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WO2014006315A1 - Stub-axle bracket with hollow portions by core-making - Google Patents

Stub-axle bracket with hollow portions by core-making Download PDF

Info

Publication number
WO2014006315A1
WO2014006315A1 PCT/FR2013/051541 FR2013051541W WO2014006315A1 WO 2014006315 A1 WO2014006315 A1 WO 2014006315A1 FR 2013051541 W FR2013051541 W FR 2013051541W WO 2014006315 A1 WO2014006315 A1 WO 2014006315A1
Authority
WO
WIPO (PCT)
Prior art keywords
support
vehicle
connecting element
rocket
core
Prior art date
Application number
PCT/FR2013/051541
Other languages
French (fr)
Inventor
Laurent SOULAT
Original Assignee
Renault S.A.S
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 Renault S.A.S filed Critical Renault S.A.S
Publication of WO2014006315A1 publication Critical patent/WO2014006315A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D7/00Steering linkage; Stub axles or their mountings
    • B62D7/18Steering knuckles; King pins
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/10Cores; Manufacture or installation of cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D25/00Special casting characterised by the nature of the product
    • B22D25/02Special casting characterised by the nature of the product by its peculiarity of shape; of works of art

Definitions

  • the invention relates to a rocket support for the rotational mounting of a hub of a wheel of a motor vehicle, comprising a one-piece molded part (cast iron, steel, aluminum, etc.) constituting on the one hand a support element delimiting a housing intended for the rotational mounting of the hub and on the other hand a plurality of connecting elements intended to be respectively fixed to different integral members of the vehicle and respectively associated with said elements link for securing the rocket carrier to the vehicle.
  • a support element delimiting a housing intended for the rotational mounting of the hub
  • a plurality of connecting elements intended to be respectively fixed to different integral members of the vehicle and respectively associated with said elements link for securing the rocket carrier to the vehicle.
  • the invention also relates to an arrangement for a motor vehicle wheel train, in particular a front or rear axle, and a process for the casting of the rocket support.
  • each wheel of the train is associated with a substantially cylindrical hub, also known as "rocket".
  • the hub is rotatably mounted relative to a rocket or knuckle support via a bearing.
  • the rocket support currently obtained at least by a foundry operation, comprises for this purpose a support member delimiting a housing for receiving the bearing.
  • the rocket carrier also includes a plurality of link members, including:
  • the rocket support comprises each of these three connecting elements in addition to the support element, which is generally arranged in the center of the elements. link. It may also comprise fixing elements intended for fixing a braking device, in particular a brake caliper and / or a wheel lock monitoring sensor, a bearing sealing function at the interface with the transmission, disc guard fastener elements and ball joint bellows protector.
  • the object of the present invention is to provide a rocket support that overcomes the drawbacks listed above, in particular that is easy to obtain, which has a weight content while having a resistance adapted to compliance with a specification of operation. normal and shock conditions.
  • a first aspect of the invention relates to a rocket support for the rotational mounting of a hub of a wheel of a motor vehicle, comprising a one-piece molded part constituting on the one hand a support element delimiting a housing intended for the rotational mounting of the hub and on the other hand a plurality of connecting elements intended to be respectively fixed to different integral members of the hub; vehicle and respectively associated with said connecting elements for fixing the rocket support on the vehicle.
  • the one-piece molded part comprises hollow parts formed by coring both in the support element and in all the connecting elements, each of the hollow parts opening into another hollow part so that all the hollow parts communicate with each other. and defining within the one-piece molded part a cavity extending in the support member and in each of the connecting members.
  • the hollow portion formed in the support member may be arranged at the periphery of said housing, in particular in an annular manner generally included in a plane perpendicular to the axis of a bore constituting the housing.
  • the housing may be configured to allow for force-fitting of an outer cage of a hub-rotating guide bearing.
  • the plurality of connecting elements may comprise a first connecting element made of material from the support element and intended to be fixed, in particular by a first ball joint connection, to a lower suspension arm integral with the vehicle constituting a integral member of the vehicle and associated with said first connecting element.
  • the first link member may be configured such that the hollow portion formed in the first link member opens into the hollow portion formed in the support member.
  • the plurality of connecting elements may comprise a second connecting element made of material from the support element and intended to be fixed, in particular by a second ball joint connection, to a steering rod secured to the vehicle, constituting a member secured to the vehicle and associated with said second connecting element.
  • the second link member may be configured such that the hollow portion formed in the second link member opens into the hollow portion formed in the support member.
  • the plurality of connecting elements may comprise a third connecting element made of material from the support element and intended to be fixed, in particular by a screw connection or a clamping or clamping connection, to a damping device and / or spring secured to the vehicle, constituting a member integral with the vehicle and associated with said third connecting element.
  • the third link member may be configured such that the hollow portion formed in the third link member opens into the hollow portion formed in the support member.
  • the one-piece molded part may comprise fixing elements intended for fixing a braking device, in particular a brake caliper and / or a wheel lock monitoring sensor.
  • a second aspect of the invention relates to an arrangement for a motor vehicle wheel train, in particular a front or rear gear, which comprises such a rocket support, a wheel of the vehicle and a hub integral with the wheel and mounted to rotate at the the housing delimited by the support member of the integrally molded part of the rocket support.
  • the arrangement may include: at least one lower suspension arm fixed, in particular by a first ball joint, to a first connecting element of the one-piece molded part of the rocket support,
  • It may comprise a bearing for rotating the hub having an outer cage force-fitted in a bore of the housing and an outer cage force-fitted on the hub.
  • a third aspect of the invention finally relates to a method of manufacturing by casting a rocket support for the rotational mounting of a hub of a wheel of a motor vehicle, comprising a casting step of an alloy in a mold configured so as to obtain, after cooling of the cast alloy, a one-piece molded part constituting on the one hand a support element intended for the rotational mounting of the hub and on the other hand a plurality of elements linkages intended to be respectively fixed to different integral members of the vehicle and respectively associated with said connecting elements to ensure the attachment of the rocket carrier on the vehicle.
  • the method comprises a step of providing a single core and placing the core in the mold prior to the casting step, the core and its implementation being configured so that at the end of the casting step, the one-piece molded part comprises hollow parts formed by coring resulting from the presence of the core during casting, both in the support member and in all the connecting elements, and that each of the hollow parts opens into another part digs so that all of hollow portions communicate with each other and delimit, within the single-piece molded part, a single cavity corresponding to all or part of the impression left by the casting core and which extends both in the support member and in each of the connecting elements.
  • the core used may include, for its implementation in the mold:
  • FIG. 1 is a perspective view of an exemplary rocket support according to the invention
  • FIG. 2 is a longitudinal-lateral sectional view of the rocket support of FIG. 1;
  • FIG. 3 is a longitudinal cross-sectional view of the rocket support of FIG. 1; and FIG. 4 is a perspective view of an example of a core enabling the manufacture of the rocket support of FIGS. 1 to 3.
  • Figures 1 to 4 relate to an exemplary rocket support 10 according to the invention.
  • a three-dimensional orthogonal reference frame (X, Y, Z) is locally associated with the rocket support 10.
  • the X, Y, Z directions are respectively called “longitudinal”, “lateral”, “transverse”.
  • the rocket support 10 is intended for the rotational mounting of a hub (not shown) of a wheel of a motor vehicle, also called a "rocket".
  • the manufacture of the rocket support comprises a foundry operation, possibly followed by one or more machining operation (s) and / or one or more heat treatment operation (s).
  • the foundry operation comprises a step of casting an alloy (cast iron, steel, aluminum, metal, etc.) in a mold configured so as to obtain, after cooling of the cast iron, a constitutive monobloc molded part:
  • the rocket support 10 comprises, at the end of the foundry operation, a one-piece molded part constituting on the one hand a support member 1 1 delimiting a housing 15 for the rotational mounting of the hub and on the other hand a plurality of connecting elements 12, 13, 14 intended to be fixed respectively to the various members associated with the connecting elements.
  • the one-piece molded part comprises hollow parts formed by coring in both the support element 11 and in all the connecting elements 12, 13, 14, each of the hollow parts opening into another hollow part. so that all the hollow portions communicate with each other and delimit inside the one-piece molded part a cavity extending in the support member 1 1 and in each of the connecting elements 12, 13, 14.
  • the housing 15, which is intended to receive a bearing guide (not shown) in rotation of the hub, may adopt a generally bore, for example generally cylindrical bore optionally comprising radial grooves and / or shoulders.
  • the axis D of the bore constituting the housing 15 is oriented in the longitudinal direction X.
  • the housing 15 is configured so as to allow a press fitting. an outer race of the hub-turning guide bearing.
  • the hollow portion 1 1 1 formed in the support member 1 1 is arranged at the periphery of the housing 15, in particular in an annular manner generally included in a plane perpendicular to the axis D. This facilitates a particular but not mandatory organization in which the hollow portion of each of the connecting elements 12, 13, 14 opens into the hollow portion 1 January 1 of the support member 1 1, so as to form a generally octopus shaped cavity or spider centered on the hollow portion 1 1 1.
  • the plurality of connecting elements 12, 13, 14 comprises in particular in the case of a Mac-Pherson or pseudo Mac-Pherson assembly:
  • a first connecting element 12 coming from material from the support element 1 1 and intended to be fixed, in particular by a first ball joint, to a lower suspension arm (not shown) integral with the vehicle, constituting an integral member of the vehicle and associated with the first connecting element 12,
  • a second connecting element 13 made of material from the support member 11 and intended to be fixed, in particular by a second ball joint, to a steering rod (not shown) integral with the vehicle, constituting a integral member of the vehicle and associated with the second connecting element 13,
  • the first, second and third connecting elements 12, 13, 14 each comprise a hollow portion obtained by coring, respectively marked 121, 131, 141.
  • Each of the hollow portions 11, 121, 131, 141 is configured to open into at least one of the other hollow portions.
  • an advantageous provision is to provide that:
  • the first connecting element 12 is configured so that the hollow portion 121 formed in the first connecting element 12 opens into the hollow part 11 formed in the support element January 1,
  • the second connecting element 13 is configured so that the hollow portion 131 formed in the second connecting element 13 opens into the hollow part 11 formed in the support element January 1,
  • the third connecting element 14 is configured so that the hollow portion 141 formed in the third connecting element 14 opens into the hollow portion 1 1 1 formed in the support member January 1.
  • the one-piece molded part also comprises fastening elements 16 for fastening a braking device (not shown), in particular a brake caliper and / or a wheel lock monitoring sensor.
  • a rocket support 10 makes it possible to constitute an arrangement for a motor vehicle wheel train, notably a front or rear gear, advantageously of the Mac-Pherson or pseudo Mac-Pherson type.
  • the arrangement also comprises a wheel of the vehicle and a hub integral with the wheel and rotatably mounted at the housing 15 delimited by the support member 1 1 of the monoblock alloy piece of the rocket support 10.
  • the arrangement may also include:
  • the assembly being configured so as to constitute a type of wheel train
  • Mac-Pherson or pseudo Mac-Pherson.
  • the arrangement may finally comprise the rotation guide bearing of the hub.
  • This may comprise an outer cage force-fitted in the bore of the housing 15 and an outer cage force-fitted on the hub in the case of the so-called "first generation” assembly.
  • first generation outer cage force-fitted in the bore of the housing 15
  • second generation outer cage force-fitted on the hub
  • third generation the concept of the invention is not exclusive of any other rolling assembly.
  • the method of manufacturing the rocket support 10 comprises, prior to the casting step, a step of providing a single core 200 (refer to FIG.
  • the core 200 and its implementation being configured so that at the end of the casting step, the one-piece molded part comprises the hollow portions 1 1 1, 121, 131, 141 formed by coring resulting from the presence of the core 200 during casting, both in the support member 1 1 and in all the connecting elements 12, 13, 14.
  • Each of the hollow portions 1 1 1, 121, 131, 141 opens in another hollow part so that all the hollow portions 1 1 1, 121, 131, 141 communicate with each other and delimit inside the single-piece molded part a single cavity corresponding to all or part of the impression left by the core 200 to the casting and which extends both in the support element 1 1 and in each of the connecting elements 12, 13, 14.
  • the core 200 comprises:
  • a first zone 201 intended to form the hollow part 1 1 1 by coring effect in the support element January 1,
  • a third zone 203 intended to form the hollow portion 131 by coring effect in the second connecting element 13,
  • the core 200 used finally comprises, for its implementation in the mold: at least a first surface 205 for positioning the core 200 relative to the mold and arranged at the zone 202 of the core 200 forming, at the end of the casting the hollow part 121 formed in the first connecting element 12,
  • the core 200 for positioning the core 200 relative to the mold and arranged at another zone 203, 204 of the core 200 forming, after casting, the hollow portion 131, 141 formed in the second connecting element 13 and / or the third connecting element 14.
  • two such spans 206 are arranged, in the particular variant illustrated, on both sides of the zone 204 in the transverse direction Z.
  • the staves 205, 206 and their positions ensure good positioning and good stability of the core 200 in the mold and the removal of the core sand after stalling.
  • the footprints 17 left by the bearing surfaces 206 at the third connecting element 14 and the impression left by the bearing surface 205 are naturally obstructed during the assembly of the ball joint used for the connection to the lower suspension arm and during the assembly of the clevis of the damping device. This gives a sufficient seal to overcome external elements such as chippings in operation.
  • the multiplication of the hollow bearings 1 1 1, 121, 131, 141 allows a considerable weight gain of the rocket support 10, for example of the order of 12% on cast iron casting compared to solutions of the prior art.
  • the general organization allows a good resistance in operation and a good resistance to shocks.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Moulding By Coating Moulds (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

The invention relates to a stub-axle bracket (10) which includes an integral moulded part forming a support element (11) defining a recess (15) for rotatably mounting the hub as well as a plurality of linking elements (12, 13, 14) which are to be attached to various members secured to the vehicle and associated with said linking elements, respectively, in order to ensure the attachment of the stub-axle bracket onto the vehicle. The integral moulded part includes hollow portions (111, 121, 131, 141) formed by core-making in the support element as well as in all of the linking elements. Each of the hollow portions connects to another hollow portion such that all of the hollow portions communicate with one another and define, on the inside of the integral moulded part, a cavity that extends in the support element and in each of the linking elements. The invention also relates to an arrangement and a manufacturing method.

Description

Support de fusée à parties creuses par noyautage  Rocket support with hollow parts by coring
Domaine technique de l'invention L'invention concerne un support de fusée destiné au montage à rotation d'un moyeu d'une roue d'un véhicule automobile, comprenant une pièce moulée monobloc (fonte, acier, aluminium, etc ..) constitutive d'une part d'un élément de support délimitant un logement destiné au montage à rotation du moyeu et d'autre part d'une pluralité d'éléments de liaison destinés à être fixés respectivement à différents organes solidaires du véhicule et respectivement associés auxdits éléments de liaison pour assurer la fixation du support de fusée sur le véhicule. TECHNICAL FIELD OF THE INVENTION The invention relates to a rocket support for the rotational mounting of a hub of a wheel of a motor vehicle, comprising a one-piece molded part (cast iron, steel, aluminum, etc.) constituting on the one hand a support element delimiting a housing intended for the rotational mounting of the hub and on the other hand a plurality of connecting elements intended to be respectively fixed to different integral members of the vehicle and respectively associated with said elements link for securing the rocket carrier to the vehicle.
L'invention a pour objet également un agencement pour train de roues de véhicule automobile, notamment un train avant ou arrière, et un procédé de fabrication par fonderie du support de fusée. The invention also relates to an arrangement for a motor vehicle wheel train, in particular a front or rear axle, and a process for the casting of the rocket support.
État de la technique Classiquement, pour construire un train de roues de véhicule automobile, notamment un train avant, chaque roue du train est associée à un moyeu sensiblement cylindrique, également connue sous le nom « fusée ». Le moyeu est monté à rotation par rapport à un support de fusée ou porte-fusée par l'intermédiaire d'un roulement. Le support de fusée, couramment obtenu au moins par une opération de fonderie, comprend à cet effet un élément de support délimitant un logement de réception du roulement. Pour sa fixation au reste du véhicule, le support de fusée comprend aussi une pluralité d'éléments de liaison, notamment : State of the art Conventionally, to build a wheel train of a motor vehicle, including a nose gear, each wheel of the train is associated with a substantially cylindrical hub, also known as "rocket". The hub is rotatably mounted relative to a rocket or knuckle support via a bearing. The rocket support, currently obtained at least by a foundry operation, comprises for this purpose a support member delimiting a housing for receiving the bearing. For attachment to the rest of the vehicle, the rocket carrier also includes a plurality of link members, including:
un élément de liaison à un bras inférieur de suspension solidaire du véhicule, notamment avec interposition d'une rotule,  a connecting element to a lower suspension arm secured to the vehicle, in particular with the interposition of a ball joint,
et/ou un élément de liaison à une biellette de direction solidaire du véhicule, notamment avec interposition d'une rotule, et/ou un élément de liaison à un dispositif amortisseur et/ou ressort solidaire du véhicule, notamment par une liaison vissée ou une liaison encastrement par serrage ou pinçage. Dans le cas d'un train avant ou arrière de type Mac-Pherson ou pseudo Mac- Pherson, le support de fusée comprend chacun de ces trois éléments de liaison en sus de l'élément de support, lequel est globalement agencé au centre des éléments de liaison. Il peut également comprendre des éléments de fixation destinés à la fixation d'un dispositif de freinage, notamment d'un étrier de frein et/ou d'un capteur de surveillance de blocage de roue, d'une fonction étanchéité roulement à l'interface avec la transmission, d'éléments de fixations de protecteur de disque et de protecteur de soufflet de rotule. and / or a connecting element to a steering rod secured to the vehicle, in particular with the interposition of a ball joint, and / or a connecting element to a damping device and / or spring secured to the vehicle, in particular by a screw connection or a clamping or clamping connection. In the case of a Mac-Pherson or pseudo MacPherson type front or rear axle, the rocket support comprises each of these three connecting elements in addition to the support element, which is generally arranged in the center of the elements. link. It may also comprise fixing elements intended for fixing a braking device, in particular a brake caliper and / or a wheel lock monitoring sensor, a bearing sealing function at the interface with the transmission, disc guard fastener elements and ball joint bellows protector.
Il se pose donc, en sus de la facilité d'obtention, la problématique essentielle du poids formé par cet ensemble en regard du respect du cahier des charges en termes de respect des contraintes mécaniques en fonctionnement normal et en cas de choc. It thus raises, in addition to the ease of obtaining, the essential problematic of the weight formed by this set with respect to the respect of the specifications in terms of respect of the mechanical stresses in normal operation and in case of shock.
Pour tenter de répondre à ces objectifs, les documents EP1894816A2, EP0776814A1 et EP0980814A2 décrivent des solutions où l'élément de liaison du support de fusée au dispositif amortisseur comprend une partie creuse obtenue par noyautage au moment de l'opération de fonderie. In an attempt to meet these objectives, the documents EP1894816A2, EP0776814A1 and EP0980814A2 describe solutions where the connecting element of the rocket support to the damping device comprises a hollow portion obtained by coring at the time of the foundry operation.
Objet de l'invention Object of the invention
Le but de la présente invention est de proposer un support de fusée qui remédie aux inconvénients listés ci-dessus, notamment qui soit facile à obtenir, qui présente un poids contenu tout en ayant une résistance adaptée au respect d'un cahier des charges de fonctionnement normal et de conditions de choc. The object of the present invention is to provide a rocket support that overcomes the drawbacks listed above, in particular that is easy to obtain, which has a weight content while having a resistance adapted to compliance with a specification of operation. normal and shock conditions.
Un premier aspect de l'invention concerne un support de fusée destiné au montage à rotation d'un moyeu d'une roue d'un véhicule automobile, comprenant une pièce moulée monobloc constitutive d'une part d'un élément de support délimitant un logement destiné au montage à rotation du moyeu et d'autre part d'une pluralité d'éléments de liaison destinés à être fixés respectivement à différents organes solidaires du véhicule et respectivement associés auxdits éléments de liaison pour assurer la fixation du support de fusée sur le véhicule. La pièce moulée monobloc comprend des parties creuses formées par noyautage à la fois dans l'élément de support et dans tous les éléments de liaison, chacune des parties creuses débouchant dans une autre partie creuse de sorte que l'ensemble des parties creuses communiquent entre elles et délimitent à l'intérieur de la pièce moulée monobloc une cavité s'étendant dans l'élément de support et dans chacun des éléments de liaison. A first aspect of the invention relates to a rocket support for the rotational mounting of a hub of a wheel of a motor vehicle, comprising a one-piece molded part constituting on the one hand a support element delimiting a housing intended for the rotational mounting of the hub and on the other hand a plurality of connecting elements intended to be respectively fixed to different integral members of the hub; vehicle and respectively associated with said connecting elements for fixing the rocket support on the vehicle. The one-piece molded part comprises hollow parts formed by coring both in the support element and in all the connecting elements, each of the hollow parts opening into another hollow part so that all the hollow parts communicate with each other. and defining within the one-piece molded part a cavity extending in the support member and in each of the connecting members.
La partie creuse formée dans l'élément de support peut être agencée en périphérie dudit logement, notamment de manière annulaire globalement incluse dans un plan perpendiculaire à l'axe d'un alésage constitutif du logement. The hollow portion formed in the support member may be arranged at the periphery of said housing, in particular in an annular manner generally included in a plane perpendicular to the axis of a bore constituting the housing.
Le logement peut être configuré de sorte à permettre un emmanchement à force d'une cage extérieure d'un roulement de guidage à rotation du moyeu. The housing may be configured to allow for force-fitting of an outer cage of a hub-rotating guide bearing.
La pluralité d'éléments de liaison peut comprendre un premier élément de liaison venant de matière depuis l'élément de support et destiné à être fixé, notamment par une première liaison rotule, à un bras inférieur de suspension solidaire du véhicule, constitutif d'un organe solidaire du véhicule et associé audit premier élément de liaison. The plurality of connecting elements may comprise a first connecting element made of material from the support element and intended to be fixed, in particular by a first ball joint connection, to a lower suspension arm integral with the vehicle constituting a integral member of the vehicle and associated with said first connecting element.
Le premier élément de liaison peut être configuré de sorte que la partie creuse formée dans le premier élément de liaison débouche dans la partie creuse formée dans l'élément de support. The first link member may be configured such that the hollow portion formed in the first link member opens into the hollow portion formed in the support member.
La pluralité d'éléments de liaison peut comprendre un deuxième élément de liaison venant de matière depuis l'élément de support et destiné à être fixé, notamment par une deuxième liaison rotule, à une biellette de direction solidaire du véhicule, constitutive d'un organe solidaire du véhicule et associé audit deuxième élément de liaison. Le deuxième élément de liaison peut être configuré de sorte que la partie creuse formée dans le deuxième élément de liaison débouche dans la partie creuse formée dans l'élément de support. The plurality of connecting elements may comprise a second connecting element made of material from the support element and intended to be fixed, in particular by a second ball joint connection, to a steering rod secured to the vehicle, constituting a member secured to the vehicle and associated with said second connecting element. The second link member may be configured such that the hollow portion formed in the second link member opens into the hollow portion formed in the support member.
La pluralité d'éléments de liaison peut comprendre un troisième élément de liaison venant de matière depuis l'élément de support et destiné à être fixé, notamment par une liaison vissée ou une liaison encastrement par serrage ou pinçage, à un dispositif amortisseur et/ou ressort solidaire du véhicule, constitutif d'un organe solidaire du véhicule et associé audit troisième élément de liaison. The plurality of connecting elements may comprise a third connecting element made of material from the support element and intended to be fixed, in particular by a screw connection or a clamping or clamping connection, to a damping device and / or spring secured to the vehicle, constituting a member integral with the vehicle and associated with said third connecting element.
Le troisième élément de liaison peut être configuré de sorte que la partie creuse formée dans le troisième élément de liaison débouche dans la partie creuse formée dans l'élément de support. La pièce moulée monobloc peut comprendre des éléments de fixation destinés à la fixation d'un dispositif de freinage, notamment d'un étrier de frein et/ou d'un capteur de surveillance de blocage de roue. The third link member may be configured such that the hollow portion formed in the third link member opens into the hollow portion formed in the support member. The one-piece molded part may comprise fixing elements intended for fixing a braking device, in particular a brake caliper and / or a wheel lock monitoring sensor.
Un deuxième aspect de l'invention concerne un agencement pour train de roues de véhicule automobile, notamment un train avant ou arrière, qui comprend un tel support de fusée, une roue du véhicule et un moyeu solidaire de la roue et monté à rotation au niveau du logement délimité par l'élément de support de la pièce moulée monobloc du support de fusée. L'agencement peut comprendre : au moins un bras inférieur de suspension fixé, notamment par une première liaison rotule, à un premier élément de liaison de la pièce moulée monobloc du support de fusée, A second aspect of the invention relates to an arrangement for a motor vehicle wheel train, in particular a front or rear gear, which comprises such a rocket support, a wheel of the vehicle and a hub integral with the wheel and mounted to rotate at the the housing delimited by the support member of the integrally molded part of the rocket support. The arrangement may include: at least one lower suspension arm fixed, in particular by a first ball joint, to a first connecting element of the one-piece molded part of the rocket support,
et/ou une biellette de direction fixée, notamment par une deuxième liaison rotule, à un deuxième élément de liaison de la pièce moulée monobloc du support de fusée,  and / or a steering rod fixed, in particular by a second ball joint, to a second connecting element of the one-piece molded part of the rocket support,
et/ou un dispositif amortisseur et/ou ressort fixé, notamment par une liaison vissée ou une liaison encastrement par serrage ou pinçage, à un troisième élément de liaison de la pièce moulée monobloc du support de fusée, - l'ensemble étant configuré de sorte à constituer un train de roues de type Mac-Pherson ou pseudo Mac-Pherson.  and / or a damping and / or spring device fixed, in particular by a screw connection or a clamping or clamping connection, to a third connecting element of the one-piece molding of the rocket support, the assembly being configured so that to build a Mac-Pherson or pseudo Mac-Pherson wheelset.
Il peut comprendre un roulement de guidage en rotation du moyeu ayant une cage extérieure emmanchée à force dans un alésage du logement et une cage extérieure emmanchée à force sur le moyeu. It may comprise a bearing for rotating the hub having an outer cage force-fitted in a bore of the housing and an outer cage force-fitted on the hub.
Un troisième aspect de l'invention concerne enfin un procédé de fabrication par fonderie d'un support de fusée destiné au montage à rotation d'un moyeu d'une roue d'un véhicule automobile, comprenant une étape de coulée d'un alliage dans un moule configuré de sorte à obtenir, après refroidissement de l'alliage coulé, une pièce moulée monobloc constitutive d'une part d'un élément de support destiné au montage à rotation du moyeu et d'autre part d'une pluralité d'éléments de liaison destinés à être fixés respectivement à différents organes solidaires du véhicule et respectivement associés auxdits éléments de liaison pour assurer la fixation du support de fusée sur le véhicule. Le procédé comprend une étape de fourniture d'un noyau unique et de mise en place du noyau dans le moule préalablement à l'étape de coulée, le noyau et sa mise en place étant configurés de sorte qu'à l'issue de l'étape de coulée, la pièce moulée monobloc comprend des parties creuses formées par noyautage résultant de la présence du noyau durant la coulée, à la fois dans l'élément de support et dans tous les éléments de liaison, et que chacune des parties creuses débouche dans une autre partie creuse de sorte que l'ensemble des parties creuses communiquent entre elles et délimitent à l'intérieur de la pièce moulée monobloc une cavité unique correspondant à tout ou partie de l'empreinte laissée par le noyau à la coulée et qui s'étend à la fois dans l'élément de support et dans chacun des éléments de liaison. A third aspect of the invention finally relates to a method of manufacturing by casting a rocket support for the rotational mounting of a hub of a wheel of a motor vehicle, comprising a casting step of an alloy in a mold configured so as to obtain, after cooling of the cast alloy, a one-piece molded part constituting on the one hand a support element intended for the rotational mounting of the hub and on the other hand a plurality of elements linkages intended to be respectively fixed to different integral members of the vehicle and respectively associated with said connecting elements to ensure the attachment of the rocket carrier on the vehicle. The method comprises a step of providing a single core and placing the core in the mold prior to the casting step, the core and its implementation being configured so that at the end of the casting step, the one-piece molded part comprises hollow parts formed by coring resulting from the presence of the core during casting, both in the support member and in all the connecting elements, and that each of the hollow parts opens into another part digs so that all of hollow portions communicate with each other and delimit, within the single-piece molded part, a single cavity corresponding to all or part of the impression left by the casting core and which extends both in the support member and in each of the connecting elements.
Le noyau utilisé peut comprendre, pour sa mise en place dans le moule : The core used may include, for its implementation in the mold:
au moins une première portée pour positionner le noyau relativement au moule et agencée au niveau d'une zone du noyau formant, à l'issue de la coulée, la partie creuse formée dans un élément de liaison de la pièce moulée monobloc, notamment venant de matière depuis son élément de support et destiné à être fixé, notamment par une liaison rotule, à un bras inférieur de suspension solidaire du véhicule,  at least a first scope for positioning the core relative to the mold and arranged at a zone of the core forming, after casting, the hollow portion formed in a connecting element of the one-piece molded part, in particular coming from material from its support member and intended to be fixed, in particular by a ball joint connection, to a lower suspension arm integral with the vehicle,
et au moins une deuxième portée pour positionner le noyau relativement au moule et agencée au niveau d'une autre zone du noyau formant, à l'issue de la coulée, la partie creuse formée dans un autre élément de liaison de la pièce moulée monobloc, notamment un élément de liaison venant de matière depuis son élément de support et destiné à être fixé, notamment par une liaison vissée ou une liaison encastrement par serrage ou pinçage, à un dispositif amortisseur et/ou ressort solidaire du véhicule.  and at least one second span for positioning the core relative to the mold and arranged at another region of the core forming, after casting, the hollow portion formed in another connecting element of the one-piece molded part, in particular a connecting element made of material from its support member and intended to be fixed, in particular by a screw connection or a clamping or clamping connection, to a damping device and / or spring secured to the vehicle.
Description sommaire des dessins Brief description of the drawings
D'autres avantages et caractéristiques ressortiront plus clairement de la description qui va suivre de modes particuliers de réalisation de l'invention donnés à titre d'exemples non limitatifs et représentés sur les dessins annexés, dans lesquels : Other advantages and features will emerge more clearly from the following description of particular embodiments of the invention given as non-restrictive examples and shown in the accompanying drawings, in which:
- la figure 1 est une vue en perspective d'un exemple de support de fusée selon l'invention,  FIG. 1 is a perspective view of an exemplary rocket support according to the invention,
- la figure 2 est une vue en coupe longitudinale-latérale du support de fusée de la figure 1 ,  FIG. 2 is a longitudinal-lateral sectional view of the rocket support of FIG. 1;
- la figure 3 est une vue en coupe longitudinale-transversale du support de fusée de la figure 1 , - et la figure 4 est une vue en perspective d'un exemple d'un noyau permettant la fabrication du support de fusée des figures 1 à 3. FIG. 3 is a longitudinal cross-sectional view of the rocket support of FIG. 1; and FIG. 4 is a perspective view of an example of a core enabling the manufacture of the rocket support of FIGS. 1 to 3.
Description de modes préférentiels de l'invention Description of preferred modes of the invention
Les figures 1 à 4 sont relatives à un exemple de support de fusée 10 selon l'invention. Figures 1 to 4 relate to an exemplary rocket support 10 according to the invention.
Pour une meilleure clarté, un référentiel orthogonal tridimensionnel (X, Y, Z) est localement associé au support de fusée 10. Les directions X, Y, Z sont respectivement nommées « longitudinale », « latérale », « transversale ». For better clarity, a three-dimensional orthogonal reference frame (X, Y, Z) is locally associated with the rocket support 10. The X, Y, Z directions are respectively called "longitudinal", "lateral", "transverse".
Le support de fusée 10 est destiné au montage à rotation d'un moyeu (non représenté) d'une roue d'un véhicule automobile, aussi appelé « fusée ». La fabrication du support de fusée comprend une opération de fonderie, éventuellement suivie d'une ou plusieurs opération(s) d'usinage et/ou d'une ou plusieurs opération(s) de traitement thermique. The rocket support 10 is intended for the rotational mounting of a hub (not shown) of a wheel of a motor vehicle, also called a "rocket". The manufacture of the rocket support comprises a foundry operation, possibly followed by one or more machining operation (s) and / or one or more heat treatment operation (s).
L'opération de fonderie comprend une étape de coulée d'un alliage (fonte, acier, aluminium, métal, etc ..) dans un moule configuré de sorte à obtenir, après refroidissement de la fonte coulée, une pièce moulée monobloc constitutive : The foundry operation comprises a step of casting an alloy (cast iron, steel, aluminum, metal, etc.) in a mold configured so as to obtain, after cooling of the cast iron, a constitutive monobloc molded part:
d'une part d'un élément de support 1 1 destiné au montage à rotation du moyeu,  on the one hand a support element 1 1 intended for the rotational mounting of the hub,
- et d'autre part d'une pluralité d'éléments de liaison 12, 13, 14 destinés à être fixés respectivement à différents organes (non représentés) solidaires du véhicule et respectivement associés auxdits éléments de liaison 12, 13, 14 pour assurer la fixation du support de fusée 10 sur le véhicule. Autrement dit, le support de fusée 10 comprend, dès l'issue de l'opération de fonderie, une pièce moulée monobloc constitutive d'une part d'un élément de support 1 1 délimitant un logement 15 destiné au montage à rotation du moyeu et d'autre part d'une pluralité d'éléments de liaison 12, 13, 14 destinés à être fixés respectivement aux différents organes associés aux éléments de liaison. and on the other hand a plurality of connecting elements 12, 13, 14 intended to be fastened respectively to different members (not shown) integral with the vehicle and respectively associated with said connecting elements 12, 13, 14 to ensure the fixing the rocket support 10 on the vehicle. In other words, the rocket support 10 comprises, at the end of the foundry operation, a one-piece molded part constituting on the one hand a support member 1 1 delimiting a housing 15 for the rotational mounting of the hub and on the other hand a plurality of connecting elements 12, 13, 14 intended to be fixed respectively to the various members associated with the connecting elements.
Selon une caractéristique essentielle, la pièce moulée monobloc comprend des parties creuses formées par noyautage à la fois dans l'élément de support 1 1 et dans tous les éléments de liaison 12, 13, 14, chacune des parties creuses débouchant dans une autre partie creuse de sorte que l'ensemble des parties creuses communiquent entre elles et délimitent à l'intérieur de la pièce moulée monobloc une cavité s'étendant dans l'élément de support 1 1 et dans chacun des éléments de liaison 12, 13, 14. According to an essential characteristic, the one-piece molded part comprises hollow parts formed by coring in both the support element 11 and in all the connecting elements 12, 13, 14, each of the hollow parts opening into another hollow part. so that all the hollow portions communicate with each other and delimit inside the one-piece molded part a cavity extending in the support member 1 1 and in each of the connecting elements 12, 13, 14.
Le logement 15, qui est destiné à recevoir un roulement de guidage (non représenté) en rotation du moyeu, peut adopter une forme générale d'alésage, par exemple globalement cylindrique comprenant éventuellement des gorges radiales et/ou des épaulements. L'axe D de l'alésage constitutif du logement 15 est orienté selon la direction longitudinale X. En particulier dans le cas d'un montage dit « de première génération », le logement 15 est configuré de sorte à permettre un emmanchement à force d'une cage extérieure du roulement de guidage à rotation du moyeu. The housing 15, which is intended to receive a bearing guide (not shown) in rotation of the hub, may adopt a generally bore, for example generally cylindrical bore optionally comprising radial grooves and / or shoulders. The axis D of the bore constituting the housing 15 is oriented in the longitudinal direction X. In particular in the case of a so-called "first generation" assembly, the housing 15 is configured so as to allow a press fitting. an outer race of the hub-turning guide bearing.
La partie creuse 1 1 1 formée dans l'élément de support 1 1 est agencée en périphérie du logement 15, notamment de manière annulaire globalement incluse dans un plan perpendiculaire à l'axe D. Ceci facilite une organisation particulière mais non obligatoire dans laquelle la partie creuse de chacun des éléments de liaison 12, 13, 14 débouche dans la partie creuse 1 1 1 de l'élément de support 1 1 , de sorte à former une cavité en forme générale de pieuvre ou d'araignée centrée sur la partie creuse 1 1 1 . The hollow portion 1 1 1 formed in the support member 1 1 is arranged at the periphery of the housing 15, in particular in an annular manner generally included in a plane perpendicular to the axis D. This facilitates a particular but not mandatory organization in which the hollow portion of each of the connecting elements 12, 13, 14 opens into the hollow portion 1 January 1 of the support member 1 1, so as to form a generally octopus shaped cavity or spider centered on the hollow portion 1 1 1.
La pluralité d'éléments de liaison 12, 13, 14 comprend notamment dans le cas d'un montage Mac-Pherson ou pseudo Mac-Pherson : The plurality of connecting elements 12, 13, 14 comprises in particular in the case of a Mac-Pherson or pseudo Mac-Pherson assembly:
un premier élément de liaison 12 venant de matière depuis l'élément de support 1 1 et destiné à être fixé, notamment par une première liaison rotule, à un bras inférieur de suspension (non représenté) solidaire du véhicule, constitutif d'un organe solidaire du véhicule et associé au premier élément de liaison 12, a first connecting element 12 coming from material from the support element 1 1 and intended to be fixed, in particular by a first ball joint, to a lower suspension arm (not shown) integral with the vehicle, constituting an integral member of the vehicle and associated with the first connecting element 12,
et/ou un deuxième élément de liaison 13 venant de matière depuis l'élément de support 1 1 et destiné à être fixé, notamment par une deuxième liaison rotule, à une biellette de direction (non représentée) solidaire du véhicule, constitutive d'un organe solidaire du véhicule et associé au deuxième élément de liaison 13,  and / or a second connecting element 13 made of material from the support member 11 and intended to be fixed, in particular by a second ball joint, to a steering rod (not shown) integral with the vehicle, constituting a integral member of the vehicle and associated with the second connecting element 13,
et/ou un troisième élément de liaison 14 venant de matière depuis l'élément de support 1 1 et destiné à être fixé, notamment par une liaison vissée ou une liaison encastrement par serrage ou pinçage, à un dispositif amortisseur et/ou ressort solidaire du véhicule (non représentés), constitutif d'un organe solidaire du véhicule et associé au troisième élément de liaison 14. D'après ce qui précède, les premier, deuxième et troisième éléments de liaison 12, 13, 14 comprennent chacun une partie creuse obtenue par noyautage, respectivement repérées 121 , 131 , 141 . Chacune des parties creuses 1 1 1 , 121 , 131 , 141 est configurée de sorte à déboucher dans au moins l'une des autres parties creuses.  and / or a third connecting element 14 made of material from the support element January 1 and intended to be fixed, in particular by a screw connection or a connection by clamping or clamping, to a damping device and / or spring secured to vehicle (not shown) constituting an integral member of the vehicle and associated with the third connecting member 14. According to the above, the first, second and third connecting elements 12, 13, 14 each comprise a hollow portion obtained by coring, respectively marked 121, 131, 141. Each of the hollow portions 11, 121, 131, 141 is configured to open into at least one of the other hollow portions.
Comme indiqué précédemment, une disposition avantageuse consiste à prévoir que : As noted above, an advantageous provision is to provide that:
le premier élément de liaison 12 soit configuré de sorte que la partie creuse 121 formée dans le premier élément de liaison 12 débouche dans la partie creuse 1 1 1 formée dans l'élément de support 1 1 ,  the first connecting element 12 is configured so that the hollow portion 121 formed in the first connecting element 12 opens into the hollow part 11 formed in the support element January 1,
le deuxième élément de liaison 13 soit configuré de sorte que la partie creuse 131 formée dans le deuxième élément de liaison 13 débouche dans la partie creuse 1 1 1 formée dans l'élément de support 1 1 ,  the second connecting element 13 is configured so that the hollow portion 131 formed in the second connecting element 13 opens into the hollow part 11 formed in the support element January 1,
le troisième élément de liaison 14 soit configuré de sorte que la partie creuse 141 formée dans le troisième élément de liaison 14 débouche dans la partie creuse 1 1 1 formée dans l'élément de support 1 1 . La pièce moulée monobloc comprend aussi des éléments de fixation 16 destinés à la fixation d'un dispositif de freinage (non représenté), notamment d'un étrier de frein et/ou d'un capteur de surveillance de blocage de roue. Un tel support de fusée 10 permet de constituer un agencement pour train de roues de véhicule automobile, notamment un train avant ou arrière, avantageusement de type Mac-Pherson ou pseudo Mac-Pherson. L'agencement comprend aussi une roue du véhicule et un moyeu solidaire de la roue et monté à rotation au niveau du logement 15 délimité par l'élément de support 1 1 de la pièce en alliage monobloc du support de fusée 10. the third connecting element 14 is configured so that the hollow portion 141 formed in the third connecting element 14 opens into the hollow portion 1 1 1 formed in the support member January 1. The one-piece molded part also comprises fastening elements 16 for fastening a braking device (not shown), in particular a brake caliper and / or a wheel lock monitoring sensor. Such a rocket support 10 makes it possible to constitute an arrangement for a motor vehicle wheel train, notably a front or rear gear, advantageously of the Mac-Pherson or pseudo Mac-Pherson type. The arrangement also comprises a wheel of the vehicle and a hub integral with the wheel and rotatably mounted at the housing 15 delimited by the support member 1 1 of the monoblock alloy piece of the rocket support 10.
L'agencement peut aussi comprendre : The arrangement may also include:
au moins un bras inférieur de suspension fixé, notamment par une première liaison rotule, au premier élément de liaison 12,  at least one lower suspension arm fixed, in particular by a first ball joint, to the first connecting element 12,
- et/ou une biellette de direction fixée, notamment par une deuxième liaison rotule, au deuxième élément de liaison 13, and / or a steering rod fixed, in particular by a second ball joint, to the second connecting element 13,
et/ou un dispositif amortisseur et/ou ressort fixé, notamment par une liaison vissée ou une liaison encastrement par serrage ou pinçage, au troisième élément de liaison 14,  and / or a damping and / or spring device fixed, in particular by a screw connection or a clamping or clamping connection, to the third connecting element 14,
- l'ensemble étant configuré de sorte à constituer un train de roues de typethe assembly being configured so as to constitute a type of wheel train
Mac-Pherson ou pseudo Mac-Pherson. Mac-Pherson or pseudo Mac-Pherson.
L'agencement peut enfin comprendre le roulement de guidage en rotation du moyeu. Celui-ci peut comprendre une cage extérieure emmanchée à force dans l'alésage du logement 15 et une cage extérieure emmanchée à force sur le moyeu dans le cas du montage dit « de première génération ». Il reste que le concept de l'invention n'est pas exclusif de tout autre montage de roulement. Notamment, il est possible de prévoir un montage du roulement par vissage sur le support de fusée 10 dans le cas d'un montage dit « de deuxième génération » ou un montage du roulement par vissage sur le support de fusée 10 d'un ensemble formé préalablement par assemblage entre le moyeu et le roulement dans le cas d'un montage dit « de troisième génération ». Il résulte de ce qui précède que le procédé de fabrication du support de fusée 10 comprend, préalablement à l'étape de coulée, une étape de fourniture d'un noyau 200 unique (se référer à la figure 4) et de mise en place du noyau 200 dans le moule, le noyau 200 et sa mise en place étant configurés de sorte qu'à l'issue de l'étape de coulée, la pièce moulée monobloc comprend les parties creuses 1 1 1 , 121 , 131 , 141 formées par noyautage résultant de la présence du noyau 200 durant la coulée, à la fois dans l'élément de support 1 1 et dans tous les éléments de liaison 12, 13, 14. Chacune des parties creuses 1 1 1 , 121 , 131 , 141 débouche dans une autre partie creuse de sorte que l'ensemble des parties creuses 1 1 1 , 121 , 131 , 141 communiquent entre elles et délimitent à l'intérieur de la pièce moulée monobloc une cavité unique correspondant à tout ou partie de l'empreinte laissée par le noyau 200 à la coulée et qui s'étend à la fois dans l'élément de support 1 1 et dans chacun des éléments de liaison 12, 13, 14. The arrangement may finally comprise the rotation guide bearing of the hub. This may comprise an outer cage force-fitted in the bore of the housing 15 and an outer cage force-fitted on the hub in the case of the so-called "first generation" assembly. The fact remains that the concept of the invention is not exclusive of any other rolling assembly. In particular, it is possible to provide mounting of the bearing by screwing on the rocket support 10 in the case of a so-called "second generation" assembly or mounting of the bearing by screwing on the rocket support 10 of a formed assembly previously by assembly between the hub and the bearing in the case of a so-called "third generation" assembly. It follows from the foregoing that the method of manufacturing the rocket support 10 comprises, prior to the casting step, a step of providing a single core 200 (refer to FIG. 4) and of setting up the core 200 in the mold, the core 200 and its implementation being configured so that at the end of the casting step, the one-piece molded part comprises the hollow portions 1 1 1, 121, 131, 141 formed by coring resulting from the presence of the core 200 during casting, both in the support member 1 1 and in all the connecting elements 12, 13, 14. Each of the hollow portions 1 1 1, 121, 131, 141 opens in another hollow part so that all the hollow portions 1 1 1, 121, 131, 141 communicate with each other and delimit inside the single-piece molded part a single cavity corresponding to all or part of the impression left by the core 200 to the casting and which extends both in the support element 1 1 and in each of the connecting elements 12, 13, 14.
Sur la figure 4, le noyau 200 comprend : In FIG. 4, the core 200 comprises:
une première zone 201 destinée à former la partie creuse 1 1 1 par effet de noyautage dans l'élément de support 1 1 ,  a first zone 201 intended to form the hollow part 1 1 1 by coring effect in the support element January 1,
une deuxième zone 202 destinée à former la partie creuse 121 par effet de noyautage dans le premier élément de liaison 12,  a second zone 202 intended to form the hollow part 121 by coring effect in the first connecting element 12,
une troisième zone 203 destinée à former la partie creuse 131 par effet de noyautage dans le deuxième élément de liaison 13,  a third zone 203 intended to form the hollow portion 131 by coring effect in the second connecting element 13,
et une quatrième zone 204 destinée à former la partie creuse 141 par effet de noyautage dans le troisième élément de liaison 14.  and a fourth zone 204 for forming the hollow portion 141 by coring effect in the third connecting element 14.
Le noyau 200 utilisé comprend enfin, pour sa mise en place dans le moule : au moins une première portée 205 pour positionner le noyau 200 relativement au moule et agencée au niveau de la zone 202 du noyau 200 formant, à l'issue de la coulée, la partie creuse 121 formée dans le premier élément de liaison 12, The core 200 used finally comprises, for its implementation in the mold: at least a first surface 205 for positioning the core 200 relative to the mold and arranged at the zone 202 of the core 200 forming, at the end of the casting the hollow part 121 formed in the first connecting element 12,
et au moins une deuxième portée 206 pour positionner le noyau 200 relativement au moule et agencée au niveau d'une autre zone 203, 204 du noyau 200 formant, à l'issue de la coulée, la partie creuse 131 , 141 formée dans le deuxième élément de liaison 13 et/ou le troisième élément de liaison 14. Par exemple, deux telles portées 206 sont disposées, dans la variante particulière illustrée, de part et d'autre de la zone 204 selon la direction transversale Z. and at least one second span 206 for positioning the core 200 relative to the mold and arranged at another zone 203, 204 of the core 200 forming, after casting, the hollow portion 131, 141 formed in the second connecting element 13 and / or the third connecting element 14. For example, two such spans 206 are arranged, in the particular variant illustrated, on both sides of the zone 204 in the transverse direction Z.
Les portées 205, 206 et leurs positions assurent un bon positionnement et une bonne stabilité du noyau 200 dans le moule et l'évacuation du sable à noyau après décochage. Les empreintes 17 laissées par les portées 206 au niveau du troisième élément de liaison 14 et l'empreinte laissée par la portée 205 sont obstruées naturellement lors du montage de la rotule utilisée pour la liaison au bras de suspension inférieur et lors du montage de la chape du dispositif amortisseur. Ceci confère une étanchéité suffisante pour s'affranchir d'éléments externes tels que des gravillons en fonctionnement. The staves 205, 206 and their positions ensure good positioning and good stability of the core 200 in the mold and the removal of the core sand after stalling. The footprints 17 left by the bearing surfaces 206 at the third connecting element 14 and the impression left by the bearing surface 205 are naturally obstructed during the assembly of the ball joint used for the connection to the lower suspension arm and during the assembly of the clevis of the damping device. This gives a sufficient seal to overcome external elements such as chippings in operation.
Outre ces facilités de fabrication, la multiplication des portées creuses 1 1 1 , 121 , 131 , 141 permet un gain de poids considérable du support de fusée 10, par exemple de l'ordre de 12% sur pièce moulée en fonte par rapport à des solutions de l'art antérieur. L'organisation générale permet une bonne résistance en fonctionnement et une bonne tenue aux chocs. In addition to these manufacturing facilities, the multiplication of the hollow bearings 1 1 1, 121, 131, 141 allows a considerable weight gain of the rocket support 10, for example of the order of 12% on cast iron casting compared to solutions of the prior art. The general organization allows a good resistance in operation and a good resistance to shocks.

Claims

REVENDICATIONS
1 . Support de fusée (10) destiné au montage à rotation d'un moyeu d'une roue d'un véhicule automobile, comprenant une pièce moulée monobloc constitutive d'une part d'un élément de support (1 1 ) délimitant un logement (15) destiné au montage à rotation du moyeu et d'autre part d'une pluralité d'éléments de liaison (12, 13, 14) destinés à être fixés respectivement à différents organes solidaires du véhicule et respectivement associés auxdits éléments de liaison pour assurer la fixation du support de fusée sur le véhicule, caractérisé en ce que la pièce moulée monobloc comprend des parties creuses (1 1 1 , 121 , 131 , 141 ) formées par noyautage à la fois dans l'élément de support et dans tous les éléments de liaison, chacune des parties creuses débouchant dans une autre partie creuse de sorte que l'ensemble des parties creuses communiquent entre elles et délimitent à l'intérieur de la pièce moulée monobloc une cavité s'étendant dans l'élément de support et dans chacun des éléments de liaison. 1. Rocket support (10) for the rotational mounting of a hub of a wheel of a motor vehicle, comprising a one-piece molded part constituting on the one hand a support element (1 1) delimiting a housing (15). ) for the rotational mounting of the hub and secondly of a plurality of connecting elements (12, 13, 14) intended to be respectively fixed to different integral members of the vehicle and respectively associated with said connecting elements to ensure the fixing the rocket support to the vehicle, characterized in that the one-piece molded part comprises hollow parts (1 1 1, 121, 131, 141) formed by coring both in the support element and in all the elements of connection, each of the hollow portions opening into another hollow portion so that all the hollow portions communicate with each other and delimit inside the one-piece molded part a cavity extending in the element d e support and in each of the connecting elements.
2. Support de fusée selon la revendication 1 , caractérisé en ce que la partie creuse (1 1 1 ) formée dans l'élément de support (1 1 ) est agencée en périphérie dudit logement (15), notamment de manière annulaire globalement incluse dans un plan perpendiculaire à l'axe (D) d'un alésage constitutif du logement. 2. rocket support according to claim 1, characterized in that the hollow portion (1 1 1) formed in the support member (1 1) is arranged at the periphery of said housing (15), in particular ring-shaped generally included in a plane perpendicular to the axis (D) of a bore constituting the housing.
3. Support de fusée selon l'une des revendications 1 et 2, caractérisé en ce que le logement est configuré de sorte à permettre un emmanchement à force d'une cage extérieure d'un roulement de guidage à rotation du moyeu. 3. rocket support according to one of claims 1 and 2, characterized in that the housing is configured to allow a force fitting of an outer cage of a hub rotation bearing bearing.
4. Support de fusée selon l'une des revendications 1 à 3, caractérisé en ce que la pluralité d'éléments de liaison comprend un premier élément de liaisonRocket support according to one of claims 1 to 3, characterized in that the plurality of connecting elements comprises a first connecting element
(12) venant de matière depuis l'élément de support (1 1 ) et destiné à être fixé, notamment par une première liaison rotule, à un bras inférieur de suspension solidaire du véhicule, constitutif d'un organe solidaire du véhicule et associé audit premier élément de liaison. (12) made of material from the support member (1 1) and intended to be fixed, in particular by a first ball joint, to a lower suspension arm integral with the vehicle, constituting a member secured to the vehicle and associated with said first link element.
5. Support de fusée selon la revendication 4, caractérisé en ce que le premier élément de liaison est configuré de sorte que la partie creuse (121 ) formée dans le premier élément de liaison débouche dans la partie creuse (1 1 1 ) formée dans l'élément de support (1 1 ). Rocket support according to claim 4, characterized in that the first connecting element is configured so that the hollow part (121) formed in the first connecting element opens into the hollow part (1 1 1) formed in the support member (1 1).
6. Support de fusée selon l'une des revendications 1 à 5, caractérisé en ce que la pluralité d'éléments de liaison comprend un deuxième élément de liaisonRocket support according to one of claims 1 to 5, characterized in that the plurality of connecting elements comprises a second connecting element
(13) venant de matière depuis l'élément de support (1 1 ) et destiné à être fixé, notamment par une deuxième liaison rotule, à une biellette de direction solidaire du véhicule, constitutive d'un organe solidaire du véhicule et associé audit deuxième élément de liaison. (13) from material from the support member (1 1) and intended to be fixed, in particular by a second ball joint, to a steering rod integral with the vehicle, constituting a member secured to the vehicle and associated with said second connecting element.
7. Support de fusée selon la revendication 6, caractérisé en ce que le deuxième élément de liaison est configuré de sorte que la partie creuse (131 ) formée dans le deuxième élément de liaison débouche dans la partie creuse (1 1 1 ) formée dans l'élément de support (1 1 ). Rocket support according to claim 6, characterized in that the second connecting element is configured so that the hollow part (131) formed in the second connecting element opens into the hollow part (1 1 1) formed in the support member (1 1).
8. Support de fusée selon l'une des revendications 1 à 7, caractérisé en ce que la pluralité d'éléments de liaison comprend un troisième élément de liaisonRocket support according to one of claims 1 to 7, characterized in that the plurality of connecting elements comprises a third connecting element
(14) venant de matière depuis l'élément de support (1 1 ) et destiné à être fixé, notamment par une liaison vissée ou une liaison encastrement par serrage ou pinçage, à un dispositif amortisseur et/ou ressort solidaire du véhicule, constitutif d'un organe solidaire du véhicule et associé audit troisième élément de liaison. (14) made of material from the support element (1 1) and intended to be fixed, in particular by a screw connection or a connection fitting by clamping or clamping, to a damping device and / or spring secured to the vehicle, constituting a an integral member of the vehicle and associated with said third connecting element.
9. Support de fusée selon la revendication 8, caractérisé en ce que le troisième élément de liaison est configuré de sorte que la partie creuse (141 ) formée dans le troisième élément de liaison débouche dans la partie creuse (1 1 1 ) formée dans l'élément de support (1 1 ). Rocket holder according to Claim 8, characterized in that the third connecting element is configured such that the hollow part (141) formed in the third connecting element opens into the hollow part (11 1) formed in the support member (1 1).
10. Support de fusée selon l'une des revendications 1 à 9, caractérisé en ce que la pièce moulée monobloc comprend des éléments de fixation (16) destinés à la fixation d'un dispositif de freinage, notamment d'un étrier de frein et/ou d'un capteur de surveillance de blocage de roue. Rocket support according to one of claims 1 to 9, characterized in that the one-piece molded part comprises fastening elements (16) for fixing a braking device, in particular a brake caliper and / or a wheel lock monitoring sensor.
1 1 . Agencement pour train de roues de véhicule automobile, notamment un train avant ou arrière, caractérisé en ce qu'il comprend un support de fusée (10) selon l'une quelconque des revendications 1 à 10, une roue du véhicule et un moyeu solidaire de la roue et monté à rotation au niveau du logement (15) délimité par l'élément de support de la pièce moulée monobloc du support de fusée. 1 1. Arrangement for a motor vehicle wheel train, in particular a front or rear axle, characterized in that it comprises a rocket support (10) according to any one of claims 1 to 10, a wheel of the vehicle and a hub integral with the wheel and rotatably mounted at the housing (15) defined by the support member of the integrally molded part of the rocket support.
12. Agencement selon la revendication 1 1 , caractérisé en ce qu'il comprend : au moins un bras inférieur de suspension fixé, notamment par une première liaison rotule, à un premier élément de liaison (12) de la pièce moulée monobloc du support de fusée (10), 12. Arrangement according to claim 1 1, characterized in that it comprises: at least one lower suspension arm fixed, in particular by a first ball joint, to a first connecting element (12) of the one-piece molded part of the support of rocket (10),
- et/ou une biellette de direction fixée, notamment par une deuxième liaison rotule, à un deuxième élément de liaison (13) de la pièce moulée monobloc du support de fusée (10), and / or a steering rod fixed, in particular by a second ball joint, to a second connecting element (13) of the one-piece molded part of the rocket support (10),
et/ou un dispositif amortisseur et/ou ressort fixé, notamment par une liaison vissée ou une liaison encastrement par serrage ou pinçage, à un troisième élément de liaison (14) de la pièce moulée monobloc du support de fusée (10),  and / or a damping and / or spring device fixed, in particular by a screw connection or a clamping or clamping connection, to a third connecting element (14) of the one-piece molding of the rocket support (10),
l'ensemble étant configuré de sorte à constituer un train de roues de type Mac-Pherson ou pseudo Mac-Pherson.  the assembly being configured so as to constitute a Mac-Pherson or pseudo Mac-Pherson wheelset.
13. Agencement selon l'une des revendications 1 1 et 12, caractérisé en ce qu'il comprend un roulement de guidage en rotation du moyeu ayant une cage extérieure emmanchée à force dans un alésage du logement (15) et une cage extérieure emmanchée à force sur le moyeu. 13. Arrangement according to one of claims 1 1 and 12, characterized in that it comprises a bearing for rotating the hub having an outer cage force-fitted in a bore of the housing (15) and an outer cage fitted to force on the hub.
14. Procédé de fabrication par fonderie d'un support de fusée (10) destiné au montage à rotation d'un moyeu d'une roue d'un véhicule automobile, comprenant une étape de coulée d'un alliage dans un moule configuré de sorte à obtenir, après refroidissement de l'alliage coulé, une pièce moulée monobloc constitutive d'une part d'un élément de support (1 1 ) destiné au montage à rotation du moyeu et d'autre part d'une pluralité d'éléments de liaison (12, 13, 14) destinés à être fixés respectivement à différents organes solidaires du véhicule et respectivement associés auxdits éléments de liaison pour assurer la fixation du support de fusée (10) sur le véhicule, procédé caractérisé en ce qu'il comprend une étape de fourniture d'un noyau (200) unique et de mise en place du noyau dans le moule préalablement à l'étape de coulée, le noyau et sa mise en place étant configurés de sorte qu'à l'issue de l'étape de coulée, la pièce moulée monobloc comprend des parties creuses (1 1 1 , 121 , 131 , 141 ) formées par noyautage résultant de la présence du noyau (200) durant la coulée, à la fois dans l'élément de support (1 1 ) et dans tous les éléments de liaison (12, 13, 14), et que chacune des parties creuses débouche dans une autre partie creuse de sorte que l'ensemble des parties creuses communiquent entre elles et délimitent à l'intérieur de la pièce moulée monobloc une cavité unique correspondant à tout ou partie de l'empreinte laissée par le noyau (200) à la coulée et qui s'étend à la fois dans l'élément de support (1 1 ) et dans chacun des éléments de liaison (12, 13, 14). 14. A method of manufacturing by casting a rocket support (10) for the rotational mounting of a hub of a wheel of a motor vehicle, comprising a step of casting an alloy in a mold configured so to obtain, after cooling of the cast alloy, a one-piece molded part constituting on the one hand a support element (1 1) intended for the rotational mounting of the hub and on the other hand a plurality of elements of link (12, 13, 14) intended to be fixed respectively to various members integral with the vehicle and respectively associated with said connecting elements to ensure the attachment of the rocket support (10) to the vehicle, characterized in that it comprises a step of providing a single core (200) and placing the core in the mold prior to the casting step, the core and its implementation being configured so that at the end of the step casting, the one-piece molded part comp makes hollow portions (11, 121, 131, 141) formed by coring resulting from the presence of the core (200) during casting, both in the support member (1 1) and in all the elements of link (12, 13, 14), and that each of the hollow portions opens into another hollow portion so that all the hollow portions communicate with each other and delimit inside the single-piece molded part a single cavity corresponding to all or part of the impression left by the casting core (200) and which extends into both the support member (1 1) and each of the connecting members (12, 13, 14).
15. Procédé selon la revendication 14, caractérisé en ce que le noyau utilisé comprend, pour sa mise en place dans le moule : 15. The method of claim 14, characterized in that the core used comprises, for its implementation in the mold:
au moins une première portée (205) pour positionner le noyau (200) relativement au moule et agencée au niveau d'une zone (202) du noyau formant, à l'issue de la coulée, la partie creuse (121 ) formée dans un élément de liaison (12) de la pièce moulée monobloc, notamment venant de matière depuis son élément de support (1 1 ) et destiné à être fixé, notamment par une liaison rotule, à un bras inférieur de suspension solidaire du véhicule,  at least a first bearing surface (205) for positioning the core (200) relative to the mold and arranged at a zone (202) of the core forming, at the end of the casting, the hollow portion (121) formed in a connecting element (12) of the one-piece molded part, in particular material coming from its support member (1 1) and intended to be fixed, in particular by a ball joint connection, to a lower suspension arm integral with the vehicle,
- et au moins une deuxième portée (206) pour positionner le noyau (200) relativement au moule et agencée au niveau d'une autre zone (203, 204) du noyau formant, à l'issue de la coulée, la partie creuse (131 , 141 ) formée dans un autre élément de liaison (13, 14) de la pièce moulée monobloc, notamment un élément de liaison (14) venant de matière depuis son élément de support (1 1 ) et destiné à être fixé, notamment par une liaison vissée ou une liaison encastrement par serrage ou pinçage, à un dispositif amortisseur et/ou ressort solidaire du véhicule. and at least one second span (206) for positioning the core (200) relative to the mold and arranged at another zone (203, 204) of the core forming, at the end of the casting, the hollow part (131, 141) formed in another connecting element (13, 14) of the one-piece molded part, in particular a connecting element (14) coming from its material since its support element (1 1) and intended to be fixed, in particular by a screw connection or a connection fitting by clamping or clamping, to a damping device and / or spring secured to the vehicle.
PCT/FR2013/051541 2012-07-05 2013-07-01 Stub-axle bracket with hollow portions by core-making WO2014006315A1 (en)

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FR1256452A FR2992892B1 (en) 2012-07-05 2012-07-05 ROCKER BRACKET HINGED BY HOLES
FR1256452 2012-07-05

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014116823A1 (en) 2013-11-26 2015-05-28 Ksm Castings Group Gmbh wheel carrier
DE102014212514A1 (en) 2014-06-27 2015-12-31 Volkswagen Aktiengesellschaft pivot bearing
FR3052134A1 (en) * 2016-06-06 2017-12-08 Peugeot Citroen Automobiles Sa FRONT VEHICLE TRAIN WITH MODULAR INTERFACE PARTS FOR PIVOT / SUSPENSION TRIANGLE BODY CONNECTIONS
CN107985401A (en) * 2017-10-27 2018-05-04 浙江吉利控股集团有限公司 A kind of knuckle for vehicle
EP3418157A4 (en) * 2016-06-06 2019-01-02 Mazda Motor Corporation Automobile knuckle manufacturing method and automobile knuckle
CN112208634A (en) * 2020-09-30 2021-01-12 浙江零跑科技有限公司 Lightweight aluminum steering knuckle structure

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0776814A1 (en) 1995-11-28 1997-06-04 Alusuisse Technology & Management AG Manufacturing process for a pivoted support of the wheel suspension of a vehicle
EP0980814A2 (en) 1998-07-31 2000-02-23 Delphi Technologies, Inc. Steering knuckle and method of manufacture
EP1894816A2 (en) 2006-09-01 2008-03-05 Zeschky Galvanik GMBH & Co.KG Pivot bearing for automobile front wheel suspension
US20120049477A1 (en) * 2010-08-31 2012-03-01 Gm Global Technology Operations, Inc. Steering knuckle and method of forming same

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0776814A1 (en) 1995-11-28 1997-06-04 Alusuisse Technology & Management AG Manufacturing process for a pivoted support of the wheel suspension of a vehicle
EP0980814A2 (en) 1998-07-31 2000-02-23 Delphi Technologies, Inc. Steering knuckle and method of manufacture
EP1894816A2 (en) 2006-09-01 2008-03-05 Zeschky Galvanik GMBH & Co.KG Pivot bearing for automobile front wheel suspension
US20120049477A1 (en) * 2010-08-31 2012-03-01 Gm Global Technology Operations, Inc. Steering knuckle and method of forming same

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014116823A1 (en) 2013-11-26 2015-05-28 Ksm Castings Group Gmbh wheel carrier
DE102014212514A1 (en) 2014-06-27 2015-12-31 Volkswagen Aktiengesellschaft pivot bearing
FR3052134A1 (en) * 2016-06-06 2017-12-08 Peugeot Citroen Automobiles Sa FRONT VEHICLE TRAIN WITH MODULAR INTERFACE PARTS FOR PIVOT / SUSPENSION TRIANGLE BODY CONNECTIONS
EP3418157A4 (en) * 2016-06-06 2019-01-02 Mazda Motor Corporation Automobile knuckle manufacturing method and automobile knuckle
US10926583B2 (en) 2016-06-06 2021-02-23 Mazda Motor Corporation Method for manufacturing automobile knuckle and automobile knuckle
CN107985401A (en) * 2017-10-27 2018-05-04 浙江吉利控股集团有限公司 A kind of knuckle for vehicle
CN112208634A (en) * 2020-09-30 2021-01-12 浙江零跑科技有限公司 Lightweight aluminum steering knuckle structure
CN112208634B (en) * 2020-09-30 2021-10-22 浙江零跑科技股份有限公司 Lightweight aluminum steering knuckle structure

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FR2992892A1 (en) 2014-01-10

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