastening area, each of the lateral ends of the first row having at least one elementary pattern of which a first side extends substantially parallel to the longitudinal direction and at least a second side is inclined relative to the longitudinal direction, the elementary patterns arranged in the center of the first row are oriented so that the first side
  • the solder has at the longitudinal ends of the fastening zone second rows having a second sequence of elementary patterns, in which the first side of each pattern of the second row is oriented substantially parallel to the lateral direction; the patterns are spaced apart by an interval of 1 mm in the longitudinal and lateral directions;
  • the length of the first side is greater than that of the second side
  • the pattern has an oblong shape
  • the weld comprises at least three second rows of patterns arranged according to the second sequence at each of the longitudinal ends of the fastening zone;
  • each first row of the first sequence comprises two central motifs aligned in the longitudinal direction and oriented so that the first side is perpendicular to the longitudinal direction, and, on either side of these central patterns, the first row comprises two peripheral patterns aligned in the lateral direction and oriented so that the first side is parallel to the longitudinal direction;
  • the elementary pattern has rounded corners
  • the elementary patterns do not extend beyond the fixing zone, on the free side of the hinge;
  • the data pages is polycarbonate and hinge is polyurethane.
  • FIG. 1 illustrates an elevational view of a hinge welded to a data page, the weld having a preferred pattern arrangement
  • FIG. 2 illustrates a detail view of FIG.
  • FIG. 3 illustrates a perspective view of a sonotrode for making the weld visible in FIG. 1,
  • Figure 4 illustrates a side view of the sonotrode shown in Figure 3.
  • Figure 5 shows a schematic sectional view of an open passport manufactured according to the method of the invention.
  • the present invention relates to electronic documents intended to contain information for identifying the holder of said document. More particularly, the invention relates to passports 10.
  • Passports 10 are documents in the form of a book.
  • the passports 10 comprise at least: a) a booklet 12 of sheets 14 comprising a set of pages called visa pages because they are intended to receive the visa stamps, b) a cover 16 and c) sheets forming the pages 18 which are pasted on the cover 16 of the passport 10 and which are intended to receive specific information from the country distributing the passport.
  • the cover 16 of the passport 10 is made of a material having a greater thickness than that of the sheets 14 constituting the booklet 12.
  • the cover 16 must have characteristics of resistance to wear and is generally made of material textile or paper, covered with a varnish.
  • a data page 20 formed of a rigid material, such as polycarbonate.
  • the data page 20 includes information relating to the holder of the passport 10 and may further include a microcircuit for storing information and security data, performing operations or even communicating by means of an integrated antenna in this page.
  • the data page 20 may also contain secure data readable directly by a third party or by means of appropriate detection equipment.
  • the data page 20 is inserted between a cover page 18 and a visa page of the booklet 12 of sheets, as shown schematically in the appended FIG.
  • the data page 20 is attached to the booklet 12 of sheets 14 by means of a hinge 22.
  • the hinge is fixed on the face of the data page 20, oriented on the cover page side 18.
  • the hinge 22 is made of a sufficiently flexible material to allow the movement of the rigid page, and strong enough not to tear during frequent manipulation.
  • the hinge 22 has a first portion 24, forming a fastening area, attached to the data page 20 and a second portion 23 inserted into the sheet and sewn on the sheet.
  • the present invention proposes a method of fixing which makes it possible to fix the hinge 22 in a simple manner, while ensuring a good maintenance of the hinge 22 on the data page 20.
  • the method according to the invention consists in fixing, in a specific manner, the hinge 22 made of a strip of flexible plastic material, such as polyurethane, on a data sheet 20 made of rigid plastic, such as polycarbonate.
  • the materials of hinge 22 and data page 20 are chosen to have substantially near and high melting temperatures. These properties allow to merge the two materials and to obtain a bonding layer combining the two materials reinforcing the adhesion properties of the layers together.
  • the polyurethane and the polycarbonate respectively have a melting temperature of 145 ° C. and 140 ° C.
  • the first step of the method is to position the hinge 22 on the data page 20.
  • the data page 20 has a substantially rectangular shape and extends in a lateral direction X and a longitudinal direction Y.
  • the hinge 22 is arranged so to overlap the data page along its entire length.
  • the hinge 22 has the same length as the data page 20 and partially overlaps the page by defining the attachment zone 24 extending laterally over a portion of the width of the data page and longitudinally along the entire length of the page. page.
  • This fixing zone 24 will delimit the location of the weld allowing the joining of the two materials.
  • the welding is done by ultrasound. It allows a very strong and hermetic assembly.
  • the present invention relates to the weld pattern 26 made in the fastening zone 24.
  • the weld patterns 26 are chosen to obtain a secure fastening, and also to optimize the welding step in order to reduce and concentrate the weld. applied energy while ensuring a good quality and resistant welding.
  • the weld is produced by a set of elementary solder patterns 26, shown in FIGS. 1 and 2.
  • the patterns 26 are spaced from each other and arranged in the fastening zone 24 so that the weld presents several rows 28, 34 of 26 elementary patterns.
  • Each row 28, 34 extends substantially in the lateral direction X of the fastening zone 24.
  • the rows 28, 34 are arranged parallel to each other at a regular interval.
  • the weld is composed of at least several rows 28 having a first sequence of elementary patterns 26, which will be called first rows 28 in the following description.
  • each of the first rows 28 the weld extends along the X axis and the weld proportion represents at least 30% to 60%, preferably 50%, of the width of the fastening zone 24. sufficient weld area for the proper retention of the hinge 22.
  • Each of the lateral ends of the first row 28 has an elementary pattern 26a whose first side 30 extends substantially parallel to the longitudinal direction Y. More precisely each first row 28 is delimited at its lateral ends by a first side 30 of patterns 26 which extend parallel to the longitudinal direction Y.
  • the hinge 22 has a high degree of welding along its longitudinal edge 31 which ensures a better resistance to peeling or peeling force oriented perpendicular to the longitudinal direction Y.
  • At least one second side 32 of the pattern 26a disposed at the lateral ends is inclined with respect to the longitudinal direction Y.
  • the second side 32 is perpendicular to the first side 30.
  • the first side 30 is chosen longer than the second side 32 to enhance the quality of adhesion and tear resistance of the weld formed by the pattern.
  • each first row 28 of the first sequence is arranged as follows: two central patterns 26b aligned in the longitudinal direction and oriented so that the first side 30 is perpendicular to the longitudinal direction Y, and, on either side of these central patterns 26b, each first row 28 comprises two peripheral patterns 26a aligned in the lateral direction X and oriented so that the first side 30 is parallel to the longitudinal direction Y
  • each first row 28 comprises two peripheral patterns 26a aligned in the lateral direction X and oriented so that the first side 30 is parallel to the longitudinal direction Y
  • the weld has several first rows of patterns arranged in a first sequence 28. Thus even if a first row 28 gives way, there are others.
  • the first rows 28 are equidistant.
  • the first rows 28 are arranged parallel to each other and parallel to the lateral direction X, equidistant from each other.
  • Each first row 28 (n) has at least one pattern 26 (n) aligned with the pattern 26 (n + 1) of the first consecutive row 28 (n + 1) in the longitudinal direction Y.
  • These arrangements provide a better hold according to the longitudinal direction and decreases the risk of start of pulling.
  • the first rows 28 are symmetrical with respect to the median plane of two first consecutive rows 28. This arrangement is visible on the hinge 22 of Figure 1 or in the detail view of Figure 2.
  • the first rows 28 of patterns 26 are arranged aligned in the longitudinal direction Y.
  • the weld has, at the longitudinal ends 24a, 24b of the fastening zone 24 of the hinge 22, an arrangement of patterns 26 in a second sequence, forming a second row 34, in which the first 30 of each pattern 26 is oriented perpendicular to the longitudinal direction Y.
  • the second row 34 has three patterns 26 extending in the lateral direction X.
  • the first side 30 of the patterns 26 of the second row 34 is longer than the second side 32. All of these provisions allow to create a barrier phenomenon against any attempt to peel or tear in said longitudinal direction Y from the longitudinal ends 24a, 24b of the hinge 22, and to avoid a tear initiation in the longitudinal direction Y.
  • the weld comprises at least three second rows 34 of patterns 26 arranged in the second sequence at each of the longitudinal ends 24a, 24b.
  • the patterns 26 have an oblong shape.
  • a rectangular shape is conceivable, but it is preferable that the pattern 26 has no sharp angles that could pierce the hinge 22 if the power of the equipment is too important.
  • the patterns 26 are spaced apart by an interval "e" of 1 mm along the longitudinal Y and lateral X directions. It is thus preferable to have several identical patterns 26 on a given axis rather than only one overall reason because of the power limits of the current ultrasound machines. In addition, these arrangements make it possible to obtain the best welded surface ratio with respect to the non-welded surface for the entire weld. The pull-out resistance is also increased because the welded areas and the non-welded areas do not have the same pull-out resistance, which causes the hinge 22 to deteriorate when it is desired to remove it. In addition, the spacing of 1 mm between each weld makes it possible to ensure that the deformations of the material forming the contours of each pattern 26 do not overlap with each other.
  • the patterns have dimensions less than 1 mm, for example at most equal to 0.8 mm.
  • the pattern extends along 0.5 mm in the longitudinal direction and 0.8 mm in the lateral direction.
  • the first and second rows 28, 34 are included in the attachment zone 24 so that the elementary patterns 26 do not extend beyond the attachment zone 24.
  • the pattern 26 is not made beyond the hinge 22, as this could cause embrittlement thereof or a peel or peel primer.
  • some elementary patterns 26 partially overlap the hinge 22 and the data page 20. This arrangement forms a security element.
  • the data page 20 polycarbonate has a portion of the pattern 26 etched by welding and the continuity of the pattern 26 on both materials provides a safe element.
  • the sonotrode 36 for performing the weld according to the invention comprises a metal body 38 having a set of teeth 40 in relief which produces impressions corresponding to the patterns 26 of welding.
  • the sonotrode 36 is capable of returning the energy received from ultrasounds to the plastics to be welded.
  • Figures 3 and 4 illustrate a sonotrode 36 according to the invention.
  • the sonotrode 36 cooperates with an anvil (not shown) to apply the energy required for the parts to be welded.
  • the attachment zone 24 is sandwiched between the sonotrode 36 and the anvil.
  • the mechanical vibrations of the sonotrode 36 are transmitted to the plastic part and the friction creates a heating which causes the intermolecular fusion on the welded parts in the overlap zone of the data page 20 and the hinge 22.
  • the method of manufacturing a passport 10 comprises the following steps: fixing by ultrasonic welding of a hinge 22 on the data page 20 according to the method of one of the preceding claims, then fixing the page 20 and sheets 14 of the booklet 12 by stitching, substantially along a median axis of the sheets 14 of the booklet 12, the data page being disposed between the cover page 18 of the booklet 12 and another page of said booklet 12, and finally collage of the cover page 18 of the booklet 12 on the cover page 16 of the passport.
  • the cover 16 and the sheets 14 constituting the booklet 12 initially have a dimension equal to or greater than twice the dimensions of a page of the passport.
  • the sheets 14 of the booklet 12 are sewn together according to a median plane of the sheet, then the cover 16 is fixed by gluing to the cover pages 18, and a folding step along the central seam makes it possible to obtain the document in the form of a book.
  • a cutting step usually with a cutter, may be necessary so that the dimensions of the passport 10 comply with the regulations specified in ICAO 9303.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Credit Cards Or The Like (AREA)

Abstract

The invention concerns a method for attaching a hinge (22) partially covering the page, defining an attachment area (24) extending laterally and longitudinally, the hinge (22) being attached to the page by ultrasonic welding, the welding being carried out by a set of elementary welding patterns (26) spaced apart from each other and arranged in the attachment area (24) such that the welding has a plurality of rows (28, 34) of elementary patterns (26), the rows (28) extending substantially in the lateral direction of the attachment area (24) and having at least a first row (28) according to a first sequence of elementary patterns (26) in which: the welding extends over 30% to 60% of the width of the attachment area (24), each of the lateral ends of the first row (28) comprises an elementary pattern (26) of which a first side (30) extends substantially parallel to the longitudinal direction (Y) and at least a second side (32) is inclined relative to the longitudinal direction (Y), the elementary patterns (26) disposed at the centre of the first row (28) are oriented such that the first side (30) is disposed substantially perpendicular to the longitudinal direction (Y).

Description

PROCEDE DE FIXATION D'UNE CHARNIERE SUR UNE PAGE  METHOD FOR FIXING A HINGE ON A PAGE
ET PROCEDE DE FABRICATION D'UN PASSEPORT  METHOD AND METHOD FOR MANUFACTURING A PASSPORT
La présente invention se rapporte aux documents de type livres, tels qu'un passeport et aux procédés de fabrication de tels passeports. The present invention relates to documents of the type books, such as a passport and methods of manufacturing such passports.
Plus précisément elle porte sur les passeports comportant une page de données, constituée, par exemple, d'un matériau plastique et destinée à être insérée dans un livret de feuilles constituant les pages visa et les pages de garde du passeport. II est connu de l'art antérieur de réaliser telles pages de données en plastique rigide. Ces pages de données comprennent des informations relatives au titulaire du passeport, appelées données de personnalisation. Ces données peuvent être imprimées sur la page et/ou contenues dans un microcircuit intégré dans la page de données. Les pages de données comprennent habituellement des données de sécurisation du document, ces données étant accessibles directement visuellement ou par l'intermédiaire d'équipements appropriés, de sorte que l'authenticité ou une falsification éventuelle du passeport puisse être détectée facilement. More specifically it relates to passports comprising a data page, consisting, for example, of a plastic material and intended to be inserted in a booklet of sheets constituting the visa pages and the cover pages of the passport. It is known from the prior art to make such rigid plastic data pages. These data pages include information about the holder of the passport, called personalization data. This data can be printed on the page and / or contained in a microcircuit integrated in the data page. The data pages usually include security data of the document, which data can be accessed directly visually or via appropriate equipment, so that the authenticity or possible falsification of the passport can be easily detected.
Ces pages de données sont destinées à être attachées au livret de feuilles du passeport au moyen d'une charnière. De préférence, la page de données est insérée entre une page de garde du livret et une page visa de ce dernier. Elle y est attachée au moyen d'une charnière. La charnière est fixée d'une part à la page de données par des moyens qui font l'objet de la présente invention et d'autre part au livret de feuille par une couture réalisée dans un plan médian des feuilles du livret. These data pages are intended to be attached to the passbook of the passport by means of a hinge. Preferably, the data page is inserted between a cover page of the booklet and a visa page of the latter. It is attached by means of a hinge. The hinge is fixed on the one hand to the data page by means which are the subject of the present invention and on the other hand to the leaflet by a seam made in a median plane of the leaves of the booklet.
Il est connu de l'art antérieur, notamment du document EPI 008 459 de fixer une telle page de données au moyen d'une charnière fixée sur la page de données par des moyens mécaniques, par exemple au moyen d'une bandelette enserrant la charnière sur ladite page. It is known from the prior art, in particular from EPI 008 459, to fix such a data page by means of a hinge fixed on the data page by mechanical means, for example by means of a strip encircling the hinge. on that page.
Il est aussi connu du document EP 1 878 589 de fixer la charnière directement sur la page de données, puis de coudre la charnière au livret de feuilles. Le procédé de fixation de la charnière sur la page consiste à réaliser une soudure par ultrason. Le document WO2014 023 482 décrit un procédé pour fixer une page en polycarbonate au moyen d'une charnière constituée d'un matériau textile. Le procédé consiste à réaliser une soudure par ultra-son, réalisée à des intervalles réguliers. It is also known from EP 1 878 589 to fix the hinge directly on the data page, then to sew the hinge leaflet. The method of fixing the hinge on the page is to perform an ultrasonic weld. WO2014 023 482 discloses a method for fixing a polycarbonate page by means of a hinge made of a textile material. The method consists of performing an ultrasonic welding, performed at regular intervals.
Toutefois les procédés de fixation de l'art antérieur ne répondent pas aux exigences de fixation et de sécurité nécessaire pour les documents d'identité tels que les passeports. However, the attachment methods of the prior art do not meet the requirements of fixing and security necessary for identity documents such as passports.
Il est apparu nécessaire de réaliser une soudure présentant : a) des caractéristiques de maintien suffisantes pour résister à la manipulation et à l'usure dans le temps (les passeports étant délivrés pour une durée de 10 ans), b) des caractéristiques limitant les amorces de pelage, et c) des caractéristiques garantissant une liaison sûre, c'est-à-dire une fixation permettant de détecter toute tentative d'arrachement de la page de donnée, par exemple par rupture de la charnière. De plus, il est aussi apparu nécessaire de mettre en œuvre un procédé de fixation de la charnière rapide, peu complexe, avec des moyens existants sur les lignes de production de sorte à limiter les coûts de fabrication et permettant de garder un rythme de production soutenu pour la fabrication des passeports, tout en garantissant une fixation résistante de la charnière sur la page. It has been found necessary to perform a weld with: a) sufficient holding characteristics to resist handling and wear over time (passports are issued for 10 years), b) characteristics limiting the primers peel, and c) characteristics ensuring a secure connection, that is to say a fixing to detect any attempt to tear the page data, for example by breaking the hinge. In addition, it also appeared necessary to implement a process for fixing the hinge fast, little complex, with existing means on the production lines so as to limit manufacturing costs and to keep a steady pace of production for the manufacture of passports, while ensuring a strong attachment of the hinge on the page.
Pour pallier les problèmes énoncés ci-dessus, la présente invention propose un procédé de fixation d'une charnière constituée d'un premier matériau, sur une page constituée d'un deuxième matériau, le premier et le deuxième matériaux présentant des températures de fusion sensiblement identiques, la charnière recouvrant partiellement la page et définissant une zone de fixation s'étendant latéralement et longitudinalement, la charnière étant fixée à la page par soudure ultra-son, la soudure étant réalisée par un ensemble de motifs élémentaires de soudure espacés les uns des autres et agencés dans la zone de fixation de sorte que la soudure présente plusieurs rangées de motifs élémentaires, les rangées s'étendant sensiblement parallèlement entre elles selon la direction latérale de la zone de fixation entre deux extrémités et présentant au moins une première rangée selon première séquence de motifs élémentaires dans laquelle la soudure s'étend sur 30% à 60% de la largeur de la zone de fixation, chacune des extrémités latérales de la première rangée comportant au moins un motif élémentaire dont un premier côté s'étend sensiblement parallèlement à la direction longitudinale et au moins un deuxième côté est incliné par rapport à la direction longitudinale, les motifs élémentaires disposés au centre de la première rangée sont orientés pour que le premier côté soit disposé sensiblement perpendiculairement à la direction longitudinale. To overcome the problems stated above, the present invention provides a method of fixing a hinge consisting of a first material, on a page made of a second material, the first and second materials having substantially melting temperatures. identical, the hinge partially covering the page and defining a fastening zone extending laterally and longitudinally, the hinge being fixed to the page by ultrasonic welding, the welding being performed by a set of elementary solder patterns spaced apart from each other; other and arranged in the fastening zone so that the weld has several rows of elementary patterns, the rows extending substantially parallel to each other in the lateral direction of the fastening zone between two ends and having at least a first row according to first sequence of elementary patterns in which the solder goes out nd over 30% to 60% of the width of the fastening area, each of the lateral ends of the first row having at least one elementary pattern of which a first side extends substantially parallel to the longitudinal direction and at least a second side is inclined relative to the longitudinal direction, the elementary patterns arranged in the center of the first row are oriented so that the first side is disposed substantially perpendicular to the longitudinal direction.
Ces dispositions assurent une bonne adhésion de la charnière par la soudure ultra-son, de plus la discontinuité et l'agencement des motifs garantissent un maintien mécanique suffisant pour résister à la manipulation et à l'usure dans le temps. La disposition des motifs permet en outre de limiter les amorces d'arrachement ou de pelage de la charnière et assure une détection facile de toute tentative d'arrachement par détérioration de la charnière lors de l'arrachage de celle-ci. Selon d'autres caractéristiques These provisions ensure a good adhesion of the hinge by ultra-sound welding, moreover the discontinuity and the arrangement of the grounds guarantee a mechanical support sufficient to resist handling and wear over time. The arrangement of the patterns furthermore makes it possible to limit the tearing or peeling primers of the hinge and ensures easy detection of any attempt to tear it off by damaging the hinge when tearing it off. According to other characteristics
- la soudure présente aux extrémités longitudinales de la zone de fixation des deuxièmes rangées présentant une deuxième séquence de motifs élémentaires, dans laquelle le premier côté de chaque motif de la deuxième rangée est orienté sensiblement parallèlement à la direction latérale ; -les motifs sont espacés d'un intervalle de 1mm selon les directions longitudinale et latérale ; the solder has at the longitudinal ends of the fastening zone second rows having a second sequence of elementary patterns, in which the first side of each pattern of the second row is oriented substantially parallel to the lateral direction; the patterns are spaced apart by an interval of 1 mm in the longitudinal and lateral directions;
- La longueur du premier coté est supérieure à celle du deuxième coté ; - The length of the first side is greater than that of the second side;
- le motif présente une forme oblongue ; - the pattern has an oblong shape;
- la soudure comporte au moins trois deuxièmes rangées de motifs agencés selon la deuxième séquence à chacune des extrémités longitudinales de la zone de fixation ; the weld comprises at least three second rows of patterns arranged according to the second sequence at each of the longitudinal ends of the fastening zone;
- chaque première rangée de la première séquence comporte deux motifs centraux alignées selon la direction longitudinale et orientés de sorte que le premier côté soit perpendiculaire à la direction longitudinale, et, de part et d'autre de ces motifs centraux, la première rangée comporte deux motifs périphériques alignés selon la direction latérale et orientés de sorte que le premier côté soit parallèle à la direction longitudinale ; each first row of the first sequence comprises two central motifs aligned in the longitudinal direction and oriented so that the first side is perpendicular to the longitudinal direction, and, on either side of these central patterns, the first row comprises two peripheral patterns aligned in the lateral direction and oriented so that the first side is parallel to the longitudinal direction;
- le motif élémentaire présente des angles arrondi ; the elementary pattern has rounded corners;
- les motifs élémentaires ne s'étendent pas au-delà de la zone de fixation, du côté libre de la charnière ; the elementary patterns do not extend beyond the fixing zone, on the free side of the hinge;
- au moins un motif élémentaire chevauche la charnière et la page de données ; -les pages de données est en polycarbonate et charnière est en polyuréthane. at least one elementary pattern overlaps the hinge and the data page; -The data pages is polycarbonate and hinge is polyurethane.
La présente invention sera mieux comprise à la lecture de la description qui suit et des figures annexées dans lesquelles : The present invention will be better understood on reading the description which follows and the appended figures in which:
La figure 1 illustre une vue en élévation d'une charnière soudée à une page de données, la soudure présentant un agencement de motifs préféré, La figure 2 illustre une vue de détails de la figure 1, FIG. 1 illustrates an elevational view of a hinge welded to a data page, the weld having a preferred pattern arrangement, FIG. 2 illustrates a detail view of FIG.
La figure 3 illustre une vue en perspective d'une sonotrode pour réaliser la soudure visible à la figure 1, FIG. 3 illustrates a perspective view of a sonotrode for making the weld visible in FIG. 1,
La figure 4 illustre une vue de côté de la sonotrode illustrée sur la figure 3. La figure 5 représente une vue schématique en coupe d'un passeport ouvert fabriqué selon le procédé de l'invention. Figure 4 illustrates a side view of the sonotrode shown in Figure 3. Figure 5 shows a schematic sectional view of an open passport manufactured according to the method of the invention.
La présente invention se rapporte aux documents électroniques destinés à contenir des informations pour identifier le titulaire dudit document. Plus particulièrement, l'invention porte sur des passeports 10. Les passeports 10 sont des documents se présentant sous la forme d'un livre. De manière générale, les passeports 10 comprennent au moins : a) un livret 12 de feuilles 14 comprenant un ensemble de pages appelées pages visa car elles sont destinées à recevoir les tampons visas, b) une couverture 16 et c) des feuilles formant les pages de garde 18 qui sont collés sur la couverture 16 du passeport 10 et qui sont destinées à recevoir des informations spécifiques du pays distribuant le passeport. The present invention relates to electronic documents intended to contain information for identifying the holder of said document. More particularly, the invention relates to passports 10. Passports 10 are documents in the form of a book. In general, the passports 10 comprise at least: a) a booklet 12 of sheets 14 comprising a set of pages called visa pages because they are intended to receive the visa stamps, b) a cover 16 and c) sheets forming the pages 18 which are pasted on the cover 16 of the passport 10 and which are intended to receive specific information from the country distributing the passport.
La couverture 16 du passeport 10 est constituée d'un matériau présentant une plus grande épaisseur que celle des feuilles 14 constituant le livret 12. Par exemple, la couverture 16 doit présenter des caractéristiques de résistance à l'usure et est généralement fait en matériau en matière textile ou papier, recouvert d'un vernis. II est connu d'intégrer au passeport 10 une page de données 20 formée d'une matière rigide, tel que du polycarbonate. La page de données 20 comporte des informations relatives au titulaire du passeport 10 et peut en outre comporter un microcircuit permettant de stocker des données 20 d'informations et de sécurité, de réaliser des opérations ou bien encore de communiquer au moyen d'une antenne intégrée dans ladite page. La page de données 20 peut contenir aussi des données sécurisées lisibles directement par un tiers ou bien au moyen d'un équipement de détection approprié. The cover 16 of the passport 10 is made of a material having a greater thickness than that of the sheets 14 constituting the booklet 12. For example, the cover 16 must have characteristics of resistance to wear and is generally made of material textile or paper, covered with a varnish. It is known to integrate in the passport 10 a data page 20 formed of a rigid material, such as polycarbonate. The data page 20 includes information relating to the holder of the passport 10 and may further include a microcircuit for storing information and security data, performing operations or even communicating by means of an integrated antenna in this page. The data page 20 may also contain secure data readable directly by a third party or by means of appropriate detection equipment.
Généralement, la page de données 20 est insérée entre une page de garde 18 et une page visa du livret 12 de feuilles, comme cela est représenté schématiquement sur la figure 5 annexée. La page de données 20 est attachée au livret 12 de feuilles 14 au moyen d'une charnière 22. De préférence, la charnière est fixée sur la face de la page de données 20, orientée du côté page de garde 18. Ces dispositions permettent à un accès visuel à la totalité de l'autre face de la page de données, l'autre face comportant des informations relatives à l'identité du titulaire du passeport. Generally, the data page 20 is inserted between a cover page 18 and a visa page of the booklet 12 of sheets, as shown schematically in the appended FIG. The data page 20 is attached to the booklet 12 of sheets 14 by means of a hinge 22. Preferably, the hinge is fixed on the face of the data page 20, oriented on the cover page side 18. These arrangements allow visual access to the the other side of the data page, the other side containing information relating to the identity of the holder of the passport.
La charnière 22 est constituée d'un matériau suffisamment souple pour permettre le débattement de la page rigide, et suffisamment résistant pour ne pas se déchirer lors de fréquentes manipulations. La charnière 22 présente une première partie 24, formant une zone de fixation, fixée sur la page de données 20 et une deuxième partie 23 insérée dans le feuillet et fixée par couture sur le feuillet. The hinge 22 is made of a sufficiently flexible material to allow the movement of the rigid page, and strong enough not to tear during frequent manipulation. The hinge 22 has a first portion 24, forming a fastening area, attached to the data page 20 and a second portion 23 inserted into the sheet and sewn on the sheet.
Pour répondre aux exigences de sécurité et d'authentification nécessaires pour les documents d'identité, tels que les passeports, il est apparu important que la première partie 24 de la charnière soit fixée sur la page de données 20 de manière sûre. A cet effet, la présente invention propose un procédé de fixation qui permet de fixer la charnière 22 de manière simple, tout en garantissant un bon maintien de la charnière 22 sur la page de données 20. In order to meet the necessary security and authentication requirements for identity documents, such as passports, it has become important that the first part 24 of the hinge is securely attached to the data page 20. For this purpose, the present invention proposes a method of fixing which makes it possible to fix the hinge 22 in a simple manner, while ensuring a good maintenance of the hinge 22 on the data page 20.
Le procédé selon l'invention consiste à fixer, d'une manière spécifique, la charnière 22 constituée d'une bande de matériau en plastique souple, tel que du polyuréthane, sur une page de données 20 en plastique rigide, tel que du polycarbonate. Les matériaux de la charnière 22 et de la page de données 20 sont choisis de sorte à présenter des températures de fusion sensiblement proches et élevées. Ces propriétés permettent de fusionner les deux matériaux et d'obtenir une couche de liaison combinant les deux matériaux renforçant les propriétés d'adhésion des couches entre elles. The method according to the invention consists in fixing, in a specific manner, the hinge 22 made of a strip of flexible plastic material, such as polyurethane, on a data sheet 20 made of rigid plastic, such as polycarbonate. The materials of hinge 22 and data page 20 are chosen to have substantially near and high melting temperatures. These properties allow to merge the two materials and to obtain a bonding layer combining the two materials reinforcing the adhesion properties of the layers together.
A titre d'exemple, le polyuréthane et le polycarbonate présentent respectivement une température de fusion de 145°C et de 140°C. By way of example, the polyurethane and the polycarbonate respectively have a melting temperature of 145 ° C. and 140 ° C.
La première étape du procédé consiste à positionner la charnière 22 sur la page de données 20. La page de données 20 présente une forme sensiblement rectangulaire et s'étend selon une direction latérale X et une direction longitudinale Y. La charnière 22 est disposée de sorte à chevaucher la page de données sur toute sa longueur. De préférence la charnière 22 présente la même longueur que la page de données 20 et recouvre partiellement la page en définissant la zone de fixation 24 s'étendant latéralement sur une partie de la largeur de la page de donnée et longitudinalement sur toute la longueur de la page. The first step of the method is to position the hinge 22 on the data page 20. The data page 20 has a substantially rectangular shape and extends in a lateral direction X and a longitudinal direction Y. The hinge 22 is arranged so to overlap the data page along its entire length. Preferably the hinge 22 has the same length as the data page 20 and partially overlaps the page by defining the attachment zone 24 extending laterally over a portion of the width of the data page and longitudinally along the entire length of the page. page.
Cette de zone de fixation 24 va délimiter l'emplacement de la soudure permettant la jonction des deux matériaux. La soudure est réalisée par ultrasons. Elle permet un assemblage très résistant et hermétique. Plus particulièrement, la présente invention porte sur le motif 26 de soudure réalisé dans la zone de fixation 24. En effet les motifs 26 de soudure sont choisis pour obtenir une fixation sûre, et aussi optimiser l'étape de soudage afin de réduire et concentrer l'énergie appliquée tout en garantissant une soudure de bonne qualité, et résistante. This fixing zone 24 will delimit the location of the weld allowing the joining of the two materials. The welding is done by ultrasound. It allows a very strong and hermetic assembly. More particularly, the present invention relates to the weld pattern 26 made in the fastening zone 24. In fact, the weld patterns 26 are chosen to obtain a secure fastening, and also to optimize the welding step in order to reduce and concentrate the weld. applied energy while ensuring a good quality and resistant welding.
Selon l'invention la soudure est réalisée par un ensemble de motifs 26 élémentaires de soudure, représentés sur les figures 1 et 2. Les motifs 26 sont espacés les uns des autres et agencés dans la zone de fixation 24 de sorte que, la soudure présente plusieurs rangées 28, 34 de motifs 26 élémentaires. Chaque rangée 28, 34 s'étend sensiblement selon la direction latérale X de la zone de fixation 24. Les rangées 28, 34 sont disposées parallèlement entre elles, selon un intervalle régulier. La soudure est composée d'au moins plusieurs rangées 28 présentant une première séquence de motifs 26 élémentaires, qui seront appelées première rangées 28 dans la suite de la description. According to the invention the weld is produced by a set of elementary solder patterns 26, shown in FIGS. 1 and 2. The patterns 26 are spaced from each other and arranged in the fastening zone 24 so that the weld presents several rows 28, 34 of 26 elementary patterns. Each row 28, 34 extends substantially in the lateral direction X of the fastening zone 24. The rows 28, 34 are arranged parallel to each other at a regular interval. The weld is composed of at least several rows 28 having a first sequence of elementary patterns 26, which will be called first rows 28 in the following description.
Dans chacune des premières rangées 28, la soudure s'étend selon l'axe X et la proportion de soudure représente au moins 30% à 60%, de préférence 50%, de la largeur de la zone de fixation 24. Ces dispositions assurent une surface de soudure suffisante pour le bon maintien de la charnière 22. Chacune des extrémités latérales de la première rangée 28 comporte un motif 26a élémentaire dont un premier côté 30 s'étend sensiblement parallèlement à la direction longitudinale Y. Plus précisément chaque première rangée 28 est délimitée à ses extrémités latérales par un premier côté 30 de motifs 26 qui s'étendent parallèlement à la direction longitudinale Y. Grâce à ces dispositions, la charnière 22 présente un taux de soudure important le long de son bord longitudinal 31 ce qui assure une meilleure résistance à une force d'arrachement ou de pelage orientée perpendiculairement à la direction longitudinale Y. In each of the first rows 28, the weld extends along the X axis and the weld proportion represents at least 30% to 60%, preferably 50%, of the width of the fastening zone 24. sufficient weld area for the proper retention of the hinge 22. Each of the lateral ends of the first row 28 has an elementary pattern 26a whose first side 30 extends substantially parallel to the longitudinal direction Y. More precisely each first row 28 is delimited at its lateral ends by a first side 30 of patterns 26 which extend parallel to the longitudinal direction Y. With these provisions, the hinge 22 has a high degree of welding along its longitudinal edge 31 which ensures a better resistance to peeling or peeling force oriented perpendicular to the longitudinal direction Y.
Par ailleurs, au moins un deuxième côté 32 du motif 26a disposé aux extrémités latérales est incliné par rapport à la direction longitudinale Y. Dans les figures annexées, le deuxième côté 32 est perpendiculaire au premier côté 30. De préférence le premier côté 30 est choisi plus long que le deuxième côté 32 pour renforcer la qualité d'adhérence et de résistance à l'arrachement de la soudure formée par le motif. Moreover, at least one second side 32 of the pattern 26a disposed at the lateral ends is inclined with respect to the longitudinal direction Y. In the appended figures, the second side 32 is perpendicular to the first side 30. Preferably the first side 30 is chosen longer than the second side 32 to enhance the quality of adhesion and tear resistance of the weld formed by the pattern.
Les motifs 26b élémentaires disposés au centre de la première rangée 28 sont orientés pour que le premier côté 30 soit disposé sensiblement perpendiculairement à la direction longitudinale Y. Ces dispositions assurent un maintien et une résistance à une force d'arrachement orientée selon la direction longitudinale Y. Selon le mode de réalisation illustré sur les figures 1 et 2, chaque première rangée 28 de la première séquence est agencée de la manière suivante : deux motifs 26 centraux 26b alignées selon la direction longitudinale et orientés de sorte que le premier côté 30 soit perpendiculaire à la direction longitudinale Y, et, de part et d'autre de ces motifs centraux 26b, chaque première rangée 28 comporte deux motifs périphériques 26a alignés selon la direction latérale X et orientés de sorte que le premier côté 30 soit parallèle à la direction longitudinale Y. Ainsi plusieurs motifs 26 consolident le maintien des premières rangées 28. The elementary patterns 26b arranged in the center of the first row 28 are oriented so that the first side 30 is disposed substantially perpendicular to the longitudinal direction Y. These arrangements provide a holding and resistance to a tearing force oriented in the longitudinal direction Y . According to the embodiment illustrated in Figures 1 and 2, each first row 28 of the first sequence is arranged as follows: two central patterns 26b aligned in the longitudinal direction and oriented so that the first side 30 is perpendicular to the longitudinal direction Y, and, on either side of these central patterns 26b, each first row 28 comprises two peripheral patterns 26a aligned in the lateral direction X and oriented so that the first side 30 is parallel to the longitudinal direction Y Thus several reasons 26 consolidate the maintenance of the first rows 28.
De plus la soudure comporte plusieurs premières rangées de motifs agencés selon une première séquence 28. Ainsi même si une première rangée 28 cède, il en existe d'autres. Les premières rangées 28 sont équidistantes. In addition the weld has several first rows of patterns arranged in a first sequence 28. Thus even if a first row 28 gives way, there are others. The first rows 28 are equidistant.
Selon une caractéristiques additionnelle, les premières rangées 28 sont disposées parallèles entre elles et parallèlement à la direction latérale X, à équidistance les unes des autres. Chaque première rangée 28(n) présente au moins un motif 26(n) aligné avec le motif 26(n+l) de la première rangée consécutive 28 (n+1) selon la direction longitudinale Y. Ces dispositions assurent un meilleur maintien selon la direction longitudinale et diminue le risque d'amorce d'arrachage. De manière avantageuse, les premières rangées 28 sont symétriques par rapport au plan médian de deux premières rangées 28 consécutives. Cet agencement est visible sur la charnière 22 de la figure 1 ou sur la vue de détails de la figure 2. Les premières rangées 28 de motifs 26 disposés sont alignées selon la direction longitudinale Y. According to an additional feature, the first rows 28 are arranged parallel to each other and parallel to the lateral direction X, equidistant from each other. Each first row 28 (n) has at least one pattern 26 (n) aligned with the pattern 26 (n + 1) of the first consecutive row 28 (n + 1) in the longitudinal direction Y. These arrangements provide a better hold according to the longitudinal direction and decreases the risk of start of pulling. Advantageously, the first rows 28 are symmetrical with respect to the median plane of two first consecutive rows 28. This arrangement is visible on the hinge 22 of Figure 1 or in the detail view of Figure 2. The first rows 28 of patterns 26 are arranged aligned in the longitudinal direction Y.
Tel que visible sur les figures 1 et 2, la soudure comporte aux extrémités longitudinales 24a, 24b de la zone de fixation 24 de la charnière 22, un agencement de motifs 26 selon une deuxième séquence, formant une deuxième rangée 34, dans lequel le premier côté 30 de chaque motif 26 est orienté perpendiculairement à la direction longitudinale Y. Sur la figure 1 annexée, la deuxième rangée 34 comporte trois motifs 26 s'étendant selon la direction latérale X. As can be seen in FIGS. 1 and 2, the weld has, at the longitudinal ends 24a, 24b of the fastening zone 24 of the hinge 22, an arrangement of patterns 26 in a second sequence, forming a second row 34, in which the first 30 of each pattern 26 is oriented perpendicular to the longitudinal direction Y. In Figure 1 attached, the second row 34 has three patterns 26 extending in the lateral direction X.
Avantageusement, le premier côté 30 des motifs 26 de la deuxième rangée 34 est plus long que le deuxième côté 32. L'ensemble de ces dispositions permettent de créer un phénomène de barrière contre toute tentative de pelage ou d'arrachement selon ladite direction longitudinale Y à partir des extrémités longitudinales 24a, 24b de la charnière 22, et d'éviter une amorce d'arrachement selon la direction longitudinale Y. Selon un mode de réalisation préféré, la soudure comporte au moins trois deuxièmes rangées 34 de motifs 26 agencés selon la deuxième séquence à chacune des extrémités longitudinales 24a, 24b. Advantageously, the first side 30 of the patterns 26 of the second row 34 is longer than the second side 32. All of these provisions allow to create a barrier phenomenon against any attempt to peel or tear in said longitudinal direction Y from the longitudinal ends 24a, 24b of the hinge 22, and to avoid a tear initiation in the longitudinal direction Y. According to a method of preferred embodiment, the weld comprises at least three second rows 34 of patterns 26 arranged in the second sequence at each of the longitudinal ends 24a, 24b.
Sur ces figures les motifs 26 présentent une forme oblongue. Une forme rectangulaire est envisageable, mais il est préférable que le motif 26 ne présente pas d'angles vifs qui pourraient percer la charnière 22 si la puissance de l'équipement est trop importante. In these figures the patterns 26 have an oblong shape. A rectangular shape is conceivable, but it is preferable that the pattern 26 has no sharp angles that could pierce the hinge 22 if the power of the equipment is too important.
Selon une variante de réalisation de la soudure, les motifs 26 sont espacés d'un intervalle « e » de 1mm selon les directions longitudinale Y et latérale X. Il est ainsi préférable d'avoir plusieurs motifs 26 identiques sur un axe donné plutôt qu'un seul motif 26 global à cause des limites de puissance des machines à ultrasons actuelles. De plus ces dispositions permettent d'obtenir le meilleur rapport de surface soudée par rapport à la surface non soudée pour l'ensemble de la soudure. La résistance à l'arrachement est aussi augmentée, car les zones soudées et les zones non soudées ne présentent pas la même résistance à l'arrachement, ce qui entraine la détérioration de la charnière 22 lorsqu'on souhaite la retirer. De plus l'espacement de 1 mm entre chaque soudure permet d'assurer que les déformations de la matière formant les contours de chaque motif 26 ne se superposent pas entre eux. According to an embodiment variant of the weld, the patterns 26 are spaced apart by an interval "e" of 1 mm along the longitudinal Y and lateral X directions. It is thus preferable to have several identical patterns 26 on a given axis rather than only one overall reason because of the power limits of the current ultrasound machines. In addition, these arrangements make it possible to obtain the best welded surface ratio with respect to the non-welded surface for the entire weld. The pull-out resistance is also increased because the welded areas and the non-welded areas do not have the same pull-out resistance, which causes the hinge 22 to deteriorate when it is desired to remove it. In addition, the spacing of 1 mm between each weld makes it possible to ensure that the deformations of the material forming the contours of each pattern 26 do not overlap with each other.
Selon une variante de réalisation, les motifs présentent des dimensions inférieures à 1mm par exemple au plus égales à 0,8 mm. Par exemple, le motif s'étend selon 0,5 mm selon la direction longitudinale et 0,8 mm selon la direction latérale. Ainsi la précision de reproduction des motifs est augmentée et rendue difficile pour le fraudeur. Il est alors difficile, après arrachement partiel ou total de la charnière initialement soudée, d'aligner une charnière frauduleuse avec les motifs restants de la charnière initiale, ou encore avec les marquages sur la couche de plastique de la page de donnée, ces marquages étant dus à la soudure initiale par ultra son. According to an alternative embodiment, the patterns have dimensions less than 1 mm, for example at most equal to 0.8 mm. For example, the pattern extends along 0.5 mm in the longitudinal direction and 0.8 mm in the lateral direction. Thus the precision of reproduction of the reasons is increased and made difficult for the fraudster. It is then difficult, after partial or complete tearing of the hinge initially welded, to align a fraudulent hinge with the remaining patterns of the initial hinge, or with the markings on the plastic layer of the data page, these markings being due to the initial welding by ultra sound.
De préférence, les premières et deuxièmes rangées 28, 34 sont incluses dans la zone de fixation 24 de sorte que les motifs 26 élémentaires ne s'étendent pas au-delà de la zone de fixation 24. Preferably, the first and second rows 28, 34 are included in the attachment zone 24 so that the elementary patterns 26 do not extend beyond the attachment zone 24.
Du côté libre de la charnière 22, il est impératif que le motif 26 ne soit pas réalisé au-delà de la charnière 22, car cela pourrait engendrer une fragilisation de celle-ci ou une amorce d'arrachage ou de pelage. Selon une variante de réalisation, du côté du bord longitudinal 31 de la charnière, certains motifs 26 élémentaires chevauchent partiellement la charnière 22 et la page de données 20. Cette disposition forme un élément de sécurité. En effet la page de données 20 en polycarbonate comporte une partie du motif 26 gravé par soudure et la continuité du motif 26 sur les deux matériaux apporte un élément sécuritaire. On the free side of the hinge 22, it is imperative that the pattern 26 is not made beyond the hinge 22, as this could cause embrittlement thereof or a peel or peel primer. According to an alternative embodiment, on the side of the longitudinal edge 31 of the hinge, some elementary patterns 26 partially overlap the hinge 22 and the data page 20. This arrangement forms a security element. Indeed, the data page 20 polycarbonate has a portion of the pattern 26 etched by welding and the continuity of the pattern 26 on both materials provides a safe element.
L'agencement des motifs 26 décrit ci-dessus n'est pas limitatif et tout agencement de motifs 26 de soudure respectant les règles énoncées ci-dessus font partie de la présente invention. En effet ces règles ont été établies pour que la soudure soit durable dans le temps malgré la manipulation des passeports 10, et soit sûre, c'est-à-dire indiquant toute tentative d'arrachement par détérioration de la charnière 22 et de la page de données 20. The arrangement of the patterns 26 described above is not limiting and any arrangement of welding patterns 26 complying with the rules set out above are part of the present invention. Indeed, these rules have been established so that the weld is durable over time despite the handling of the passports 10, and is safe, that is to say indicating any attempt of tearing by deterioration of the hinge 22 and the page data 20.
La sonotrode 36 permettant de réaliser la soudure selon l'invention comporte un corps 38 métallique présentant une denture 40 en relief qui réalise des empreintes correspondant aux motifs 26 de soudure. La sonotrode 36 est capable de restituer l'énergie reçue des ultra-sons aux plastiques à souder. Les figures 3 et 4 illustrent une sonotrode 36 selon l'invention. La sonotrode 36 coopère avec une enclume (non représentée) pour appliquer l'énergie nécessaire aux pièces à souder. La zone de fixation 24 est enserrée entre la sonotrode 36 et l'enclume. Les vibrations mécaniques de la sonotrode 36 sont transmises à la pièce en plastique et la friction crée un échauffement qui entraîne la fusion intermoléculaire sur les parties soudées dans la zone de recouvrement de la page de données 20 et de la charnière 22. The sonotrode 36 for performing the weld according to the invention comprises a metal body 38 having a set of teeth 40 in relief which produces impressions corresponding to the patterns 26 of welding. The sonotrode 36 is capable of returning the energy received from ultrasounds to the plastics to be welded. Figures 3 and 4 illustrate a sonotrode 36 according to the invention. The sonotrode 36 cooperates with an anvil (not shown) to apply the energy required for the parts to be welded. The attachment zone 24 is sandwiched between the sonotrode 36 and the anvil. The mechanical vibrations of the sonotrode 36 are transmitted to the plastic part and the friction creates a heating which causes the intermolecular fusion on the welded parts in the overlap zone of the data page 20 and the hinge 22.
Le procédé de fabrication d'un passeport 10 selon l'invention comprend les étapes suivantes : fixation par soudure à ultrasons d'une charnière 22 sur la page de données 20 selon le procédé de l'une des revendications précédentes, puis fixation de la page de données 20 et des feuilles 14 du livret 12 par couture, sensiblement selon un axe médian des feuilles 14 du livret 12, la page de donnée étant disposée entre la page de garde 18 du livret 12 et une autre page dudit livret 12, et enfin collage de la page de garde 18 du livret 12 sur la page de couverture 16 du passeport. The method of manufacturing a passport 10 according to the invention comprises the following steps: fixing by ultrasonic welding of a hinge 22 on the data page 20 according to the method of one of the preceding claims, then fixing the page 20 and sheets 14 of the booklet 12 by stitching, substantially along a median axis of the sheets 14 of the booklet 12, the data page being disposed between the cover page 18 of the booklet 12 and another page of said booklet 12, and finally collage of the cover page 18 of the booklet 12 on the cover page 16 of the passport.
La couverture 16 et les feuilles 14 constituant le livret 12 présentent initialement une dimension égale ou supérieure au double des dimensions d'une page du passeport. Généralement les feuilles 14 du livret 12 sont assemblées par couture selon un plan médian de la feuille, puis la couverture 16 est fixée par collage aux pages de garde 18, et une étape de pliage le long de la couture centrale permet d'obtenir le document sous forme de livre. Une étape de découpage, généralement au massicot, peut être nécessaire pour que les dimensions du passeport 10 satisfassent aux réglementations spécifiées dans la Norme ICAO 9303. The cover 16 and the sheets 14 constituting the booklet 12 initially have a dimension equal to or greater than twice the dimensions of a page of the passport. Generally, the sheets 14 of the booklet 12 are sewn together according to a median plane of the sheet, then the cover 16 is fixed by gluing to the cover pages 18, and a folding step along the central seam makes it possible to obtain the document in the form of a book. A cutting step, usually with a cutter, may be necessary so that the dimensions of the passport 10 comply with the regulations specified in ICAO 9303.

Claims

Revendications claims
1. Procédé de fixation d'une cha rnière (22), constituée d'u n premier matériau, sur une page, constituée d'u n deuxième matériau, le premier et le deuxième matériaux présentant des tem pératures de fusion sensi blement identiques, la charnière (22) recouvrant partiellement la page en définissant une zone de fixation (24) s' étenda nt selon u ne direction latérale (X) et selon une direction longitudinale (Y), la charnière (22) étant fixée à la page par soudure ultra-son, la soudu re étant réalisée pa r un ensem ble de motifs (26) élémentaires de soudure espacés les uns des autres et agencés dans la zone de fixation (24) de sorte que la soudure présente plusieurs rangées (28, 34) de motifs (26) élémentaires, les rangées (28) s'étendant sensiblement selon la direction latéra le de la zone de fixation (24) et présentant au moins un première ra ngée (28) selon une première séquence de motifs (26) élémentaires dans laquelle : 1. Method of fixing a chain (22), consisting of a first material, on a page, made of a second material, the first and the second materials having substantially identical melting temperatures, the hinge (22) partially covering the page by defining a fastening zone (24) is arranged in a lateral direction (X) and in a longitudinal direction (Y), the hinge (22) being attached to the page by ultrasonic welding, the weld being performed by a plurality of elementary weld patterns (26) spaced from each other and arranged in the fastening zone (24) so that the weld has a plurality of rows (28, 34 ) of elementary patterns (26), the rows (28) extending substantially in the lateral direction of the fastening zone (24) and having at least one first edge (28) in a first pattern of patterns (26). in which:
- la soudu re s'étend sur 30% à 60% de la largeur de la zone de fixation (24),  the weld re extends over 30% to 60% of the width of the fastening zone (24),
- chacune des extrémités latérales de la première ra ngée (28) com porte un motif (26) élémentaire dont u n premier côté (30) s'étend sensi blement parallèlement à la direction longitudina le (Y) et au moins u n deuxième côté (32) est incliné par rapport à la direction longitudina le (Y), each of the lateral ends of the first section (28) has an elementary pattern (26), a first side (30) extending substantially parallel to the longitudinal direction (Y) and at least one second side (32). ) is inclined with respect to the longitudinal direction (Y),
- les motifs (26) élémentai res disposés au centre de la première rangée (28) sont orientés pou r que le premier côté (30) soit disposé sensiblement perpendicu lairement à la direction longitudinale (Y).  the elementary patterns (26) arranged in the center of the first row (28) are oriented so that the first side (30) is arranged substantially perpendicular to the longitudinal direction (Y).
2. Procédé de fixation d'u ne charnière (22) selon la revendication précédente, dans lequel la soudu re présente aux extrémités longitudinales de la zone de fixation (24) des deuxièmes rangées (34) présentant une deuxième séquence de motifs (26) élémentaires, dans laquelle le premier côté (30) de chaque motif (26) de la deuxième ra ngée est orienté sensiblement pa rallèlement à la direction latéra le (X). 2. A method of fixing a hinge (22) according to the preceding claim, wherein the weld re has at the longitudinal ends of the fastening zone (24) second rows (34) having a second sequence of patterns (26). elementary members, wherein the first side (30) of each pattern (26) of the second section is oriented substantially parallel to the lateral direction (X).
3. Procédé de fixation d'une charnière (22) selon l'u ne des revendications précédentes, dans lequel les motifs (26) sont espacés d'un interva lle (e) de 1m m selon les directions longitudina le et latérale. 3. A method of fixing a hinge (22) according to one of the preceding claims, wherein the patterns (26) are spaced apart a gap (e) of 1 m in longitudinal and lateral directions.
4. Procédé de fixation d'une charnière (22) selon l'u ne des revendications précédentes, dans lequel la longueur du premier coté (30) est supérieu re à celle du deuxième coté (32). 4. Method of fixing a hinge (22) according to one of the preceding claims, wherein the length of the first side (30) is greater than that of the second side (32).
5. Procédé de fixation d'une charnière (22) selon l'u ne des revendications précédentes, dans lequel le motif (26) présente u ne forme oblongue. 5. A method of fixing a hinge (22) according to one of the preceding claims, wherein the pattern (26) has an oblong shape.
6. Procédé de fixation d'une charnière (22) selon l'une des revendications précédentes, dans lequel la soudure comporte au moins trois deuxièmes rangées (34) de motifs (26) agencés selon la deuxième séquence à chacune des extrémités longitudinales de la zone de fixation (24). 6. A method of fixing a hinge (22) according to one of the preceding claims, wherein the weld comprises at least three second rows (34) of patterns (26) arranged in the second sequence at each of the longitudinal ends of the fixing area (24).
7. Procédé de fixation d'une charnière (22) selon l'une des revendications précédentes, dans lequel chaque première rangée (28) de la première séquence comporte deux motifs (26) centraux (26b) alignées selon la direction longitudinale et orientés de sorte que le premier côté (30) soit perpendiculaire à la direction longitudinale (Y), et, de part et d'autre de ces motifs centraux (26a), la première rangée (28) comporte, deux motifs périphériques (26a) alignés selon la direction latérale (X) et orientés de sorte que le premier côté (30) soit parallèle à la direction longitudinale (Y). 7. A method of fixing a hinge (22) according to one of the preceding claims, wherein each first row (28) of the first sequence comprises two patterns (26) central (26b) aligned in the longitudinal direction and oriented of so that the first side (30) is perpendicular to the longitudinal direction (Y), and, on either side of these central patterns (26a), the first row (28) comprises two peripheral patterns (26a) aligned according to the lateral direction (X) and oriented so that the first side (30) is parallel to the longitudinal direction (Y).
8. Procédé de fixation d'une charnière (22) selon l'une des revendications précédentes, dans lequel le motif (26) élémentaire présente des angles arrondis. 8. A method of fixing a hinge (22) according to one of the preceding claims, wherein the pattern (26) element has rounded corners.
9. Procédé de fixation d'une charnière (22) selon l'une des revendications précédentes, dans lequel les motifs (26) élémentaires ne s'étendent pas au-delà de la zone de fixation9. A method of fixing a hinge (22) according to one of the preceding claims, wherein the units (26) elementary do not extend beyond the fixing area
(24), du côté libre de la charnière (22). (24) on the free side of the hinge (22).
10. Procédé de fixation d'une charnière (22) selon l'une des revendications précédentes, dans lequel au moins un motif (26) élémentaire chevauche la charnière (22) et la page de données (20). A method of fixing a hinge (22) according to one of the preceding claims, wherein at least one elementary pattern (26) overlaps the hinge (22) and the data page (20).
11. Procédé de fixation d'une charnière (22) selon l'une des revendications précédentes, dans lequel la page de données (20) est en polycarbonate et la charnière (22) est en pl3. olyuréthane. 11. A method of fixing a hinge (22) according to one of the preceding claims, wherein the data page (20) is polycarbonate and the hinge (22) is pl3. olyuréthane.
12. Procédé de fixation d'une charnière selon l'une quelconque des revendications précédentes, dans lequel les motifs présentent des dimensions inférieures à 1mm. 12. A method of fixing a hinge according to any one of the preceding claims, wherein the patterns have dimensions less than 1mm.
13. Procédé de fabrication d'un passeport (10) comprenant un livret (12) de feuilles, une couverture (16) et une page de donnée, caractérisé en ce qu'il comporte les étapes suivantes : 13. A method of manufacturing a passport (10) comprising a booklet (12) of sheets, a cover (16) and a data page, characterized in that it comprises the following steps:
- fixation par soudure à ultrasons d'une charnière (22) sur la page de données (20) selon le procédé de l'une des revendications précédentes,  - ultrasonic welding of a hinge (22) on the data page (20) according to the method of one of the preceding claims,
- fixation de la page de données (20) et des feuilles (14) du livret (12) par couture, sensiblement selon une direction médiane des feuilles (14) du livret (12), la page de donnée étant disposée entre la page de garde (18) du livret (12) et une autre page dudit livret (12), - Attaching the data page (20) and leaves (14) of the booklet (12) by sewing, substantially in a median direction of the sheets (14) of the booklet (12), the data page being arranged between the page of guard (18) of the booklet (12) and another page of said booklet (12),
- collage de la page de garde (18) du livret (12) sur la page de couverture (16) du passeport.  - pasting of the cover page (18) of the booklet (12) on the cover page (16) of the passport.
PCT/FR2015/051263 2014-05-19 2015-05-13 Method for attaching a hinge to a page and method for producing a passport WO2015177440A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1454455A FR3020985B1 (en) 2014-05-19 2014-05-19 METHOD OF FIXING A HINGE ON A PAGE AND METHOD OF MANUFACTURING A PASSPORT
FR1454455 2014-05-19

Publications (1)

Publication Number Publication Date
WO2015177440A1 true WO2015177440A1 (en) 2015-11-26

Family

ID=51261083

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2015/051263 WO2015177440A1 (en) 2014-05-19 2015-05-13 Method for attaching a hinge to a page and method for producing a passport

Country Status (2)

Country Link
FR (1) FR3020985B1 (en)
WO (1) WO2015177440A1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017105859A1 (en) * 2017-03-17 2018-09-20 Bundesdruckerei Gmbh Method for producing a data page for a book-type document and data page
CN110442193A (en) * 2018-05-04 2019-11-12 仁宝电脑工业股份有限公司 Pivot and electronic device
DE102018114456A1 (en) 2018-06-15 2019-12-19 Bundesdruckerei Gmbh Tab for a data page, data page for a book-like document and method for its production
EP3595910B1 (en) 2017-03-17 2021-12-01 Bundesdruckerei GmbH Method for producing a data page and a book block for a book-type document, and data page for a book-type document

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4532166A (en) * 1983-10-03 1985-07-30 Xerox Corporation Welding of web materials
EP0340334A2 (en) * 1988-05-05 1989-11-08 Drescher Geschäftsdrucke Gmbh Apparatus for joining two or multilayered paper articles together
EP1008459A1 (en) 1998-12-13 2000-06-14 SDU Identification B.V. Method for manufacturing a booklet, booklet manufactured according to the method and booklet
US6713159B1 (en) * 2000-08-30 2004-03-30 Kimberly-Clark Worldwide, Inc. Tear-resistant bond pattern
EP1878589A1 (en) 2006-07-11 2008-01-16 Setec Oy Method for producing information page and information page
WO2010000498A1 (en) * 2008-07-03 2010-01-07 Bundesdruckerei Gmbh Method for producing a document card which can be inserted into a security document that is present in the form of a book and document card
WO2014023482A1 (en) 2012-08-06 2014-02-13 Bundesdruckerei Gmbh Method for connecting at least one connection piece to a document sheet, method for producing a security document and security document

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4532166A (en) * 1983-10-03 1985-07-30 Xerox Corporation Welding of web materials
EP0340334A2 (en) * 1988-05-05 1989-11-08 Drescher Geschäftsdrucke Gmbh Apparatus for joining two or multilayered paper articles together
EP1008459A1 (en) 1998-12-13 2000-06-14 SDU Identification B.V. Method for manufacturing a booklet, booklet manufactured according to the method and booklet
US6713159B1 (en) * 2000-08-30 2004-03-30 Kimberly-Clark Worldwide, Inc. Tear-resistant bond pattern
EP1878589A1 (en) 2006-07-11 2008-01-16 Setec Oy Method for producing information page and information page
WO2010000498A1 (en) * 2008-07-03 2010-01-07 Bundesdruckerei Gmbh Method for producing a document card which can be inserted into a security document that is present in the form of a book and document card
WO2014023482A1 (en) 2012-08-06 2014-02-13 Bundesdruckerei Gmbh Method for connecting at least one connection piece to a document sheet, method for producing a security document and security document

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017105859A1 (en) * 2017-03-17 2018-09-20 Bundesdruckerei Gmbh Method for producing a data page for a book-type document and data page
WO2018166982A1 (en) 2017-03-17 2018-09-20 Bundesdruckerei Gmbh Method for producing a data page for a book-like document, and data page
EP3595910B1 (en) 2017-03-17 2021-12-01 Bundesdruckerei GmbH Method for producing a data page and a book block for a book-type document, and data page for a book-type document
CN110442193A (en) * 2018-05-04 2019-11-12 仁宝电脑工业股份有限公司 Pivot and electronic device
CN110442193B (en) * 2018-05-04 2024-02-06 仁宝电脑工业股份有限公司 Pivot mechanism and electronic device
DE102018114456A1 (en) 2018-06-15 2019-12-19 Bundesdruckerei Gmbh Tab for a data page, data page for a book-like document and method for its production
WO2019238305A1 (en) 2018-06-15 2019-12-19 Bundesdruckerei Gmbh Tab for a data page, data page for a book-like document and method for producing the same

Also Published As

Publication number Publication date
FR3020985A1 (en) 2015-11-20
FR3020985B1 (en) 2018-03-16

Similar Documents

Publication Publication Date Title
WO2015177440A1 (en) Method for attaching a hinge to a page and method for producing a passport
RU2344938C2 (en) Method of making page with data and page with data
WO2008141982A1 (en) Method for producing a device comprising a transponder antenna connected to contact pins and device obtained
WO1999038118A2 (en) Integrated circuit contact card, comprising a detachable minicard
EP3201842A1 (en) Electronic document having angled antenna ends, antenna holder for such an electronic document and method for manufacturing such a document
EP0916144A1 (en) Method for making a transponder coil and transponder produced by said method
FR2745528A1 (en) DOCUMENT PROTECTIVE DEVICE AND METHOD OF MANUFACTURING SUCH A DEVICE
EP1530519A2 (en) Customised multi-layer card comprising fracture initiation scores and method of producing one such card
CA2646813A1 (en) Radiofrequency device
EP2004421B1 (en) Passport comprising a sewn reinforcing strip
EP2298571B1 (en) Security document and method of making same
EP1106039B1 (en) Method for producing a contact between two conductive layers separated by an insulating layer
US8926779B2 (en) Method for making laminate sheets with flexible hinges for binding into security documents
FR3043015A1 (en) METHOD OF MANUFACTURING A HINGE INTENDED TO BE PLACED ALONG A BONDING LINE OF A SAFETY DOCUMENT HAVING THE FORM OF A BOOKLET
WO1996017730A1 (en) System for binding printed works
EP1634223B1 (en) Multilayer card made of thermoplastic material, and method for securing the multilayer card
FR3127439A1 (en) Method of making insert for passport book data page
FR2549775A1 (en) PROCESS FOR MANUFACTURING PLASTICATED IDENTIFICATION CARDS
FR2572027A1 (en) Composite article of the file or binder type used for stationery, and method of manufacture of the same
EP4293569A1 (en) Inlay for an electronic document, method for producing an electronic document comprising such an inlay, and resulting electronic document
EP0726853A1 (en) Method for permanently transferring a diffraction network, transfer film and device for carrying out said method
EP1892329B1 (en) Sheet of fibrous material comprising tactile safety elements
WO2024110427A1 (en) Pre-laminate for forming a data page of an identification booklet and method for manufacturing the data page
FR3041131A1 (en) ELECTRONIC DOCUMENT COMPRISING A COATING TO THE LAW OF THE CAVITY AND METHOD OF MANUFACTURING SUCH A DOCUMENT
EP2766854B1 (en) Method and device for manufacturing a substrate for receiving an electronic device, and corresponding substrate

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 15732302

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 15732302

Country of ref document: EP

Kind code of ref document: A1