EP3237132A1 - Bohrverfahren und vorrichtung zur implementierung dieses verfahrens - Google Patents

Bohrverfahren und vorrichtung zur implementierung dieses verfahrens

Info

Publication number
EP3237132A1
EP3237132A1 EP15817819.4A EP15817819A EP3237132A1 EP 3237132 A1 EP3237132 A1 EP 3237132A1 EP 15817819 A EP15817819 A EP 15817819A EP 3237132 A1 EP3237132 A1 EP 3237132A1
Authority
EP
European Patent Office
Prior art keywords
drilling
barrel
axis
main axis
point
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.)
Withdrawn
Application number
EP15817819.4A
Other languages
English (en)
French (fr)
Inventor
Philippe Le Vacon
Damien Chablat
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.)
Airbus SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Publication of EP3237132A1 publication Critical patent/EP3237132A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B35/00Methods for boring or drilling, or for working essentially requiring the use of boring or drilling machines; Use of auxiliary equipment in connection with such methods
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B49/00Measuring or gauging equipment on boring machines for positioning or guiding the drill; Devices for indicating failure of drills during boring; Centering devices for holes to be bored
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B2215/00Details of workpieces
    • B23B2215/04Aircraft components

Definitions

  • the present invention relates to a method of drilling a workpiece which makes it easy to orient the drilling axis of a drilling tool relative to the surface of this workpiece to ensure that it is normal to this surface at the point of the surface. to pierce.
  • the dimensional and geometrical precision of the hole the good normality of the axis of the hole with the surface of the fuselage as well as the precision of positioning of the hole are important quality criteria.
  • Patent application WO201 11 ⁇ 57933 A1 is known in the name of the present applicant, a method of positioning the normal of a translation axis of a jack device.
  • This method implements a cross-table architecture X, Y on which a carriage carrying an automated drilling unit (UPA) is movable in displacement.
  • UPA automated drilling unit
  • This drilling unit has a mechanical architecture of the slide and double gimbal type to position the axis of the normal piercing pin to the skin of the aircraft to be pierced.
  • This architecture for bringing the drilling axis into normalcy is a passive system which requires, prior to the execution of the operation of drilling, calculate from the theoretical geometry of the skin of the aircraft, a locking point of the carriage on the cross table, the distance separating this locking point from the point of the surface of the piece to be pierced being determined so that the normal projection of this locking point on the surface of the workpiece is the center of the point to be pierced.
  • the movements of the carriage carrying the automated drilling unit are programmed in the plane of the crossed table, to be translated into piercing points on a curved surface of the skin of the aircraft.
  • the present invention therefore proposes a method and a machine for drilling the surface of a workpiece, which are particularly simple in their design and in their operating mode, and which are reliable and which make the drilling axis easier to position in the angular position.
  • the invention relates to a piercing method at a point on the surface of a workpiece, in which a drilling barrel having a main axis is used.
  • said barrel being rotatable about a pivot point on said main axis, orienting said main axis so that it is perpendicular to the osculator plane of the part at this point to be pierced, by pivoting said barrel of drilling relative to said pivot point, said pivot point being fixed in said plane (x, y),
  • step a) the main axis of the barrel is placed vertically above the point of the surface of the part to be pierced.
  • said pivot point is taken so as to be placed at the free end of the drilling barrel.
  • the drilling barrel being a hollow press member comprising, at this free end, a press surface, also called bearing surface, the pivot point is thus placed in the center of the press surface of the drilling barrel.
  • This pivot point at the bearing surface of the drilling gun facilitates the pivoting of the main axis of the drilling barrel, and therefore its orientation, so that a low power actuator is only necessary .
  • drilling point locations are determined on the workpiece surface
  • said drilling barrel being movable in the plane (x, y), said barrel is moved in step a) with respect to the surface of said piece,
  • said drilling barrel having a bearing surface at its free end, said pivot point belonging to the plane passing through said press surface, before applying to drilling in step d), a force predefined compression means by means of said drilling barrel so as to ensure drilling without burrs.
  • step b) the actual shape of at least a part of the surface of the part containing said point to be pierced is determined.
  • step a) determining the position of said main axis in the plane (x, y) to verify that said main axis is positioned vertically or vertically, from the theoretical point of the surface of the piece to be pierced.
  • the present invention also relates to a machine for implementing the drilling method as described above, in a reference (x, y, z) linked to this machine, said machine comprising:
  • said drilling assembly comprising a drilling barrel having a main axis and means for translating said drilling assembly along the z-axis,
  • said drilling assembly also comprises means for angularly orienting said main axis in an angular range extending between at least a first position in which said main axis of the barrel is parallel to the axis z so as to be placed at the plumb with said piercing point on the surface of the workpiece, up to at least a second position in which said main axis is perpendicular to the osculator plane of the workpiece at this point to be pierced, said means for translational movement of said piercing assembly on along the axis z and said part being stationary in position in the plane (x, y).
  • this piercing gun receives a piercing tool which is coaxial with the piercing barrel, being movable in translation inside this piercing barrel.
  • This drilling tool comprises, for example, a rod having a piercing head, the longitudinal axis of this rod, or spindle, coinciding with the main axis of the drilling barrel.
  • the main axis of the drilling barrel then defines the drilling axis of the drilling tool.
  • this drilling barrel thus serves here also as a sleeve for the drilling tool.
  • This drilling barrel also makes it possible to apply a plating force to a stack of parts to be pierced, prior to drilling, in order to guarantee the absence of chips between the parts.
  • this means for angularly orienting said main axis allows a pivoting of the drilling barrel, and therefore of the main axis of this drilling barrel, with respect to a pivot point.
  • This pivot point which is placed on the main axis of the drilling barrel is advantageously positioned at the free end of the drilling barrel.
  • said means for angularly orienting said main axis comprises means for pivoting said main axis with respect to a pivot point.
  • said means for angularly orienting said main axis comprises:
  • a first element for receiving and carrying at least said piercing barrel said first element comprising a ball section having a first opening through which the piercing barrel passes, and
  • a second element having a substantially cylindrical support which accommodates said ball section, said support having a second opening for the passage of at least said piercing barrel and its angular displacement.
  • the second opening has an inverted truncated cone shape.
  • said first element receives and carries said drilling barrel.
  • said first and second elements are placed at one end of said means for translating said drilling assembly along the z axis, this end being intended to be placed on the side of the surface of the part to be pierced.
  • the second element is an integral part of said means for translating this drilling assembly along the z axis, these first and second elements being placed at the free end of said means for translating this set of drilling.
  • said means for translating said drilling assembly along the z-axis comprises a jack device configured to align the translation axis z of the jack in a manner coinciding with the main axis of the piercing gun;
  • said means for effecting a relative movement in the plane (x, y) of a drilling assembly and said workpiece comprises:
  • a support intended to be immobilized with respect to said workpiece during operating sequences comprising a carriage for positioning the drilling assembly, a translation unit Y ensuring a free movement in translation of the carriage along the axis y, and a unit translation X ensuring a free movement in translation of the carriage along the x axis, and
  • this machine comprises a positioning and centering device for positioning the main axis of said drilling barrel vertically or vertically, from the point of the surface of the part to be pierced,
  • this machine comprises a mechanical means for determining the osculating plane of the surface of the part to be drilled in order to position orthogonally said main axis of the drilling gun with respect to this plane.
  • this mechanical means comprises at least two feelers placed on either side of said drilling barrel, these probes for determining the actual shape of the surface of the piece to be drilled around the point to be pierced and to ensure automatically setting in position orthogonal to the main axis of the drilling gun at the osculator plane passing at this point of the surface of the piece to be pierced.
  • FIG. 1 is a partial sectional view of a drilling machine, according to a particular embodiment of the present invention, showing the main axis of the drilling gun positioned in line with the point of the surface of the piece to be pierced;
  • FIG. 2 is a very diagrammatic view of the drilling machine of FIG. 1, in which the main axis is perpendicular to the osculator plane passing at this point of the part to be pierced;
  • FIG. 3 is a very diagrammatic view of the drilling machine of FIG. 1, wherein the end of the piercing gun bears against the surface of the workpiece, the main axis of the piercing gun passing through this point of the workpiece to be pierced;
  • FIG. 4 is a very diagrammatic and perspective view of the drilling module of the drilling machine of FIG. 1 without the piercing tool;
  • FIG. 5 is a longitudinal sectional view of the module of FIG. 4 without the piercing tool
  • FIG. 6 is a very diagrammatic cross-sectional view of the module of FIG. 4 without the piercing tool
  • FIG. 7 is a widened perspective view of the upper part of the drilling module of FIG. 4;
  • FIG. 8 is a very diagrammatic and partial view of a drilling machine according to another embodiment, this machine comprising means for determining the osculating plane of the surface of the part;
  • FIG. 9 is a very diagrammatic representation in section of the means for determining the osculating plane of FIG. 8; DETAILED DESCRIPTION OF EMBODIMENTS OF
  • Figures 1 to 7 show partial and perspective views of a machine 10 for drilling the surface of a workpiece according to a particular embodiment of the present invention.
  • This machine 10 comprises a carriage January 1 to ensure the positioning of a mobile drilling module in the plane of a cross table X, Y.
  • This crossed table comprises a support intended to be immobilized with respect to said part to be pierced during operating sequences.
  • this table comprises in addition to the carriage 1 1, a translation unit Y ensuring a free movement in translation of the carriage 1 1 along the y axis, and a translational unit X ensuring a free movement in translation of the carriage 1 1 along the x axis.
  • this carriage 1 1 comprises for example an opening to allow the passage of the lower end of the drilling module.
  • the table also comprises means for locking the free translational movements in position along the x-axis and along the y-axis of the carriage 1 1 supporting the drilling module.
  • This cross table thus provides a positioning in the plane (x, y) of a mark (x, y, z) of the drilling module relative to the part 18 to be pierced.
  • This drilling module comprises a jack device 12 arranged so that the axis of movement of the cylinder coincides with the axis z 13.
  • This jack device 12 comprises at its free end placed on the side of the part 18 to be drilled, a section 14 with a ball and a substantially cylindrical support 1 6 which accommodates this section 14 ball to allow the rotation of this section 14 to ball around a pivot point.
  • This ball-and-socket section 14 is provided with a first opening through which a hollow cylindrical element 15 piercing, which is secured to this section 14 ball so that the latter supports the hollow cylindrical member.
  • the substantially cylindrical support 16 has a second inverted truncated cone-shaped opening to allow movement of this piercing barrel within a defined angular range.
  • This piercing barrel forms a press member having a press surface. At the intersection of the plane containing this press surface and the z axis is placed the pivot point.
  • the shape of the press surface, or of support is annular and of dimension close to the hole to be made.
  • This drilling barrel 15 also forms a drill tool holder sleeve 17.
  • This drilling tool 17 comprises a rod having a longitudinal axis, which is secured to a piston for moving the rod along a drilling axis, which coincides with the longitudinal axis of this rod.
  • the drilling tool 17 further comprises a piercing head placed at the free end of its rod.
  • the drilling module thus comprises three axes (x, y, z) controlled which ensure the contacting of the press surface of the drilling gun 15 and the introduction of the pressing force on the part 18 which may comprise a stack of sheets, as well as the angular orientation of the drilling axis.
  • the technical solution implemented therefore consists in making the pivot point of the ball section 14 bearing the drilling barrel 15 coincide, and therefore, in view of the arrangement made, the pivot point of the drilling axis with the center of the support surface of his press organ.
  • this pivot point being placed in the center of the bearing surface and on the drilling axis, this pivot point is then coincident with the point of the surface of the part 18 to be pierced. All that remains is to drill the piece 18 along the drilling axis to ensure that a hole of normal axis is formed on the surface of the piece 18 at this point.
  • the upper part of the piston receives the mechanism for angular orientation.
  • This mechanism consists of a toothed crown 21 having a buttonhole 22, in which slides a nut, which receives the upper end of the drilling barrel, tool holder 17 piercing.
  • the ring gear 21 is engaged by a geared motor 19 provided with an encoder 20, the sliding nut in the buttonhole 22 is actuated by a linear jack 23 such as a pneumatic piston provided with a linear position sensor.
  • the combination of the angular orientation a of ring 21 and the linear position of the piston makes it possible to precisely orient the angular position of the main axis 13 of the drilling gun.
  • FIGS. 8 and 9 show a very schematic and partial view of a drilling machine 10 according to another embodiment, this machine 10 comprising a means for determining the osculating plane of the surface of the part 18, and whatever the actual geometrical shape of the piece to be drilled.
  • the distance separating the two feelers 24, 25 of surface being small compared to the radius of curvature of the workpiece 18 to be pierced, the surface profile between these two points is advantageously likened to a plane.
  • These feelers 24, 25 of surface which each comprise an identical compression element of stiffness k such as a spring, send measurement signals to a processing unit.
  • a closed-loop servo-control makes it possible, by balancing the two distance measurements AA 'and BB', on either side of the drilling barrel 15, to ensure the normality of the drilling axis with respect to the osculator plane at the surface of the workpiece to be drilled (Fig. 8).

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Drilling And Boring (AREA)
EP15817819.4A 2014-12-23 2015-12-18 Bohrverfahren und vorrichtung zur implementierung dieses verfahrens Withdrawn EP3237132A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1463186A FR3030325B1 (fr) 2014-12-23 2014-12-23 Procede de percage et machine pour la mise en oeuvre de ce procede
PCT/EP2015/080626 WO2016102392A1 (fr) 2014-12-23 2015-12-18 Procédé de perçage et machine pour la mise en oeuvre de ce procédé

Publications (1)

Publication Number Publication Date
EP3237132A1 true EP3237132A1 (de) 2017-11-01

Family

ID=53008617

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15817819.4A Withdrawn EP3237132A1 (de) 2014-12-23 2015-12-18 Bohrverfahren und vorrichtung zur implementierung dieses verfahrens

Country Status (3)

Country Link
EP (1) EP3237132A1 (de)
FR (1) FR3030325B1 (de)
WO (1) WO2016102392A1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3054463B1 (fr) 2016-07-29 2018-12-07 Seti Tec Dispositif de percage a vitesse d'avance automatique ou controlee a broche auto alignante
CN117340308A (zh) * 2023-09-12 2024-01-05 成都飞机工业(集团)有限责任公司 一种飞机蒙皮锪窝装置及其方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4752160A (en) * 1984-03-19 1988-06-21 Ltv Aerospace & Defense Company Automated tool positioning system
US4613262A (en) * 1984-12-28 1986-09-23 The Boeing Company Drill motor assembly with gimbal normality and clamp-up capability
ITBO20040217A1 (it) * 2004-04-16 2004-07-16 Jobs Spa Testa operatrice per macchine utensili pluriasse
DE102005058493A1 (de) * 2005-12-02 2007-06-06 Dürr Special Material Handling GmbH Bearbeitungsvorrichtung
FR2961425B1 (fr) * 2010-06-16 2012-08-17 Eads Europ Aeronautic Defence Procede de positionnement a la normale d'un axe de translation d'un dispositif de verin
JP2014073571A (ja) * 2012-10-05 2014-04-24 Mitsubishi Heavy Ind Ltd 面直倣い機構、これを備えた加工装置および加工方法

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
None *
See also references of WO2016102392A1 *

Also Published As

Publication number Publication date
FR3030325A1 (fr) 2016-06-24
WO2016102392A1 (fr) 2016-06-30
FR3030325B1 (fr) 2017-07-14

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