EP0734996A1 - Easy assembly vehicle jack - Google Patents

Easy assembly vehicle jack Download PDF

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Publication number
EP0734996A1
EP0734996A1 EP96400669A EP96400669A EP0734996A1 EP 0734996 A1 EP0734996 A1 EP 0734996A1 EP 96400669 A EP96400669 A EP 96400669A EP 96400669 A EP96400669 A EP 96400669A EP 0734996 A1 EP0734996 A1 EP 0734996A1
Authority
EP
European Patent Office
Prior art keywords
jack
nut
support leg
axis
head
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.)
Granted
Application number
EP96400669A
Other languages
German (de)
French (fr)
Other versions
EP0734996B1 (en
Inventor
Gilles Ruffie
David Framboisier
Jean-Jacques Tate
Bernard Figueras
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.)
BOWDEN FRANCE SA
Original Assignee
BOWDEN FRANCE SA
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 BOWDEN FRANCE SA filed Critical BOWDEN FRANCE SA
Publication of EP0734996A1 publication Critical patent/EP0734996A1/en
Application granted granted Critical
Publication of EP0734996B1 publication Critical patent/EP0734996B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66FHOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F3/00Devices, e.g. jacks, adapted for uninterrupted lifting of loads
    • B66F3/08Devices, e.g. jacks, adapted for uninterrupted lifting of loads screw operated
    • B66F3/12Devices, e.g. jacks, adapted for uninterrupted lifting of loads screw operated comprising toggle levers

Definitions

  • the present invention relates to a vehicle jack comprising a support leg and a lifting arm pivotally mounted on the support leg, to be moved by means of a control screw to lift the vehicle.
  • Cree of this type commonly known as "Cree Y” are described for example in patent applications EP-0 320 613, EP-0 565 801, GB-2 176 458 and FR-2 663 015.
  • the control screw rotates in a part forming a nut pivotally received in recesses in the support leg.
  • An object of the present invention is to provide a jack of the aforementioned type, of simplified mounting and executable by a robot.
  • the piece forming a nut is retained on the support leg by engagement of a retaining element, integral with the piece forming a nut, in at least one curvilinear opening formed on the support leg and centered on the articulation axis of the nut-forming part.
  • each recess in the support leg receiving the piece forming a nut constitutes a groove the bottom of which is delimited by a semi-circular edge and the opening width of which is greater than or equal to the diameter of said semi-circular edge.
  • the support leg has the general shape of a profile of U-shaped cross section, and said retaining element is a rivet passing through the piece forming a nut and axially bearing on the external faces of the two wings of the profile.
  • the wall of the wings of said profile bordering said recesses is curved to increase the bearing surface in contact with the part forming a nut.
  • the jack comprises a jack head arranged in alignment with the control screw so that the latter is in axial support on the head of the jack at least during the operation of the jack when the latter is working empty and the screw control is actuated in the direction tending to fold the jack.
  • control screw has a stepped head resting axially against a thrust ball bearing at least during the operation of the jack when the latter is loaded.
  • this thrust ball bearing is housed in a yoke articulated on the lifting arm around the same axis of rotation as the jack head.
  • the jack head is articulated on the lifting arm around an axis of rotation perpendicularly cutting the longitudinal axis of the control screw.
  • the jack 1 shown in the figures comprises a support leg 2 intended to rest, by a lower end forming a foot 3, on the ground.
  • a lifting arm 4 is articulated at one end on this support leg 2, and supports at the other end a head 5 intended to come into contact with the vehicle to be lifted.
  • a control screw 6, on which a drive handle 7 is articulated at one end, makes it possible to move the lifting arm 4 to raise or lower the head 5.
  • the lifting arm 4 is articulated on the supporting leg 2 around an axis of rotation X perpendicular to the plane of FIG. 1.
  • the head 5 of the jack 1 is articulated on the lifting arm 4 around a axis of rotation Y parallel to the axis X.
  • the control screw 6 extends along a longitudinal axis W parallel to the plane of FIG. 1, intersecting the axis X perpendicularly. It passes through a piece forming a nut 8 hinged on the supporting leg 2 around an axis of rotation Z intersecting the axis W and parallel to the axis X.
  • the jack 1 is symmetrical with respect to a plane of symmetry containing the axis W and perpendicular to the axis X.
  • the head 5 of the jack 1 is shown in isolation in Figures 3 to 5. It is preferably made of plastic, and comprises a body 50 crossed by a cylindrical bore 51 of revolution about the Y axis, for the passage of a hinge pin 98 of the head 5 on the lifting arm 4.
  • Two fingers 52, 53 extend the body 50 superiorly (when the jack is in the deployed lifting position of a vehicle as shown in FIG. 1) and define between them a groove 54, opening upwards, for the engagement of the head 5 on a weld bead or a rebate of the body of the vehicle, projecting downwards, or on any other part of the vehicle provided for this purpose.
  • the respective surfaces 540, 541 of the fingers 52, 53, facing each other, are plane and parallel.
  • the head 5 has stop surfaces 520, the role of which will be explained below, located at the base of the finger 52 and extending, planar, forming an angle of 44 ° 30 'with the plane of the surfaces 540 and 541.
  • the lower ends of these stop surfaces 520 have been referenced 521.
  • the body 50 also has a surface 55, cylindrical of revolution around the axis Y, extending over an angular sector of 60 °.
  • the control screw 6 has a helical thread 60 extending along the axis W, engaged in the part forming the nut 8, and comprises at one axial end a shouldered head 61. It is provided at the opposite axial end with a tip 66 on which the handle 7 is articulated, about an axis of rotation perpendicularly cutting the axis W.
  • the shouldered head 61 rests by its axial end edge 63 against the surface 55 of the head with and by its shoulder, referenced 64, on a ball stop 62 bearing on a yoke 9.
  • This ball stop 62 comprises, in a manner known per se, two rings 62a, 62b of axis W, defining raceways for balls 62c interposed between the rings 62a, 62b.
  • the yoke 9 is shown in isolation in Figures 6 to 8. It has two flanges 90, planes and parallel to each other, joined by a base 91. The latter extends perpendicular to the plane of the flanges 90. Holes 92 of axis Y are provided on the flanges 90 for the passage of the aforementioned articulation pin 98, and the rotational mounting of the yoke 9 on the lifting arm 4 around the axis Y.
  • the base 91 is crossed by a bore 93 for the passage of the control screw 6.
  • the ring 62b of the ball bearing 62 rests against the face 910 of the base 91 facing towards the interior of the flanges 90.
  • the latter are perforated at 94 as shown in FIG.
  • the lifting arm 4 is shown in isolation in FIGS. 9 to 14.
  • the latter is preferably produced by stamping, cutting and bending a sheet to form a metal section elongated in the direction of a longitudinal axis V perpendicular to the axes.
  • X and Y This profile has a cross section having the general shape of a U, as shown more particularly in Figures 11 to 13. It comprises two wings 40 joined by a back 41 extending generally perpendicular to the wings 40. Des oblong recesses 42 from stamping extend parallel to the axis V on the wings 40 to stiffen the profile. These recesses 42 protrude into the interior space of the profile located between the wings 40.
  • An oblong recess 43, projecting inward, is made on the back 41 for the same purpose.
  • the wings 40 are pierced at a longitudinal end, at 44, for the passage of the aforementioned pin 98 and the rotational assembly of the head 5, the yoke 9 and the lifting arm 4.
  • These holes 44 are made at one end longitudinal of the recesses 42.
  • the wings 40 are pierced at the opposite longitudinal end, at 46, for the passage of a pin 28 of axis X serving for the articulation of the lifting arm 4 on the support leg 2.
  • These holes 46 are made on circular stampings 47 projecting towards the outside of the profile, as shown more particularly in FIG. 12.
  • the back 41 is extended, at the end of the lifting arm 4 articulated on the support leg 2, by a wall 48 extending obliquely between the wings 40 and forming a spacer.
  • the wall 48 results from a cutting and a folding of the sheet metal used to produce the profile, as illustrated in FIG. 14.
  • the longitudinal ends of the wings 40 have at the end articulated on the support leg 2 a generally triangular profile, observed in the direction of the X axis. This profile is delimited by two orthogonal rectilinear edges 401, 402 joined by an edge in an arc of a circle 403 centered on the X axis.
  • the wall 48 s 'extends in the plane of the edges 401 and forms with the back 41 a corner dihedral at the top 238 °.
  • the nut forming part 8 is shown in isolation in FIGS. 15 to 19.
  • the latter is preferably made of plastic. It comprises a body 80 traversed along the axis W by a tapping 81 adapted to receive the threaded body 60 of the control screw 6. Lateral parts 82 form protrusions on either side of the body 80 for the articulation of the piece forming a nut 8 on the support leg 2. These lateral parts 82 are delimited radially, on the outside, by cylindrical surfaces of revolution around the axis Z, and axially by end sections 83 which are planar and perpendicular to the axis Z.
  • the piece forming a nut 8 also comprises two tabs 84 crossed by bores 85 of axis T parallel to the axis Z, for mounting means for retaining the piece forming a nut 8 on the leg of support 2, as will be explained below.
  • the lugs 84 are connected to the body 80 by providing annular grooves 86 centered on the Z axis with the cylindrical surfaces 82.
  • the dihedral from the top of the Z axis, delimited by the plane perpendicular to the W axis and by the plane containing the axis T, has an angle at the top 60 °.
  • FIG. 24 to 29 shows the support leg 2 in isolation.
  • the latter is preferably produced by stamping, cutting and bending a sheet to form an elongated section along a longitudinal axis G perpendicular to the axis Z.
  • This profile has a cross section having the general shape of a U, comprising two wings 20 joined by a back 21.
  • Each wing 20 has an oblong recess 22 coming from stamping, projecting into the interior space of the profile located between the wings 20, and intended to stiffen the profile.
  • the foot 3 is formed by cutting and folding as illustrated in FIG. 29. More specifically, the foot 3 has a first planar wall 30 connected to the back 21 by a fold line 31 and forming, in the assembled position of the jack, an angle 43 ° with the back 21 as shown in Figure 24.
  • This wall 30 is extended downwards by a flat wall 32 intended to serve as a bearing surface on the ground.
  • the fold line extending at the junction of the walls 30 and 32 has been referenced 33.
  • the dihedral having the fold line 33 at the top and delimited by the planes of the walls 30 and 32 has an angle at the top of 142 °.
  • the wall 30 widens away from the back 21 until it reaches a width approximately twice that of the back 21 at the fold line 33.
  • the width of the wall 32 is constant. The latter rests, by its face opposite to that coming to bear on the ground, against the edge of the wings 20.
  • the free edges 23 of the wings 20 are curved outwards as shown more particularly on the cross sections of Figures 27 and 28, for the purpose of stiffening the profile.
  • the cross section of the support leg 2 is generally constant from the foot 3 to about half the height of the support leg 2, where the width of the wings 20 increases and becomes maximum at the level of a bore. 24 serving for the passage of the pivot 28 of articulation of the lifting arm 4.
  • the width of the wings 20 then decreases up to the height of the upper longitudinal ends 26 of the recesses 22, where the wings 20 form notches 211.
  • the back 21 is interrupts at the height of these notches 211.
  • the width of the wings 20 increases above the notches 211 in the direction of the upper end of the support leg 2, situated opposite the foot 3, up to recesses 25 formed on the wings 20, serving as articulation bearings around the axis Z to the nut-forming part 8.
  • curvilinear lights 27 On the portion of the wings 20 extending between the upper ends 26 of the oblong recesses 22 and the plane containing the axis Z and perpendicular to the axis longitudinal G, are formed curvilinear lights 27. The latter participate in the retention of the part forming a nut in the recesses 25.
  • the back 21 forms, at the height of the holes 24, a dihedral projecting outwards, of angle at the top 152 °.
  • edges 23 extend rectilinearly, parallel to the recesses 22, from their lower end in abutment against the wall 32 to the plane containing the axis Z and perpendicular to the axis G.
  • the edges 23 extend beyond this plane, according to arcs of a circle 230 and end in rectilinear portions 231 perpendicular to the axis G.
  • the recesses 25 have, as shown in FIG. 24, edges in the shape of a semicircle 250, centered on the axis Z and of radius adapted to that of the cylindrical surfaces 82. These semicircular edges 250 are extended below by rectilinear edges 251 perpendicular to the longitudinal axis G, and above, by rectilinear edges 252 extending parallel to the edges 251 but over a distance corresponding to about a quarter of the length of the rectilinear edges 25l.
  • the edges 250, 251 and 252 are curved towards the interior space situated between the wings 20 to form bearing surfaces 253 coming into contact with the cylindrical surfaces 82 of the nut-forming part 8. These bearing surfaces 253 are of generatrix parallel to the Z axis.
  • the recesses 25 define grooves whose the bottom is formed by the semicircular edges 250 and whose opening width, that is to say the distance separating the straight edges 251 and 252, is at least equal to the diameter of the semicircular edges 250.
  • Each curvilinear lumen 27 extends along a median line K in an arc of a circle situated at the same distance from the axis Z as the distance separating the latter and the axis T of the bores 85, and has at its longitudinal ends half edges -circulars 270 and 271.
  • the dihedral having the Z axis at its apex, delimited by the planes containing the axes of the semicircular edges 270 and 271, has an angle at the apex 115 °.
  • the plane containing the axis Z and the axis of the semi-circular holes 270 extends parallel to the straight edges 251.
  • the mounting of the nut forming part 8 on the support leg 2 is easily carried out, by engaging the nut forming part 8 provided with the control screw 6 in the recesses 25, until the cylindrical surfaces 82 stop against the edges. semicircular 250.
  • the introduction of the nut forming part 8 can be carried out by a simple translational movement in a direction perpendicular to the axis Z and is suitable for mechanized execution.
  • the holes 85 of the tabs 84 of the piece forming the nut 8 are then positioned opposite the curved lights 27.
  • a rivet 89 is introduced into the curved lights 27 and the holes 85 for retaining the piece forming the nut 8 on the support leg 2 After the riveting operation, the rivet 89 comes to bear axially at its axial ends on the external surface 200 of the wings 20 bordering the curvilinear openings 27.
  • the operation of the jack 1 is as follows.
  • the lifting arm 4 folds down between the wings 20 of the support leg 2, the head coming into abutment by the stop surfaces 520 on the curved edges 23.
  • the end edge 63 of the control screw 6 rests on the end of the cylindrical surface 55 adjacent to the finger 53, as shown more particularly in Figure 23.
  • the handle 7 can advantageously fold back against the external surface of a wing 20 as shown in FIG. 21.
  • the rivet 89 abuts against the semi-circular edges 271.
  • the user turns the handle 7 and rotates the control screw 6 around the axis W.
  • the longitudinal movement of the control screw 6 which results from its rotation in the internal thread 81 causes the lifting arm 4 to pivot clockwise in FIG. 1 and the upward movement of the head 5.
  • the rotation of the lifting arm 4 is accompanied by a displacement of the rivet 89 in the curved slots 27 until the latter stops against the semi-circular edges 270.
  • the jack 1 is then in its maximum lifting position and the control screw is subjected to tensile forces when the jack is loaded.
  • the surfaces 540 and 541 are normally oriented vertically in the lifting position of the vehicle, as shown in FIG.
  • the user turns the control screw 6.
  • the control screw 6 works in traction and the ball bearing 62 is axially stressed in compression.
  • the control screw 6 axially abuts by the end edge 63 against the surface 55 of the head 5. This ensures the drive of the lifting arm 4 without using a stop sleeve engaged on the control screw as is the case with known cries.
  • a jack according to the invention has a space requirement in the folded position that is sufficiently small for its housing in a spare wheel rim, in particular thanks to the particular arrangement of the control screw 6 on the jack 1.
  • the assembly of the jack is easy to perform and can be executed by a robot.
  • the positioning of the axes of rotation X, Y and Z, in particular the intersection of the axes W and Y is advantageous from the kinematic point of view.
  • the rivet 89 increases the safety of use of the jack by preventing the wings of the support leg 2 from moving apart. A stop sleeve is not necessary and the free rotation of the head to on the lifting arm 4 reduces the risk of damage to the vehicle body in the event of improper positioning of the jack.

Abstract

The lift jack (1) has a strut (2) and a lever arm (4) mounted for pivoting on the strut when actuated by a screw rod (6), turning in a nut (8), articulated in cut outs (25) in the strut. The nut is held on the strut by engagement of a retainer (89) fixed to the nut. This is done using at least one curvilinear aperture (27) formed in the strut and centred on the axis of articulation of the nut on the strut. Each cut out in the strut can be formed as a groove with its base formed by a semi-circular face.

Description

La présente invention concerne un cric de véhicule comprenant une jambe d'appui et un bras de levage monté à pivotement sur la jambe d'appui, à déplacer au moyen d'une vis de commande pour soulever le véhicule.The present invention relates to a vehicle jack comprising a support leg and a lifting arm pivotally mounted on the support leg, to be moved by means of a control screw to lift the vehicle.

Des cries de ce type, communément appelés "cries Y", sont décrits par exemple dans les demandes de brevet EP-0 320 613, EP-0 565 801, GB-2 176 458 et FR-2 663 015. Dans ces cries connus, la vis de commande tourne dans une pièce formant écrou reçue de manière pivotante dans des évidements de la jambe d'appui.Cree of this type, commonly known as "Cree Y", are described for example in patent applications EP-0 320 613, EP-0 565 801, GB-2 176 458 and FR-2 663 015. In these known cries , the control screw rotates in a part forming a nut pivotally received in recesses in the support leg.

Un objet de la présente invention est de proposer un cric du type précité, de montage simplifié et exécutable par un robot.An object of the present invention is to provide a jack of the aforementioned type, of simplified mounting and executable by a robot.

Elle y parvient par le fait que la pièce formant écrou est retenue sur la jambe d'appui par engagement d'un élément de retenue, solidaire de la pièce formant écrou, dans au moins une lumière curviligne ménagée sur la jambe d'appui et centrée sur l'axe d'articulation de la pièce formant écrou.It achieves this by the fact that the piece forming a nut is retained on the support leg by engagement of a retaining element, integral with the piece forming a nut, in at least one curvilinear opening formed on the support leg and centered on the articulation axis of the nut-forming part.

Avantageusement, chaque évidement de la jambe d'appui recevant la pièce formant écrou constitue une gorge dont le fond est délimité par un bord demi-circulaire et dont la largeur d'ouverture est supérieure ou égale au diamètre dudit bord demi-circulaire.Advantageously, each recess in the support leg receiving the piece forming a nut constitutes a groove the bottom of which is delimited by a semi-circular edge and the opening width of which is greater than or equal to the diameter of said semi-circular edge.

Avantageusement, la jambe d'appui a la forme générale d'un profilé de section transversale en U, et ledit élément de retenue est un rivet traversant la pièce formant écrou et prenant axialement appui sur les faces externes des deux ailes du profilé.Advantageously, the support leg has the general shape of a profile of U-shaped cross section, and said retaining element is a rivet passing through the piece forming a nut and axially bearing on the external faces of the two wings of the profile.

Avantageusement, la paroi des ailes dudit profilé bordant lesdits évidements est recourbée pour augmenter la surface de portée au contact de la pièce formant écrou.Advantageously, the wall of the wings of said profile bordering said recesses is curved to increase the bearing surface in contact with the part forming a nut.

Avantageusement, le cric comporte une tête de cric disposée dans l'alignement de la vis de commande de sorte que cette dernière est en appui axialement sur la tête du cric au moins lors du fonctionnement du cric lorsque ce dernier travaille à vide et que la vis de commande est actionnée dans le sens tendant à replier le cric.Advantageously, the jack comprises a jack head arranged in alignment with the control screw so that the latter is in axial support on the head of the jack at least during the operation of the jack when the latter is working empty and the screw control is actuated in the direction tending to fold the jack.

Avantageusement, la vis de commande présente une tête épaulée reposant axialement contre une butée à billes au moins lors du fonctionnement du cric lorsque ce dernier est en charge.Advantageously, the control screw has a stepped head resting axially against a thrust ball bearing at least during the operation of the jack when the latter is loaded.

Avantageusement; cette butée à billes est logée dans une chape articulée sur le bras de levage autour du même axe de rotation que la tête de cric.Advantageously; this thrust ball bearing is housed in a yoke articulated on the lifting arm around the same axis of rotation as the jack head.

Avantageusement, la tête de cric est articulée sur le bras de levage autour d'un axe de rotation coupant perpendiculairement l'axe longitudinal de la vis de commande.Advantageously, the jack head is articulated on the lifting arm around an axis of rotation perpendicularly cutting the longitudinal axis of the control screw.

D'autres caractéristiques et avantages de la présente invention apparaîtront à la lecture de la description détaillée qui va suivre, d'un exemple de réalisation non limitatif de l'invention, et à l'examen du dessin annexé sur lequel :

  • la figure 1 est une vue de côté d'un cric conforme à l'invention, en position déployée de levage d'un véhicule,
  • la figure 2 est une coupe schématique dans un plan contenant l'axe de rotation de la vis de commande, montrant certains éléments constitutifs du cric représenté sur la figure 1,
  • la figure 3 est une vue de côté de la tête du cric représenté sur la figure 1,
  • la figure 4 est une vue frontale de la tête représentée sur la figure 3,
  • la figure 5 est une vue de dessus de la tête représentée sur la figure 3,
  • la figure 6 est une vue frontale de la chape du cric représenté sur la figure 1,
  • la figure 7 est une vue de dessus de la chape représentée sur la figure 6,
  • la figure 8 est une vue de côté de la chape représentée sur la figure 6,
  • la figure 9 est une vue de côté du bras de levage du cric représenté sur la figure 1,
  • la figure 10 est une vue de dessus du bras de levage représenté sur la figure 9,
  • la figure 11 est une section selon le trait de coupe XI de la figure 9,
  • la figure 12 est une section selon le trait de coupe XII de la figure 9,
  • la figure 13 est une section selon le trait de coupe XIII de la figure 9,
  • la figure 14 montre, à plat, une extrémité de la tôle servant à réaliser le bras de levage,
  • la figure 15 est une vue de côté de la pièce formant écrou du cric représenté sur la figure 1,
  • la figure 16 est une vue de dessus de la pièce formant écrou représentée sur la figure 15,
  • la figure 17 est une section selon le trait de coupe XVII de la figure 16,
  • la figure 18 est une section selon le trait de coupe XVIII de la figure 16,
  • la figure 19 est une vue frontale de la pièce formant écrou représentée sur la figure 15,
  • la figure 20 montre, en vue de côté, le cric représenté sur la figure 1 en position repliée,
  • la figure 21 est une vue de dessus du cric représenté sur la figure 20,
  • la figure 22 montre, à échelle agrandie, la tête du cric lorsque ce dernier est en position déployée,
  • la figure 23 montre, à échelle agrandie, la tête du cric lorsque ce dernier est en position repliée,
  • la figure 24 est une vue de côté de la jambe d'appui du cric représenté sur la figure 1,
  • la figure 25 est une vue frontale de la jambe d'appui représentée sur la figure 24,
  • la figure 26 est une vue de dessus de la jambe d'appui représentée sur la figure 24,
  • la figure 27 est une section selon le trait de coupe XXVII de la figure 24,
  • la figure 28 est une section selon le trait de coupe XXVIII de la figure 24,
  • la figure 29 montre, à plat, une extrémité de la tôle servant à réaliser la jambe d'appui.
Other characteristics and advantages of the present invention will appear on reading the detailed description which follows, of a non-limiting exemplary embodiment of the invention, and on examining the appended drawing in which:
  • FIG. 1 is a side view of a jack according to the invention, in the deployed position for lifting a vehicle,
  • FIG. 2 is a diagrammatic section in a plane containing the axis of rotation of the control screw, showing certain elements constituting the jack shown in FIG. 1,
  • FIG. 3 is a side view of the head of the jack shown in FIG. 1,
  • FIG. 4 is a front view of the head shown in FIG. 3,
  • FIG. 5 is a top view of the head shown in FIG. 3,
  • FIG. 6 is a front view of the clevis of the jack shown in FIG. 1,
  • FIG. 7 is a top view of the yoke shown in FIG. 6,
  • FIG. 8 is a side view of the yoke shown in FIG. 6,
  • FIG. 9 is a side view of the jack lifting arm shown in FIG. 1,
  • FIG. 10 is a top view of the lifting arm shown in FIG. 9,
  • FIG. 11 is a section along the section line XI of FIG. 9,
  • FIG. 12 is a section along the section line XII in FIG. 9,
  • FIG. 13 is a section along the section line XIII in FIG. 9,
  • FIG. 14 shows, flat, one end of the sheet used to make the lifting arm,
  • FIG. 15 is a side view of the part forming the jack nut shown in FIG. 1,
  • FIG. 16 is a top view of the part forming a nut shown in FIG. 15,
  • FIG. 17 is a section along the section line XVII of FIG. 16,
  • FIG. 18 is a section along the section line XVIII in FIG. 16,
  • FIG. 19 is a front view of the nut-forming part shown in FIG. 15,
  • FIG. 20 shows, in side view, the jack shown in FIG. 1 in the folded position,
  • FIG. 21 is a top view of the jack shown in FIG. 20,
  • FIG. 22 shows, on an enlarged scale, the head of the jack when the latter is in the deployed position,
  • FIG. 23 shows, on an enlarged scale, the head of the jack when the latter is in the folded position,
  • FIG. 24 is a side view of the support leg of the jack shown in FIG. 1,
  • FIG. 25 is a front view of the support leg shown in FIG. 24,
  • FIG. 26 is a top view of the support leg shown in FIG. 24,
  • FIG. 27 is a section along the section line XXVII of FIG. 24,
  • FIG. 28 is a section along the section line XXVIII of FIG. 24,
  • Figure 29 shows, flat, one end of the sheet used to make the support leg.

Le cric 1 représenté sur les figures comporte une jambe d'appui 2 destinée à reposer, par une extrémité inférieure formant pied 3, sur le sol. Un bras de levage 4 s'articule à une extrémité sur cette jambe d'appui 2, et supporte à l'autre extrémité une tête 5 destinée à venir au contact du véhicule à soulever. Une vis de commande 6, sur laquelle s'articule à une extrémité une poignée d'entraînement 7, permet de déplacer le bras de levage 4 pour lever ou descendre la tête 5.The jack 1 shown in the figures comprises a support leg 2 intended to rest, by a lower end forming a foot 3, on the ground. A lifting arm 4 is articulated at one end on this support leg 2, and supports at the other end a head 5 intended to come into contact with the vehicle to be lifted. A control screw 6, on which a drive handle 7 is articulated at one end, makes it possible to move the lifting arm 4 to raise or lower the head 5.

Le bras de levage 4 s'articule sur la jambe d'appui 2 autour d'un axe de rotation X perpendiculaire au plan de la figure 1. La tête 5 du cric 1 s'articule sur le bras de levage 4 autour d'un axe de rotation Y parallèle à l'axe X. La vis de commande 6 s'étend selon un axe longitudinal W parallèle au plan de la figure 1, coupant perpendiculairement l'axe X. Elle traverse une pièce formant écrou 8 s'articulant sur la jambe d'appui 2 autour d'un axe de rotation Z coupant l'axe W et parallèle à l'axe X. Le cric 1 est symétrique par rapport à un plan de symétrie contenant l'axe W et perpendiculaire à l'axe X.The lifting arm 4 is articulated on the supporting leg 2 around an axis of rotation X perpendicular to the plane of FIG. 1. The head 5 of the jack 1 is articulated on the lifting arm 4 around a axis of rotation Y parallel to the axis X. The control screw 6 extends along a longitudinal axis W parallel to the plane of FIG. 1, intersecting the axis X perpendicularly. It passes through a piece forming a nut 8 hinged on the supporting leg 2 around an axis of rotation Z intersecting the axis W and parallel to the axis X. The jack 1 is symmetrical with respect to a plane of symmetry containing the axis W and perpendicular to the axis X.

La tête 5 du cric 1 est représentée isolément sur les figures 3 à 5. Elle est de préférence réalisée en matière plastique, et comporte un corps 50 traversé par un perçage 51 cylindrique de révolution autour de l'axe Y, pour le passage d'un tourillon d'articulation 98 de la tête 5 sur le bras de levage 4. Deux doigts 52, 53 prolongent supérieurement le corps 50 (lorsque le cric est en position déployée de levage d'un véhicule comme représenté sur la figure 1) et définissent entre eux une gorge 54, s'ouvrant vers le haut, pour l'engagement de la tête 5 sur un cordon de soudure ou une feuillure de la caisse du véhicule, formant saillie vers le bas, ou sur toute autre partie du véhicule prévue à cet effet. Les surfaces 540, 541 respectives des doigts 52, 53, se faisant face, sont planes et parallèles. La tête 5 comporte des surfaces d'arrêt 520, dont le rôle sera précisé dans la suite, situées à la base du doigt 52 et s'étendant, planes, en formant un angle de 44°30' avec le plan des surfaces 540 et 541. On a référencé 521 les extrémités inférieures de ces surfaces d'arrêt 520. Le corps 50 présente également une surface 55, cylindrique de révolution autour de l'axe Y, s'étendant sur un secteur angulaire de 60°.The head 5 of the jack 1 is shown in isolation in Figures 3 to 5. It is preferably made of plastic, and comprises a body 50 crossed by a cylindrical bore 51 of revolution about the Y axis, for the passage of a hinge pin 98 of the head 5 on the lifting arm 4. Two fingers 52, 53 extend the body 50 superiorly (when the jack is in the deployed lifting position of a vehicle as shown in FIG. 1) and define between them a groove 54, opening upwards, for the engagement of the head 5 on a weld bead or a rebate of the body of the vehicle, projecting downwards, or on any other part of the vehicle provided for this purpose. The respective surfaces 540, 541 of the fingers 52, 53, facing each other, are plane and parallel. The head 5 has stop surfaces 520, the role of which will be explained below, located at the base of the finger 52 and extending, planar, forming an angle of 44 ° 30 'with the plane of the surfaces 540 and 541. The lower ends of these stop surfaces 520 have been referenced 521. The body 50 also has a surface 55, cylindrical of revolution around the axis Y, extending over an angular sector of 60 °.

La vis de commande 6 présente un filetage hélicoïdal 60 s'étendant selon l'axe W, engagé dans la pièce formant écrou 8, et comporte à une extrémité axiale une tête épaulée 61. Elle est munie à l'extrémité axiale opposée d'un embout 66 sur lequel s'articule la poignée 7, autour d'un axe de rotation coupant perpendiculairement l'axe W.The control screw 6 has a helical thread 60 extending along the axis W, engaged in the part forming the nut 8, and comprises at one axial end a shouldered head 61. It is provided at the opposite axial end with a tip 66 on which the handle 7 is articulated, about an axis of rotation perpendicularly cutting the axis W.

La tête épaulée 61 repose par sa tranche d'extrémité axiale 63 contre la surface 55 de la tête à et par son épaulement, référencé 64, sur une butée à billes 62 en appui sur une chape 9. Cette butée à billes 62 comporte, de façon connue en soi, deux bagues 62a, 62b d'axe W, définissant des chemins de roulement pour des billes 62c interposées entre les bagues 62a, 62b.The shouldered head 61 rests by its axial end edge 63 against the surface 55 of the head with and by its shoulder, referenced 64, on a ball stop 62 bearing on a yoke 9. This ball stop 62 comprises, in a manner known per se, two rings 62a, 62b of axis W, defining raceways for balls 62c interposed between the rings 62a, 62b.

La chape 9 est représentée isolément sur les figures 6 à 8. Elle comporte deux flasques 90, plans et parallèles entre eux, réunis par une base 91. Cette dernière s'étend perpendiculairement au plan des flasques 90. Des perçages 92 d'axe Y sont ménagés sur les flasques 90 pour le passage du tourillon d'articulation 98 précité, et le montage à rotation de la chape 9 sur le bras de levage 4 autour de l'axe Y. La base 91 est traversée par un perçage 93 pour le passage de la vis de commande 6. La bague 62b de la butée à billes 62 repose contre la face 910 de la base 91 tournée vers l'espace intérieur aux flasques 90. Ces derniers sont ajourés en 94 comme représenté sur la figure 8 pour réaliser un gain de matière. Ils présentent, observés dans la direction de l'axe Y, un contour généralement triangulaire, délimité latéralement par deux bords rectilignes 95 convergeant en rapprochement de l'axe Y, ces bords 95 étant réunis à leur extrémité opposée à la base 91 par un bord 96 en arc de cercle, centré sur l'axe Y, et se raccordant à la base 91 par des bords rectilignes 97, parallèles à l'axe W.The yoke 9 is shown in isolation in Figures 6 to 8. It has two flanges 90, planes and parallel to each other, joined by a base 91. The latter extends perpendicular to the plane of the flanges 90. Holes 92 of axis Y are provided on the flanges 90 for the passage of the aforementioned articulation pin 98, and the rotational mounting of the yoke 9 on the lifting arm 4 around the axis Y. The base 91 is crossed by a bore 93 for the passage of the control screw 6. The ring 62b of the ball bearing 62 rests against the face 910 of the base 91 facing towards the interior of the flanges 90. The latter are perforated at 94 as shown in FIG. 8 to make saving material. They have, observed in the direction of the Y axis, a generally triangular contour, delimited laterally by two rectilinear edges 95 converging in proximity to the Y axis, these edges 95 being joined at their end opposite to base 91 by an edge 96 in an arc, centered on the axis Y, and connecting to base 91 by rectilinear edges 97, parallel to axis W.

On a représenté isolément sur les figures 9 à 14 le bras de levage 4. Ce dernier est réalisé de préférence par emboutissage, découpage et pliage d'une tôle pour former un profilé métallique allongé dans la direction d'un axe longitudinal V perpendiculaire aux axes X et Y. Ce profilé présente une section transversale ayant la forme générale d'un U, comme représenté plus particulièrement sur les figures 11 à 13. Il comporte deux ailes 40 réunies par un dos 41 s'étendant généralement perpendiculairement aux ailes 40. Des renfoncements oblongs 42 venus d'emboutissage s'étendent parallèlement à l'axe V sur les ailes 40 pour rigidifier le profilé. Ces renfoncements 42 forment saillie dans l'espace intérieur du profilé situé entre les ailes 40. Un renfoncement oblong 43, formant saillie vers l'intérieur, est réalisé sur le dos 41 dans le même but. Les ailes 40 sont percées à une extrémité longitudinale, en 44, pour le passage du tourillon 98 précité et l'assemblage en rotation de la tête 5, de la chape 9 et du bras de levage 4. Ces perçages 44 sont réalisés à une extrémité longitudinale des renfoncements 42. Les ailes 40 sont percées à l'extrémité longitudinale opposée, en 46, pour le passage d'un tourillon 28 d'axe X servant à l'articulation du bras de levage 4 sur la jambe d'appui 2. Ces perçages 46 sont réalisés sur des emboutis circulaires 47 formant saillie vers l'extérieur du profilé, comme montré plus particulièrement sur la figure 12. Ces emboutis circulaires 47 se situent dans le prolongement des renfoncements 42, ménageant un intervalle 470 avec ces derniers comme montré sur la figure 9. Le dos 41 est prolongé, à l'extrémité du bras de levage 4 articulée sur la jambe d'appui 2, par une paroi 48 s'étendant obliquement entre les ailes 40 et formant entretoise. La paroi 48 résulte d'un découpage et d'un pliage de la tôle utilisée pour réaliser le profilé, comme illustré sur la figure 14. Les extrémités longitudinales des ailes 40 présentent à l'extrémité s'articulant sur la jambe d'appui 2 un profil généralement triangulaire, observé dans la direction de l'axe X. Ce profil est délimité par deux bords rectilignes orthogonaux 401, 402 réunis par un bord en arc de cercle 403 centré sur l'axe X. Après pliage, la paroi 48 s'étend dans le plan des bords 401 et forme avec le dos 41 un dièdre d'angle au sommet 238°.The lifting arm 4 is shown in isolation in FIGS. 9 to 14. The latter is preferably produced by stamping, cutting and bending a sheet to form a metal section elongated in the direction of a longitudinal axis V perpendicular to the axes. X and Y. This profile has a cross section having the general shape of a U, as shown more particularly in Figures 11 to 13. It comprises two wings 40 joined by a back 41 extending generally perpendicular to the wings 40. Des oblong recesses 42 from stamping extend parallel to the axis V on the wings 40 to stiffen the profile. These recesses 42 protrude into the interior space of the profile located between the wings 40. An oblong recess 43, projecting inward, is made on the back 41 for the same purpose. The wings 40 are pierced at a longitudinal end, at 44, for the passage of the aforementioned pin 98 and the rotational assembly of the head 5, the yoke 9 and the lifting arm 4. These holes 44 are made at one end longitudinal of the recesses 42. The wings 40 are pierced at the opposite longitudinal end, at 46, for the passage of a pin 28 of axis X serving for the articulation of the lifting arm 4 on the support leg 2. These holes 46 are made on circular stampings 47 projecting towards the outside of the profile, as shown more particularly in FIG. 12. These circular stampings 47 are located in the extension of the recesses 42, leaving a gap 470 with the latter as shown in Figure 9. The back 41 is extended, at the end of the lifting arm 4 articulated on the support leg 2, by a wall 48 extending obliquely between the wings 40 and forming a spacer. The wall 48 results from a cutting and a folding of the sheet metal used to produce the profile, as illustrated in FIG. 14. The longitudinal ends of the wings 40 have at the end articulated on the support leg 2 a generally triangular profile, observed in the direction of the X axis. This profile is delimited by two orthogonal rectilinear edges 401, 402 joined by an edge in an arc of a circle 403 centered on the X axis. After folding, the wall 48 s 'extends in the plane of the edges 401 and forms with the back 41 a corner dihedral at the top 238 °.

On a représenté isolément sur les figures 15 à 19 la pièce formant écrou 8. Cette dernière est réalisée, de préférence, en matière plastique. Elle comporte un corps 80 traversé selon l'axe W par un taraudage 81 adapté à recevoir le corps fileté 60 de la vis de commande 6. Des parties latérales 82 forment saillie de part et d'autre du corps 80 pour l'articulation de la pièce formant écrou 8 sur la jambe d'appui 2. Ces parties latérales 82 sont délimitées radialement, à l'extérieur, par des surfaces cylindriques de révolution autour de l'axe Z, et axialement par des tranches d'extrémité 83 planes et perpendiculaires à l'axe Z. La pièce formant écrou 8 comporte également deux pattes 84 traversées par des perçages 85 d'axe T parallèle à l'axe Z, pour le montage de moyens de retenue de la pièce formant écrou 8 sur la jambe d'appui 2, comme cela sera précisé plus loin. Les pattes 84 se raccordent sur le corps 80 en ménageant avec les surfaces cylindriques 82 des gorges annulaires 86 centrées sur l'axe Z. Le dièdre de sommet l'axe Z, délimité par le plan perpendiculaire à l'axe W et par le plan contenant l'axe T, est d'angle au sommet 60°.The nut forming part 8 is shown in isolation in FIGS. 15 to 19. The latter is preferably made of plastic. It comprises a body 80 traversed along the axis W by a tapping 81 adapted to receive the threaded body 60 of the control screw 6. Lateral parts 82 form protrusions on either side of the body 80 for the articulation of the piece forming a nut 8 on the support leg 2. These lateral parts 82 are delimited radially, on the outside, by cylindrical surfaces of revolution around the axis Z, and axially by end sections 83 which are planar and perpendicular to the axis Z. The piece forming a nut 8 also comprises two tabs 84 crossed by bores 85 of axis T parallel to the axis Z, for mounting means for retaining the piece forming a nut 8 on the leg of support 2, as will be explained below. The lugs 84 are connected to the body 80 by providing annular grooves 86 centered on the Z axis with the cylindrical surfaces 82. The dihedral from the top of the Z axis, delimited by the plane perpendicular to the W axis and by the plane containing the axis T, has an angle at the top 60 °.

On a représenté isolément sur les figures 24 à 29 la jambe d'appui 2. Cette dernière est réalisée de préférence par emboutissage, découpage et pliage d'une tôle pour former un profilé allongé selon un axe longitudinal G perpendiculaire à l'axe Z. Ce profilé présente une section transversale ayant la forme générale d'un U, comportant deux ailes 20 réunies par un dos 21. Chaque aile 20 présente un renfoncement oblong 22 venu d'emboutissage, formant saillie dans l'espace intérieur du profilé situé entre les ailes 20, et destiné à rigidifier le profilé.FIG. 24 to 29 shows the support leg 2 in isolation. The latter is preferably produced by stamping, cutting and bending a sheet to form an elongated section along a longitudinal axis G perpendicular to the axis Z. This profile has a cross section having the general shape of a U, comprising two wings 20 joined by a back 21. Each wing 20 has an oblong recess 22 coming from stamping, projecting into the interior space of the profile located between the wings 20, and intended to stiffen the profile.

Le pied 3 est formé par découpage et pliage comme illustré sur la figure 29. Plus précisément, le pied 3 comporte une première paroi plane 30 se raccordant au dos 21 par une ligne de pliage 31 et formant, en position assemblée du cric, un angle de 43° avec le dos 21 comme représenté sur la figure 24. Cette paroi 30 est prolongée vers le bas par une paroi plane 32 destinée à servir de surface d'appui sur le sol. On a référencé 33 la ligne de pliage s'étendant à la jonction des parois 30 et 32. Le dièdre ayant pour sommet la ligne de pliage 33 et délimité par les plans des parois 30 et 32 a un angle au sommet de 142°. La paroi 30 s'élargit en éloignement du dos 21 jusqu'à atteindre une largeur environ double de celle du dos 21 au niveau de la ligne de pliage 33. La largeur de la paroi 32 est constante. Cette dernière repose, par sa face opposée à celle venant en appui sur le sol, contre la tranche des ailes 20.The foot 3 is formed by cutting and folding as illustrated in FIG. 29. More specifically, the foot 3 has a first planar wall 30 connected to the back 21 by a fold line 31 and forming, in the assembled position of the jack, an angle 43 ° with the back 21 as shown in Figure 24. This wall 30 is extended downwards by a flat wall 32 intended to serve as a bearing surface on the ground. The fold line extending at the junction of the walls 30 and 32 has been referenced 33. The dihedral having the fold line 33 at the top and delimited by the planes of the walls 30 and 32 has an angle at the top of 142 °. The wall 30 widens away from the back 21 until it reaches a width approximately twice that of the back 21 at the fold line 33. The width of the wall 32 is constant. The latter rests, by its face opposite to that coming to bear on the ground, against the edge of the wings 20.

Les bords libres 23 des ailes 20 sont recourbés vers l'extérieur comme représenté plus particulièrement sur les sections transversales des figures 27 et 28, à des fins de rigidification du profilé. La section transversale de la jambe d'appui 2 est généralement constante depuis le pied 3 jusqu'à la moitié environ de la hauteur de la jambe d'appui 2, où la largeur des ailes 20 augmente et devient maximum à hauteur d'un perçage 24 servant au passage du tourillon 28 d'articulation du bras de levage 4. La largeur des ailes 20 décroît ensuite jusqu'à hauteur des extrémités longitudinales supérieures 26 des renfoncements 22, où les ailes 20 forment des encoches 211. Le dos 21 s'interrompt à hauteur de ces encoches 211. La largeur des ailes 20 augmente au-dessus des encoches 211 en direction de l'extrémité supérieure de la jambe d'appui 2, située à l'opposé du pied 3, jusqu'à des évidements 25 ménagés sur les ailes 20, servant de paliers d'articulation autour de l'axe Z à la pièce formant écrou 8. Sur la portion des ailes 20 s'étendant entre les extrémités supérieures 26 des renfoncements oblongs 22 et le plan contenant l'axe Z et perpendiculaire à l'axe longitudinal G, sont ménagées des lumières curvilignes 27. Ces dernières participent à la retenue de la pièce formant écrou dans les évidements 25. Le dos 21 forme, à hauteur des perçages 24, un dièdre saillant vers l'extérieur, d'angle au sommet 152°. Les bords 23 s'étendent rectilignement, parallèlement aux renfoncements 22, depuis leur extrémité inférieure en appui contre la paroi 32 jusqu'au plan contenant l'axe Z et perpendiculaire à l'axe G. Les bords 23 se prolongent, au-delà de ce plan, selon des arcs de cercle 230 et se terminent par des portions rectilignes 231 perpendiculaires à l'axe G.The free edges 23 of the wings 20 are curved outwards as shown more particularly on the cross sections of Figures 27 and 28, for the purpose of stiffening the profile. The cross section of the support leg 2 is generally constant from the foot 3 to about half the height of the support leg 2, where the width of the wings 20 increases and becomes maximum at the level of a bore. 24 serving for the passage of the pivot 28 of articulation of the lifting arm 4. The width of the wings 20 then decreases up to the height of the upper longitudinal ends 26 of the recesses 22, where the wings 20 form notches 211. The back 21 is interrupts at the height of these notches 211. The width of the wings 20 increases above the notches 211 in the direction of the upper end of the support leg 2, situated opposite the foot 3, up to recesses 25 formed on the wings 20, serving as articulation bearings around the axis Z to the nut-forming part 8. On the portion of the wings 20 extending between the upper ends 26 of the oblong recesses 22 and the plane containing the axis Z and perpendicular to the axis longitudinal G, are formed curvilinear lights 27. The latter participate in the retention of the part forming a nut in the recesses 25. The back 21 forms, at the height of the holes 24, a dihedral projecting outwards, of angle at the top 152 °. The edges 23 extend rectilinearly, parallel to the recesses 22, from their lower end in abutment against the wall 32 to the plane containing the axis Z and perpendicular to the axis G. The edges 23 extend beyond this plane, according to arcs of a circle 230 and end in rectilinear portions 231 perpendicular to the axis G.

Les évidements 25 présentent, comme représenté sur la figure 24, des bords en forme de demi-cercle 250, centrés sur l'axe Z et de rayon adapté à celui des surfaces cylindriques 82. Ces bords demi-circulaires 250 sont prolongés inférieurement par des bords rectilignes 251 perpendiculaires à l'axe longitudinal G, et supérieurement, par des bords rectilignes 252 s'étendant parallèlement aux bords 251 mais sur une distance correspondant à un quart environ de la longueur des bords rectilignes 25l. Les bords 250, 251 et 252 sont recourbés vers l'espace intérieur situé entre les ailes 20 pour former des surfaces de portée 253 venant au contact des surfaces cylindriques 82 de la pièce formant écrou 8. Ces surfaces de portée 253 sont de génératrice parallèle à l'axe Z. Les évidements 25 définissent des gorges dont le fond est constitué par les bords demi-circulaires 250 et dont la largeur d'ouverture, c'est-à-dire la distance séparant les bords rectilignes 251 et 252, est au moins égale au diamètre des bords demi-circulaires 250.The recesses 25 have, as shown in FIG. 24, edges in the shape of a semicircle 250, centered on the axis Z and of radius adapted to that of the cylindrical surfaces 82. These semicircular edges 250 are extended below by rectilinear edges 251 perpendicular to the longitudinal axis G, and above, by rectilinear edges 252 extending parallel to the edges 251 but over a distance corresponding to about a quarter of the length of the rectilinear edges 25l. The edges 250, 251 and 252 are curved towards the interior space situated between the wings 20 to form bearing surfaces 253 coming into contact with the cylindrical surfaces 82 of the nut-forming part 8. These bearing surfaces 253 are of generatrix parallel to the Z axis. The recesses 25 define grooves whose the bottom is formed by the semicircular edges 250 and whose opening width, that is to say the distance separating the straight edges 251 and 252, is at least equal to the diameter of the semicircular edges 250.

Chaque lumière curviligne 27 s'étend selon une ligne médiane K en arc de cercle située à la même distance de l'axe Z que la distance séparant ce dernier et l'axe T des perçages 85, et présente à ses extrémités longitudinales des bords demi-circulaires 270 et 271. Le dièdre ayant pour sommet l'axe Z, délimité par les plans contenant les axes des bords demi-circulaires 270 et 271, est d'angle au sommet 115°. Le plan contenant l'axe Z et l'axe des perçages demi-circulaires 270 s'étend parallèlement aux bords rectilignes 251.Each curvilinear lumen 27 extends along a median line K in an arc of a circle situated at the same distance from the axis Z as the distance separating the latter and the axis T of the bores 85, and has at its longitudinal ends half edges -circulars 270 and 271. The dihedral having the Z axis at its apex, delimited by the planes containing the axes of the semicircular edges 270 and 271, has an angle at the apex 115 °. The plane containing the axis Z and the axis of the semi-circular holes 270 extends parallel to the straight edges 251.

Le montage de la pièce formant écrou 8 sur la jambe d'appui 2 s'effectue aisément, en engageant la pièce formant écrou 8 munie de la vis de commande 6 dans les évidements 25, jusqu'à butée des surfaces cylindriques 82 contre les bords demi-circulaires 250. L'introduction de la pièce formant écrou 8 peut s'effectuer par un simple mouvement de translation dans une direction perpendiculaire à l'axe Z et convient à une exécution mécanisée. Les perçages 85 des pattes 84 de la pièce formant écrou 8 sont alors positionnés en regard des lumières curvilignes 27. Un rivet 89 est introduit dans les lumières curvilignes 27 et les perçages 85 pour retenir la pièce formant écrou 8 sur la jambe d'appui 2. Après l'opération de rivetage, le rivet 89 vient axialement en appui à ses extrémités axiales sur la surface externe 200 des ailes 20 bordant les lumières curvilignes 27. Le fonctionnement du cric 1 est le suivant.The mounting of the nut forming part 8 on the support leg 2 is easily carried out, by engaging the nut forming part 8 provided with the control screw 6 in the recesses 25, until the cylindrical surfaces 82 stop against the edges. semicircular 250. The introduction of the nut forming part 8 can be carried out by a simple translational movement in a direction perpendicular to the axis Z and is suitable for mechanized execution. The holes 85 of the tabs 84 of the piece forming the nut 8 are then positioned opposite the curved lights 27. A rivet 89 is introduced into the curved lights 27 and the holes 85 for retaining the piece forming the nut 8 on the support leg 2 After the riveting operation, the rivet 89 comes to bear axially at its axial ends on the external surface 200 of the wings 20 bordering the curvilinear openings 27. The operation of the jack 1 is as follows.

A l'état replié, comme montré sur les figures 20, 21 et 23, le bras de levage 4 se rabat entre les ailes 20 de la jambe d'appui 2, la tête à venant en butée par les surfaces d'arrêt 520 sur les bords recourbés 23. Dans la position repliée du cric 1, la tranche d'extrémité 63 de la vis de commande 6 repose sur l'extrémité de la surface cylindrique 55 adjacente au doigt 53, comme représenté plus particulièrement sur la figure 23. La poignée 7 peut avantageusement se rabattre contre la surface externe d'une aile 20 comme montré sur la figure 21. Le rivet 89 bute contre les bords demi-circulaires 271.In the folded state, as shown in FIGS. 20, 21 and 23, the lifting arm 4 folds down between the wings 20 of the support leg 2, the head coming into abutment by the stop surfaces 520 on the curved edges 23. In the folded position of the jack 1, the end edge 63 of the control screw 6 rests on the end of the cylindrical surface 55 adjacent to the finger 53, as shown more particularly in Figure 23. The handle 7 can advantageously fold back against the external surface of a wing 20 as shown in FIG. 21. The rivet 89 abuts against the semi-circular edges 271.

Pour déplier le cric 1, l'utilisateur tourne la poignée 7 et entraine en rotation la vis de commande 6 autour de l'axe W. Le déplacement longitudinal de la vis de commande 6 qui résulte de sa rotation dans le taraudage 81 provoque un pivotement du bras de levage 4 dans le sens horaire sur la figure 1 et le déplacement vers le haut de la tête 5. La rotation du bras de levage 4 s'accompagne d'un déplacement du rivet 89 dans les lumières curvilignes 27 jusqu'à butée de ce dernier contre les bords demi-circulaires 270. Le cric 1 est alors dans sa position de levage maximum et la vis de commande est soumise à des efforts de traction lorsque le cric est en charge. Les surfaces 540 et 541 sont normalement orientées verticalement en position de levage du véhicule, comme représenté sur la figure 1, et la surface frontale 63 de la butée à billes 62 est alors située à l'extrémité de la surface cylindrique 55 la plus éloignée des doigts 52 et 53. Toute rotation supplémentaire de la tête à dans le sens anti-horaire est empêchée par butée des extrémités inférieures 521 des surfaces d'arrêt 520 contre les tranches d'extrémité 201 des ailes 20, comme illustré sur la figure 22 plus particulièrement.To unfold the jack 1, the user turns the handle 7 and rotates the control screw 6 around the axis W. The longitudinal movement of the control screw 6 which results from its rotation in the internal thread 81 causes the lifting arm 4 to pivot clockwise in FIG. 1 and the upward movement of the head 5. The rotation of the lifting arm 4 is accompanied by a displacement of the rivet 89 in the curved slots 27 until the latter stops against the semi-circular edges 270. The jack 1 is then in its maximum lifting position and the control screw is subjected to tensile forces when the jack is loaded. The surfaces 540 and 541 are normally oriented vertically in the lifting position of the vehicle, as shown in FIG. 1, and the front surface 63 of the ball bearing 62 is then located at the end of the cylindrical surface 55 farthest from the fingers 52 and 53. Any further rotation of the head to counterclockwise is prevented by abutment of the lower ends 521 of the stop surfaces 520 against the end edges 201 of the wings 20, as illustrated in FIG. 22 more particularly.

Pour replier le cric 1, l'utilisateur tourne la vis de commande 6. Tant que le cric 1 soulève le véhicule, c'est-à-dire travaille en charge, la vis de commande 6 travaille en traction et la butée à billes 62 est sollicitée axialement en compression. Lorsque le cric a été suffisamment replié et ne soulève plus le véhicule, c'est-à-dire travaille à vide, la vis de commande 6 vient axialement en butée par la tranche d'extrémité 63 contre la surface 55 de la tête 5. On assure ainsi l'entraînement du bras de levage 4 sans utiliser de fourreau d'arrêt engagé sur la vis de commande comme c'est le cas sur les cries connus.To fold the jack 1, the user turns the control screw 6. As long as the jack 1 lifts the vehicle, that is to say it is working under load, the control screw 6 works in traction and the ball bearing 62 is axially stressed in compression. When the jack has been folded enough and no longer lifts the vehicle, that is to say when it is working when empty, the control screw 6 axially abuts by the end edge 63 against the surface 55 of the head 5. This ensures the drive of the lifting arm 4 without using a stop sleeve engaged on the control screw as is the case with known cries.

Finalement, un cric selon l'invention présente un encombrement en position repliée suffisamment faible pour son logement dans une jante de roue de secours, notamment grâce à l'agencement particulier de la vis de commande 6 sur le cric 1. L'assemblage du cric s'effectue aisément et peut être exécuté par un robot. Le positionnement des axes de rotation X, Y et Z, notamment l'intersection des axes W et Y est avantageux du point de vue cinématique. Le rivet 89 accroît la sécurité d'utilisation du cric en empêchant les ailes de la jambe d'appui 2 de s'écarter. Un fourreau d'arrêt n'est pas nécessaire et la libre rotation de la tête à sur le bras de levage 4 diminue le risque d'endommagement de la caisse du véhicule en cas de mauvais positionnement du cric.Finally, a jack according to the invention has a space requirement in the folded position that is sufficiently small for its housing in a spare wheel rim, in particular thanks to the particular arrangement of the control screw 6 on the jack 1. The assembly of the jack is easy to perform and can be executed by a robot. The positioning of the axes of rotation X, Y and Z, in particular the intersection of the axes W and Y is advantageous from the kinematic point of view. The rivet 89 increases the safety of use of the jack by preventing the wings of the support leg 2 from moving apart. A stop sleeve is not necessary and the free rotation of the head to on the lifting arm 4 reduces the risk of damage to the vehicle body in the event of improper positioning of the jack.

Claims (9)

Cric de véhicule (1) comprenant une jambe d'appui (2) et un bras de levage (4) monté à pivotement sur cette dernière, à déplacer au moyen d'une vis de commande (6) tournant dans une pièce formant écrou (8) reçue de manière articulée dans des évidements (25) de la jambe d'appui (2), caractérisé en ce que la pièce formant écrou (8) est retenue sur la jambe d'appui par engagement d'un élément de retenue (89), solidaire de la pièce formant écrou (8), dans au moins une lumière curviligne (27) ménagée sur la jambe d'appui (2) et centrée sur l'axe d'articulation (Z) de la pièce formant écrou (8) sur la jambe d'appui (2).Vehicle jack (1) comprising a support leg (2) and a lifting arm (4) pivotally mounted on the latter, to be moved by means of a control screw (6) rotating in a nut-forming part ( 8) received in an articulated manner in recesses (25) in the support leg (2), characterized in that the nut-forming part (8) is retained on the support leg by engagement of a retaining element ( 89), integral with the nut-forming part (8), in at least one curvilinear opening (27) formed on the support leg (2) and centered on the articulation axis (Z) of the nut-forming part ( 8) on the support leg (2). Cric selon la revendication 1, caractérisé en ce que chaque évidement (25) de la jambe d'appui (2) recevant la pièce formant écrou (8) constitue une gorge dont le fond est délimité par un bord demi-circulaire (250) et dont la largeur d'ouverture est supérieure ou égale au diamètre dudit bord demi-circulaire.Jack according to claim 1, characterized in that each recess (25) of the support leg (2) receiving the piece forming a nut (8) constitutes a groove the bottom of which is delimited by a semicircular edge (250) and whose opening width is greater than or equal to the diameter of said semicircular edge. Cric selon l'une des revendications 1 et 2, la jambe d'appui (2) ayant la forme générale d'un profilé de section transversale en U, caractérisé en ce que ledit élément de retenue est un rivet (89) prenant axialement appui sur les faces externes des deux ailes (20) du profilé.Jack according to one of claims 1 and 2, the support leg (2) having the general shape of a U-shaped cross section profile, characterized in that said retaining element is a rivet (89) axially supported on the external faces of the two wings (20) of the profile. Cric selon l'un des revendications 1 à 3, la jambe d'appui (2) ayant la forme générale d'un profilé de section transversale en U, caractérisé en ce que la paroi des ailes dudit profilé bordant lesdits évidements (25) est recourbée pour augmenter la surface de portée au contact de la pièce formant écrou (8).Jack according to one of claims 1 to 3, the support leg (2) having the general shape of a U-shaped cross section profile, characterized in that the wall of the wings of said profile bordering said recesses (25) is curved to increase the bearing surface in contact with the part forming a nut (8). Cric selon l'une des revendications 1 à 4, le cric comportant une tête de cric destinée à venir au contact du véhicule, caractérisé en ce que la tête de cric est disposée dans l'alignement de la vis de commande de sorte que cette dernière est axialement en appui sur la tête du cric au moins lors du fonctionnement du cric lorsque ce dernier travaille à vide et que la vis de commande est actionnée dans le sens tendant à replier le cric.Jack according to one of claims 1 to 4, the jack comprising a jack head intended to come into contact with the vehicle, characterized in that the jack head is arranged in alignment with the control screw so that the latter is axially supported on the head of the jack at least during the operation of the jack when the latter is working empty and the control screw is actuated in the direction tending to fold the jack. Cric selon la revendication 5, caractérisé en ce qu'il comporte une tête de cric (5) articulée sur le bras de levage (4) autour d'un axe de rotation (Y) coupant perpendiculairement l'axe longitudinal (W) de la vis de commande (6).Jack according to claim 5, characterized in that it comprises a jack head (5) articulated on the lifting arm (4) about an axis of rotation (Y) perpendicularly cutting the longitudinal axis (W) of the control screw (6). Cric selon l'une des revendications 1 à 6, caractérisé en ce que la vis de commande (6) présente une tête épaulée (61) reposant contre une butée à billes (62) au moins lors du fonctionnement du cric lorsque le cric est en charge.Jack according to one of claims 1 to 6, characterized in that the control screw (6) has a stepped head (61) resting against a ball bearing (62) at least when the jack is in operation when the jack is loaded. Cric selon la revendication 7, caractérisé en ce que la butée à billes (62) est logée dans une chape (9) articulée sur le bras de levage (4).Jack according to claim 7, characterized in that the ball stop (62) is housed in a yoke (9) articulated on the lifting arm (4). Cric selon la revendication 8, caractérisé en ce que la chape (9) est montée à rotation autour du même axe de rotation (Y) que la tête de cric (5).Jack according to claim 8, characterized in that the yoke (9) is rotatably mounted about the same axis of rotation (Y) as the jack head (5).
EP19960400669 1995-03-31 1996-03-28 Easy assembly vehicle jack Expired - Lifetime EP0734996B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9503832 1995-03-31
FR9503832A FR2732325B1 (en) 1995-03-31 1995-03-31 VEHICLE JACK WITH SIMPLIFIED ASSEMBLY

Publications (2)

Publication Number Publication Date
EP0734996A1 true EP0734996A1 (en) 1996-10-02
EP0734996B1 EP0734996B1 (en) 2000-05-31

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ID=9477634

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19960400669 Expired - Lifetime EP0734996B1 (en) 1995-03-31 1996-03-28 Easy assembly vehicle jack

Country Status (3)

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EP (1) EP0734996B1 (en)
DE (1) DE69608603D1 (en)
FR (1) FR2732325B1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0785166A3 (en) * 1996-01-22 1999-04-07 Batz, S. Coop. Jack for vehicles
WO2002036477A1 (en) * 2000-10-31 2002-05-10 Thyssenkrupp Bilstein Gmbh Displacement nut for a lifting device, and corresponding lifting device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2176458A (en) * 1985-05-10 1986-12-31 Metallifacture Ltd Vehicle jacks
EP0565801A1 (en) * 1992-04-14 1993-10-20 E.P.I., EUROPEENNE DE PARTICIPATIONS INDUSTRIELLE, Société Anonyme Vehicle jack

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2176458A (en) * 1985-05-10 1986-12-31 Metallifacture Ltd Vehicle jacks
EP0565801A1 (en) * 1992-04-14 1993-10-20 E.P.I., EUROPEENNE DE PARTICIPATIONS INDUSTRIELLE, Société Anonyme Vehicle jack

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0785166A3 (en) * 1996-01-22 1999-04-07 Batz, S. Coop. Jack for vehicles
WO2002036477A1 (en) * 2000-10-31 2002-05-10 Thyssenkrupp Bilstein Gmbh Displacement nut for a lifting device, and corresponding lifting device
CN100430310C (en) * 2000-10-31 2008-11-05 泰森克鲁普比尔斯坦有限责任公司 Displacement nut for lifting device, and corresponding lifting device

Also Published As

Publication number Publication date
DE69608603D1 (en) 2000-07-06
FR2732325A1 (en) 1996-10-04
FR2732325B1 (en) 1997-06-20
EP0734996B1 (en) 2000-05-31

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