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EP0688925B1 - Rotary latch adapted for improved assembly - Google Patents

Rotary latch adapted for improved assembly Download PDF

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Publication number
EP0688925B1
EP0688925B1 EP19950109434 EP95109434A EP0688925B1 EP 0688925 B1 EP0688925 B1 EP 0688925B1 EP 19950109434 EP19950109434 EP 19950109434 EP 95109434 A EP95109434 A EP 95109434A EP 0688925 B1 EP0688925 B1 EP 0688925B1
Authority
EP
European Patent Office
Prior art keywords
rotor
sleeve
axial
stator
rotary lock
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
EP19950109434
Other languages
German (de)
French (fr)
Other versions
EP0688925A1 (en
Inventor
Ghislain Gaudiau
Philippe Garcin
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.)
Valeo Comfort and Driving Assistance SAS
Original Assignee
Valeo Securite Habitacle 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 Valeo Securite Habitacle SAS filed Critical Valeo Securite Habitacle SAS
Publication of EP0688925A1 publication Critical patent/EP0688925A1/en
Application granted granted Critical
Publication of EP0688925B1 publication Critical patent/EP0688925B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B9/00Lock casings or latch-mechanism casings ; Fastening locks or fasteners or parts thereof to the wing
    • E05B9/08Fastening locks or fasteners or parts thereof, e.g. the casings of latch-bolt locks or cylinder locks to the wing
    • E05B9/084Fastening of lock cylinders, plugs or cores
    • E05B9/086Fastening of rotors, plugs or cores to an outer stator

Definitions

  • the present invention relates to a rotary lock.
  • the invention relates in particular to a rotary lock for driving a lock mechanism fitted to a opening of a motor vehicle such as a vehicle tailgate automobile.
  • the invention relates to a rotary lock of the type comprising a stator, in the form of a socket, and a rotor cylindrical mounted for rotation in the stator and comprising an eccentric pin relative to the axis of rotation of the rotor and which projects axially beyond a radial face end of the stator, for example for training a lock mechanism.
  • a type of lock is described and represented in document FR-A-2,642,463 which describes and represents a disengageable mechanism for controlling a lock of the type comprising a lock which comprises a body bolt which receives in rotation a stator in the form of socket which is angularly indexed relative to the body bolt by elastic erasable means which rotatably receives a rotor which is immobilized in rotation relative to the stator in the absence of a key, or when a wrong key is inserted into the lock, and that is likely to cause a finger to rotate of the lock mechanism which is coaxial with rotor and socket when these elements rotate simultaneously, against erasable elastic means, so as not to entrain the mechanism of lock, and which is integral with a first lever which is articulated around a first axis integral with the socket and offset from the axis of rotation of the sleeve and the rotor and which is driven by a pin of the rotor eccentric with respect to the latter's axis of rotation
  • the object of the present invention is to provide a improvement to the rotary lock which enables simple and automated assembly of different components, including the assembly of elastic means for returning the rotor to rotation by report to the stator.
  • the invention provides a rotary lock of the type mentioned above, characterized in that it includes a double-acting return spring of the rotor relative to the bush in a position angular median of rest which is arranged between a bottom radial end of sleeve and end face radial of the rotor, in that the spring is a spring hairspring with two end branches substantially parallel and each of which is likely to cooperate with one of the lateral drive faces of the nipple body and with a lateral abutment surface of a stop notch formed on the sleeve, and in that, in view of the assembly of these components, the spring, carried by the axial end of the rotor and the sleeve has means for automatic engagement of branches ends of the return spring with the surfaces lateral of the thrust notch, by rotation of the rotor by compared to the socket.
  • the lock 10 consists essentially of by a stator 14 in the form of a cylindrical socket, a rotor 12 and a return spring 16.
  • the stator 14 has a cylindrical wall internal 18 which delimits an open end 20 of the bush for axial insertion of rotor 12 and bottom axial end radial 22.
  • the rotor 12 is essentially constituted by a cylindrical body 24 which is intended to be introduced axially and rotatably mounted inside the sleeve forming stator 14.
  • the body 24 of the rotor 12 has a head 26 which is in particular intended to allow the introduction of a key (not shown) which controls the movements of a set of sequins 28 which are received in slots 30 formed in the rotor 12 and in slots 32 formed in the annular cylindrical wall of the stator 14.
  • the radial end face 34 of the rotor 12 which is intended to be received inside the stator 14 comprises a central extension in the form of a cylindrical core 36 which is concentric with the axis of rotation X-X of the rotor 12 relative to stator 14.
  • This core is designed to receive the body 38 of the return spring 16 which is a spring of the spiral type.
  • the spring 16 thus comprises a central body coiled 38 and two end branches 40A, 40B which extend radially outward and substantially parallel to each other.
  • the radial end face 34 of the rotor 12 also includes an eccentric drive stud 42.
  • the nipple 42 consists essentially of a body of nipple 44 which is offset radially outwards by relative to the external cylindrical surface of the body 24 of the rotor 12 and which extends axially from the surface radial end 34.
  • the body 44 thus defines an extra thickness 46 which extends radially outward from the surface 24 and which is rotated axially opposite the radial end face 34, while the free end of the body 44 of the drive stud has a spout 48 which is intended to cooperate with a component of a lock mechanism (not shown) in view of the rotational drive of the latter by the rotor 12.
  • the body 44 of the drive stud delimits two lateral drive sides 50A and 50B (see in particular Figures 6 and 7) each of which is likely to cooperate with an associated radial end branch 40A, 40B of the return spring 16.
  • the spring of reminder 16 When it is placed in position on the core 36, as illustrated in figure 3, the spring of reminder 16 is arranged so that the radial branches end 40A and 40B resiliently enclose the faces lateral drive 50A and 50B of the body 44 of the stud training 42.
  • the rotor 12 fitted with its return spring 16 constitutes a sub-assembly, which also includes the sequins 28, which can be inserted axially into the cylindrical bore 18 of stator 14 according to arrow I in FIG. 3.
  • the bore 18 has an axial groove 52 which opens in the open end 20 of the bore 18 and which opens into the radial end bottom 22.
  • the axial groove 52 opens into an annular opening 54 which is formed in the cylindrical wall 56 of the socket 14.
  • the annular lumen 54 extends substantially over half a circumference and is delimited at its two ends by two abutment faces 58A and 58B.
  • end faces 58A and 58B thus delimit the angular travel of the rotor 12 relative to the stator 14, the lateral drive faces 50A and 50B being likely to come in contact with end faces 58A and 58B of light 54, with interposition of the corresponding end branch 40A, 40B of the return spring 16.
  • the lumen 54 defines an annular radial end edge of the cylindrical wall of the stator 14 which is divided into two parts 60A and 60B offset axially, one by relative to each other and separated by a stop notch 62.
  • Part 60A is thus located further from the bottom radial end 22 as part 60B.
  • the stop notch 62 projects axially from the annular end edge 60A, 60B and extends substantially in the middle position, i.e. angularly in the middle of the light 54.
  • the stop notch 62 extends axially up to right from the radial end bottom 22 of the stator 14.
  • the stop notch 62 delimits two lateral surfaces 64A and 64B each of which, as will be explained later, is likely to cooperate with a corresponding end branch 40A, 40B of the spring 16.
  • the transverse end surface 64A is extends axially towards the free end edge 66 of the stop notch 62, by an inclined ramp 68.
  • Part 60A of the annular end edge of the socket 14 is provided to cooperate with the additional thickness 46, over a portion of the angular travel of the rotor 12, the latter also cooperating with a portion 70, located in the same plane as part 60A, of the wall cylindrical annular sleeve 14.
  • the nipple 42 also drives the industry end 40A.
  • the rotor 12 is also retained axially by report to stator 14 due to the cooperation of extra thickness 46 with the corresponding portions of the edge annular end of the stator socket 14.
  • the maximum angular positions of the rotor 12 by relative to stator 14 are delimited by the faces end 58A and 58B of the light 54.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Lock And Its Accessories (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Braking Arrangements (AREA)
  • Rotary Pumps (AREA)

Description

La présente invention concerne un verrou rotatif.The present invention relates to a rotary lock.

L'invention concerne notamment un verrou rotatif pour l'entraínement d'un mécanisme de serrure équipant un ouvrant de véhicule automobile tel qu'un hayon de véhicule automobile.The invention relates in particular to a rotary lock for driving a lock mechanism fitted to a opening of a motor vehicle such as a vehicle tailgate automobile.

L'invention concerne un verrou rotatif du type comportant un stator, en forme de douille, et un rotor cylindrique monté à rotation dans le stator et comportant un téton excentré par rapport à l'axe de rotation du rotor et qui fait saillie axialement au-delà d'une face radiale d'extrémité du stator, par exemple pour l'entraínement d'un mécanisme de serrure.The invention relates to a rotary lock of the type comprising a stator, in the form of a socket, and a rotor cylindrical mounted for rotation in the stator and comprising an eccentric pin relative to the axis of rotation of the rotor and which projects axially beyond a radial face end of the stator, for example for training a lock mechanism.

Un exemple d'un tel type de verrou est décrit et représenté dans le document FR-A-2.642.463 qui décrit et représente un mécanisme débrayable de commande d'une serrure du type comportant un verrou qui comporte un corps de verrou qui reçoit à rotation un stator en forme de douille qui est indexée angulairement par rapport au corps de verrou par des moyens élastiques effaçables et qui reçoit à rotation un rotor qui est immobilisé en rotation par rapport au stator en l'absence de clé, ou lorsqu'une fausse clé est introduite dans le verrou, et qui est susceptible d'entraíner en rotation un doigt d'entraínement du mécanisme de serrure qui est coaxial au rotor et à la douille lorsque ces éléments tournent simultanément, à l'encontre de moyens élastiques effaçables, de manière à ne pas entraíner le mécanisme de serrure, et qui est solidaire d'un premier levier qui est articulé autour d'un premier axe solidaire de la douille et excentré par rapport à l'axe de rotation de la douille et du rotor et qui est entraíné par un téton du rotor excentré par rapport à l'axe de rotation de ce dernier, le doigt d'entraínement coopérant avec un second levier de la commande de la serrure articulée par rapport au corps de verrou autour d'un second axe excentré par rapport à l'axe de rotation de la douille et du rotor.An example of such a type of lock is described and represented in document FR-A-2,642,463 which describes and represents a disengageable mechanism for controlling a lock of the type comprising a lock which comprises a body bolt which receives in rotation a stator in the form of socket which is angularly indexed relative to the body bolt by elastic erasable means which rotatably receives a rotor which is immobilized in rotation relative to the stator in the absence of a key, or when a wrong key is inserted into the lock, and that is likely to cause a finger to rotate of the lock mechanism which is coaxial with rotor and socket when these elements rotate simultaneously, against erasable elastic means, so as not to entrain the mechanism of lock, and which is integral with a first lever which is articulated around a first axis integral with the socket and offset from the axis of rotation of the sleeve and the rotor and which is driven by a pin of the rotor eccentric with respect to the latter's axis of rotation, the drive finger cooperating with a second lever of the control of the articulated lock relative to the body of latch around a second axis offset from the axis sleeve and rotor rotation.

Du point de vue fonctionnel et de sa fiabilité, une telle conception est satisfaisante dans la mesure où elle permet d'empêcher toute ouverture frauduleuse de la serrure.From a functional and reliability point of view, such a design is satisfactory insofar as it prevents fraudulent opening of the lock.

La présente invention a pour but de proposer un perfectionnement au verrou rotatif qui permet de réaliser de manière simple et automatisée l'assemblage des différents composants, et notamment l'assemblage des moyens élastiques de rappel en rotation du rotor par rapport au stator.The object of the present invention is to provide a improvement to the rotary lock which enables simple and automated assembly of different components, including the assembly of elastic means for returning the rotor to rotation by report to the stator.

En effet, ces opérations sont particulièrement complexes et effectuées manuellement, ces opérations étant par ailleurs compliquées par l'assemblage des autres composants du verrou tels que par exemple les paillettes du verrou et les ressorts de paillettes.Indeed, these operations are particularly complex and performed manually, these operations being otherwise complicated by the assembly of others components of the lock such as for example glitter of the lock and the glitter springs.

Dans ce but, l'invention propose un verrou rotatif du type mentionné précédemment, caractérisé en ce qu'il comporte un ressort, à double-effet, de rappel en rotation du rotor par rapport à la douille dans une position angulaire médiane de repos qui est agencé entre un fond radial d'extrémité de la douille et face d'extrémité radiale du rotor, en ce que le ressort est un ressort spiral dont les deux branches d'extrémités sont sensiblement parallèles et dont chacune est susceptible de coopérer avec une des faces latérales d'entraínement du corps de téton et avec une surface latérale de butée d'un cran de butée formé sur la douille, et en ce que, en vue de l'assemblage de ces composants, le ressort, porté par l'extrémité axiale du rotor et la douille, comporte des moyens pour l'engagement automatique des branches d'extrémités du ressort de rappel avec les surfaces latérales du cran de butée, par rotation du rotor par rapport à la douille. To this end, the invention provides a rotary lock of the type mentioned above, characterized in that it includes a double-acting return spring of the rotor relative to the bush in a position angular median of rest which is arranged between a bottom radial end of sleeve and end face radial of the rotor, in that the spring is a spring hairspring with two end branches substantially parallel and each of which is likely to cooperate with one of the lateral drive faces of the nipple body and with a lateral abutment surface of a stop notch formed on the sleeve, and in that, in view of the assembly of these components, the spring, carried by the axial end of the rotor and the sleeve has means for automatic engagement of branches ends of the return spring with the surfaces lateral of the thrust notch, by rotation of the rotor by compared to the socket.

Selon d'autres réalisations avantageuses de l'invention :

  • l'extrémité axiale du cran comporte une rampe qui coopère avec une des deux branches d'extrémités du ressort ;
  • le corps du ressort spiral est enroulé autour d'un noyau concentrique qui est formé à l'extrémité axiale du ressort et dont la face radiale d'extrémité s'étend en regard du front radial d'extrémité de la douille ;
  • le téton d'entraínement est formé sur un prolongement axial excentré formé à l'extrémité axiale du rotor et la surface cylindrique interne de la douille comporte une rainure axiale pour le passage du téton et des branches d'extrémités du ressort lors de l'introduction axiale du rotor dans la douille ;
  • le fond de la douille de stator comporte une lumière annulaire pour le passage axial et la rotation du téton ;
  • le cran de butée est agencé angulairement au milieu de la lumière et les extrémités de la lumière définissent les positions angulaires extrêmes du rotor par rapport à la douille ;
  • la rainure axiale débouche au voisinage de l'une des deux extrémités de la lumière annulaire ;
  • en position de repos, le téton d'entraínement s'étend axialement vis-à-vis du cran de butée, radialement vers l'intérieur par rapport à ce dernier ;
  • le téton d'entraínement comporte une surépaisseure en saillie radialement vers l'extérieur qui s'étend en regard d'un bord axial d'extrémité de la douille pour retenir axialement le rotor par rapport à la douille.
According to other advantageous embodiments of the invention:
  • the axial end of the notch has a ramp which cooperates with one of the two end branches of the spring;
  • the body of the spiral spring is wound around a concentric core which is formed at the axial end of the spring and the radial end face of which extends opposite the radial front end of the sleeve;
  • the drive stud is formed on an eccentric axial extension formed at the axial end of the rotor and the internal cylindrical surface of the sleeve has an axial groove for the passage of the stud and spring end branches during introduction axial of the rotor in the sleeve;
  • the bottom of the stator socket has an annular opening for the axial passage and the rotation of the stud;
  • the stop notch is arranged angularly in the middle of the lumen and the ends of the lumen define the extreme angular positions of the rotor relative to the bush;
  • the axial groove opens in the vicinity of one of the two ends of the annular opening;
  • in the rest position, the drive stud extends axially with respect to the stop notch, radially inwardly relative to the latter;
  • the drive stud has a thickening protruding radially outwardly which extends opposite an axial edge of the end of the sleeve to axially retain the rotor relative to the sleeve.

D'autres qualités et avantages de l'invention apparaítront à la lecture détaillée qui va suivre pour la compréhension de laquelle on se reportera aux dessins annexés dans lesquels :

  • la figure 1 est une vue en perspective éclatée des principaux composants d'un verrou rotatif selon l'invention ;
  • la figure 2 est une vue en perspective éclatée, à plus grande échelle, illustrant le stator, le ressort de rappel et le rotor avant leur assemblage ;
  • la figure 3 est une vue similaire à celle de la figure 2 qui illustre le ressort de rappel en place sur l'extrémité axiale du rotor avant l'introduction axiale de ce dernier dans le stator ;
  • les figures 4 à 9 sont des vues en perspectives illustrant successivement les positions relatives occupées par les trois composants illustrés aux figures 2 et 3, au cours de leur assemblage définitif et lors de l'utilisation du verrou.
Other qualities and advantages of the invention will appear on detailed reading which follows for the understanding of which reference will be made to the appended drawings in which:
  • Figure 1 is an exploded perspective view of the main components of a rotary lock according to the invention;
  • Figure 2 is an exploded perspective view, on a larger scale, illustrating the stator, the return spring and the rotor before their assembly;
  • Figure 3 is a view similar to that of Figure 2 which illustrates the return spring in place on the axial end of the rotor before the axial introduction of the latter into the stator;
  • Figures 4 to 9 are perspective views successively illustrating the relative positions occupied by the three components illustrated in Figures 2 and 3, during their final assembly and when using the lock.

Comme on peut le voir sur les figures 1 et 2, le verrou 10 selon l'invention est constitué pour l'essentiel par un stator 14 en forme de douille cylindrique, un rotor 12 et un ressort de rappel 16.As can be seen in Figures 1 and 2, the lock 10 according to the invention consists essentially of by a stator 14 in the form of a cylindrical socket, a rotor 12 and a return spring 16.

Le stator 14 comporte une paroi cylindrique interne 18 qui délimite une extrémité ouverte 20 de la douille pour l'introduction axiale du rotor 12 et un fond radial d'extrémité axiale 22.The stator 14 has a cylindrical wall internal 18 which delimits an open end 20 of the bush for axial insertion of rotor 12 and bottom axial end radial 22.

Le rotor 12 est pour l'essentiel constitué par un corps cylindrique 24 qui est prévu pour être introduit axialement et monté à rotation à l'intérieur de la douille formant stator 14.The rotor 12 is essentially constituted by a cylindrical body 24 which is intended to be introduced axially and rotatably mounted inside the sleeve forming stator 14.

Le corps 24 du rotor 12 comporte une tête 26 qui est notamment prévu pour permettre l'introduction d'une clé (non représentée) qui commande les déplacements d'un ensemble de paillettes 28 qui sont reçues dans des fentes 30 formées dans le rotor 12 et dans des fentes 32 formées dans la paroi cylindrique annulaire du stator 14.The body 24 of the rotor 12 has a head 26 which is in particular intended to allow the introduction of a key (not shown) which controls the movements of a set of sequins 28 which are received in slots 30 formed in the rotor 12 and in slots 32 formed in the annular cylindrical wall of the stator 14.

La face radiale d'extrémité 34 du rotor 12 qui est prévu pour être reçu à l'intérieur du stator 14 comporte un prolongement central en forme de noyau cylindrique 36 qui est concentrique à l'axe de rotation X-X du rotor 12 par rapport au stator 14.The radial end face 34 of the rotor 12 which is intended to be received inside the stator 14 comprises a central extension in the form of a cylindrical core 36 which is concentric with the axis of rotation X-X of the rotor 12 relative to stator 14.

Ce noyau est prévu pour recevoir le corps 38 du ressort de rappel 16 qui est un ressort du type spiral.This core is designed to receive the body 38 of the return spring 16 which is a spring of the spiral type.

Le ressort 16 comporte ainsi un corps central enroulé 38 et deux branches d'extrémités 40A, 40B qui s'étendent radialement vers l'extérieur et sensiblement parallèlement l'une à l'autre.The spring 16 thus comprises a central body coiled 38 and two end branches 40A, 40B which extend radially outward and substantially parallel to each other.

La face radiale d'extrémité 34 du rotor 12 comporte également un téton excentré d'entraínement 42.The radial end face 34 of the rotor 12 also includes an eccentric drive stud 42.

Comme on peut le voir sur les figures 1 et 2, le téton 42 est constitué pour l'essentiel par un corps de téton 44 qui est excentré radialement vers l'extérieur par rapport à la surface cylindrique externe du corps 24 du rotor 12 et qui s'étend axialement depuis la surface radiale d'extrémité 34.As can be seen in Figures 1 and 2, the nipple 42 consists essentially of a body of nipple 44 which is offset radially outwards by relative to the external cylindrical surface of the body 24 of the rotor 12 and which extends axially from the surface radial end 34.

Le corps 44 délimite ainsi une surépaisseur 46 qui s'étend radialement vers l'extérieur par rapport à la surface 24 et qui est tournée axialement à l'opposé de la face radiale d'extrémité 34, tandis que l'extrémité libre du corps 44 du téton d'entraínement comporte un bec d'entraínement 48 qui est prévu pour coopérer avec un composant d'un mécanisme de serrure (non représenté) en vu de l'entraínement en rotation de ce dernier par le rotor 12.The body 44 thus defines an extra thickness 46 which extends radially outward from the surface 24 and which is rotated axially opposite the radial end face 34, while the free end of the body 44 of the drive stud has a spout 48 which is intended to cooperate with a component of a lock mechanism (not shown) in view of the rotational drive of the latter by the rotor 12.

Le corps 44 du téton d'entraínement délimite deux faces latérales d'entraínement 50A et 50B (voir notamment les figures 6 et 7) dont chacune est susceptible de coopérer avec une branche radiale d'extrémité associée 40A, 40B du ressort de rappel 16.The body 44 of the drive stud delimits two lateral drive sides 50A and 50B (see in particular Figures 6 and 7) each of which is likely to cooperate with an associated radial end branch 40A, 40B of the return spring 16.

Lorsqu'il est mis en position sur le noyau 36, comme cela est illustré sur la figure 3, le ressort de rappel 16 est disposé de manière que les branches radiales d'extrémité 40A et 40B enserrent élastiquement les faces latérales d'entraínement 50A et 50B du corps 44 du téton d'entraínement 42.When it is placed in position on the core 36, as illustrated in figure 3, the spring of reminder 16 is arranged so that the radial branches end 40A and 40B resiliently enclose the faces lateral drive 50A and 50B of the body 44 of the stud training 42.

Comme on peut le voir sur la figure 3, le rotor 12 équipé de son ressort de rappel 16 constitue un sous-ensemble, qui comporte également les paillettes 28, qui peut être introduit axialement dans l'alésage cylindrique 18 du stator 14 selon la flèche I de la figure 3.As can be seen in Figure 3, the rotor 12 fitted with its return spring 16 constitutes a sub-assembly, which also includes the sequins 28, which can be inserted axially into the cylindrical bore 18 of stator 14 according to arrow I in FIG. 3.

A cet effet, et pour permettre l'introduction axiale du téton d'entraínement 42 et des branches 40A, 40B du ressort 16, l'alésage 18 comporte une rainure axiale 52 qui s'ouvre dans l'extrémité ouverte 20 de l'alésage 18 et qui débouche dans le fond radial d'extrémité 22.To this end, and to allow the introduction axial of the drive stud 42 and the branches 40A, 40B of the spring 16, the bore 18 has an axial groove 52 which opens in the open end 20 of the bore 18 and which opens into the radial end bottom 22.

Comme on peut le voir notamment sur la figure 2, la rainure axiale 52 débouche dans une lumière annulaire 54 qui est formée dans la paroi cylindrique 56 de la douille 14.As we can see in particular in Figure 2, the axial groove 52 opens into an annular opening 54 which is formed in the cylindrical wall 56 of the socket 14.

La lumière annulaire 54 s'étend sensiblement sur une demi-circonférence et est délimitée à ses deux extrémités par deux faces de butée 58A et 58B.The annular lumen 54 extends substantially over half a circumference and is delimited at its two ends by two abutment faces 58A and 58B.

Les faces d'extrémités 58A et 58B délimitent ainsi la course angulaire du rotor 12 par rapport au stator 14, les faces latérales d'entraínement 50A et 50B étant susceptibles de venir alternativement en contact avec les faces d'extrémités 58A et 58B de la lumière 54, avec interposition de la branche d'extrémité correspondante 40A, 40B du ressort de rappel 16.The end faces 58A and 58B thus delimit the angular travel of the rotor 12 relative to the stator 14, the lateral drive faces 50A and 50B being likely to come in contact with end faces 58A and 58B of light 54, with interposition of the corresponding end branch 40A, 40B of the return spring 16.

Comme on peut le voir notamment sur la figure 2, la lumière 54 définit un bord radial annulaire d'extrémité de la paroi cylindrique du stator 14 qui est partagée en deux parties 60A et 60B décalées axialement l'une par rapport à l'autre et séparées par un cran de butée 62.As we can see in particular in Figure 2, the lumen 54 defines an annular radial end edge of the cylindrical wall of the stator 14 which is divided into two parts 60A and 60B offset axially, one by relative to each other and separated by a stop notch 62.

La partie 60A est ainsi située plus loin du fond radial d'extrémité 22 que la partie 60B.Part 60A is thus located further from the bottom radial end 22 as part 60B.

Le cran de butée 62 fait saillie axialement depuis le bord annulaire d'extrémité 60A, 60B et s'étend sensiblement en position médiane, c'est-à-dire angulairement au milieu de la lumière 54.The stop notch 62 projects axially from the annular end edge 60A, 60B and extends substantially in the middle position, i.e. angularly in the middle of the light 54.

Le cran de butée 62 s'étend axialement jusqu'au droit du fond radial d'extrémité 22 du stator 14.The stop notch 62 extends axially up to right from the radial end bottom 22 of the stator 14.

Le cran de butée 62 délimite deux surfaces latérales de butée 64A et 64B dont chacune, comme cela sera expliqué par la suite, est susceptible de coopérer avec une branche d'extrémité correspondante 40A, 40B du ressort 16.The stop notch 62 delimits two lateral surfaces 64A and 64B each of which, as will be explained later, is likely to cooperate with a corresponding end branch 40A, 40B of the spring 16.

La surface transversale d'extrémité 64A se prolonge axialement vers le bord d'extrémité libre 66 du cran de butée 62, par une rampe inclinée 68.The transverse end surface 64A is extends axially towards the free end edge 66 of the stop notch 62, by an inclined ramp 68.

La partie 60A du bord annulaire d'extrémité de la douille 14 est prévue pour coopérer avec la surépaisseur 46, sur une portion de la course angulaire du rotor 12, cette dernière coopérant également avec une portion 70, située dans le même plan que la partie 60A, de la paroi annulaire cylindrique de la douille 14.Part 60A of the annular end edge of the socket 14 is provided to cooperate with the additional thickness 46, over a portion of the angular travel of the rotor 12, the latter also cooperating with a portion 70, located in the same plane as part 60A, of the wall cylindrical annular sleeve 14.

On décrira maintenant l'assemblage des différents composants en partant de la position illustrée sur la figure 3 dans laquelle le ressort spiral de rappel 16 est déjà monté sur le noyau d'extrémité 36 du rotor 14.We will now describe the assembly of the different components starting from the position illustrated on the Figure 3 in which the spiral return spring 16 is already mounted on the end core 36 of the rotor 14.

Dans cette position, le téton d'entraínement 42 est situé angulairement en regard de la rainure axiale 52 et il est possible d'introduire le rotor 12 et le ressort 16 dans le stator 14. Cette introduction se poursuit jusqu'à la position illustrée sur la figure 4 dans laquelle la face radiale d'extrémité 37 du noyau 36 (voir figure 3) est venue en butée contre le fond radial d'extrémité 22 de la douille formant stator 14.In this position, the drive pin 42 is located angularly opposite the axial groove 52 and it is possible to introduce the rotor 12 and the spring 16 in stator 14. This introduction continues to the position illustrated in Figure 4 in which the radial end face 37 of the core 36 (see Figure 3) came into abutment against the radial bottom end 22 of the stator socket 14.

Le téton d'entraínement 42 et les branches d'extrémités 40A et 40B qui font saillie axialement au-delà de la partie 60A du bord annulaire d'extrémité du stator 14, se trouve situé en regard de la face d'extrémité 58A de la lumière 54. The driving pin 42 and the branches 40A and 40B ends which protrude axially beyond of part 60A of the annular end edge of the stator 14, is located opposite the face 58A end of light 54.

L'assemblage se poursuit en provoquant une rotation relative du rotor 12 par rapport au stator 14 dans la direction indiquée par la flèche R de la figure 4.The assembly continues, causing a relative rotation of rotor 12 with respect to stator 14 in the direction indicated by the arrow R in Figure 4.

Au cours de cette rotation, la branche d'extrémité 40B du ressort de rappel qui est située axialement la plus proche du fond radial 22 par rapport à la branche d'extrémité 40A, vient en contact avec la rampe 68 formée sur le cran de butée 62, comme cela est illustré sur la figure 5.During this rotation, the end branch 40B of the return spring which is located axially the most close to the radial bottom 22 relative to the branch end 40A, comes into contact with the ramp 68 formed on the stop notch 62, as illustrated on the figure 5.

Au cours de cette rotation, le téton d'entraínement 42 entraíne également la branche d'extrémité 40A.During this rotation, the nipple 42 also drives the industry end 40A.

En poursuivant la rotation du rotor 12 par rapport au stator 14 dans le sens indiqué par la flèche R sur la figure 5, la coopération de la branche d'extrémité 40B avec la rampe 68 va provoquer le passage de celle-ci au-delà de la face d'extrémité 66 du cran de butée 62 et sa venue en coopération avec la surface latérale de butée 64B du cran de butée 62 tandis que la branche d'extrémité 40A vient en vis-à-vis de la surface latérale de butée 64A.Continuing the rotation of the rotor 12 relative stator 14 in the direction indicated by arrow R on the Figure 5, the cooperation of the end branch 40B with the ramp 68 will cause the passage of it beyond of the end face 66 of the stop notch 62 and its came in cooperation with the lateral stop surface 64B of the stop notch 62 while the end branch 40A comes opposite the lateral abutment surface 64A.

Cette position assemblée est illustrée aux figures 6 et 7 dans lesquelles le rotor 12 se trouve en position médiane de repos par rapport au stator 14, cette position étant définie par la coopération des branches d'extrémités 40A et 40B respectivement avec les faces latérales d'entraínement 50A, 50B et les surfaces latérales de butée 64A et 64B.This assembled position is illustrated in the figures 6 and 7 in which the rotor 12 is in position median rest relative to stator 14, this position being defined by the cooperation of the end branches 40A and 40B respectively with the side faces 50A, 50B and the lateral abutment surfaces 64A and 64B.

Le rotor 12 est également retenu axialement par rapport au stator 14 du fait de la coopération de surépaisseur 46 avec les portions correspondantes du bord annulaire d'extrémité de la douille formant stator 14.The rotor 12 is also retained axially by report to stator 14 due to the cooperation of extra thickness 46 with the corresponding portions of the edge annular end of the stator socket 14.

En fonctionnement, et comme cela est illustré aux figures 8 et 9, le rotor 12 et le téton d'entraínement 42 entraíne alternativement l'une ou l'autre des branches d'extrémités 40A, 40B, tandis que la branche non entraínée reste en butée contre l'une ou l'autre des surfaces latérales de butée 64B, 64A du cran 62, provoquant ainsi une accumulation de force dans le ressort 16 qui provoque ensuite le rappel élastique vers la position médiane de repos illustré aux figures 6 et 7.In operation, and as illustrated in Figures 8 and 9, the rotor 12 and the drive stud 42 alternately drives either branch ends 40A, 40B, while the untrained branch remains in abutment against either surface lateral stop 64B, 64A of notch 62, thus causing an accumulation of force in the spring 16 which causes then the elastic return to the middle position of rest illustrated in Figures 6 and 7.

Les positions angulaires maximales du rotor 12 par rapport au stator 14 sont délimitées par les faces d'extrémité 58A et 58B de la lumière 54.The maximum angular positions of the rotor 12 by relative to stator 14 are delimited by the faces end 58A and 58B of the light 54.

Ainsi, la simple introduction axiale selon la direction I du rotor 12 équipé du ressort 16 puis sa rotation selon la direction R assure la mise en place automatique en position de fonctionnement du ressort 16 et l'immobilisation axiale relative du rotor 12 par rapport au stator 14 .Thus, the simple axial introduction according to the direction I of the rotor 12 fitted with the spring 16 then its rotation in the direction R ensures the establishment automatic in the operating position of the spring 16 and the relative axial immobilization of the rotor 12 relative to stator 14.

Même au cas ou cette première rotation relative du rotor 12 par rapport au stator 14 n'aurait pas été effectuée lors de l'assemblage, la première utilisation du verrou par entraínement du rotor 12 au moyen d'une clé provoquera la mise en place du ressort 16 selon la procédure exposée précédemment.Even if this first relative rotation of the rotor 12 relative to stator 14 would not have been performed during assembly, the first use of the lock by driving the rotor 12 by means of a key will cause the spring 16 to be put in place according to the previously described procedure.

Claims (9)

  1. A rotary lock (10) of the type comprising a stator (14) in the form of a sleeve, together with a cylindrical rotor (12) mounted for rotation in the stator (14) and including a head (42), which is eccentric with respect to the axis of rotation (X-X) of the rotor and which projects axially beyond a radial end face of the stator (14), for actuating a latch mechanism for example, characterised in that it includes a double-acting spring (16) for returning the rotor (12), in rotation with respect to the sleeve (14), into an angular rest position which is defined midway between a radial terminal base (22) of the sleeve (14) and a radial end face (34) of the rotor (12), in that the spring (16) is a spiral spring, the two terminal branches (40A, 40B) of which are substantially parallel, and each of which is arranged to cooperate with one of the lateral faces (50A, 50B) of the body (44) of the drive head (42) and with a lateral abutment surface (64A, 64B) of an abutment lug (62) formed on the sleeve (14), and in that, for the purposes of assembly of these components, the return spring (16), carried by the axial end (36) of the rotor (12) and the sleeve (14), has means (68) for automatic engagement of the terminal branches (40A, 40B) of the spring (16) with the lateral surfaces (64A, 64B) of the abutment lug (62) by rotation of the rotor (12) with respect to the sleeve (14).
  2. A rotary lock according to Claim 1, characterised in that the axial end of the abutment lug (62) comprises a ramp (68) which cooperates with one (40A) of the two terminal branches of the return spring (16).
  3. A rotary lock according to Claim 1 or Claim 2, characterised in that the body (38) of the spiral spring (16) is wound on a concentric core (36) which is formed at the axial end of the rotor, and of which the radial end face (37) lies facing the radial terminal base (22) of the sleeve (14).
  4. A rotary lock according to any one of the preceding Claims, characterised in that the drive head (42) is formed on an eccentric axial extension (44) defined at the axial end (34) of the rotor (12), and in that the cylindrical internal surface (18) of the sleeve (14) has an axial groove (52) for passage of the head (42) and of the terminal branches (40A, 40B) of the spring through it during introduction of the rotor (12) axially into the sleeve (14).
  5. A rotary lock according to any one of the preceding Claims, characterised in that the base (22) of the stator sleeve (14) has an annular rebate (54), for axial passage of the drive head (42), and rotation of the latter, therein.
  6. A rotary lock according to Claim 5, characterised in that the abutment lug (62) is disposed circumferentially in the middle of the rebate (54), and in that the ends (58A, 58B) of the rebate (54) define the extreme angular positions of the rotor (12) with respect to the sleeve (14).
  7. A rotary lock according to Claim 5 or Claim 6 taken in combination with Claim 4, characterised in that the axial groove (52) is open in the vicinity of one (58A) of the two ends of the annular rebate (54).
  8. A rotary lock according to any one of the preceding Claims, characterised in that in the rest position, the drive head (42) lies in axial facing relationship with the abutment lug (62), radially inwards with respect to the latter.
  9. A rotary lock according to any one of the preceding Claims, characterised in that the drive head (42) includes a thickened portion (46) which projects radially outwards and which lies facing an axial terminal edge of the sleeve (14), so as to retain the rotor (12) axially in place with respect to the sleeve (14).
EP19950109434 1994-06-24 1995-06-19 Rotary latch adapted for improved assembly Expired - Lifetime EP0688925B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9407905 1994-06-24
FR9407905A FR2721647B1 (en) 1994-06-24 1994-06-24 Rotary lock comprising improved assembly means.

Publications (2)

Publication Number Publication Date
EP0688925A1 EP0688925A1 (en) 1995-12-27
EP0688925B1 true EP0688925B1 (en) 1999-01-27

Family

ID=9464713

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19950109434 Expired - Lifetime EP0688925B1 (en) 1994-06-24 1995-06-19 Rotary latch adapted for improved assembly

Country Status (6)

Country Link
EP (1) EP0688925B1 (en)
CN (1) CN1075587C (en)
BR (1) BR9502851A (en)
DE (1) DE69507546T2 (en)
ES (1) ES2129706T3 (en)
FR (1) FR2721647B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10340272A1 (en) * 2003-08-29 2005-03-24 BÖCO Böddecker & Co. GmbH & Co. KG Apparatus for fastening a lock barrel for a vehicle door to a mounting surface on the vehicle esp. for the door of the trunk and being made of two fastener components
FR2912174B1 (en) * 2007-02-02 2009-05-01 Valeo Securite Habitacle Sas METHOD FOR MANUFACTURING A ROTARY LATCH OF A MOTOR VEHICLE
CN105257121A (en) * 2015-10-10 2016-01-20 陈建成 Anti-theft lock

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1742254A (en) * 1928-10-25 1930-01-07 Briggs & Stratton Corp Lock
US2883848A (en) * 1956-08-27 1959-04-28 Illinois Lock Co Lock
US4272975A (en) * 1979-07-06 1981-06-16 Hudson Lock, Inc. Cylinder lock with key removable core
FR2589926B1 (en) * 1985-11-14 1993-12-31 Neiman Sa PISTON LOCK WITH SLIDING ROTOR, CLUTCHABLE WITH CONTROL UNIT
FR2642463B1 (en) * 1989-01-30 1991-03-29 Neiman Sa RELEASABLE LOCK WITH ROTATING STATOR

Also Published As

Publication number Publication date
BR9502851A (en) 1996-04-23
ES2129706T3 (en) 1999-06-16
EP0688925A1 (en) 1995-12-27
DE69507546D1 (en) 1999-03-11
FR2721647A1 (en) 1995-12-29
CN1075587C (en) 2001-11-28
FR2721647B1 (en) 1996-07-26
CN1114998A (en) 1996-01-17
DE69507546T2 (en) 1999-06-02

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