EP1320427B1 - Method and installation for making a workpiece comprising at least a tubular section - Google Patents

Method and installation for making a workpiece comprising at least a tubular section Download PDF

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Publication number
EP1320427B1
EP1320427B1 EP01972204A EP01972204A EP1320427B1 EP 1320427 B1 EP1320427 B1 EP 1320427B1 EP 01972204 A EP01972204 A EP 01972204A EP 01972204 A EP01972204 A EP 01972204A EP 1320427 B1 EP1320427 B1 EP 1320427B1
Authority
EP
European Patent Office
Prior art keywords
bending
plate
edge
component
folding
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.)
Expired - Lifetime
Application number
EP01972204A
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German (de)
French (fr)
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EP1320427A1 (en
Inventor
Jean-Claude Jeandeaud
Jean-Pierre Reyal
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.)
JEANDEAUD JEAN CLAUDE
Tors Sa
Aperam Alloys Imphy SAS
Original Assignee
Imphy Ugine Precision SA
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Filing date
Publication date
Application filed by Imphy Ugine Precision SA filed Critical Imphy Ugine Precision SA
Publication of EP1320427A1 publication Critical patent/EP1320427A1/en
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Publication of EP1320427B1 publication Critical patent/EP1320427B1/en
Anticipated expiration legal-status Critical
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D5/00Bending sheet metal along straight lines, e.g. to form simple curves
    • B21D5/04Bending sheet metal along straight lines, e.g. to form simple curves on brakes making use of clamping means on one side of the work
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J29/00Details of cathode-ray tubes or of electron-beam tubes of the types covered by group H01J31/00
    • H01J29/02Electrodes; Screens; Mounting, supporting, spacing or insulating thereof
    • H01J29/06Screens for shielding; Masks interposed in the electron stream
    • H01J29/07Shadow masks for colour television tubes
    • H01J29/073Mounting arrangements associated with shadow masks
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J9/00Apparatus or processes specially adapted for the manufacture, installation, removal, maintenance of electric discharge tubes, discharge lamps, or parts thereof; Recovery of material from discharge tubes or lamps
    • H01J9/02Manufacture of electrodes or electrode systems
    • H01J9/14Manufacture of electrodes or electrode systems of non-emitting electrodes
    • H01J9/142Manufacture of electrodes or electrode systems of non-emitting electrodes of shadow-masks for colour television tubes
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J2229/00Details of cathode ray tubes or electron beam tubes
    • H01J2229/07Shadow masks
    • H01J2229/0722Frame

Definitions

  • the invention relates to a method and an installation. for manufacturing a part comprising at least one part tubular obtained by folding a sheet according to the preambles of claims 1 and 16.
  • This process and this installation are, in particular, suitable for the manufacture of a shadow mask support frame for a cathode ray tube viewing.
  • Cathode ray tubes color visualization include a sheet metallic, pierced with a multitude of holes or slots, called “shadow mask” or “shadow mask” and arranged between the electron gun and the display screen.
  • shadow mask is supported by a frame, usually of rectangular shape, which keeps it in position in the vicinity of the display screen and, if necessary, ensures that the mask is stretched in order to limit the resulting deformations local overheating generated by the electron beams.
  • An object of the present invention is to provide a folding process using a folding machine allowing to manufacture parts comprising at least part tubular, in particular a part constituting one or more amounts of a shadow mask support frame.
  • the invention relates to a method of manufacture of a part comprising at least one section tubular obtained by folding a metal plate according to au minus a longitudinal edge, characterized in that it includes steps consisting in pre-folding the plate according to minus two folding edges then to exercise, during folding, a clamping force of at least part of the plate by compared to a folding member.
  • the metal plate is effectively moved by the folding member, without risk of slipping may result in imprecise bending at the ridge. Thanks to pre-folding, the plate is kept in position on the apron or box spring on which it rests, without risk of buckling during subsequent folding.
  • the effort of clamping or retaining the plate relative to the edge of folding keeps the plate in position relative to its environment without having to use pliers fasteners that could hardly be used inside tubular parts because they would interfere with folding operations.
  • the invention also relates to an installation allowing to implement the method described above and, more specifically an installation comprising at least one member for folding a metal plate along an edge longitudinal of a tubular section of the frame, characterized in that this folding member is equipped with means allowing to exert a clamping force on part of the plate opposing a sliding of part of the plate along of the folding member, while this folding member is articulated around a virtual geometric axis located inside of the corresponding tubular section.
  • the invention finally relates to the use of the process or of the installation mentioned above for manufacturing a shadow mask support frame for cathode ray tube.
  • FIG 1 there is shown schematically a shadow mask 1 mounted on a frame 2 mask support shade.
  • Frame 2 has a generally rectangular shape and has two lateral uprights 3, 3 'and two uprights 4, 4 'ends.
  • the shadow mask consists of a thin metal foil, e.g. iron-nickel alloy low expansion coefficient, drilled with 5 holes and fixed by welding on upper edges 6, 6 'of the uprights end 4, 4 '.
  • Different forms of shadow mask are possible depending on the cathode ray tube to which it must be associated.
  • the shadow mask is generally planar, but it can also be bent in portion of cylinder.
  • the mask 1 can also be stretched, i.e. subject to tension parallel to the uprights side 3, 3 'of frame 2.
  • the uprights 3, 3 ', 4 and 4' are formed by folding a sheet metal so as to each constitute a tubular element. These four uprights can be obtained by folding a single metal plate. It is also possible to plan to use a folded plate for each upright or a plate for two contiguous amounts.
  • a single metal plate 10 is used for the realization of four tubular uprights 3, 3 ', 4 and 4'. This plate appears partially in Figure 3 after steps of cutting of assembly tabs 11 and of pre-marking longitudinal edges 12 to 17.
  • the plate 10 forms the end upright 4. At the edges 12 and 15 to 17, the plate 10 forms the lateral upright 3.
  • the part of the plate 10 shown in Figure 3 corresponds to the corner 7 of frame 2 at the level of which the junction between amounts 3 and 4.
  • the plate 10 is shaped in the configuration of FIG. 3 by cutting, stamping and folding operations using, in particular, punches intended to create in the plate 10 an edge 12 extending over substantially its entire length while the edges 13 to 17 extend over only part of the plate 10, the edges 13 and 15 being parallel to each other but offset, that is to say distant from the edge 12 by distances d 1 and d 2 different.
  • the pre-folding of the plate 10 is carried out by immobilizing this plate on an apron or counter blade 101 thanks to a blank holder 107 and by folding the plate 10 as shown by the arrows F, which has the effect of creating the lines of folding 12 and 13.
  • Another blank holder is used at the amount 3, which allows to continue the creation of the line of fold 12 and create the fold line 15.
  • This second hold-down is also configured to allow creation fold lines 16 and 17.
  • the plate 10 is immobilized in relation to the installation of the invention because it is in abutment along the two folding edges 12 and 13 or 12 and 15 which are generally parallel.
  • Pre-folding can be prepared by marking the fold lines, for example by punching on a part of the thickness of the plate 10, in particular 25%.
  • the pre-folding of the plate 10 can be performed on the machine shown in the figures or on another machine, without going beyond the scope of this invention.
  • preliminary pre-folding are necessary to make the edges of the type of edges 16 and 17. Such preliminary pre-folding is also used in the case of the amount 4 for the realization of the edge 14.
  • the installation of the invention 100 includes the apron 101 on which a central part 21 of the plate 10 is placed. Pawns, only one of which is visible in the figures with the reference 102, extend from this plate 101 and are intended to pass through openings 22 provided in the part 21, so as to position the plate 10 on the base plate 101.
  • From part 21 extend two wings 23 and 24 of the plate 10 intended to form the upright 4. From this same central part 21 extend two other wings 25 and 26 intended to form the amount 3.
  • the wings 23 and 25 are connected to the part 21 along the edge 12.
  • the wings 24 and 26 are respectively connected to the part 21 along the edges 13 and 15.
  • the wing 23 is connected to an edge 27 by the fold line or edge 14 while the wings 25 and 26 are both divided into two panels 25 a , 25 b respectively 26 a , 26 b by the fold lines or edges 16 and 17.
  • the installation 100 comprises a folding jaw 103 intended to fold the wing 23 in the direction of the part 21 by means of a force represented by the arrow F 1 .
  • the jaw 103 comprises a plate 103 a whose length, parallel to a longitudinal axis XX ′ of the installation 100, is adapted to the length of the wing 23.
  • the face 103 a 1 of the plate 103 a is intended to be in contact with wing 23 is generally flat.
  • the plate 103 a is equipped, on its face 103 a 2 opposite the face 103 a 1, with two ribs 103 b , extending opposite the wing 23 in directions generally perpendicular to the axis X- X '.
  • ribs 103 b each form a convex surface 103 c in a portion of a cylinder with a circular base centered on a virtual axis a.
  • virtual is meant the fact that the axis a is not defined by a hinge, but as being the geometrical location joining the centers of curvature of the surfaces 103 c .
  • This axis is located inside the upright 4 and is parallel to the axis XX '.
  • the installation 100 also includes a cradle 113 defining an internal surface 113 c that is cylindrical and with a circular base against which the ribs 103 b slide by their surfaces 103 c .
  • the axis of symmetry of the surface 113 a is also the axis a.
  • the radii of curvature R 103 and R 113 of the surfaces 103 c and 113 c are equal. It is thus possible to rotate the jaw 103 in the cradle 113 around the axis a , as shown by the arrow F 2 in Figure 4, by relative sliding of the surfaces 103 c and 113 c .
  • a second jaw 104 comprises a plate 104 a intended to come to bear, by a face 104 a 1, against the wing 24 and to exert on it a force F 3 allowing it to be folded down in the direction of the base plate 101 and of the central part 21.
  • the plate 104 a is provided, on its face 104 a 2 opposite the face 104 a 1, of ribs 104 b of which an external or convex surface 104 c is cylindrical with a circular base and capable of coming into bearing against an internal cylindrical or concave surface with a circular base 114 c of a cradle 114.
  • c the common central geometric axis of the surfaces 104 c , this axis being parallel to the axis XX 'and located in the interior volume of the amount 4.
  • 114 c and R 104 and R 114 the respective radii of the surfaces 104 c and 114 c, these radii being of the same length.
  • the jaw 104 can pivot around the axis c while being guided by the cradle 114, as shown by the arrow F ′ 2 .
  • the jaws 103 and 104 are each fitted with a heel 103 f , 104 f capable of exerting an effort on the wings 23 and 24, respectively noted F 7 and F 8 ; directed generally towards the edges 12 and 13, that is to say opposing a sliding of the wings 23 and 24 in the direction of the arrows F 5 and F 6 .
  • the forces F 7 and F 8 therefore constitute efforts for clamping or retaining the wings 23 and 24 relative to the jaws 103 and 104.
  • the wings 23 and 24 are not likely to project radially outside the jaws 103 and 104.
  • the heels 103 f and 104 f form stops for the displacement of the wings 23 and 24 in the direction of the arrows F 5 and F 6 .
  • the forces F 7 and F 8 are exerted from the outside of the upright 4.
  • the plate 10 is held on the deck 101 without the use of an insert, such as a sidewall clamp, which is favorable because a sidewall would be difficult to set up and remove once the plate folded.
  • a sidewall could not extend to the level of the upright 3.
  • the invention therefore allows folding of the plate 10 in one tubular structure without the introduction of a jamming inside its different sections.
  • the heel 103 f is in one piece with the plate 103 a , this heel being intended to cover the edge 27 of the wing 23.
  • This heel 103 f extends over the entire length of the jaw 103 parallel to the axis XX ' , which guarantees that the upper edge of the upright 4, on which the mask 1 is intended to be stretched, is free from irregularities.
  • the bead 103f has a smooth surface on the side of the edge 27 because the heel 103 f used for forming the edge which should be as regular as possible for the mask 1, which is stretched over the upper edge of upright 4, does not have a wave or relief capable of disturbing the image generated in the cathode ray tube.
  • the heel 104 f which extends over the entire length of the jaw 104, is capable of moving perpendicular to the plate 104 a and to the wing 24, as shown by the arrow F 9 in FIG. 4.
  • the jaw 104 When the plate 10 has been positioned on the deck 101 and pre-folded using the blank holder 107, the jaw 104 is moved by an electric or hydraulic pneumatic jack, so that it folds down, thanks to the force F 3 exerted by the plate 104 a , the plate 24 in the direction of the part 21.
  • the heel 104 f exerts on the wing 24 a force F 8 directed towards the edge 12, which guarantees a good positioning of the wing 24 by relative to the jaw 104.
  • the jaw 103 is actuated so that it flaps the wing 23 in the direction of the part 21 by exerting the force F 1 , as shown in FIG. 7.
  • the jaws 103 and 104 are guided in their displacements F 2 and F ' 2 thanks to the cooperation of the convex cylindrical surfaces 103 c , 104 c and concave 113 c , 114
  • the heel 104 f is distant from the wing 24, as shown by the arrow F ′ 9 in FIG. 7.
  • the angle ⁇ is less than 90 ° ensures effective positioning of the 'wing 24, including in the case of removal of the force F 8 .
  • the force F 8 is not essential because the plate 104 effectively maintains the flange 24 in position relative to the c axis.
  • FIG. 15 is an enlargement of detail XV in Figure 4.
  • the plate 10 has a thickness e not zero.
  • the transition from the position shown in solid lines to the position shown in dashed lines, which corresponds substantially to that of FIG. 7, has the effect of reducing the height h of the wing 23 in the configuration in dashed lines relative to the length l of this wing in the configuration in solid lines because the neutral fiber f of the plate 10 forms an arc of circle centered on the axis a in the configuration shown in broken lines.
  • the axis a is located inside the area intended to form the edge 12 with a distance d from the neutral fiber f and taking the example of a plate bent from from a flat configuration to arrive at a configuration folded at 90 °, the difference between the height h and the length l is 1/2 ⁇ d. In the present case, it is less insofar as the edge 12 is already pre-marked in the configuration of FIG. 4. It is however not zero.
  • the value of the force F 7 should be adapted so that it effectively immobilizes the plate 10 in the region of the edge 12 throughout the rotational movement of the jaw 103 around the axis a.
  • a system of cams makes it possible to vary the intensity of the force F 7 as a function of the angular orientation of the jaw 103 around the axis a, during the pivoting F 2 .
  • the heel 103 f can be in one piece with plate 103 has jaw 103.
  • the heel 104 f can also be provided with means making it possible to vary the intensity of the force F 8 as a function of the jaw position 104 around the axis c during the pivoting F ′ 2 .
  • the position of the axis c can also be provided for variable to compensate for the variations in length and / or height of the wing 24.
  • the lateral upright 3 is of quadrangular section.
  • a jaw 105 is provided to cooperate with the wing 25 and comprises a base plate 105 a , one face 105 a 1 in contact with the wing 25 allows exerting a force F 11 to fold the wing 25 towards the elements 21 and 101.
  • the jaw 105 is equipped with ribs 105 b defining convex cylindrical surfaces 105 c centered on the axis a and making it possible to cooperate with a cradle 115 defining a concave surface 115 c for sliding the surfaces 105 c , the surface 115 c being, like the surfaces 105 c , with a circular base and centered on the axis a.
  • the jaw 105 is equipped with several heels 105 f distributed over its length parallel to the axis XX ′, these heels being designed to come into contact with the wing 25 at the edge 17 by constituting a stop at a possible sliding of the wing 25.
  • the heels 105 f exert on the wing 25 a clamping force F 12 directed towards the edge 12 and parallel to the panel 25 a .
  • the force F 12 has the same function as the forces F 7 and F 8 previously mentioned. It makes it possible to effectively position the wing 25 relative to the axis a throughout the folding operation carried out thanks to the force F 11 .
  • a jaw 106 is provided to cooperate with the wing 26 and comprises a plate 106a forming a face 106 a 1 bearing against the wing 26 and equipped with ribs 106 b whose convex external radial surfaces 106 c cooperate with a concave surface 116 c of a cradle 116.
  • the surfaces 106 c and 116 c are centered on a geometric axis or virtual axis b constituting the center of the edge 15 and located, like the axis a, in the volume inside the upright 3.
  • the jaw 106 is equipped with heels 106 f making it possible to retain the wing 26 in position relative to the plate 106 a during the folding of the edge 15.
  • the plate 106 a is not flat but forms a concave zone of receiving the panels 26 a and 26 b , the plate 106 a being itself formed by two panels oriented relative to each other with an angle ⁇ corresponding to the angle of orientation of the panels 26 a and 26 b relative to each other.
  • the heels 106 f are arranged to bear against the free edge 26 c of the panel 26 b .
  • the heels 106 f are distributed over the length of the plate 106 a .
  • the heels 105 f on the one hand and 106 f on the other hand are staggered relative to each other by being offset along the axis XX ', a heel 105 f being opposite an interval free 106 g defined between two heels 106 f , while a heel 106 f is placed opposite a free interval 105 g defined between two heels 105 f .
  • a force is exerted on the jaw 105 by any suitable means, so that it is moved and exerts the force folding F 11 of the wing 25 in the direction of the part 21, the heels 105 f overlapping the junction zone 25 c , defined between the panels 25 a and 25 b and which includes the edge 17.
  • the force F 11 allows the wing 25 to be folded down into the position of FIG. 9 where the panel 25 a is generally perpendicular to the part 21, the panel 25 b being generally parallel to this part.
  • the force F 12 effectively retains the wing 25 in position relative to the jaw 105 and to the edge 12.
  • the jaw 106 is then activated, to pass from the position of FIG. 9 to that of FIG. 10, a force F 13 in bending the wing 26 in the direction of the part 21 being exerted by the plate 106 a while a force F 14 is exerted by the heels 106 f on the wing 26 parallel to this wing and generally in the direction of the edge 15.
  • the forces F 12 and F 14 can be modulated as a function of the orientation of the jaws 105 and 106 around the axes a and b.
  • the axes a and b can be offset from their representation in FIGS. 8 to 10 in order to compensate for the variations in length of the wings 25 and 26.
  • the force F 12 can be relaxed or reduced by a movement of the heel 105 f in a direction away from the edge 12, so that, due to the elasticity of the plate 10, the panel 25 b comes into firm elastic abutment against the face of the panel 26 b oriented towards the part 21. It is then possible to weld the panels 25 b and 26 b point by point using a beam high energy directed between two heels 105 f and 106 f adjacent.
  • the folding angle between the panels 25 a and 25 b is slightly more open than that obtained in the configuration of FIG. 10, so that an elastic support is obtained in this configuration without it being necessary to release the force F 12 .
  • the frame 2 is shaped, after shaping the different uprights 3, 3 ', 4 and 4', by folding.
  • the plate 10 extends overall in the direction X-X 'in four sections connected by 8, 8 'and 8' 'junction zones.
  • a tool 200 is provided for the shaping of frame 2 and includes four parts 201, 202, 203 and 204 each intended to receive one of the amounts 3, 3 ', 4 or 4'.
  • flaps 201 to 204 are each formed of two mass pieces 201 a , 201 b , 202 a , 202 b , 203 a , 203 b , 204 a , 204 b connected by a screw-nut system 201 c , 202 c , 203 c or 204 c for adjusting the length of the flaps 201 to 204.
  • Guide rods 201 c ', 202 c ', 203 c 'and 204 c ' are associated with systems 201 c to 204 c .
  • the length of each flap 201 to 204 is adjusted, parallel to its largest dimension X 1 to X 4 , to the length of the amount that it must receive.
  • the flaps 201 to 204 are provided adjustable in length to allow the manufacture of frames 2 of different sizes.
  • the parts 201 a and 201 b are respectively provided with angles 201 d , 201 e for receiving the amount 4.
  • Jaws 201 f , 201 g are provided for immobilizing the amount 4 against the angles 201 d and 201 e .
  • the flaps 202, 203 and 204 are respectively equipped with angles 202 d to 204 e and jaws 202 f to 204 g .
  • the jaws are shaped as a function of the geometry of the wings 24 and 26.
  • the flaps 201 and 202 are articulated together around an axis Y 1 essentially perpendicular to the main direction XX 'of the uprights 3, 4, 3' and 4 '.
  • the axis Y 1 is also perpendicular to the direction X 1 in which the flap 201 is adjustable in length.
  • the flaps 202 and 203 are articulated together around an axis Y 2 while the flaps 203 and 204 are articulated together around an axis Y 3 , these axes Y 2 and Y 3 being generally perpendicular to the 'axis XX' and to the directions X 1 , X 2 , X 3 and X 4 for adjusting the length of the different flaps.
  • Three cylinders 205, 206 and 207 respectively connect the flaps 201 and 202, the flaps 202 and 203 and the flaps 203 and 204, so that they are capable of exerting on them closing forces represented by the arrows F 16 , F 17 and F 18 in FIG. 14. These efforts make it possible to bring the tool 200 into a generally rectangular configuration in a plane perpendicular to the axes Y 1 to Y 3 , which makes it possible to fold the frame 2 at the level of the zones 8, 8 'and 8''and to form corners such as corner 7, as shown in FIGS. 12 and 13.
  • the force F 17 has the effect of bringing the sides of the flaps 202 and 203 together by the cylinder 206, which results in a folding of the plate 10 along a line 18 parallel to the axis Y 2 .
  • the tabs 11 formed on the upright 4 are thus brought into overlap with the edge 3a of the upright 3, these tongues and this edge can then be welded by a high energy beam.
  • the tool 200 forms a rectangle whose flaps 201 to 204 constitute the four sides. This rectangle is closed at an area of junction between shutters 201 and 204 where means are provided not shown locking associated with means of guidance also not shown. So the rectangle shown in Figure 14 is defined precisely by the cooperation of flaps 201 to 204, so that the geometry of frame 2 thus obtained is also defined so precise.
  • the jaw 106 is equipped with a blade 106h forming a shear with the plate 101 and making it possible to cut, when folding the upright 3, the plate 10 in the junction zone of the uprights 3 and 4 so as to create a notch 19 visible in FIG. 11 compatible with the folding movement around the axis Y 2 . Due to the use of the blade 106 h , the notch is created at the end of the operations of shaping the tubular uprights 3, 3 ', 4 and 4'. Before the use of this blade, the plate 10 has continuity in the zones 8, 8 'and 8''of junction between the uprights 3 and 4.
  • the incorporation of the blade 106 h on the jaw 106 allows the notch 19 to be produced just before the use of the tooling 200, which avoids excessive stresses at the level of the line 18 during the production of the tubular parts.
  • the blade 106 h can have a double cutting edge, so that it allows the plate 10 to be cut along two parallel lines 28 and 29 defining between them the notch 19 until a bore 30 previously formed in the plate 10.
  • the jaws 103, 104 and 105 can also be fitted with blades forming shears.
  • jaws 103 to 106 which can slide on cradles 113 to 116 of different geometric axes, such as axes a and c , makes it possible to produce non-aligned edges, such as edges 13 and 15, which would not be possible. with conformation jaws articulated on common hinges.
  • the jaws 103 and 105 and the cradles 113 and 115 have been shown as two separate units. It could however be the same unit forming a folding member for both uprights 3 and 4, because the folding axis a is the same for the entire edge 12 over the length of the plate 10. C 'is why, the plates 103 a and 105 a on the one hand and the cradles 103 d and 105 d could be made in one piece.
  • the plate to be folded is thin and in order to avoid a phenomenon of buckling of its wings under the effect of the clamping forces, provision may be made to press the sheet against the plates 103 a to 106 has jaws 103 to 106 by suction. or by magnetic attraction.
  • the jaws 103 to 106 can be provided with channels opening on the faces 103 to 1, 103 to 2, 105 to 1 and 106 to 1 and connected to a vacuum source.
  • the jaws can also be equipped with permanent magnets or electromagnets allowing immobilization of the wings 23 to 26.
  • the jaws can be guided by cradles, such as the cradle 114 by means of telescopic circular segments 1041 and 1042 which allow, for a given geometry of a cradle 114 to obtain effective guidance for a movement F 20 of pivoting of the jaw 104 around the axis c of great amplitude.
  • the segment 1041 is integral with the jaw 104 while it is fitted inside the segment 1042, this segment 1042 itself being movable in abutment against the internal cylindrical surface 114 c of the cradle 114.
  • Segment 1042 is hollow while segment 1041 is full and less than the width of the volume inside segment 1042.
  • the segment 1042 is provided with rollers 1042g arranged along its internal surface 1042 h and able to cooperate with the section 1041 c of the segment 1041. These rollers facilitate the relative sliding between the segments 1041 and 1042.
  • the section 1042 c of the segment 1042 is also provided with rollers 1042 i able to cooperate with the internal surface 114 c of the cradle 114. This facilitates the pivoting of the segment 1042.
  • segment 1041 and / or cradle 114 can be fitted with sliding balls or rollers.
  • the invention has been described, with reference to the first embodiment, with jaws equipped with ribs whose end surfaces 103 c , 104 c , 105 c and 106 c are provided to slide against the cylindrical surfaces 113 c to 116 c cradles 113 to 116.
  • the ribs 103 b to 106 b can be fitted with ball or roller skates, these balls or rollers being designed to roll on surfaces 113 c to 116 c .
  • angles 201 d to 204 e and the jaws 201 f to 204 g of the first embodiment can be replaced by profiles with a generally U-shaped cross section, two of which are shown in Figure 18, with the references 202 m and 203 m .
  • These profiles have a cross section adapted to receive respectively the amounts 3 and 4 'by being fixed on flaps similar to flaps 202 and 203 of the first embodiment.
  • Wedges 202 p and 203 p are respectively associated with profiles 202 m and 203 m to wedge the uprights 3 and 4 'in position.
  • These shims have a generally triangular section with a truncated angle, that is to say in fact a trapezoidal section.
  • the shims are introduced into the profiles as represented by the arrows F 20 , the geometry of the shims 202 p and 203 p being such that they are each provided with a surface 202 g , 203 g adapted to rest against certain wings 24 or 26 of the sections 3 and 4 '.
  • Each wedge 202 p or 203 p is provided with a blind hole 202 r , 203 r for receiving a plug 202 s , 203 s intended to pass through an orifice 202 t , 203 t of the profiles 202 m and 203 m .
  • the introduction of the plug 202 s into the orifice 202 t and the blind hole 202 r is represented by the arrows F 21 .
  • the invention has been shown with jaws whose internal surfaces 103 a 1 to 106 a 1 are planar while the wings 23 to 26 are also planar. Of course, these surfaces and these wings can be left depending on the geometry sought for the amounts 3, 3 ', 4 and 4'.
  • the invention has been shown during its implementation for the production of shadow mask support frames.
  • Such frames can be made in one, two or four pieces, each piece forming one, two or all four uprights of the frame.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Bending Of Plates, Rods, And Pipes (AREA)
  • Heat Treatment Of Articles (AREA)
  • Rigid Pipes And Flexible Pipes (AREA)
  • Insulators (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)

Abstract

A method of forming a tubular workpiece which consists in pre-bending a metal plate along at least two longitudinal lines of bend ( 12-13 ) then in bending the plate along at least one of the lines of bend ( 12-13 ) using a bending member ( 103-104 ) that exerts an external clamping force (F<SUB>7</SUB>, F<SUB>8</SUB>) along a part ( 23, 24 ) of the plate towards the at least one of the lines of bend ( 12, 13 ). Thereby preventing any sliding of part ( 23, 24 ) of the plate along the bending member ( 103-104 ) as the bending member bends the part. The bending member is articulated about a virtual geometrical axis (a, c) located inside a tubular section of the workpiece.

Description

L'invention a trait à un procédé et à une installation de fabrication d'une pièce comportant au moins une partie tubulaire obtenue par pliage d'une tôle selon les préambules des revendications 1 et 16. Ce procédé et cette installation sont, notamment, adaptés à la fabrication d'un cadre de support de masque d'ombre pour un tube cathodique de visualisation.The invention relates to a method and an installation. for manufacturing a part comprising at least one part tubular obtained by folding a sheet according to the preambles of claims 1 and 16. This process and this installation are, in particular, suitable for the manufacture of a shadow mask support frame for a cathode ray tube viewing.

Un tel cadre est utilisé, par exemple, dans le domaine de la fabrication des téléviseurs couleur. Les tubes cathodiques de visualisation en couleur comprennent une feuille métallique, percée d'une multitude de trous ou de fentes, appelée "masque d'ombre" ou "shadow mask" et disposée entre le canon à électrons et l'écran de visualisation. Un tel masque d'ombre est supporté par un cadre, généralement de forme rectangulaire, qui le maintient en position au voisinage de l'écran de visualisation et, le cas échéant, assure que le masque est tendu afin de limiter les déformations résultant des échauffements locaux engendrés par les faisceaux d'électrons.Such a framework is used, for example, in the field of the manufacture of color televisions. Cathode ray tubes color visualization include a sheet metallic, pierced with a multitude of holes or slots, called "shadow mask" or "shadow mask" and arranged between the electron gun and the display screen. Such shadow mask is supported by a frame, usually of rectangular shape, which keeps it in position in the vicinity of the display screen and, if necessary, ensures that the mask is stretched in order to limit the resulting deformations local overheating generated by the electron beams.

Il est connu de EP-A-0 809 272 de réaliser un cadre de masque d'ombre à partir de deux bandes métalliques minces accolées l'une à l'autre et comportant des nervures de rigidification. Un tel cadre est léger et rigide, ce qui permet de l'utiliser pour un masque d'ombre tendu ainsi que pour un masque d'ombre embouti. Par la demande FR-A-2 790 140, on connaít un cadre de masque d'ombre comportant des parties tubulaires formées par pliage d'une tôle. Le pliage de la tôle peut être effectué par différents procédés, en particulier à la main, un pliage manuel cependant n'étant pas compatible avec une production industrielle à cadence élevée. Par ailleurs, les procédés connus de pliage à l'aide de machines comportant un tablier, parfois dénommé "contrelame", sur lequel est maintenu une tôle à plier à l'aide d'un serre-flan, et un volet de pliage articulé, ne permettent pas de fabriquer aisément des parties tubulaires. It is known from EP-A-0 809 272 to produce a frame for shadow mask from two thin metal strips attached to each other and having ribs of stiffening. Such a frame is light and rigid, which allows to use it for a stretched shadow mask as well as for a deep shadow mask. By request FR-A-2 790 140, we know a shadow mask frame with parts tubular formed by folding a sheet. Folding the sheet can be carried out by different methods, in particular at by hand, manual folding, however, is not compatible with industrial production at a high rate. Through elsewhere, the known methods of folding using machines with an apron, sometimes called a "counterblade", on which is maintained a sheet to be folded using a blank holder, and an articulated folding flap, do not allow to manufacture easily tubular parts.

Un but de la présente invention est de proposer un procédé de pliage à l'aide d'une machine de pliage permettant de fabriquer des pièces comportant au moins une partie tubulaire, notamment une pièce constituant un ou plusieurs montants d'un cadre support de masque d'ombre.An object of the present invention is to provide a folding process using a folding machine allowing to manufacture parts comprising at least part tubular, in particular a part constituting one or more amounts of a shadow mask support frame.

Dans cet esprit, l'invention concerne un procédé de fabrication d'une pièce comportant au moins une section tubulaire obtenue par pliage d'une plaque métallique selon au moins une arête longitudinale, caractérisé en ce qu'il comprend des étapes consistant à pré-plier la plaque selon au moins deux arêtes de pliage puis à exercer, lors du pliage, un effort de bridage d'au moins une partie de la plaque par rapport à un organe de pliage.In this spirit, the invention relates to a method of manufacture of a part comprising at least one section tubular obtained by folding a metal plate according to au minus a longitudinal edge, characterized in that it includes steps consisting in pre-folding the plate according to minus two folding edges then to exercise, during folding, a clamping force of at least part of the plate by compared to a folding member.

Grâce à l'invention, la plaque métallique est efficacement déplacée par l'organe de pliage, sans risque de glissement pouvant résulter dans un pliage imprécis au niveau de l'arête. Grâce au pré-pliage, la plaque est maintenue en position sur le tablier ou sommier sur lequel elle repose, sans risque de flambage lors du pliage ultérieur. L'effort de bridage ou de retenue de la plaque par rapport à l'arête de pliage permet de maintenir la plaque en position par rapport à son environnement sans avoir recours à des pinces de fixation qui ne pourraient que difficilement être utilisées à l'intérieur de parties tubulaires car elles gêneraient les opérations de pliage.Thanks to the invention, the metal plate is effectively moved by the folding member, without risk of slipping may result in imprecise bending at the ridge. Thanks to pre-folding, the plate is kept in position on the apron or box spring on which it rests, without risk of buckling during subsequent folding. The effort of clamping or retaining the plate relative to the edge of folding keeps the plate in position relative to its environment without having to use pliers fasteners that could hardly be used inside tubular parts because they would interfere with folding operations.

Selon des aspects avantageux mais non obligatoires de l'invention, le procédé incorpore une ou plusieurs des caractéristiques suivantes :

  • le pré-pliage est effectué en immobilisant la plaque sur un tablier au moyen d'un serre-flan rétractable. On peut en outre prévoir une étape de préparation du pré-pliage par affaiblissement de la tôle le long des arêtes de pliage. Cet affaiblissement peut être effectué par marquage ou poinçonnage sur une partie de l'épaisseur de la tôle, ou par tout autre procédé adapté
  • on plie la plaque selon des arêtes différentes sur la longueur de la pièce à fabriquer, de telle sorte qu'il est formé des sections tubulaires de profils de base différents. Ceci permet de réaliser des pièces de géométrie élaborée, telles que des cadres support de masque d'ombre.
  • on plie la plaque autour d'au moins un axe géométrique virtuel défini par la coopération de l'organe de pliage et de moyens de guidage associés.
  • on exerce l'effort de bridage essentiellement par l'extérieur d'une section tubulaire de la pièce, en l'absence d'un effort de serrage exercé par un serre-flanc ou un matériel analogue. Ceci tient compte du fait que l'utilisation d'un serre-flanc est délicate avec une pièce tubulaire, voire impossible si elle présente des sections de profils de base différents.
  • l'effort de bridage est dirigé globalement en direction de l'arête de pliage.
  • l'effort de bridage est globalement perpendiculaire à l'arête de pliage.
  • l'effort de bridage contraint une partie de la plaque métallique parallèlement à elle-même et perpendiculairement à l'effort de pliage exercé sur cette partie par l'organe de pliage.
  • l'effort de bridage est adapté en fonction de la position de l'organe de pliage. Cet aspect de l'invention permet de tenir compte des variations dimensionnelles de la plaque au cours de l'opération de pliage, ces variations résultant notamment des contraintes localisées au niveau de l'arête et de son rayon de courbure. Il permet également d'éviter une interférence entre les éléments permettant d'exercer un effort de bridage au niveau de deux bords opposés de la plaque.
  • le procédé comprend en outre une étape consistant, à amener une première partie de la plaque en recouvrement d'une seconde partie de celle-ci et à diminuer l'effort de bridage exercé sur la seconde partie avant soudage de ces parties ensemble. Cet aspect de l'invention assure que les parties en recouvrement sont en contact élastique lors du soudage, ce qui permet à ce soudage d'être efficace et durable.
  • le procédé comprend également une étape consistant à plier la plaque autour d'au moins un axe virtuel défini comme l'axe géométrique d'un berceau cylindrique de guidage de l'organe de pliage. L'utilisation d'un axe virtuel permet de manoeuvrer l'organe de pliage sans avoir recours à une charnière susceptible d'interférer avec d'autres parties de l'installation dédiées à un pliage selon une autre arête. On peut, en particulier, prévoir de plier la plaque autour d'axes de pliage différents selon la longueur de la pièce en utilisant des organes de pliage guidés par des berceaux d'axes géométriques différents correspondant à ces axes de pliage.
  • le procédé comprend une étape consistant, après formation de plusieurs sections tubulaires, à les conformer en un cadre fermé par pliage de sections de liaison, entre deux sections tubulaires adjacentes, perpendiculairement aux directions principales de ces sections tubulaires.
  • le procédé comprend une étape consistant à plaquer, par aspiration ou attraction magnétique, une partie de la plaque de tôle contre une partie de l'organe de pliage.
According to advantageous but not compulsory aspects of the invention, the method incorporates one or more of the following characteristics:
  • pre-folding is carried out by immobilizing the plate on an apron by means of a retractable blank holder. It is also possible to provide a step for preparing the pre-folding by weakening the sheet along the folding edges. This weakening can be carried out by marking or punching over part of the thickness of the sheet, or by any other suitable method.
  • the plate is folded according to different edges along the length of the workpiece, so that it is formed of tubular sections of different base profiles. This makes it possible to produce parts of elaborate geometry, such as shadow mask support frames.
  • the plate is folded around at least one virtual geometric axis defined by the cooperation of the folding member and associated guide means.
  • the clamping force is exerted essentially from the outside of a tubular section of the part, in the absence of a clamping force exerted by a clamp or the like. This takes into account the fact that the use of a clamp is difficult with a tubular piece, or even impossible if it has sections of different basic profiles.
  • the clamping force is directed generally in the direction of the folding edge.
  • the clamping force is generally perpendicular to the folding edge.
  • the clamping force constrains a part of the metal plate parallel to itself and perpendicular to the folding force exerted on this part by the folding member.
  • the clamping force is adapted as a function of the position of the folding member. This aspect of the invention makes it possible to take account of the dimensional variations of the plate during the folding operation, these variations resulting in particular from the localized stresses at the level of the edge and its radius of curvature. It also avoids interference between the elements making it possible to exert a clamping force at two opposite edges of the plate.
  • the method further comprises a step consisting in bringing a first part of the plate into overlap with a second part thereof and in reducing the clamping force exerted on the second part before welding these parts together. This aspect of the invention ensures that the overlapping parts are in elastic contact during welding, which allows this welding to be effective and durable.
  • the method also comprises a step consisting in folding the plate around at least one virtual axis defined as the geometric axis of a cylindrical cradle for guiding the folding member. The use of a virtual axis makes it possible to maneuver the folding member without having recourse to a hinge capable of interfering with other parts of the installation dedicated to folding along another edge. One can, in particular, provide to fold the plate around different folding axes according to the length of the part using folding members guided by cradles of different geometric axes corresponding to these folding axes.
  • the method comprises a step consisting, after the formation of several tubular sections, in forming them into a closed frame by folding connecting sections, between two adjacent tubular sections, perpendicular to the main directions of these tubular sections.
  • the method comprises a step consisting in pressing, by suction or magnetic attraction, a part of the sheet metal plate against a part of the folding member.

L'invention concerne également une installation permettant de mettre en oeuvre le procédé précédemment décrit et, plus spécifiquement une installation comportant au moins un organe de pliage d'une plaque métallique selon une arête longitudinale d'une section tubulaire du cadre, caractérisée en ce que cet organe de pliage est équipé de moyens permettant d'exercer sur une partie de la plaque un effort de bridage s'opposant à un glissement d'une partie de la plaque le long de l'organe de pliage, alors que cet organe de pliage est articulé autour d'un axe géométrique virtuel situé à l'intérieur de la section tubulaire correspondante.The invention also relates to an installation allowing to implement the method described above and, more specifically an installation comprising at least one member for folding a metal plate along an edge longitudinal of a tubular section of the frame, characterized in that this folding member is equipped with means allowing to exert a clamping force on part of the plate opposing a sliding of part of the plate along of the folding member, while this folding member is articulated around a virtual geometric axis located inside of the corresponding tubular section.

Selon des aspects avantageux mais non obligatoires de l'invention, l'installation incorpore une ou plusieurs des caractéristiques suivantes :

  • plusieurs organes de pliage sont aptes à plier la plaque selon des arêtes distinctes, de telle sorte qu'il est formé des sections tubulaires de profils de base différents.
  • les moyens de bridage sont constitués par au moins un talon formant une butée d'appui de la plaque. Ce talon peut s'étendre sur sensiblement toute la longueur de l'arête. On peut également prévoir plusieurs talons répartis sur la longueur de l'arête de pliage et séparés par des espaces de réception de talons de retenue utilisés pour le pliage de la plaque selon une autre arête.
  • les moyens de bridage ont une position variable par rapport à l'arête de pliage. Ceci peut provenir du fait que l'installation comprend des moyens de réglage ou d'adaptation de l'effort exercé par les moyens de bridage sur la plaque.
  • l'organe de pliage comprend au moins une surface d'appui contre la plaque et au moins une surface cylindrique à base circulaire apte à coopérer avec une surface cylindrique à base circulaire d'un berceau, ces surfaces cylindriques étant centrées sur un axe virtuel de pliage de la plaque. L'utilisation d'un tel berceau permet de guider l'organe de pliage sans avoir recours à une charnière susceptible d'interférer avec des dispositifs voisins. Dans ce cas, on peut prévoir que l'installation comprend plusieurs organes de pliage répartis sur la longueur de la plaque et coopérant avec des berceaux dont les surfaces cylindriques ont des axes géométriques parallèles et décalés les uns par rapport aux autres. Ceci permet de plier la plaque suivant des arêtes longitudinales distinctes, sur sa longueur, ce qui permet de conformer des sections tubulaires de géométries différentes correspondant, par exemple, à des côtés distincts d'un cadre à réaliser. Le ou les organes de pliage sont avantageusement équipés d'une nervure externe formant une surface cylindrique apte à coopérer avec la surface cylindrique du berceau correspondant, ces surfaces cylindriques étant sensiblement de mêmes rayons. Selon un mode de réalisation avantageux de l'invention permettant des basculements de grande amplitude, le ou les organes de pliage sont guidés par rapport à la surface cylindrique du berceau par des segments télescopiques qui coulissent l'un dans l'autre. Les surfaces des nervures, les segments télecopiques et/ou les surfaces des berceaux peuvent être équipés de billes ou rouleaux de glissement.
  • l'installation comprend un outillage de conformation de la pièce, cet outillage incluant des éléments de support de sections tubulaires de la pièce pourvus de moyens de réception et d'immobilisation de ces parties tubulaires, ces éléments étant articulés les uns par rapport aux autres. Cet outillage permet la mise en forme finale du cadre après réalisation des parties tubulaires. On peut prévoir que l'un au moins des éléments articulés est réglable en longueur, ce qui permet d'adapter l'outillage à la fabrication de cadres de dimensions différentes. On peut également prévoir que les éléments articulés sont aptes à former ensemble une figure fermée de géométrie prédéterminée correspondant à la géométrie d'un cadre formé par la pièce fabriquée. Le caractère fermé de la figure obtenue permet d'obtenir une précision géométrique accrue grâce à un positionnement univoque des différents éléments constitutifs de cet outillage. Selon un mode de réalisation avantageux de l'invention, l'un au moins des éléments articulés est équipé d'un organe, à section transversale globalement en forme de U et apte à recevoir au moins une cale de blocage d'une section tubulaire en place dans cet élément, des moyens étant prévus pour immobiliser la cale sur cet organe.
  • l'un au moins des organes de pliage est équipé d'une lame formant cisaille de découpe de la plaque lors de son pliage.
According to advantageous but not compulsory aspects of the invention, the installation incorporates one or more of the following characteristics:
  • several folding members are capable of folding the plate according to distinct edges, so that tubular sections of different basic profiles are formed.
  • the clamping means consist of at least one heel forming a support stop for the plate. This heel can extend over substantially the entire length of the edge. It is also possible to provide several heels distributed over the length of the folding edge and separated by spaces for receiving retaining heels used for folding the plate along another edge.
  • the clamping means have a variable position relative to the folding edge. This can come from the fact that the installation comprises means for adjusting or adapting the force exerted by the clamping means on the plate.
  • the folding member comprises at least one bearing surface against the plate and at least one cylindrical surface with a circular base capable of cooperating with a cylindrical surface with a circular base of a cradle, these cylindrical surfaces being centered on a virtual axis of folding the plate. The use of such a cradle makes it possible to guide the folding member without resorting to a hinge capable of interfering with neighboring devices. In this case, provision can be made for the installation to comprise several folding members distributed over the length of the plate and cooperating with cradles whose cylindrical surfaces have parallel geometric axes and offset with respect to each other. This makes it possible to fold the plate along distinct longitudinal edges, along its length, which makes it possible to conform tubular sections of different geometries corresponding, for example, to distinct sides of a frame to be produced. The folding member (s) are advantageously equipped with an external rib forming a cylindrical surface capable of cooperating with the cylindrical surface of the corresponding cradle, these cylindrical surfaces being of substantially the same radius. According to an advantageous embodiment of the invention allowing tilting of large amplitude, the folding member or members are guided relative to the cylindrical surface of the cradle by telescopic segments which slide one inside the other. The surfaces of the ribs, the telescopic segments and / or the surfaces of the cradles can be fitted with sliding balls or rollers.
  • the installation comprises a tool for shaping the part, this tool including elements for supporting tubular sections of the part provided with means for receiving and immobilizing these tubular parts, these elements being articulated with respect to each other. This tool allows the final shaping of the frame after completion of the tubular parts. It can be provided that at least one of the articulated elements is adjustable in length, which makes it possible to adapt the tool to the production of frames of different dimensions. It can also be provided that the articulated elements are capable of forming together a closed figure of predetermined geometry corresponding to the geometry of a frame formed by the manufactured part. The closed character of the figure obtained makes it possible to obtain increased geometrical precision thanks to an unequivocal positioning of the various constituent elements of this tool. According to an advantageous embodiment of the invention, at least one of the articulated elements is equipped with a member, with a generally U-shaped cross section and able to receive at least one blocking wedge for a tubular section in place in this element, means being provided for immobilizing the wedge on this member.
  • at least one of the folding members is equipped with a blade forming a shear for cutting the plate during its folding.

L'invention concerne enfin l'utilisation du procédé ou de l'installation mentionnés ci-dessus pour la fabrication d'un cadre support de masque d'ombre pour tube cathodique.The invention finally relates to the use of the process or of the installation mentioned above for manufacturing a shadow mask support frame for cathode ray tube.

L'invention sera mieux comprise et d'autres avantages de celle-ci apparaítront plus clairement à la lumière de la description qui va suivre de deux modes de réalisation d'une installation de fabrication d'un cadre support de masque d'ombre et de son procédé de mise en oeuvre, donnée uniquement à titre d'exemple et faite en référence aux dessins annexés dans lesquels :

  • la figure 1 représente de façon schématique un cadre de masque d'ombre sur lequel est disposé un masque d'ombre partiellement représenté ;
  • la figure 2 est une représentation schématique de principe en perspective d'une partie d'une installation de fabrication du cadre de la figure 1, le cadre n'étant pas représenté ;
  • la figure 3 est une représentation schématique de principe d'une partie du cadre de la figure 1 lorsqu'il est en place dans l'installation de la figure 2 ;
  • la figure 4 est une coupe de principe selon la ligne IV-IV à la figure 2, le cadre étant représenté en place dans l'installation ;
  • la figure 5 est une coupe analogue à la figure 4 lors d'une première étape du procédé de l'invention, antérieure à la configuration de la figure 4 ;
  • la figure 6 est une coupe analogue à la figure 4 lors d'une étape ultérieure du procédé de l'invention, postérieure à la configuration de la figure 4 ;
  • la figure 7 est une coupe analogue à la figure 4 lors d'une seconde étape ultérieure du procédé de l'invention ;
  • la figure 8 est une coupe de principe selon la ligne VIII-VIII à la figure 2, le cadre étant représenté en place dans l'installation ;
  • la figure 9 est une coupe analogue à la figure 8 lors d'une étape ultérieure du procédé de l'invention ;
  • la figure 10 est une coupe analogue à la figure 8 lors d'une seconde étape ultérieure du procédé de l'invention ;
  • la figure 11 est une vue en perspective d'une autre partie de l'installation de l'invention, un cadre en cours de fabrication étant représenté au-dessus de cette partie de l'installation ;
  • la figure 12 est une vue à plus grande échelle du détail XII à la figure 11, le cadre étant en place sur l'outillage ;
  • la figure 13 est une vue analogue à la figure 12 lors d'une étape ultérieure de fabrication du cadre ;
  • la figure 14 est une vue de dessus de la partie de l'installation représentée aux figures 11 à 13, en cours d'utilisation ;
  • la figure 15 est une représentation schématique partielle en coupe d'une partie d'une plaque en cours de pliage ;
  • la figure 16 est une représentation schématique de principe, en perspective, d'une partie de l'installation ;
  • la figure 17 est une coupe schématique d'une partie d'une installation conforme à un second mode de réalisation de l'invention ;
  • la figure 18 est une vue analogue à la figure 13 pour l'installation de la figure 17 et
  • la figure 19 est une coupe de principe selon la ligne XIX-XIX à la figure 18.
The invention will be better understood and other advantages thereof will appear more clearly in the light of the following description of two embodiments of an installation for manufacturing a support frame for shadow mask and its method of implementation, given solely by way of example and made with reference to the appended drawings in which:
  • Figure 1 schematically shows a shadow mask frame on which is disposed a partially shown shadow mask;
  • FIG. 2 is a schematic representation in principle in perspective of a part of an installation for manufacturing the frame of FIG. 1, the frame not being shown;
  • Figure 3 is a schematic representation of a part of the frame of Figure 1 when in place in the installation of Figure 2;
  • Figure 4 is a principle section along the line IV-IV in Figure 2, the frame being shown in place in the installation;
  • Figure 5 is a section similar to Figure 4 during a first step of the method of the invention, prior to the configuration of Figure 4;
  • Figure 6 is a section similar to Figure 4 during a subsequent step of the method of the invention, after the configuration of Figure 4;
  • Figure 7 is a section similar to Figure 4 during a second subsequent step of the method of the invention;
  • Figure 8 is a section in principle along the line VIII-VIII in Figure 2, the frame being shown in place in the installation;
  • Figure 9 is a section similar to Figure 8 during a subsequent step of the method of the invention;
  • Figure 10 is a section similar to Figure 8 during a second subsequent step of the method of the invention;
  • FIG. 11 is a perspective view of another part of the installation of the invention, a frame during manufacture being shown above this part of the installation;
  • Figure 12 is an enlarged view of detail XII in Figure 11, the frame being in place on the tooling;
  • Figure 13 is a view similar to Figure 12 during a subsequent step of manufacturing the frame;
  • Figure 14 is a top view of the part of the installation shown in Figures 11 to 13, in use;
  • Figure 15 is a partial schematic representation in section of a portion of a plate being folded;
  • Figure 16 is a schematic representation in principle, in perspective, of part of the installation;
  • Figure 17 is a schematic sectional view of part of an installation according to a second embodiment of the invention;
  • Figure 18 is a view similar to Figure 13 for the installation of Figure 17 and
  • FIG. 19 is a principle section along the line XIX-XIX in FIG. 18.

A la figure 1, on a représenté de façon schématique un masque d'ombre 1 monté sur un cadre 2 support de masque d'ombre. Le cadre 2 a une forme généralement rectangulaire et comporte deux montants latéraux 3, 3' et deux montants d'extrémités 4, 4'. Le masque d'ombre est constitué d'une feuille métallique mince, par exemple en alliage fer-nickel à faible coefficient de dilatation, percée de trous 5 et fixée par soudage sur des bords supérieurs 6, 6' des montants d'extrémité 4, 4'. Différentes formes de masque d'ombre sont possibles en fonction du tube cathodique auquel il doit être associé. Dans l'exemple représenté, le masque d'ombre est globalement plan, mais il peut également être cintré en portion de cylindre. Le masque 1 peut être en outre tendu, c'est-à-dire soumis à une tension parallèlement aux montants latéraux 3, 3' du cadre 2.In Figure 1, there is shown schematically a shadow mask 1 mounted on a frame 2 mask support shade. Frame 2 has a generally rectangular shape and has two lateral uprights 3, 3 'and two uprights 4, 4 'ends. The shadow mask consists of a thin metal foil, e.g. iron-nickel alloy low expansion coefficient, drilled with 5 holes and fixed by welding on upper edges 6, 6 'of the uprights end 4, 4 '. Different forms of shadow mask are possible depending on the cathode ray tube to which it must be associated. In the example shown, the shadow mask is generally planar, but it can also be bent in portion of cylinder. The mask 1 can also be stretched, i.e. subject to tension parallel to the uprights side 3, 3 'of frame 2.

Les montants 3, 3', 4 et 4' sont formés par pliage d'une tôle de façon à constituer chacun un élément tubulaire. Ces quatre montants peuvent être obtenus par pliage d'une unique plaque métallique. Il est également possible de prévoir d'utiliser une plaque pliée pour chaque montant ou une plaque pour deux montants contigus.The uprights 3, 3 ', 4 and 4' are formed by folding a sheet metal so as to each constitute a tubular element. These four uprights can be obtained by folding a single metal plate. It is also possible to plan to use a folded plate for each upright or a plate for two contiguous amounts.

Dans l'exemple illustré sur les figures, une unique plaque métallique 10 est utilisée pour la réalisation des quatre montants tubulaires 3, 3', 4 et 4'. Cette plaque apparaít partiellement à la figure 3 après des étapes de découpage de languettes d'assemblage 11 et de pré-marquage d'arêtes longitudinales 12 à 17. In the example illustrated in the figures, a single metal plate 10 is used for the realization of four tubular uprights 3, 3 ', 4 and 4'. This plate appears partially in Figure 3 after steps of cutting of assembly tabs 11 and of pre-marking longitudinal edges 12 to 17.

Au niveau des arêtes 12 à 14, la plaque 10 forme le montant d'extrémité 4. Au niveau des arêtes 12 et 15 à 17, la plaque 10 forme le montant latéral 3. En pratique, la partie de la plaque 10 représentée à la figure 3 correspond au coin 7 du cadre 2 au niveau duquel est réalisée la jonction entre les montants 3 et 4.At the edges 12 to 14, the plate 10 forms the end upright 4. At the edges 12 and 15 to 17, the plate 10 forms the lateral upright 3. In practice, the part of the plate 10 shown in Figure 3 corresponds to the corner 7 of frame 2 at the level of which the junction between amounts 3 and 4.

La plaque 10 est conformée dans la configuration de la figure 3 par des opérations de découpage, d'emboutissage et de pliage utilisant, notamment, des poinçons destinés à créer dans la plaque 10 une arête 12 s'étendant sur sensiblement toute sa longueur alors que les arêtes 13 à 17 s'étendent sur une partie seulement de la plaque 10, les arêtes 13 et 15 étant parallèles l'une à l'autre mais décalées, c'est-à-dire distantes de l'arête 12 de distances d1 et d2 différentes.The plate 10 is shaped in the configuration of FIG. 3 by cutting, stamping and folding operations using, in particular, punches intended to create in the plate 10 an edge 12 extending over substantially its entire length while the edges 13 to 17 extend over only part of the plate 10, the edges 13 and 15 being parallel to each other but offset, that is to say distant from the edge 12 by distances d 1 and d 2 different.

Comme il ressort plus particulièrement de la figure 5, le pré-pliage de la plaque 10 est effectué en immobilisant cette plaque sur un tablier ou contre-lame 101 grâce à un serre-flan 107 et en pliant la plaque 10 comme représenté par les flèches F, ce qui a pour effet de créer les lignes de pliage 12 et 13. Un autre serre-flan est utilisé au niveau du montant 3, ce qui permet de poursuivre la création de la ligne de pliage 12 et de créer la ligne de pliage 15. Ce second serre-flan est également configuré pour permettre la création des lignes de pliage 16 et 17.As can be seen more particularly from FIG. 5, the pre-folding of the plate 10 is carried out by immobilizing this plate on an apron or counter blade 101 thanks to a blank holder 107 and by folding the plate 10 as shown by the arrows F, which has the effect of creating the lines of folding 12 and 13. Another blank holder is used at the amount 3, which allows to continue the creation of the line of fold 12 and create the fold line 15. This second hold-down is also configured to allow creation fold lines 16 and 17.

Ces opérations de pré-pliage permettent d'atteindre la configuration de la figure 4 dans laquelle le serre-flan 107 est rétracté ou retiré de l'espace intérieur de la plaque 10 comme représenté par la flèche F'. On note que la forme du serre-flan 107 est compatible avec son retrait de l'intérieur de la plaque 10 dans la configuration de la figure 4.These pre-folding operations achieve the configuration of Figure 4 in which the blank holder 107 is retracted or removed from the interior of the plate 10 as represented by the arrow F '. We note that the shape of the hold-down 107 is compatible with its removal from the inside of plate 10 in the configuration of FIG. 4.

Grâce à cette opération de pré-pliage, la plaque 10 est immobilisée par rapport à l'installation de l'invention car elle est en butée le long des deux arêtes de pliage 12 et 13 ou 12 et 15 qui sont globalement parallèles.Thanks to this pre-folding operation, the plate 10 is immobilized in relation to the installation of the invention because it is in abutment along the two folding edges 12 and 13 or 12 and 15 which are generally parallel.

Le pré-pliage peut être préparé par un marquage des lignes de pliage, par exemple par un poinçonnage sur une partie de l'épaisseur de la plaque 10, notamment 25%.Pre-folding can be prepared by marking the fold lines, for example by punching on a part of the thickness of the plate 10, in particular 25%.

De façon générale, le pré-pliage de la plaque 10 peut être effectué sur la machine représentée sur les figures ou sur une autre machine, sans sortir du cadre de la présente invention.Generally, the pre-folding of the plate 10 can be performed on the machine shown in the figures or on another machine, without going beyond the scope of this invention.

Dans le cas où l'on réalise un montant de section à plus de trois côtés, comme le montant 3, des pré-pliages préliminaires sont nécessaires pour réaliser les arêtes du types des arêtes 16 et 17. Un tel pré-pliage préliminaire est également utilisé dans le cas du montant 4 pour la réalisation de l'arête 14.In the case where a section amount of more is achieved on three sides, like the upright 3, preliminary pre-folding are necessary to make the edges of the type of edges 16 and 17. Such preliminary pre-folding is also used in the case of the amount 4 for the realization of the edge 14.

L'installation de l'invention 100 comprend le tablier 101 sur lequel est posée une partie centrale 21 de la plaque 10. Des pions, dont un seul est visible sur les figures avec la référence 102, s'étendent à partir de cette plaque 101 et sont destinés à traverser des ouvertures 22 prévues dans la partie 21, de façon à positionner la plaque 10 sur la plaque de base 101.The installation of the invention 100 includes the apron 101 on which a central part 21 of the plate 10 is placed. Pawns, only one of which is visible in the figures with the reference 102, extend from this plate 101 and are intended to pass through openings 22 provided in the part 21, so as to position the plate 10 on the base plate 101.

A partir de la partie 21 s'étendent deux ailes 23 et 24 de la plaque 10 destinées à former le montant 4. A partir de cette même partie centrale 21 s'étendent deux autres ailes 25 et 26 destinées à former le montant 3.From part 21 extend two wings 23 and 24 of the plate 10 intended to form the upright 4. From this same central part 21 extend two other wings 25 and 26 intended to form the amount 3.

Les ailes 23 et 25 sont reliées à la partie 21 le long de l'arête 12. Les ailes 24 et 26 sont respectivement reliées à la partie 21 le long des arêtes 13 et 15. L'aile 23 est reliée à une bordure 27 par la ligne de pliage ou arête 14 alors que les ailes 25 et 26 sont toutes deux divisées en deux panneaux 25a, 25b respectivement 26a, 26b par les lignes de pliage ou arêtes 16 et 17.The wings 23 and 25 are connected to the part 21 along the edge 12. The wings 24 and 26 are respectively connected to the part 21 along the edges 13 and 15. The wing 23 is connected to an edge 27 by the fold line or edge 14 while the wings 25 and 26 are both divided into two panels 25 a , 25 b respectively 26 a , 26 b by the fold lines or edges 16 and 17.

L'installation 100 comprend un mors de pliage 103 destiné à rabattre l'aile 23 en direction de la partie 21 grâce à un effort représenté par la flèche F1. Le mors 103 comprend une plaque 103a dont la longueur, parallèlement à un axe longitudinal X-X' de l'installation 100, est adapté à la longueur de l'aile 23. La face 103a1 de la plaque 103a destinée à être en contact avec l'aile 23 est globalement plane. La plaque 103a est équipée, sur sa face 103a2 opposée à la face 103a1, de deux nervures 103b, s'étendant à l'opposé de l'aile 23 selon des directions globalement perpendiculaires à l'axe X-X'. Ces nervures 103b forment chacune une surface convexe 103c en portion de cylindre à base circulaire centrée sur un axe virtuel a. On entend par "virtuel" le fait que l'axe a n'est pas défini par une charnière, mais comme étant le lieu géométrique joignant les centres de courbure des surfaces 103c. Cet axe est situé à l'intérieur du montant 4 et est parallèle à l'axe X-X'.The installation 100 comprises a folding jaw 103 intended to fold the wing 23 in the direction of the part 21 by means of a force represented by the arrow F 1 . The jaw 103 comprises a plate 103 a whose length, parallel to a longitudinal axis XX ′ of the installation 100, is adapted to the length of the wing 23. The face 103 a 1 of the plate 103 a is intended to be in contact with wing 23 is generally flat. The plate 103 a is equipped, on its face 103 a 2 opposite the face 103 a 1, with two ribs 103 b , extending opposite the wing 23 in directions generally perpendicular to the axis X- X '. These ribs 103 b each form a convex surface 103 c in a portion of a cylinder with a circular base centered on a virtual axis a. By "virtual" is meant the fact that the axis a is not defined by a hinge, but as being the geometrical location joining the centers of curvature of the surfaces 103 c . This axis is located inside the upright 4 and is parallel to the axis XX '.

L'installation 100 comprend également un berceau 113 définissant une surface interne 113c cylindrique et à base circulaire contre laquelle sont en appui glissant les nervures 103b par leurs surfaces 103c. L'axe de symétrie de la surface 113a est également l'axe a. Les rayons de courbure R103 et R113 des surfaces 103c et 113c sont égaux. Il est ainsi possible de faire pivoter le mors 103 dans le berceau 113 autour de l'axe a, comme représenté par la flèche F2 à la figure 4, par glissement relatif des surfaces 103c et 113c.The installation 100 also includes a cradle 113 defining an internal surface 113 c that is cylindrical and with a circular base against which the ribs 103 b slide by their surfaces 103 c . The axis of symmetry of the surface 113 a is also the axis a. The radii of curvature R 103 and R 113 of the surfaces 103 c and 113 c are equal. It is thus possible to rotate the jaw 103 in the cradle 113 around the axis a , as shown by the arrow F 2 in Figure 4, by relative sliding of the surfaces 103 c and 113 c .

Un second mors 104 comprend une plaque 104a destinée à venir en appui, par une face 104a1, contre l'aile 24 et à exercer sur celle-ci un effort F3 permettant de la rabattre en direction de la plaque de base 101 et de la partie centrale 21. La plaque 104a est pourvue, sur sa face 104a2 opposée à la face 104a1, de nervures 104b dont une surface externe ou convexe 104c est cylindrique à base circulaire et apte à venir en appui contre une surface cylindrique interne ou concave à base circulaire 114c d'un berceau 114. On note c l'axe géométrique central commun des surfaces 104c, cet axe étant parallèle à l'axe X-X' et situé dans le volume intérieur du montant 4. On note 114c et R104 et R114 les rayons respectifs des surfaces 104c et 114c ces rayons étant de même longueur. Le mors 104 peut pivoter autour de l'axe c en étant guidé par le berceau 114, comme représenté par la flèche F'2.A second jaw 104 comprises a plate 104 a intended to come to bear, by a face 104 a 1, against the wing 24 and to exert on it a force F 3 allowing it to be folded down in the direction of the base plate 101 and of the central part 21. The plate 104 a is provided, on its face 104 a 2 opposite the face 104 a 1, of ribs 104 b of which an external or convex surface 104 c is cylindrical with a circular base and capable of coming into bearing against an internal cylindrical or concave surface with a circular base 114 c of a cradle 114. We denote by c the common central geometric axis of the surfaces 104 c , this axis being parallel to the axis XX 'and located in the interior volume of the amount 4. We denote 114 c and R 104 and R 114 the respective radii of the surfaces 104 c and 114 c, these radii being of the same length. The jaw 104 can pivot around the axis c while being guided by the cradle 114, as shown by the arrow F ′ 2 .

En se reportant plus particulièrement aux figures 4, 6 et 7, on comprend qu'il est possible de conformer la plaque 10 en une section tubulaire à base globalement triangulaire grâce aux efforts F1 et F3.With particular reference to FIGS. 4, 6 and 7, it is understood that it is possible to conform the plate 10 into a tubular section with a generally triangular base thanks to the forces F 1 and F 3 .

Cependant, à partir de la position de la figure 4, si les efforts F1 et F3 sont exercés alors que les ailes 23 et 24 reposent respectivement contre les plaques 103a et 104a sans autre effort, la plaque 10 risque de se soulever dans le sens de la flèche F4 à la figure 4 car les ailes 23 et 24 risquent de glisser le long des surfaces 103a1 et 104a1, comme représenté respectivement par les flèches F5 et F6. Ceci pourrait résulter dans un pliage imprécis au niveau des arêtes 12 et 13 dont le centre de courbure ne serait alors plus confondu avec les axes géométriques a et c.However, from the position of FIG. 4, if the forces F 1 and F 3 are exerted while the wings 23 and 24 rest respectively against the plates 103 a and 104 a without any other force, the plate 10 risks being lifted in the direction of the arrow F 4 in FIG. 4 because the wings 23 and 24 risk sliding along the surfaces 103 a 1 and 104 a 1, as represented by the arrows F 5 and F 6 respectively . This could result in imprecise bending at the edges 12 and 13, the center of curvature of which would then no longer coincide with the geometric axes a and c .

Pour éviter des mouvements relatifs entre les ailes 23 et 24 et les surfaces 103a et 104a, les mors 103 et 104 sont chacun équipés d'un talon 103f, 104f apte à exercer sur les ailes 23 et 24 un effort, respectivement noté F7 et F8; dirigé globalement vers les arêtes 12 et 13, c'est-à-dire s'opposant à un glissement des ailes 23 et 24 dans le sens des flèches F5 et F6. Les efforts F7 et F8 constituent donc des efforts de bridage ou de retenue des ailes 23 et 24 par rapport aux mors 103 et 104. En particulier, les ailes 23 et 24 ne risquent pas de faire saillie radialement à l'extérieur des mors 103 et 104.To avoid relative movements between the wings 23 and 24 and the surfaces 103 a and 104 a , the jaws 103 and 104 are each fitted with a heel 103 f , 104 f capable of exerting an effort on the wings 23 and 24, respectively noted F 7 and F 8 ; directed generally towards the edges 12 and 13, that is to say opposing a sliding of the wings 23 and 24 in the direction of the arrows F 5 and F 6 . The forces F 7 and F 8 therefore constitute efforts for clamping or retaining the wings 23 and 24 relative to the jaws 103 and 104. In particular, the wings 23 and 24 are not likely to project radially outside the jaws 103 and 104.

En d'autres termes, les talons 103f et 104f forment des butées au déplacement des ailes 23 et 24 dans le sens des flèches F5 et F6.In other words, the heels 103 f and 104 f form stops for the displacement of the wings 23 and 24 in the direction of the arrows F 5 and F 6 .

On note que les efforts F7 et F8 sont exercés par l'extérieur du montant 4. Ainsi, la plaque 10 est maintenue sur le tablier 101 sans utilisation d'un élément rapporté, tel qu'un serre-flanc, ce qui est favorable car un serre-flanc serait délicat à mettre en place et à retirer une fois la plaque pliée. En outre, un serre-flanc ne pourrait pas se prolonger jusqu'au niveau du montant 3.It is noted that the forces F 7 and F 8 are exerted from the outside of the upright 4. Thus, the plate 10 is held on the deck 101 without the use of an insert, such as a sidewall clamp, which is favorable because a sidewall would be difficult to set up and remove once the plate folded. In addition, a sidewall could not extend to the level of the upright 3.

L'invention permet donc un pliage de la plaque 10 en une structure tubulaire sans introduction d'un dispositif de coincement à l'intérieur de ses différentes sections.The invention therefore allows folding of the plate 10 in one tubular structure without the introduction of a jamming inside its different sections.

Le talon 103f est monobloc avec la plaque 103a, ce talon étant destiné à coiffer la bordure 27 de l'aile 23. Ce talon 103f s'étend sur toute la longueur du mors 103 parallèlement à l'axe X-X', ce qui garantit que l'arête supérieure du montant 4, sur laquelle est destiné à être tendu le masque 1, est dépourvu d'irrégularités. A cet effet, le talon 103f présente une surface régulière du côté de la bordure 27 car le talon 103f sert au formage de cette bordure qui doit être aussi régulière que possible pour que le masque 1, qui est tendu sur l'arête supérieure du montant 4, ne présente pas de vague ou de relief susceptibles de perturber l'image générée dans le tube cathodique.The heel 103 f is in one piece with the plate 103 a , this heel being intended to cover the edge 27 of the wing 23. This heel 103 f extends over the entire length of the jaw 103 parallel to the axis XX ' , which guarantees that the upper edge of the upright 4, on which the mask 1 is intended to be stretched, is free from irregularities. For this purpose, the bead 103f has a smooth surface on the side of the edge 27 because the heel 103 f used for forming the edge which should be as regular as possible for the mask 1, which is stretched over the upper edge of upright 4, does not have a wave or relief capable of disturbing the image generated in the cathode ray tube.

Le talon 104f, qui s'étend sur toute la longueur du mors 104, est susceptible de se déplacer perpendiculairement à la plaque 104a et à l'aile 24, comme représenté par la flèche F9 à la figure 4.The heel 104 f , which extends over the entire length of the jaw 104, is capable of moving perpendicular to the plate 104 a and to the wing 24, as shown by the arrow F 9 in FIG. 4.

Le fonctionnement est le suivant :The operation is as follows:

Lorsque la plaque 10 a été positionnée sur le tablier 101 et pré-pliée grâce au serre-flan 107, le mors 104 est déplacé par un vérin pneumatique électrique ou hydraulique, de telle sorte qu'il rabat, grâce à l'effort F3 exercé par la plaque 104a, la plaque 24 en direction de la partie 21. Le talon 104f exerce sur l'aile 24 un effort F8 dirigé vers l'arête 12, ce qui garantit un bon positionnement de l'aile 24 par rapport au mors 104. On atteint alors la position de la figure 6 où l'angle α entre l'aile 24 et la partie 21 est inférieur à 90°. A partir de cette position, le mors 103 est actionné de telle sorte qu'il rabat l'aile 23 en direction de la partie 21 en exerçant l'effort F1, comme représenté à la figure 7. Les mors 103 et 104 sont guidés dans leurs déplacements F2 et F'2 grâce à la coopération des surfaces cylindriques convexes 103c, 104c et concaves 113c, 114c.When the plate 10 has been positioned on the deck 101 and pre-folded using the blank holder 107, the jaw 104 is moved by an electric or hydraulic pneumatic jack, so that it folds down, thanks to the force F 3 exerted by the plate 104 a , the plate 24 in the direction of the part 21. The heel 104 f exerts on the wing 24 a force F 8 directed towards the edge 12, which guarantees a good positioning of the wing 24 by relative to the jaw 104. We then reach the position of Figure 6 where the angle α between the wing 24 and the part 21 is less than 90 °. From this position, the jaw 103 is actuated so that it flaps the wing 23 in the direction of the part 21 by exerting the force F 1 , as shown in FIG. 7. The jaws 103 and 104 are guided in their displacements F 2 and F ' 2 thanks to the cooperation of the convex cylindrical surfaces 103 c , 104 c and concave 113 c , 114 c .

Pour éviter une interférence entre les talons 103f et 104f, le talon 104f est éloigné de l'aile 24, comme représenté par la flèche F'9 à la figure 7. En effet, il est possible de supprimer l'effort F8 dans la configuration de la figure 6 car aucun déplacement de l'aile 24 n'est nécessaire entre les configurations des figures 6 et 7. De plus, le fait que l'angle α est inférieur à 90° assure un positionnement efficace de l'aile 24, y compris en cas de suppression de l'effort F8.To avoid interference between the heels 103 f and 104 f , the heel 104 f is distant from the wing 24, as shown by the arrow F ′ 9 in FIG. 7. In fact, it is possible to remove the force F 8 in the configuration of FIG. 6 because no movement of the wing 24 is necessary between the configurations of FIGS. 6 and 7. In addition, the fact that the angle α is less than 90 ° ensures effective positioning of the 'wing 24, including in the case of removal of the force F 8 .

En d'autres termes, dans les configurations des figures 6 et 7, l'effort F8 n'est pas indispensable car la plaque 104a maintient efficacement l'aile 24 en position par rapport à l'axe c. In other words, in the configurations of Figures 6 and 7, the force F 8 is not essential because the plate 104 effectively maintains the flange 24 in position relative to the c axis.

Selon une variante de réalisation de l'invention, on peut prévoir que plusieurs talons 104f sont répartis sur la longueur de la plaque 104a, parallèlement aux axes X-X' et c.According to an alternative embodiment of the invention, it can be provided that several heels 104 f are distributed over the length of the plate 104 a , parallel to the axes XX 'and c .

On se reporte maintenant à la figure 15 qui est un agrandissement du détail XV à la figure 4. La plaque 10 a une épaisseur e non nulle. Le passage de la position représentée en traits pleins à la position représentée en traits mixtes, qui correspond sensiblement à celle de la figure 7, a pour effet de diminuer la hauteur h de l'aile 23 dans la configuration en traits mixtes par rapport à la longueur l de cette aile dans la configuration en traits pleins car la fibre neutre f de la plaque 10 forme un arc de cercle centré sur l'axe a dans la configuration représentée en traits mixtes. Si l'on considère que l'axe a est situé à l'intérieur de la zone destinée à former l'arête 12 avec une distance d par rapport à la fibre neutre f et en prenant l'exemple d'une plaque cintrée à partir d'une configuration plane pour arriver à une configuration pliée à 90°, la différence entre la hauteur h et la longueur l est de 1/2 πd. Dans le cas d'espèce, elle est moindre dans la mesure où l'arête 12 est déjà pré-marquée dans la configuration de la figure 4. Elle est cependant non nulle.Referring now to Figure 15 which is an enlargement of detail XV in Figure 4. The plate 10 has a thickness e not zero. The transition from the position shown in solid lines to the position shown in dashed lines, which corresponds substantially to that of FIG. 7, has the effect of reducing the height h of the wing 23 in the configuration in dashed lines relative to the length l of this wing in the configuration in solid lines because the neutral fiber f of the plate 10 forms an arc of circle centered on the axis a in the configuration shown in broken lines. If we consider that the axis a is located inside the area intended to form the edge 12 with a distance d from the neutral fiber f and taking the example of a plate bent from from a flat configuration to arrive at a configuration folded at 90 °, the difference between the height h and the length l is 1/2 πd. In the present case, it is less insofar as the edge 12 is already pre-marked in the configuration of FIG. 4. It is however not zero.

Compte tenu de cette différence de valeurs entre la hauteur h et la longueur l, il convient d'adapter la valeur de l'effort F7 pour que celui-ci immobilise efficacement la plaque 10 dans la zone de l'arête 12 tout au long du mouvement de rotation du mors 103 autour de l'axe a. Pour ce faire, on prévoit que le talon 103f est chargé élastiquement en direction de l'axe a ou de l'arête 12. Dans ce cas, le talon 103f n'est pas monobloc avec la plaque 103a. Selon une autre approche, on peut prévoir qu'un système de cames permet de faire varier l'intensité de l'effort F7 en fonction de l'orientation angulaire du mors 103 autour de l'axe a, au cours du pivotement F2.In view of this difference in values between the height h and the length l , the value of the force F 7 should be adapted so that it effectively immobilizes the plate 10 in the region of the edge 12 throughout the rotational movement of the jaw 103 around the axis a. To do this, provision is made for the heel 103 f to be loaded elastically in the direction of the axis a or the edge 12. In this case, the heel 103 f is not in one piece with the plate 103 a . According to another approach, it is possible to provide that a system of cams makes it possible to vary the intensity of the force F 7 as a function of the angular orientation of the jaw 103 around the axis a, during the pivoting F 2 .

Selon une autre approche, il est possible de compenser cette différence de valeur entre la hauteur h et la longueur l en décalant l'axe de pivotement a selon une direction perpendiculaire au plan principal du tablier 101. Dans ce cas, le talon 103f peut être monobloc avec la plaque 103a du mors 103.According to another approach, it is possible to compensate for this difference in value between the height h and the length l by shifting the pivot axis a in a direction perpendicular to the main plane of the deck 101. In this case, the heel 103 f can be in one piece with plate 103 has jaw 103.

Bien entendu, le talon 104f peut également être pourvu de moyens permettant de faire varier l'intensité de l'effort F8 en fonction de la position de mors 104 autour de l'axe c au cours du pivotement F'2. En variante, la position de l'axe c peut également être prévue variable pour compenser les variations de longueur et/ou hauteur de l'aile 24.Of course, the heel 104 f can also be provided with means making it possible to vary the intensity of the force F 8 as a function of the jaw position 104 around the axis c during the pivoting F ′ 2 . As a variant, the position of the axis c can also be provided for variable to compensate for the variations in length and / or height of the wing 24.

En se reportant plus particulièrement aux figures 8 à 10, on note que le montant latéral 3 est à section quadrangulaire. Un mors 105 est prévu pour coopérer avec l'aile 25 et comprend une plaque de base 105a dont une face 105a1 en contact avec l'aile 25 permet d'exercer un effort F11 pour rabattre l'aile 25 en direction des éléments 21 et 101. Comme le mors 103, le mors 105 est équipé de nervures 105b définissant des surfaces convexes cylindriques 105c centrées sur l'axe a et permettant de coopérer avec un berceau 115 définissant une surface concave 115c de glissement des surfaces 105c, la surface 115c étant, tout comme les surfaces 105c, à base circulaire et centrée sur l'axe a. Le mors 105 est équipé de plusieurs talons 105f répartis sur sa longueur parallèlement à l'axe X-X', ces talons étant prévus pour venir au contact de l'aile 25 au niveau de l'arête 17 en constituant une butée à un éventuel glissement de l'aile 25. Les talons 105f exercent sur l'aile 25 un effort de bridage F12 dirigé vers l'arête 12 et parallèle au panneau 25a. L'effort F12 a la même fonction que les efforts F7 et F8 précédemment évoqués. Il permet de positionner efficacement l'aile 25 par rapport à l'axe a tout au long de l'opération de pliage réalisée grâce à l'effort F11.Referring more particularly to Figures 8 to 10, it is noted that the lateral upright 3 is of quadrangular section. A jaw 105 is provided to cooperate with the wing 25 and comprises a base plate 105 a , one face 105 a 1 in contact with the wing 25 allows exerting a force F 11 to fold the wing 25 towards the elements 21 and 101. Like the jaw 103, the jaw 105 is equipped with ribs 105 b defining convex cylindrical surfaces 105 c centered on the axis a and making it possible to cooperate with a cradle 115 defining a concave surface 115 c for sliding the surfaces 105 c , the surface 115 c being, like the surfaces 105 c , with a circular base and centered on the axis a. The jaw 105 is equipped with several heels 105 f distributed over its length parallel to the axis XX ′, these heels being designed to come into contact with the wing 25 at the edge 17 by constituting a stop at a possible sliding of the wing 25. The heels 105 f exert on the wing 25 a clamping force F 12 directed towards the edge 12 and parallel to the panel 25 a . The force F 12 has the same function as the forces F 7 and F 8 previously mentioned. It makes it possible to effectively position the wing 25 relative to the axis a throughout the folding operation carried out thanks to the force F 11 .

De la même façon, un mors 106 est prévu pour coopérer avec l'aile 26 et comprend une plaque 106a formant une face 106a1 d'appui contre l'aile 26 et équipée de nervures 106b dont les surfaces radiales externes convexes 106c coopèrent avec une surface concave 116c d'un berceau 116. Les surfaces 106c et 116c sont centrées sur un axe géométrique ou axe virtuel b constituant le centre de l'arête 15 et situé, comme l'axe a, dans le volume intérieur du montant 3.In the same way, a jaw 106 is provided to cooperate with the wing 26 and comprises a plate 106a forming a face 106 a 1 bearing against the wing 26 and equipped with ribs 106 b whose convex external radial surfaces 106 c cooperate with a concave surface 116 c of a cradle 116. The surfaces 106 c and 116 c are centered on a geometric axis or virtual axis b constituting the center of the edge 15 and located, like the axis a, in the volume inside the upright 3.

Le mors 106 est équipé des talons 106f permettant de retenir l'aile 26 en position par rapport à la plaque 106a au cours du pliage de l'arête 15. La plaque 106a n'est pas plane mais forme une zone concave de réception des panneaux 26a et 26b, la plaque 106a étant elle-même formée de deux panneaux orientés l'un par rapport à l'autre avec un angle β correspondant à l'angle d'orientation des panneaux 26a et 26b l'un par rapport à l'autre. Les talons 106f sont disposés pour venir en appui contre le bord libre 26c du panneau 26b.The jaw 106 is equipped with heels 106 f making it possible to retain the wing 26 in position relative to the plate 106 a during the folding of the edge 15. The plate 106 a is not flat but forms a concave zone of receiving the panels 26 a and 26 b , the plate 106 a being itself formed by two panels oriented relative to each other with an angle β corresponding to the angle of orientation of the panels 26 a and 26 b relative to each other. The heels 106 f are arranged to bear against the free edge 26 c of the panel 26 b .

Les talons 106f sont répartis sur la longueur de la plaque 106a.The heels 106 f are distributed over the length of the plate 106 a .

Les talons 105f d'une part et 106f d'autre part sont positionnés en quinconce les uns par rapport aux autres en étant décalés le long de l'axe X-X', un talon 105f étant en regard d'un intervalle libre 106g défini entre deux talons 106f, alors qu'un talon 106f est disposé en regard d'un intervalle libre 105g défini entre deux talons 105f.The heels 105 f on the one hand and 106 f on the other hand are staggered relative to each other by being offset along the axis XX ', a heel 105 f being opposite an interval free 106 g defined between two heels 106 f , while a heel 106 f is placed opposite a free interval 105 g defined between two heels 105 f .

Le pliage du montant 3 peut être expliqué en référence aux figures 8 à 10. Dans la configuration de la figure 8, un effort est exercé sur le mors 105 par tout moyen approprié, de telle sorte qu'il est déplacé et exerce l'effort de pliage F11 de l'aile 25 en direction de la partie 21, les talons 105f venant en recouvrement de la zone de jonction 25c, définie entre les panneaux 25a et 25b et qui inclut l'arête 17. L'effort F11 permet de rabattre l'aile 25 jusque dans la position de la figure 9 où le panneau 25a est globalement perpendiculaire à la partie 21, le panneau 25b étant globalement parallèle à cette partie. Au cours de l'opération de pliage réalisé entre les configurations des figures 8 et 9, l'effort F12 retient efficacement l'aile 25 en position par rapport au mors 105 et à l'arête 12.The folding of the upright 3 can be explained with reference to Figures 8 to 10. In the configuration of Figure 8, a force is exerted on the jaw 105 by any suitable means, so that it is moved and exerts the force folding F 11 of the wing 25 in the direction of the part 21, the heels 105 f overlapping the junction zone 25 c , defined between the panels 25 a and 25 b and which includes the edge 17. The force F 11 allows the wing 25 to be folded down into the position of FIG. 9 where the panel 25 a is generally perpendicular to the part 21, the panel 25 b being generally parallel to this part. During the folding operation carried out between the configurations of FIGS. 8 and 9, the force F 12 effectively retains the wing 25 in position relative to the jaw 105 and to the edge 12.

Le mors 106 est alors activé, pour passer de la position de la figure 9 à celle de la figure 10, un effort F13 de pliage de l'aile 26 en direction de la partie 21 étant exercé par la plaque 106a alors qu'un effort F14 est exercé par les talons 106f sur l'aile 26 parallèlement à cette aile et globalement en direction de l'arête 15.The jaw 106 is then activated, to pass from the position of FIG. 9 to that of FIG. 10, a force F 13 in bending the wing 26 in the direction of the part 21 being exerted by the plate 106 a while a force F 14 is exerted by the heels 106 f on the wing 26 parallel to this wing and generally in the direction of the edge 15.

Comme précédemment, les efforts F12 et F14 peuvent être modulés en fonction de l'orientation des mors 105 et 106 autour des axes a et b. En variante, les axes a et b peuvent être décalés par rapport à leur représentation sur les figures 8 à 10 afin de compenser les variations de longueur des ailes 25 et 26.As before, the forces F 12 and F 14 can be modulated as a function of the orientation of the jaws 105 and 106 around the axes a and b. As a variant, the axes a and b can be offset from their representation in FIGS. 8 to 10 in order to compensate for the variations in length of the wings 25 and 26.

En outre, dans la configuration de la figure 10, l'effort F12 peut être relâché ou diminué par un mouvement du talon 105f dans un sens d'éloignement par rapport à l'arête 12, de telle sorte que, du fait de l'élasticité de la plaque 10, le panneau 25b vient en appui élastique ferme contre la face du panneau 26b orientée vers la partie 21. Il est alors possible de souder point par point les panneaux 25b et 26b grâce à un faisceau à haute énergie dirigé entre deux talons 105f et 106f adjacents.In addition, in the configuration of FIG. 10, the force F 12 can be relaxed or reduced by a movement of the heel 105 f in a direction away from the edge 12, so that, due to the elasticity of the plate 10, the panel 25 b comes into firm elastic abutment against the face of the panel 26 b oriented towards the part 21. It is then possible to weld the panels 25 b and 26 b point by point using a beam high energy directed between two heels 105 f and 106 f adjacent.

Pour atteindre l'appui élastique des panneaux 25d et 26d, il est également possible de prévoir que l'angle de pliage entre les panneaux 25a et 25b est légèrement plus ouvert que celui obtenu dans la configuration de la figure 10, de telle sorte qu'un appui élastique est obtenu dans cette configuration sans qu'il soit nécessaire de relâcher l'effort F12.To achieve the elastic support of the panels 25 d and 26 d , it is also possible to provide that the folding angle between the panels 25 a and 25 b is slightly more open than that obtained in the configuration of FIG. 10, so that an elastic support is obtained in this configuration without it being necessary to release the force F 12 .

Comme il ressort plus clairement des figures 11 à 14, le cadre 2 est conformé, après mise en forme des différents montants 3, 3', 4 et 4', par pliage. Lorsque les montants tubulaires ont été réalisés, la plaque 10 s'étend globalement selon la direction X-X' en quatre sections reliées par des zones de jonction 8, 8' et 8''. Un outillage 200 est prévu pour la mise en forme du cadre 2 et comprend quatre volets 201, 202, 203 et 204 destinés à recevoir chacun l'un des montants 3, 3', 4 ou 4'.As shown more clearly in Figures 11 to 14, the frame 2 is shaped, after shaping the different uprights 3, 3 ', 4 and 4', by folding. When the amounts tubes have been produced, the plate 10 extends overall in the direction X-X 'in four sections connected by 8, 8 'and 8' 'junction zones. A tool 200 is provided for the shaping of frame 2 and includes four parts 201, 202, 203 and 204 each intended to receive one of the amounts 3, 3 ', 4 or 4'.

Ces volets 201 à 204 sont chacun formés de deux pièces massiques 201a, 201b, 202a, 202b, 203a, 203b, 204a, 204b reliées par un système vis-écrou 201c, 202c, 203c ou 204c d'ajustement en longueur des volets 201 à 204. Des tiges de guidage 201c', 202c', 203c' et 204c' sont associées aux systèmes 201c à 204c. La longueur de chaque volet 201 à 204 est réglée, parallèlement à sa plus grande dimension X1 à X4, à la longueur du montant qu'il doit recevoir. Les volets 201 à 204 sont prévus ajustables en longueur afin de permettre la fabrication de cadres 2 de tailles différentes. These flaps 201 to 204 are each formed of two mass pieces 201 a , 201 b , 202 a , 202 b , 203 a , 203 b , 204 a , 204 b connected by a screw-nut system 201 c , 202 c , 203 c or 204 c for adjusting the length of the flaps 201 to 204. Guide rods 201 c ', 202 c ', 203 c 'and 204 c ' are associated with systems 201 c to 204 c . The length of each flap 201 to 204 is adjusted, parallel to its largest dimension X 1 to X 4 , to the length of the amount that it must receive. The flaps 201 to 204 are provided adjustable in length to allow the manufacture of frames 2 of different sizes.

Les pièces 201a et 201b sont respectivement pourvues de cornières 201d, 201e de réception du montant 4. Des mâchoires 201f, 201g sont prévues pour immobiliser le montant 4 contre les cornières 201d et 201e. De la même façon, les volets 202, 203 et 204 sont respectivement équipés de cornières 202d à 204e et de mâchoires 202f à 204g. Comme il ressort plus particulièrement des figures 11 et 12, les mâchoires sont conformées en fonction de la géométrie des ailes 24 et 26.The parts 201 a and 201 b are respectively provided with angles 201 d , 201 e for receiving the amount 4. Jaws 201 f , 201 g are provided for immobilizing the amount 4 against the angles 201 d and 201 e . Likewise, the flaps 202, 203 and 204 are respectively equipped with angles 202 d to 204 e and jaws 202 f to 204 g . As appears more particularly from FIGS. 11 and 12, the jaws are shaped as a function of the geometry of the wings 24 and 26.

Les volets 201 et 202 sont articulés ensemble autour d'un axe Y1 essentiellement perpendiculaire à la direction principale X-X' des montants 3, 4, 3' et 4'. L'axe Y1 est également perpendiculaire à la direction X1 selon laquelle le volet 201 est réglable en longueur. De la même façon, les volets 202 et 203 sont articulés ensemble autour d'un axe Y2 alors que les volets 203 et 204 sont articulés ensemble autour d'un axe Y3, ces axes Y2 et Y3 étant globalement perpendiculaires à l'axe X-X' et aux directions X1, X2, X3 et X4 de réglage en longueur des différents volets.The flaps 201 and 202 are articulated together around an axis Y 1 essentially perpendicular to the main direction XX 'of the uprights 3, 4, 3' and 4 '. The axis Y 1 is also perpendicular to the direction X 1 in which the flap 201 is adjustable in length. Similarly, the flaps 202 and 203 are articulated together around an axis Y 2 while the flaps 203 and 204 are articulated together around an axis Y 3 , these axes Y 2 and Y 3 being generally perpendicular to the 'axis XX' and to the directions X 1 , X 2 , X 3 and X 4 for adjusting the length of the different flaps.

Trois vérins 205, 206 et 207 relient respectivement les volets 201 et 202, les volets 202 et 203 et les volets 203 et 204, de telle sorte qu'ils sont aptes à exercer sur ceux-ci des efforts de fermeture représentés par les flèches F16, F17 et F18 à la figure 14. Ces efforts permettent d'amener l'outillage 200 dans une configuration globalement rectangulaire dans un plan perpendiculaire aux axes Y1 à Y3, ce qui permet de plier le cadre 2 au niveau des zones 8, 8' et 8'' et de former des coins tels que le coin 7, comme représenté aux figures 12 et 13. En effet, l'effort F17 a pour effet de rapprocher les côtés des volets 202 et 203 reliés par le vérin 206, ce qui résulte dans un pliage de la plaque 10 le long d'une ligne 18 parallèle à l'axe Y2. On amène ainsi en recouvrement les languettes 11 ménagées sur le montant 4 avec le bord 3a du montant 3, ces languettes et ce bord pouvant alors être soudés par un faisceau à haute énergie.Three cylinders 205, 206 and 207 respectively connect the flaps 201 and 202, the flaps 202 and 203 and the flaps 203 and 204, so that they are capable of exerting on them closing forces represented by the arrows F 16 , F 17 and F 18 in FIG. 14. These efforts make it possible to bring the tool 200 into a generally rectangular configuration in a plane perpendicular to the axes Y 1 to Y 3 , which makes it possible to fold the frame 2 at the level of the zones 8, 8 'and 8''and to form corners such as corner 7, as shown in FIGS. 12 and 13. In fact, the force F 17 has the effect of bringing the sides of the flaps 202 and 203 together by the cylinder 206, which results in a folding of the plate 10 along a line 18 parallel to the axis Y 2 . The tabs 11 formed on the upright 4 are thus brought into overlap with the edge 3a of the upright 3, these tongues and this edge can then be welded by a high energy beam.

Dans la configuration de la figure 14, l'outillage 200 forme un rectangle dont les volets 201 à 204 constituent les quatre côtés. Ce rectangle est fermé au niveau d'une zone de jonction entre les volets 201 et 204 où sont prévus des moyens de verrouillage non représentés associés à des moyens de guidage également non représentés. Ainsi, le rectangle représenté à la figure 14 est défini de façon précise par la coopération des volets 201 à 204, de sorte que la géométrie du cadre 2 ainsi obtenue est également définie de façon précise.In the configuration of FIG. 14, the tool 200 forms a rectangle whose flaps 201 to 204 constitute the four sides. This rectangle is closed at an area of junction between shutters 201 and 204 where means are provided not shown locking associated with means of guidance also not shown. So the rectangle shown in Figure 14 is defined precisely by the cooperation of flaps 201 to 204, so that the geometry of frame 2 thus obtained is also defined so precise.

Selon un aspect avantageux de l'invention représenté uniquement à la figure 16 le mors 106 est équipé d'une lame 106h formant cisaille avec la plaque 101 et permettant de découper lors du pliage du montant 3, la plaque 10 dans la zone de jonction des montants 3 et 4 de façon à créer une entaille 19 visible à la figure 11 compatible avec le mouvement de pliage autour de l'axe Y2. Du fait de l'utilisation de la lame 106h, l'entaille est créée au terme des opérations de mise en forme des montants tubulaires 3, 3', 4 et 4'. Avant l'utilisation de cette lame la plaque 10 présente une continuité dans les zones 8, 8' et 8'' de jonction entre les montants 3 et 4. En d'autres termes l'incorporation de la lame 106h sur le mors 106 permet de réaliser l'entaille 19 juste avant l'utilisation de l'outillage 200, ce qui évite des contraintes trop importantes au niveau de la ligne 18 lors de la réalisation des parties tubulaires. En pratique, la lame 106h peut être à double arête tranchante, de telle sorte qu'elle permet de découper la plaque 10 selon deux lignes 28 et 29 parallèles définissant entre elles l'entaille 19 jusqu'à un perçage 30 préalablement ménagé dans la plaque 10. Bien entendu, les mors 103, 104 et 105 peuvent également être équipés de lames formant cisailles.According to an advantageous aspect of the invention shown only in FIG. 16, the jaw 106 is equipped with a blade 106h forming a shear with the plate 101 and making it possible to cut, when folding the upright 3, the plate 10 in the junction zone of the uprights 3 and 4 so as to create a notch 19 visible in FIG. 11 compatible with the folding movement around the axis Y 2 . Due to the use of the blade 106 h , the notch is created at the end of the operations of shaping the tubular uprights 3, 3 ', 4 and 4'. Before the use of this blade, the plate 10 has continuity in the zones 8, 8 'and 8''of junction between the uprights 3 and 4. In other words the incorporation of the blade 106 h on the jaw 106 allows the notch 19 to be produced just before the use of the tooling 200, which avoids excessive stresses at the level of the line 18 during the production of the tubular parts. In practice, the blade 106 h can have a double cutting edge, so that it allows the plate 10 to be cut along two parallel lines 28 and 29 defining between them the notch 19 until a bore 30 previously formed in the plate 10. Of course, the jaws 103, 104 and 105 can also be fitted with blades forming shears.

En fonction de la géométrie du cadre 2, c'est-à-dire en fonction, notamment, de la longueur des montants et de leur section, différents jeux de mors 103 à 106 et de berceaux 113 à 116 peuvent être utilisés, les mors et les berceaux étant mis en place conjointement dans l'installation 100, ce qui permet de réaliser un échange standard rapide de l'ensemble des organes de pliage de cette installation.Depending on the geometry of frame 2, that is to say in function, in particular, of the length of the uprights and their section, different sets of jaws 103 to 106 and cradles 113 to 116 can be used, the jaws and the cradles being jointly set up in installation 100, which allows rapid standard exchange of the assembly folding members of this installation.

L'utilisation des mors 103 à 106 pouvant glisser sur des berceaux 113 à 116 d'axes géométriques différents, comme les axes a et c, permet de réaliser des arêtes non alignées, comme les arêtes 13 et 15, ce qui ne serait pas possible avec des mors de conformation articulés sur des charnières communes.The use of jaws 103 to 106 which can slide on cradles 113 to 116 of different geometric axes, such as axes a and c , makes it possible to produce non-aligned edges, such as edges 13 and 15, which would not be possible. with conformation jaws articulated on common hinges.

Sur les figures, les mors 103 et 105 et les berceaux 113 et 115 ont été représentés comme deux unités distinctes. Il pourrait cependant s'agir d'une même unité formant organe de pliage à la fois pour des montants 3 et 4, car l'axe de pliage a est le même pour toute l'arête 12 sur la longueur de la plaque 10. C'est pourquoi, les plaques 103a et 105a d'une part et les berceaux 103d et 105d pourraient être constitués d'une seule pièce.In the figures, the jaws 103 and 105 and the cradles 113 and 115 have been shown as two separate units. It could however be the same unit forming a folding member for both uprights 3 and 4, because the folding axis a is the same for the entire edge 12 over the length of the plate 10. C 'is why, the plates 103 a and 105 a on the one hand and the cradles 103 d and 105 d could be made in one piece.

Lorsque la plaque à plier est mince et afin d'éviter un phénomène de flambement de ses ailes sous l'effet des efforts de bridage, on peut prévoir de plaquer la tôle contre les plaques 103a à 106a des mors 103 à 106 par aspiration ou par attraction magnétique. Pour ce faire, les mors 103 à 106 peuvent être pourvus de canaux débouchant sur les faces 103a1, 103a2, 105a1 et 106a1 et reliés à une source de vide. Les mors peuvent également être équipés d'aimants permanents ou d'électro-aimants permettant une immobilisation des ailes 23 à 26.When the plate to be folded is thin and in order to avoid a phenomenon of buckling of its wings under the effect of the clamping forces, provision may be made to press the sheet against the plates 103 a to 106 has jaws 103 to 106 by suction. or by magnetic attraction. To do this, the jaws 103 to 106 can be provided with channels opening on the faces 103 to 1, 103 to 2, 105 to 1 and 106 to 1 and connected to a vacuum source. The jaws can also be equipped with permanent magnets or electromagnets allowing immobilization of the wings 23 to 26.

Comme représenté à la figure 17 pour une installation conforme à un second mode de réalisation de l'invention, les mors, tels que les mors 104 peuvent être guidés par des berceaux, tels que le berceau 114 grâce à des segments circulaires téléscopiques 1041 et 1042 qui permettent, pour une géométrie donnée d'un berceau 114 d'obtenir un guidage efficace pour un mouvement F20 de pivotement du mors 104 autour de l'axe c de grande amplitude. Le segment 1041 est solidaire du mors 104 alors qu'il est emboíté à l'intérieur du segment 1042, ce segment 1042 étant lui-même mobile en appui contre la surface cylindrique interne 114c du berceau 114.As shown in FIG. 17 for an installation in accordance with a second embodiment of the invention, the jaws, such as the jaws 104, can be guided by cradles, such as the cradle 114 by means of telescopic circular segments 1041 and 1042 which allow, for a given geometry of a cradle 114 to obtain effective guidance for a movement F 20 of pivoting of the jaw 104 around the axis c of great amplitude. The segment 1041 is integral with the jaw 104 while it is fitted inside the segment 1042, this segment 1042 itself being movable in abutment against the internal cylindrical surface 114 c of the cradle 114.

Le segment 1042 est creux alors que le segment 1041 est plein et de largeur inférieure à la largeur du volume intérieur du segment 1042.Segment 1042 is hollow while segment 1041 is full and less than the width of the volume inside segment 1042.

Le segment 1042 est pourvu de rouleaux 1042g disposés le long de sa surface intérieure 1042h et aptes à coopérer avec la tranche 1041c du segment 1041. Ces rouleaux facilitent le glissement relatif entre les segments 1041 et 1042. De plus, la tranche 1042c du segment 1042 est également pourvue de rouleaux 1042i aptes à coopérer avec la surface interne 114c du berceau 114. Ceci facilite le pivotement du segment 1042.The segment 1042 is provided with rollers 1042g arranged along its internal surface 1042 h and able to cooperate with the section 1041 c of the segment 1041. These rollers facilitate the relative sliding between the segments 1041 and 1042. In addition, the section 1042 c of the segment 1042 is also provided with rollers 1042 i able to cooperate with the internal surface 114 c of the cradle 114. This facilitates the pivoting of the segment 1042.

Selon des variantes non représentées de l'invention, le segment 1041 et/ou le berceau 114 peuvent être équipés de billes ou de rouleaux de glissement.According to variants not shown of the invention, the segment 1041 and / or cradle 114 can be fitted with sliding balls or rollers.

L'invention a été décrite, en référence au premier mode de réalisation, avec des mors équipés de nervures dont les surfaces d'extrémités 103c, 104c, 105c et 106c sont prévues pour glisser contre les surfaces cylindriques 113c à 116c des berceaux 113 à 116. Cependant, les nervures 103b à 106b peuvent être équipées de patins à billes ou à rouleaux, ces billes ou rouleaux étant prévus pour rouler sur les surfaces 113c à 116c.The invention has been described, with reference to the first embodiment, with jaws equipped with ribs whose end surfaces 103 c , 104 c , 105 c and 106 c are provided to slide against the cylindrical surfaces 113 c to 116 c cradles 113 to 116. However, the ribs 103 b to 106 b can be fitted with ball or roller skates, these balls or rollers being designed to roll on surfaces 113 c to 116 c .

D'autres modes de guidage des mors par les berceaux peuvent être envisagés.Other methods of guiding the jaws by the cradles can be considered.

Comme il ressort plus particulièrement des figures 18 et 19, les cornières 201d à 204e et les mâchoires 201f à 204g du premier mode de réalisation peuvent être remplacées par des profilés à section transversale globalement en forme de U dont deux sont représentés à la figure 18, avec les références 202m et 203m. Ces profilés ont une section transversale adaptée pour recevoir respectivement les montants 3 et 4' en étant fixés sur des volets analogues aux volets 202 et 203 du premier mode de réalisation.As can be seen more particularly in FIGS. 18 and 19, the angles 201 d to 204 e and the jaws 201 f to 204 g of the first embodiment can be replaced by profiles with a generally U-shaped cross section, two of which are shown in Figure 18, with the references 202 m and 203 m . These profiles have a cross section adapted to receive respectively the amounts 3 and 4 'by being fixed on flaps similar to flaps 202 and 203 of the first embodiment.

Des cales 202p et 203p sont respectivement associés aux profilés 202m et 203m pour coincer en position les montants 3 et 4'. Ces cales ont une section globalement triangulaire avec un angle tronqué, c'est-à-dire en fait une section trapézoïdale. Lorsque les montants 3 et 4' ont été mis en place dans les profilés 202m et 203m, les cales sont introduites dans les profilés comme représentées par les flèches F20, la géométrie des cales 202p et 203p étant telle qu'elles sont chacune pourvue d'une surface 202g, 203g adaptée pour reposer contre certaines ailes 24 ou 26 des profilés 3 et 4'.Wedges 202 p and 203 p are respectively associated with profiles 202 m and 203 m to wedge the uprights 3 and 4 'in position. These shims have a generally triangular section with a truncated angle, that is to say in fact a trapezoidal section. When the uprights 3 and 4 ′ have been placed in the profiles 202 m and 203 m , the shims are introduced into the profiles as represented by the arrows F 20 , the geometry of the shims 202 p and 203 p being such that they are each provided with a surface 202 g , 203 g adapted to rest against certain wings 24 or 26 of the sections 3 and 4 '.

Chaque cale 202p ou 203p est pourvue d'un trou borgne 202r, 203r de réception d'une cheville 202s, 203s prévue pour traverser un orifice 202t, 203t des profilés 202m et 203m. L'introduction de la cheville 202s dans l'orifice 202t et le trou borgne 202r est représentée par les flèches F21. Une fois les chevilles 202s et 203s en place dans les trous et orifices 202r, 202t, 203r et 203t, les câles sont immobilisées sur les profilés 202m et 203m et maintiennent en place les montants 3 et 4'.Each wedge 202 p or 203 p is provided with a blind hole 202 r , 203 r for receiving a plug 202 s , 203 s intended to pass through an orifice 202 t , 203 t of the profiles 202 m and 203 m . The introduction of the plug 202 s into the orifice 202 t and the blind hole 202 r is represented by the arrows F 21 . Once the plugs 202 s and 203 s in place in the holes and orifices 202 r , 202 t , 203 r and 203 t , the cables are immobilized on the profiles 202 m and 203 m and hold the uprights 3 and 4 'in place .

L'invention a été représentée avec des mors dont les surfaces internes 103a1 à 106a1 sont planes alors que les ailes 23 à 26 sont également planes. Bien entendu, ces surfaces et ces ailes peuvent être gauches en fonction de la géométrie recherchée pour les montants 3, 3', 4 et 4'.The invention has been shown with jaws whose internal surfaces 103 a 1 to 106 a 1 are planar while the wings 23 to 26 are also planar. Of course, these surfaces and these wings can be left depending on the geometry sought for the amounts 3, 3 ', 4 and 4'.

L'invention a été représentée lors de sa mise en oeuvre pour la fabrication de cadres supports de masque d'ombre. De tels cadres peuvent être réalisés en une, deux ou quatre pièces, chaque pièce formant un, deux ou les quatre montants du cadre.The invention has been shown during its implementation for the production of shadow mask support frames. Of such frames can be made in one, two or four pieces, each piece forming one, two or all four uprights of the frame.

Claims (33)

  1. Method for producing a casting (2) comprising at least one tubular section (3, 3', 4, 4') obtained by bending a metal plate (10) in line with at least one longitudinal edge (12-17), characterised in that it comprises steps consisting of:
    pre-bendjng (F) the said plate 10 in line with at least two bending edges (12-17), then
    exerting, during bending (F1, F3, F11, F13), a clamping force (F7, F8, F12, F14) on at least one part (23-26) of the said plate from a bending component (103-106).
  2. Method according to claim 1, characterised in that the pre-bending is achieved by immobilising the said plate on an apron (101) by means of a retractable draw-ring (107).
  3. Method according to one of claims 1 or 2, characterised in that it comprises a step consisting of preparing the said pre-bending by weakening the said plate along the said bending edges (12-17).
  4. Method according to one of the preceding claims, characterised in that it consists in bending the said plate (10) in line with the different edges (12-17) along the length of the said casting, such that tubular sections (3, 3'. 4, 4') of different base profiles are formed.
  5. Method according to one of the preceding claims, characterised in that it consists in bending the said plate (10) around at least one virtual geometric axis (a, b, c) defined by the co-operation of the said bending component (103-106) and the associated guidance means (113-116).
  6. Method according to one of the preceding claims, characterised in that it consists of exerting the said clamping force (F7, F8, F12, F14) essentially on the exterior of a tubular section (3, 3', 4, 4') of the said casting (2), in the absence of clamping force exercised by a draw-ring (107) or similar equipment.
  7. Method according to one of the preceding claims, characterised in that the said clamping force (F7, F8, F12, F14) is directed overall towards the said edge (12, 13, 15).
  8. Method according to one of the preceding claims, characterised in that the said clamping force (F7, F8, F12, F14) is perpendicular overall to the said bending edge (12-17).
  9. Method according to one of the preceding claims, characterised in that the said clamping force (F7, F8, F12, F14) forces one part (23, 24, 25a, 26b) of the said plate (10) parallel to itself and perpendicular to the bending force (F1, F3, F11, F13) exercised on this part by the bending component (103-106).
  10. Method according to one of the preceding claims, characterised in that the said clamping force (F7, F8, F12, F14) is adjusted according to the position of the said bending component (103-106).
  11. Method according to one of the preceding claims, characterised in that it comprises a step consisting of placing a first part (26) of the said plate (10) to overlap a second part (25) of the said plate and reducing the clamping force (F12) exerted on the said second part, such that the said first and second parts are in tensile support against each other, the said first and second parts then being welded together.
  12. Method according to one of the preceding claims, characterised in that the said plate (10) is bent around at least one virtual axis (a, b, c) defined as the geometric axis of a cylindrical guidance cradle (113-116) of the said bending component (103-106)
  13. Method according to claim 12, characterised in that the said plate (10) is bent around the different bending axes (a, b, c) along the length (X-X1) of the said casting (2) using the bending components (103-106) guided by cradles (113-116) of different geometric axes (a, b, c) corresponding to the said bending axes.
  14. Method according to one of the preceding claims, characterised in that it comprises a step consisting, after the formation of several tubular sections (3, 3', 4, 4'), of modelling them into a closed frame (2) by bending the linkage sections (8, 81, 811) between two adjacent tubular sections perpendicular to the principal directions (X-X1) of the said tubular sections.
  15. Method according to one of the preceding claims, characterised in that it comprises a step consisting of plating, by magnetic induction or attraction, one part (23-26) of the said plate against one part (103a-106a) of the said bending component (103-106).
  16. Apparatus for producing a casting (2) comprising at least one tubular section (3, 3', 4, 4'), the said apparatus comprising at least one component (103-106) for bending a metal plate (10) in line with a longitudinal edge (12-17) of the said tubular section, characterised in that the said bending component is provided with means (103f-106f) allowing for a clamping force (F7, F8, F12, F14) to be exerted on one part (23-26) of the said plate, countering slippage of one part (23-26) of the said plate (10) along the said bending component (103-106), whilst the said bending component is articulated around a virtual geometric axis (a, b, c) situated on the interior of the corresponding tubular section (3, 3', 4, 4')
  17. Apparatus according to claim 16, characterised in that it comprises several bending components (103-106) capable of bending the said plate (10) in line with the separate edges (12-17), such that tubular sections (3, 3', 4, 4') of different base profiles are formed.
  18. Apparatus according to one of claims 16 or 17, characterised in that the said clamping means comprise at least one lug (103f-106f) forming a butted support for the said plate (10).
  19. Apparatus according to claim 18, characterised in that the said lug (103f-104f) extends over approximately the whole length (X-X1) of the said edge (13).
  20. Apparatus according to claim 18, characterised in that the said clamping means comprise several lugs (105f-106f) spread along the length (X-X1) of the said edge (12, 15) and separated by receiving spaces (105g-106g) for the bending lugs used for bending the said plate (10) along another edge.
  21. Apparatus according to one of claims 16 to 20, characterised in that the said clamping means have a variable position (F9) in relation to the said edge (13).
  22. Apparatus according to one of claims 16 to 21, characterised in that it comprises means for regulating or adjusting the force (F7, F8, F12, F14) exerted by the said clamping means (103f-106f) on the said plate (10).
  23. Apparatus according to one of claims 16 to 22, characterised in that the said bending component (103-106) comprises at least one support surface (104a1-106a1) against the said plate (10) and at least one circular based cylindrical surface (103c-106c) capable of co-operating with a circular based cylindrical surface (113c-116c) of a cradle (113-116), the said cylindrical surfaces being centred on a virtual bending axis (a, b, c) of the said plate.
  24. Apparatus according to claim 23, characterised in that it comprises several bending components (103-106) spread along the length (X-X1) of the said plate (10) and comprising cradles (113-116) whose cylindrical surfaces (113c-116c) have geometric axes (a, b, c) that are parallel to and offset against each other.
  25. Apparatus according to one of claims 23 or 24, characterised in that the said or each bending component (103-106) is provided with an external rib (103b-106b) forming a cylindrical surface (103c-106c) capable of co-operating with a cylindrical surface (113c-116c) of the corresponding cradle (113-116), the said cylindrical surfaces being of approximately the same radius (R103, R113, R104, R114),
  26. Apparatus according to one of claims 23 to 25, characterised in that the said or each bending component (104) is guided in relation to the said surface (114c) of the said cradle (114) by telescopic segments (1041, 1042).
  27. Apparatus according to one of claims 25 or 26, characterised in that the said cylindrical surface (103c-106c) of the said rib, the said telescopic segments (1041, 1042) and/or the said surface (113c-116c) of the said cradle (113-116) are provided with sliding balls or rollers (1042g, 1042i).
  28. Apparatus according to one of claims 16 to 27, characterised in that it comprises a shaping die (200) for the said casting (2), the said die including support elements (201-204) of tubular sections (3, 3', 4, 4') of the said casting (2) provided with reception and immobilisation means (201d-204d, 201e-204e, 201f-204f, 201g-204g) for the said tubular parts, the said elements being articulated (Y1, Y2, Y3) in relation to each other.
  29. Apparatus according to claim 28, characterised in that at least one of the said articulated elements (201-204) is adjustable for length (X1, X2, X3, X4).
  30. Apparatus according to one of claims 28 or 29, characterised in that the said articulated elements (201-204) are capable of forming together a closed figure of predetermined geometry corresponding to the geometry of a frame (2) constituted by the said casting.
  31. Apparatus according to one of claims 27 to 30, characterised in that at least one of the said articulated elements (203-204) is equipped with a component (202m or 203m) with a transverse section in the overall form of a U capable of receiving in place in the said element at least one locking wedge (202p, 203p) of one of the said tubular sections (3, 3', 4, 4'), means (202s, 203s) being provided for immobiiising the said wedge on the said component.
  32. Apparatus according to one of claims 16 to 31, characterised in that at least one (106) of the said bending components (105-106) is equipped with a blade (106h) forming a cut-out shear for the said plate (10) during its bending (F13).
  33. Use of a method according to one of claims 1 to 15, or apparatus according to one of claims 16 to 32 for the manufacture of a shadow mask (1) support frame (2) for a cathode ray tube.
EP01972204A 2000-09-26 2001-09-25 Method and installation for making a workpiece comprising at least a tubular section Expired - Lifetime EP1320427B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0012240 2000-09-26
FR0012240A FR2814386B1 (en) 2000-09-26 2000-09-26 METHOD AND INSTALLATION FOR MANUFACTURING A PART COMPRISING AT LEAST ONE TUBULAR SECTION
PCT/FR2001/002970 WO2002026412A1 (en) 2000-09-26 2001-09-25 Method and installation for making a workpiece comprising at least a tubular section

Publications (2)

Publication Number Publication Date
EP1320427A1 EP1320427A1 (en) 2003-06-25
EP1320427B1 true EP1320427B1 (en) 2004-06-09

Family

ID=8854694

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01972204A Expired - Lifetime EP1320427B1 (en) 2000-09-26 2001-09-25 Method and installation for making a workpiece comprising at least a tubular section

Country Status (11)

Country Link
US (1) US6988390B2 (en)
EP (1) EP1320427B1 (en)
JP (1) JP3694715B2 (en)
KR (1) KR100826259B1 (en)
CN (1) CN1226110C (en)
AT (1) ATE268652T1 (en)
AU (1) AU2001291991A1 (en)
DE (1) DE60103769T2 (en)
FR (1) FR2814386B1 (en)
TW (1) TW571329B (en)
WO (1) WO2002026412A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7244701B2 (en) 2000-06-16 2007-07-17 Zealand Phama A/S Diuretic peptide conjugate
JP4766084B2 (en) * 2008-07-18 2011-09-07 トヨタ自動車株式会社 Work bending method and apparatus
US20100050729A1 (en) * 2008-09-01 2010-03-04 Rahul Kulkarni Die assembly for use in an apparatus for forming a workpiece
DE102008044523B4 (en) * 2008-09-15 2011-06-16 Thyssenkrupp Steel Europe Ag Warmumformprofile
CN112881213A (en) * 2019-11-29 2021-06-01 宸龙半导体有限公司 Tension-free bender equipment and correction method thereof
CN114029367B (en) * 2021-11-03 2024-04-16 扎赉诺尔煤业有限责任公司 Cylinder one-time pressing forming machine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US562877A (en) * 1896-06-30 Metal-folding machine
US422744A (en) * 1890-03-04 Sheet-metal-folding machine
US1708615A (en) * 1927-12-28 1929-04-09 Hudson Motor Car Co Method of shaping sheet metal
US3577755A (en) * 1968-12-24 1971-05-04 Alusuisse Sleeve for protecting the peg in the head of a carbon anode electrode and apparatus for producing this sleeve
DE1927520A1 (en) * 1969-05-30 1971-01-28 Dornier Ag Beding plates round small radii
DE1943884A1 (en) * 1969-08-29 1971-03-18 Kabel Metallwerke Ghh Device for reshaping a hollow body
US4365500A (en) * 1981-01-30 1982-12-28 Chesley F. Carlson Company Web bending fixture
DE3739173A1 (en) * 1987-11-19 1989-06-01 Feintool Int Holding METHOD AND DEVICE FOR BENDING WORKPIECES
FR2790140B1 (en) * 1999-02-19 2001-04-20 Imphy Ugine Precision CATHODE VIEW TUBE SHADOW MASK FRAME SUPPORT
US6412325B1 (en) * 1999-03-23 2002-07-02 3 Dimensional Services Method for phototyping parts from sheet metal

Also Published As

Publication number Publication date
KR20030065477A (en) 2003-08-06
JP3694715B2 (en) 2005-09-14
DE60103769T2 (en) 2005-08-11
CN1466498A (en) 2004-01-07
DE60103769D1 (en) 2004-07-15
WO2002026412A1 (en) 2002-04-04
FR2814386A1 (en) 2002-03-29
AU2001291991A1 (en) 2002-04-08
FR2814386B1 (en) 2003-06-20
US6988390B2 (en) 2006-01-24
EP1320427A1 (en) 2003-06-25
JP2004509764A (en) 2004-04-02
CN1226110C (en) 2005-11-09
ATE268652T1 (en) 2004-06-15
US20030192356A1 (en) 2003-10-16
TW571329B (en) 2004-01-11
KR100826259B1 (en) 2008-04-29

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