EP0331539B1 - Method of making forged blanks from bar material by upsetting, in particular for compressor blades, and tooling equipment for carrying out the method - Google Patents
Method of making forged blanks from bar material by upsetting, in particular for compressor blades, and tooling equipment for carrying out the method Download PDFInfo
- Publication number
- EP0331539B1 EP0331539B1 EP89400273A EP89400273A EP0331539B1 EP 0331539 B1 EP0331539 B1 EP 0331539B1 EP 89400273 A EP89400273 A EP 89400273A EP 89400273 A EP89400273 A EP 89400273A EP 0331539 B1 EP0331539 B1 EP 0331539B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- container
- upsetting
- bar
- stage
- section
- 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
Links
- 238000000034 method Methods 0.000 title claims description 35
- 238000004519 manufacturing process Methods 0.000 title claims description 12
- 239000000463 material Substances 0.000 title description 2
- 230000008569 process Effects 0.000 claims description 26
- 238000005242 forging Methods 0.000 claims description 6
- 230000009471 action Effects 0.000 claims description 4
- 230000007547 defect Effects 0.000 description 7
- 229910045601 alloy Inorganic materials 0.000 description 5
- 239000000956 alloy Substances 0.000 description 5
- 238000012681 fiber drawing Methods 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 241001644893 Entandrophragma utile Species 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000002427 irreversible effect Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/06—Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
- B21J5/08—Upsetting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/008—Incremental forging
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K3/00—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like
- B21K3/04—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like blades, e.g. for turbines; Upsetting of blade roots
Definitions
- the present invention relates to a process for manufacturing blanks forged at the foot of a turbomachine compressor blade by upsetting as well as a tool intended for the implementation of said process according to the preamble of claims 1 and 5.
- Figures 1a, 1b, 1c, 1d of the accompanying drawings illustrate the production of a delivery on a bar B, placed in a container A, during which during four successive operations corresponding respectively to the four figures, a reduction in length l1, l2, l3 and l4 is obtained and the phenomena which have just been reported (buckling then twisting) appear leading to the defects which have been noted (folds and disturbed fiber drawing).
- a discharge tool wrapping a bar forged blank intended for the implementation of said method is defined by the combination of characteristics of claim 5.
- the first container has a cruciform section cavity, the cylindrical bar being in contact with the interior surface of the container along four generatrices located at 90 ° from one another and the second container has a square section cavity , with rounded corners, the tops of the protuberances or lobes of the cruciform section of the bar obtained at the end of the first step being in contact respectively with one side of said square.
- the bar is held in support at least along three generatrices, thus avoiding any deformation by buckling, while the flow of the alloy can only be done in the direction hollow parts of the container, thus making any torsional deformation impossible.
- the contact maintained between the end generators of the blank and the walls of the container prevents any deformation by buckling or twisting.
- the method for manufacturing blanks forged by upsetting according to the invention applies in particular to bar products such as a cylindrical bar 1 shown in its initial form in FIGS. 2a and 2b.
- the bar 1 is placed in a first container 2 secured to a forging press or machine repress of a type known per se which is not shown in more detail in the drawings.
- a forging press or machine repress of a type known per se which is not shown in more detail in the drawings.
- one end 1a of the bar 1 is subjected to the pushing action of a punch 3 moved by the pushing and control means of said machine.
- the portion 1b of the bar 1 subjected to the upsetting thus tends to occupy the available volume of the container 2 limited by the face of the punch 3, which results in a reduction in length of said portion 1b, accompanied by an increase in the corresponding cross section. .
- the first container 2 used during the first step of the upsetting process comprises a cavity 4 which has in cross section a generally cruciform shape composed of four lobed parts 4a, 4b, 4c, 4d arranged symmetrically in pairs, thus providing four generators 5a, 5b, 5c, 5d located at 90 ° one from the other, which cooperate with four corresponding generatrices of the repressed portion 1b of the bar 1 while maintaining, from a first deformation stage, permanent contact with them during the repression step .
- Said contact following the generators between container and bar becomes necessary from the moment when during the upsetting operation there are risks of creating irreversible defects by buckling or twisting. Contact can be made from the start of the operation.
- the intermediate blank 1c obtained at the end of the first step (a) is placed in a second container 6, as shown diagrammatically in FIGS. 4a and 4b, and its end is again subjected to the pushing action of a punch 7.
- the second container 6 has a cavity 8 which has in cross section a generally square shape, with rounded corners.
- Intermediate draft 1c has a cruciform section which reproduces the shape of the cavity 4 of the first container 2 and the generators 1d, 1e, 1f and 1g corresponding to the vertices of the lobed parts of this cruciform section of the intermediate blank 1c are placed in contact with lines of corresponding support of the sides of the square of cavity of the second container 6 and in a similar manner to the first step (a), during the second step (b) of delivery, the contact is also maintained permanently, from a first deformation stage, at the level of these four symmetrical generators two by two, between the external surface of the blank 1c and the surface of the cavity 8 of the second container 6.
- a variable radial clearance from O to O, 5 mm in the present application, can be provided at the start of the second step between the cooperating generators of the bar and of the container.
- the initial upsetting portion 1b has a final section 1d of forged blank as shown in FIG. 5 in the embodiment which comes from 'be described.
- This repressed portion of bar 1b may in particular be intended to constitute the base of a turbomachine blade obtained by forging.
- 7a, 7b, 7c respectively represent, in a schematic section, other usable forms of container cavity 9a, 9b, 9c, respectively associated with a portion of bar to be driven back section 10a, 10b, 10c, 10c, 10d.
- This bar section at the start is of a shape adapted to the final part to be obtained and, in addition to being cylindrical, can in particular be rectangular or square.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Forging (AREA)
Description
La présente invention concerne un procédé de fabrication d'ébauches forgées en barre du pied d'une aube de compresseur de turbomachine par refoulage ainsi qu'un outillage destiné à la mise en oeuvre dudit procédé selon le préambule des revendications 1 et 5.The present invention relates to a process for manufacturing blanks forged at the foot of a turbomachine compressor blade by upsetting as well as a tool intended for the implementation of said process according to the preamble of
Il est courant dans la fabrication de certaines pièces telles que des aubes de compresseur à partir d'ébauches forgées d'effectuer une opération de refoulage de l'extrémité d'une barre cylindrique afin d'obtenir par augmentation de la section le volume de matière necessaire, par exemple, à la réalisation du pied dans le cas d'une aube.It is common in the manufacture of certain parts such as compressor blades from forged blanks to carry out a pressing operation at the end of a cylindrical bar in order to obtain the volume of material by increasing the section. necessary, for example, for the realization of the foot in the case of a dawn.
Dans les données de définition d'une telle opération de refoulage, on peut retenir deux types de paramètres :
- des paramètres technologiques tel que le taux de refoulage t, défini par :
où Lo est la longueur initiale de la portion de barre à refouler,
Ll est la longueur de cette même portion après refoulage,
Do est le diamètre initial de la barre à refouler ;
Lo - Ll représente la course utile du poinçon de la machine de forgeage utilisée et la limite supérieure de cette course est une donnée de construction de ladite machine ; - des paramètres métallurgiques et notamment le rapport de réduction r défini par :
où So est la section transversale initiale de la barre,
Sl est la section transversale de la barre après refoulage et Dl est le diamètre correspondant.
- technological parameters such as the delivery rate t, defined by:
where Lo is the initial length of the portion of bar to be driven back,
Ll is the length of this same portion after upsetting,
Do is the initial diameter of the bar to be driven;
Lo - Ll represents the useful stroke of the punch of the forging machine used and the upper limit of this stroke is a data of construction of said machine; - metallurgical parameters and in particular the reduction ratio r defined by:
where So is the initial cross section of the bar,
Sl is the cross section of the bar after upsetting and Dl is the corresponding diameter.
Dans les diverses applications connues du procédé de refoulage, il apparaît que pour éviter des défauts inacceptables sur les ébauches obtenues, le procédé est soumis à des limitations géométriques. Ces défauts dus à une maîtrise insuffisante de la déformation au cours de l'opération consistent notamment en replis qui peuvent être dus à un phénomène de flambage de la portion de barre à refouler ou en un fibrage perturbé, dû à un phénomène de torsion de la barre après flambage.In the various known applications of the upsetting process, it appears that to avoid unacceptable defects on the blanks obtained, the process is subject to geometric limitations. These defects due to insufficient control of the deformation during the operation consist in particular of folds which may be due to a phenomenon of buckling of the portion of bar to be driven back or to a disturbed fiber drawing, due to a phenomenon of torsion of the bar after buckling.
Les figures 1a, 1b, 1c, 1d des dessins joints en annexe illustrent la réalisation d'un refoulage sur une barre B, placée dans un conteneur A, au cours duquel lors de quatre opérations successives correspondant respectivement aux quatre figures, une réduction de longueur l₁, l₂, l₃ et l₄ est obtenue et les phénomènes qui viennent d'être signalés (flambage puis torsion) apparaissent conduisant aux défauts qui ont été notés (replis et fibrage perturbé).Figures 1a, 1b, 1c, 1d of the accompanying drawings illustrate the production of a delivery on a bar B, placed in a container A, during which during four successive operations corresponding respectively to the four figures, a reduction in length l₁, l₂, l₃ and l₄ is obtained and the phenomena which have just been reported (buckling then twisting) appear leading to the defects which have been noted (folds and disturbed fiber drawing).
Il est couramment admis que pour éviter ces défauts, une valeur limite supérieure du taux de refoulage t de 4 lorsque le refoulage est effectué en une opération ou de 6 lorsqu'il est effectué en deux opérations successives doit être respectée. Une limitation du rapport Dl/Do de 1,5 à 2 suivant le type d'alliage concerné est également fixée quelquefois.It is commonly accepted that to avoid these defects, an upper limit value of the delivery rate t of 4 when the delivery is carried out in one operation or of 6 when it is carried out in two successive operations must be respected. A limitation of the Dl / Do ratio of 1.5 to 2 depending on the type of alloy concerned is also sometimes fixed.
Diverses tentatives d'amélioration ont recherché à dépasser les limitations géométriques imposées jusqu'à présent sans encourir l'apparition des défauts. On a ainsi tenté d'effectuer l'opération de refoulage au moyen d'un outillage animé d'un mouvement de nutation sur l'extrémité à refouler de la barre, celle-ci étant simultanément déplacée vers la zone de travail d'une longueur correspondant au volume à déformer. On a également tenté d'effectuer un refoulage en plusieurs passes en avançant successivement, à chaque passe, la barre d'une longueur correspondant au volume à déformer. Des exemples de telles réalisations sont donnés par FR-A-2050 483, FR-A-2050 484, et par FR-A-2220 328. Dans ces procédés, les résultats n'ont pas été entièrement satisfaisants et notamment une orientation suffisamment régulière du fibrage ne peut pas être assurée.
On connaît par ailleurs par SU-A-804 163, qui représente l'état de la technique le plus proche, un outil de matriçage en ébauche d'un objet à section en polygonale tel qu'un écrou.Various attempts at improvement have sought to overcome the geometric limitations imposed so far without incurring the appearance of defects. An attempt was thus made to carry out the pushing-back operation by means of a tool animated by a nutation movement on the end to be pushed back of the bar, the latter being simultaneously moved towards the working area of a length corresponding to the volume to be deformed. Attempts have also been made to push back in several passes by advancing successively, with each pass, the bar of a length corresponding to the volume to be deformed. Examples of such embodiments are given by FR-A-2050 483, FR-A-2050 484, and by FR-A-2220 328. In these methods, the results have not been entirely satisfactory and in particular a sufficiently regular orientation fiberizing cannot be guaranteed.
Also known from SU-A-804 163, which represents the closest state of the art, is a die-forging tool for roughing an object with a polygonal section such as a nut.
Cet outil a une cavité de travail intérieure à faces convexes raccordées par des angles arrondis dont le rayon de courbure est tel que le contour sort des limites du contour de l'empreinte de l'outil de finition.
Le procédé de fabrication d'ébauches forgées en barre par refoulage permettant d'éviter ces inconvénients est caractérisé en ce qu'il comporte au moins deux étapes successives :
- (a) une première étape de refoulage durant laquelle, au moins à partir d'un premier stade de déformation, un contact est maintenu entre au moins trois génératrices de ladite portion de barre et la surface intérieure d'un premier conteneur qui comporte, entre deux desdites lignes de contact respectivement, une excroissance en creux longitudinale formant en section transversale une partie lobée,
- une deuxième étape de refoulage durant laquelle, au moins à partir d'un premier stade de déformation, un contact est maintenu entre les génératrices de sommet des excroissances longitudinales obtenues sur la première ébauche à l'issue de la première étape (a) et la surface intérieure d'un deuxième conteneur, ladite surface intérieure de cavité présentant une forme de contour enveloppant ladite première ébauche,
The process for manufacturing blanks forged in bar by upsetting which makes it possible to avoid these drawbacks is characterized in that it comprises at least two successive stages:
- (a) a first upsetting step during which, at least from a first deformation stage, contact is maintained between at least three generatrices of said bar portion and the interior surface of a first container which comprises, between two of said contact lines respectively, a longitudinal hollow outgrowth forming a lobed part in cross section,
- a second upsetting step during which, at least from a first deformation stage, contact is maintained between the crown generators of the longitudinal protuberances obtained on the first blank at the end of the first step (a) and the inner surface of a second container, said inner cavity surface having a contour shape enveloping said first blank,
Un outillage de refoulage enveloppant une ébauche forgée en barre destiné à la mise en oeuvre dudit procédé est défini par la combinaison de caractéristiques de la revendication 5.A discharge tool wrapping a bar forged blank intended for the implementation of said method is defined by the combination of characteristics of
Avantageusement, le premier conteneur présente une cavité de section cruciforme, la barre cylindrique étant en contact avec la surface intérieure du conteneur le long de quatre génératrices situées à 90° l'une de l'autre et le deuxième conteneur présente une cavité de section carrée, à coins arrondis, les sommets des excroissances ou lobes de la section cruciforme de la barre obtenue à l'issue de la première étape étant en contact respectivement avec un côté dudit carré.Advantageously, the first container has a cruciform section cavity, the cylindrical bar being in contact with the interior surface of the container along four generatrices located at 90 ° from one another and the second container has a square section cavity , with rounded corners, the tops of the protuberances or lobes of the cruciform section of the bar obtained at the end of the first step being in contact respectively with one side of said square.
Dans certaines applications concernant des alliages de titane, des taux de refoulage de 8 à 10 obtenus en deux opérations par le procédé conforme à l'invention nécessitaient par les procédés antérieurs connus auparavant au minimum cinq opérations successives. Selon les critères de qualité imposés et selon les applications, notamment en fonction des alliages utilisés, des taux de refoulage supérieurs peuvent être obtenus et dans tous les cas, supérieurs aux résultats antérieurs. En outre, les examens métallographiques effectués sur les ébauches forgées obtenues par le procédé de refoulage selon l'invention ont montré une nette amélioration de l'orientation du fibrage par rapport à ces procédés antérieurs ainsi qu'une absence totale de défauts. Ces résultats améliorés proviennent directement de l'application du procédé selon l'invention et peuvent s'expliquer par ses caractéristiques. En effet, lors de la première étape du procédé, la barre est maintenue en appui au moins suivant trois génératrices, évitant ainsi toute déformation par flambage, alors que l'ecoulement de l'alliage ne peut se faire qu'en direction des parties en creux du conteneur, rendant ainsi toute déformation par torsion impossible. De même, lors de la deuxième étape, le contact maintenu entre les génératrices extrêmes de l'ébauche et les parois du conteneur empêche toute déformation par flambage ou par torsion.In certain applications relating to titanium alloys, discharge rates of 8 to 10 obtained in two operations by the process in accordance with the invention required by the prior processes previously known at least five successive operations. According to the quality criteria imposed and according to the applications, in particular according to the alloys used, higher upsetting rates can be obtained and in all cases, higher than the previous results. In addition, metallographic examinations carried out on the forged blanks obtained by the upsetting process according to the invention have shown a marked improvement in the orientation of the fiber drawing compared to these previous processes as well as a total absence of defects. These improved results come directly from the application of the method according to the invention and can be explained by its characteristics. In fact, during the first step of the process, the bar is held in support at least along three generatrices, thus avoiding any deformation by buckling, while the flow of the alloy can only be done in the direction hollow parts of the container, thus making any torsional deformation impossible. Similarly, during the second step, the contact maintained between the end generators of the blank and the walls of the container prevents any deformation by buckling or twisting.
D'autres caractéristiques et avantages de l'invention seront mieux compris à la lecture de la description qui va suivre d'un mode de réalisation de l'invention, en référence aux dessins annexés sur lesquels :
- les figures 1a, 1b, 1c, 1d qui ont été précédemment décrites représentent schématiquement les déformations d'une barre lors d'opérations successives de refoulage n'appliquant pas l'invention :
- les figures 2a, 2b représentent la barre dans sa forme initiale avant refoulage, respectivement en vue de face et en vue selon une section transversale,
- les figures 3a, 3b représentent schématiquement la barre représentée aux figures 2a, 2b au cours de la première étape de l'opération de refoulage selon le procédé conforme à l'invention, respectivement en vue suivant une coupe longitudinale et selon une section transversale ;
- les figures 4a, 4b représentent schématiquement l'ébauche obtenue à l'issue de la première étape, au cours de la deuxième étape de l'opération de refoulage selon le procédé conforme à l'invention, respectivement, selon des vues analogues aux figures 3a et 3b, suivant une coupe longitudinale et selon une section transversale ;
- la figure 5 représente une vue de l'ébauche forgée finale obtenue par le procédé conforme à l'invention, selon une section transversale ;
- la figure 6 représente selon une vue analogue à la figure 4b, en section transversale, une variante de mise en oeuvre de la deuxième étape du procédé conforme à l'invention ;
- les figures 7a, 7b, 7c montrent des variantes de mise en oeuvre d'étapes du procédé de refoulage conforme à l'invention.
- FIGS. 1a, 1b, 1c, 1d which have been previously described schematically represent the deformations of a bar during successive upsetting operations not applying the invention:
- FIGS. 2a, 2b show the bar in its initial shape before upsetting, respectively in front view and in view in a cross section,
- Figures 3a, 3b schematically show the bar shown in Figures 2a, 2b during the first step of the upsetting operation according to the method according to the invention, respectively in view in a longitudinal section and in a cross section;
- Figures 4a, 4b schematically show the blank obtained at the end of the first step, during the second step of the upsetting operation according to the method according to the invention, respectively, according to views similar to Figures 3a and 3b, along a longitudinal section and along a cross section;
- FIG. 5 represents a view of the final forged blank obtained by the method according to the invention, according to a cross section;
- 6 shows a view similar to Figure 4b, in cross section, an alternative implementation of the second step of the method according to the invention;
- Figures 7a, 7b, 7c show alternative embodiments of steps of the upsetting process according to the invention.
Le procédé de fabrication d'ébauches forgées par refoulage conforme à l'invention s'applique notamment à des produits en barre tels que une barre cylindrique 1 représentée dans sa forme initiale aux figures 2a et 2b. Comme représenté schématiquement sur les figures 3a et 3b, pour la réalisation de la première étape (a) du procédé de refoulage conforme à l'invention, la barre 1 est placée dans un premier conteneur 2 solidaire d'une presse à forger ou machine à refouler d'un type connu en soi qui n'est pas représentée plus en détails sur les dessins. Au cours de cette première étape (a) de refoulage, une extrémité 1a de la barre 1 est soumise à l'action de refoulement d'un poinçon 3 mû par les moyens de poussée et de commande de ladite machine. La portion 1b de la barre 1 soumise au refoulage tend ainsi à occuper le volume disponible du conteneur 2 limité par la face du poinçon 3, ce qui entraîne une diminution de longueur de ladite portion 1b, accompagnée d'une augmentation de la section transversale correspondante. Dans le mode de réalisation de l'invention représenté sur les figures 3a et 3b, le premier conteneur 2 utilisé lors de la première étape du procédé de refoulage comporte une cavité 4 qui présente en section transversale une forme générale cruciforme composée de quatre parties lobées 4a, 4b, 4c, 4d disposées symétriquement deux à deux, ménageant ainsi quatre génératrices 5a, 5b, 5c, 5d situées à 90° l'une de l'autre, qui coopèrent avec quatre génératrices correspondantes de la portion refoulée 1b de la barre 1 en maintenant, à partir d'un premier stade de déformation, un contact permanent avec elles au cours de l'étape de refoulage. Ledit contact suivant les génératrices entre conteneur et barre devient nécessaire à partir du moment où au cours de l'opération de refoulage apparaissent des risques de création de défauts irréversibles par flambage ou torsion. Le contact peut être réalisé dès le début de l'opération. Il est souvent dans la pratique plus aisé, pour des facilités de mise en oeuvre, de prévoir un jeu radial au départ entre lesdites génératrices qui peut aller dans le présent mode de réalisation jusqu'à 0,5mm. L'action, dans le sens de l'effort appliqué et du déplacement obtenu, du poinçon 3 s'exerce suivant la flèche F tandis que les flèches f symbolisent les directions d'écoulement de l'alliage constituant la barre 1 au cours du refoulage.The method for manufacturing blanks forged by upsetting according to the invention applies in particular to bar products such as a
Pour la deuxième étape (b) du procédé de refoulage conforme à l'invention dont le déroulement est similaire à celui de la première étape (a) qui vient d'être décrit ci-dessus, l'ébauche intermédiaire 1c obtenue à l'issue de la première étape (a) est placée dans un deuxième conteneur 6, comme représenté schématiquement sur les figures 4a et 4b, et son extrémité est à nouveau soumise à une action de refoulement d'un poinçon 7. Dans le mode de réalisation de l'invention représenté aux figures 4a et 4b, le deuxième conteneur 6 comporte une cavité 8 qui présente en section transversale une forme générale carrée, à coins arrondis. L'ébauche intermédiaire 1c présente une section cruciforme qui reproduit la forme de la cavité 4 du premier conteneur 2 et les génératrices 1d, 1e, 1f et 1g correspondant aux sommets des parties lobées de cette section cruciforme de l'ébauche intermédiaire 1c sont placées au contact de lignes d'appui correspondantes des côtés du carré de cavité du deuxième conteneur 6 et de manière similaire à la première étape (a), au cours de la deuxième étape (b) de refoulage, le contact est également maintenu en permanence, à partir d'un premier stade de déformation, au niveau de ces quatre génératrices symétriques deux à deux, entre la surface externe de l'ébauche 1c et la surface de la cavité 8 du deuxième conteneur 6. Comme précédemment, un jeu radial variable, de O à O,5 mm dans la présente application, peut être ménagé au départ de la deuxième étape entre les génératrices coopérantes de la barre et du conteneur.For the second step (b) of the upsetting process according to the invention, the progress of which is similar to that of the first step (a) which has just been described above, the intermediate blank 1c obtained at the end of the first step (a) is placed in a second container 6, as shown diagrammatically in FIGS. 4a and 4b, and its end is again subjected to the pushing action of a
A l'issue de cette deuxième étape (b) du procédé de refoulage conforme à l'invention, la portion refoulée initiale 1b présente une section finale 1d d'ébauche forgée telle que représentée à la figure 5 dans le mode de réalisation qui vient d'être décrit. Cette portion refoulée de barre 1b peut notamment être destinée à constituer le pied d'une aube de turbomachine obtenue par forgeage.At the end of this second step (b) of the upsetting process according to the invention, the initial upsetting
Divers modes de réalisation appliquant les caractéristiques du procédé de refoulage conforme à l'invention qui ont été décrites peuvent être envisagées. Notamment, en fonction de la nature des alliages concernés, des pièces dont la fabrication est envisagée, du taux de refoulage recherché, un nombre différent d'étapes du procédé de refoulage peut être appliqué. Différentes formes de cavité du conteneur utilisé, ou suivant les étapes associées, peuvent également être associées à condition de ménager, conformément à l'invention, un contact permanent au cours d'une étape entre plusieurs génératrices de l'ébauche et de la surface de cavité du conteneur. Le deuxième conteneur 6 utilisé lors de la deuxième étape (b) de refoulage dans le mode de réalisation qui a été décrit et dont la section est représentée à la figure 4b peut, par exemple, comporter une cavité 8a délimitée par une surface qui est représentée par une section circulaire à la figure 6. Les figures 7a, 7b, 7c, représentent respectivement, selon une section schématique, d'autres formes utilisables de cavité de conteneur 9a, 9b, 9c, respectivement associé à une portion de barre à refouler de section 10a,10b,10c, 10c, 10d. Cette section de barre au départ est de forme adaptée à la pièce finale à obtenir et outre cylindrique peut notamment être rectangulaire ou carrée.Various embodiments applying the characteristics of the upsetting process according to the invention which have been described can be envisaged. In particular, depending on the nature of the alloys concerned, parts whose manufacture is envisaged, the desired upsetting rate, a different number of steps in the upsetting process can be applied. Different forms of cavity of the container used, or according to the associated steps, can also be associated provided that, in accordance with the invention, permanent contact is made during a step between several generators of the blank and of the container cavity surface. The second container 6 used during the second upsetting step (b) in the embodiment which has been described and the section of which is shown in FIG. 4b may, for example, include a cavity 8a delimited by a surface which is shown by a circular section in FIG. 6. FIGS. 7a, 7b, 7c respectively represent, in a schematic section, other usable forms of
Claims (8)
- Process for manufacturing blanks for turboshaft engine compressor blade roots by upsetting forged bar, in which at least one portion of bar (1b), of initial length Lo and of initial section So, of diameter Do, is transformed by upsetting a portion of bar (1d) of final length L1 and final section S1, of diameter D1 such that Lo > L1, So < S1, Do > D1, a technological parameter t or rate of upsetting being represented by- (a) a first upsetting stage during which, at least from a first stage of deformation, a contact is maintained between at least three generatrixes of the said portion of bar and the inner surface of a first container (2) which comprises, between two of the said lines of contact (5a, 5b, 5c, 5d) respectively, a protuberance (4a, 4b, 4c, 4d) of longitudinal trough shape forming in cross section a lobed part;- (b) a second upsetting stage during which, at least from a first stage of deformation, a contact is maintained between the peak generatrixes of the longitudinal protuberances obtained on the first blank (16) at the end of the first stage (a) and the inner cavity surface of a second container (6), the said inner cavity surface presenting a shape of the contour enveloping the said first blank, and in that the said upset rate (t) obtained in two passes is at least equal to 8.
- Process for producing blade root blanks by upsetting forged bar in accordance with Claim 1, in which during the first stage (a), the first container (2) presents in cross section an inner contour of generally cruciform shape and the first blank (1b, 1c) upset is maintained during the course of the said first stage (a) in accordance with four longitudinal generatrixes (5a, 5b, 5c, 5d) peripherally spaced at 90° to each other and presents at the end of the first stage (a) four longitudinal protuberances oriented at 90° from each other.
- Process for producing blanks by upsetting forged bar in accordance with either of Claims 1 and 2 in which during the second stage (b), the second container (6) presents in cross section an inner contour of generally square shape, with rounded corners.
- Process for producing blanks by upsetting forged bar in accordance with either of Claims 1 and 2 in which during the second stage (b), the second container (8a) presents in cross section a circular inner contour.
- Upsetting tool enveloping a blank (1b, 1c) forged from bar, designed for putting into practice a production process conforming to any of Claims 1 to 4 consisting of two containers (2, 6) each comprising a cavity (4, 8) in which is placed the said blank (1b, 1c) characterised in that the first container (2) suited to the carrying out of the first stage (a) of the said process presents an inner cavity surface geometry (4) such that before forging the blank (1b) is in contact, at least from a first stage of deformation, at least in accordance with three generatrixes, with the matching generatrixes (5a, 5b, 5c, 5d) of the container (2) and such that trough-shaped longitudinal protuberances (4a, 4b, 4c 4d) are formed between the said generatrixes (5a, 5b, 5c, 5d) and in that the said second container (8)[sic. 8a] adapted for the carrying out of the second stage (b) of the said process presents an inner cavity surface geometry (8) such that the cross sectional contour envelopes the inner surface cavity geometry contour of the first container and that the inner surface cavity contour shapes of the said first (2) and second containers (6) are tangents in accordance with at least three generatrixes and are secants at no point.
- Tools designed for carrying out the process of manufacturing blanks by upsetting forged bar in accordance with Claim 5 characterised in that the said first container (2) comprises a cavity presenting a cruciform cross section with four lobes, spaced at 90° from each other.
- Tools designed for carrying out the process of manufacturing blanks by upsetting forged bar in accordance with either of Claims 5 or 6 characterised in that the said second container (6) comprises a cavity (8a) of generally square shape, with rounded corners, the length of one side of the square representing the distance between two peaks of protuberances diametrically opposite (1d-1f, 1e-1g) the first container.
- Tools designed for carrying out the process of manufacturing blanks by upsetting forged bar in accordance with either of Claims 5 or 6 characterised in that the said second container comprises a cavity (8a) presenting a circular cross section whose circumference envelopes the cavity section (4) of the first container (2).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8801227A FR2626507A1 (en) | 1988-02-03 | 1988-02-03 | METHOD OF MANUFACTURING BLANK FORGED BLANKS, IN PARTICULAR FOR COMPRESSOR BLADES AND IMPLEMENTATION TOOLS |
FR8801227 | 1988-02-03 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0331539A1 EP0331539A1 (en) | 1989-09-06 |
EP0331539B1 true EP0331539B1 (en) | 1994-01-26 |
Family
ID=9362888
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP89400273A Expired - Lifetime EP0331539B1 (en) | 1988-02-03 | 1989-02-01 | Method of making forged blanks from bar material by upsetting, in particular for compressor blades, and tooling equipment for carrying out the method |
Country Status (7)
Country | Link |
---|---|
US (1) | US4970887A (en) |
EP (1) | EP0331539B1 (en) |
JP (1) | JPH0732945B2 (en) |
CA (1) | CA1330172C (en) |
DE (1) | DE68912620T2 (en) |
FR (1) | FR2626507A1 (en) |
IL (1) | IL89160A (en) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0500543A4 (en) * | 1989-09-29 | 1992-11-19 | Motorola, Inc. | Flat panel display using field emission devices |
US5007873A (en) * | 1990-02-09 | 1991-04-16 | Motorola, Inc. | Non-planar field emission device having an emitter formed with a substantially normal vapor deposition process |
US5030921A (en) * | 1990-02-09 | 1991-07-09 | Motorola, Inc. | Cascaded cold cathode field emission devices |
US5230134A (en) * | 1992-02-11 | 1993-07-27 | Laue Charles E | Method of making a petal rod |
FR2695578B1 (en) * | 1992-09-17 | 1994-10-21 | Snecma | Tooling for forging by pushing bar blanks in two stages. |
US5425286A (en) * | 1993-04-09 | 1995-06-20 | Laue; Charles E. | Two piece pedal rod and method of making same |
US5606790A (en) * | 1993-04-09 | 1997-03-04 | Charles E. Laue | Method of making a two piece pedal rod |
DE19603035C2 (en) * | 1996-01-29 | 1998-03-26 | Cdp Aluminiumtechnik Gmbh & Co | Method and device for producing semi-finished products |
JP3680421B2 (en) * | 1996-06-04 | 2005-08-10 | トヨタ自動車株式会社 | Method for forging bar work |
US6193821B1 (en) | 1998-08-19 | 2001-02-27 | Tosoh Smd, Inc. | Fine grain tantalum sputtering target and fabrication process |
DE10035224A1 (en) * | 2000-07-20 | 2002-01-31 | Man Turbomasch Ag Ghh Borsig | Process and blank for producing rhomboid blades for axial turbomachines |
US7213436B2 (en) * | 2004-05-28 | 2007-05-08 | Shape Corporation | Stamping apparatus for forming rod with configured ends |
FR2874339B1 (en) * | 2004-08-23 | 2008-12-05 | Snecma Moteurs Sa | METHOD FOR MANUFACTURING CONSTITUENT PIECES OF A HOLLOW DRAW BY DRILLING ON PRESS |
JP4301525B2 (en) * | 2006-12-01 | 2009-07-22 | トピー工業株式会社 | Compression forging method |
EP1927413B1 (en) * | 2006-12-01 | 2009-08-19 | Topy Kogyo Kabushiki Kaisha | Press forging method |
CN107249779B (en) * | 2015-02-18 | 2019-03-05 | 新日铁住金株式会社 | End upsetting metal tube and its manufacturing method |
GB201707896D0 (en) * | 2017-05-17 | 2017-06-28 | Rolls Royce Plc | Forging apparatus and method |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3154849A (en) * | 1961-01-18 | 1964-11-03 | Thompson Ramo Wooldridge Inc | Metal forging process |
US3392569A (en) * | 1966-02-03 | 1968-07-16 | Columbus Auto Parts | Insulator pin |
FR2050483B1 (en) * | 1969-07-03 | 1974-12-20 | Massey B Et S Ltd | |
SE371045B (en) * | 1969-07-03 | 1974-11-04 | Varta Ag | |
GB1282759A (en) * | 1969-08-18 | 1972-07-26 | Maurice Lachaussee | Method of manufacturing discs from wire |
FR2220328A1 (en) * | 1973-03-07 | 1974-10-04 | Inst Obrobki Plastycznes | |
SU804163A1 (en) * | 1979-04-13 | 1981-02-15 | Горьковский Конструкторско-Технологическийинститут Холодновысадочного И Пружинногопроизводства | Tool for preliminary upsetting of multiface cross-section articles |
SU821016A1 (en) * | 1979-06-08 | 1981-04-15 | Предприятие П/Я Г-4585 | Method of upsetting tubes |
US4484464A (en) * | 1980-11-21 | 1984-11-27 | Honda Giken Kogyo Kabushiki Kaisha | Electrical upsetting method and device therefor |
JPS61193739A (en) * | 1985-02-21 | 1986-08-28 | Toyota Motor Corp | Upsetting forming method |
-
1988
- 1988-02-03 FR FR8801227A patent/FR2626507A1/en active Granted
-
1989
- 1989-02-01 DE DE68912620T patent/DE68912620T2/en not_active Expired - Fee Related
- 1989-02-01 EP EP89400273A patent/EP0331539B1/en not_active Expired - Lifetime
- 1989-02-02 JP JP1024759A patent/JPH0732945B2/en not_active Expired - Fee Related
- 1989-02-02 CA CA000589879A patent/CA1330172C/en not_active Expired - Fee Related
- 1989-02-02 US US07/305,178 patent/US4970887A/en not_active Expired - Lifetime
- 1989-02-03 IL IL89160A patent/IL89160A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
FR2626507A1 (en) | 1989-08-04 |
IL89160A0 (en) | 1989-09-10 |
JPH0732945B2 (en) | 1995-04-12 |
CA1330172C (en) | 1994-06-14 |
DE68912620T2 (en) | 1994-05-19 |
IL89160A (en) | 1992-08-18 |
FR2626507B1 (en) | 1994-04-22 |
JPH01237039A (en) | 1989-09-21 |
EP0331539A1 (en) | 1989-09-06 |
US4970887A (en) | 1990-11-20 |
DE68912620D1 (en) | 1994-03-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0331539B1 (en) | Method of making forged blanks from bar material by upsetting, in particular for compressor blades, and tooling equipment for carrying out the method | |
EP0841111A1 (en) | Method of obtaining grooves on a shaft | |
FR2608078A1 (en) | METHOD FOR MANUFACTURING AN INDOOR HELICOIDAL DENTURE | |
FR2521042A1 (en) | TOOTH FORMING TOOL FOR CANNELING TUBULAR ELEMENTS | |
EP0099311A1 (en) | Steering rack for automotive vehicles, and process for producing such a rack | |
EP0310726B1 (en) | Manufacturing method of conical metal boxes and tool for carrying out this method | |
EP1071526B1 (en) | Method for making a tubular metal part and composite tubular shaft | |
EP0524098B1 (en) | Method and punch for deep-drawing containers with a continuous wall | |
WO2014135772A1 (en) | Tool for forming a collar at one end of a tube | |
EP1870180A1 (en) | Method of obtaining a precision bore in a wing of a cardan joint fork, corresponding method of manufacturing a cardan joint fork and cardan joint fork obtained thereby | |
JP2927426B2 (en) | Tooth wheel | |
EP0534818B1 (en) | Method of producing an axle with profiled ends, machine for carrying out the method and axles thus obtained | |
JPH09300041A (en) | Manufacture of gear by cold-forging and die used therefor | |
FR2698303A1 (en) | Method for hooping at least one metal part having an annular bore around a metal tube, assembly obtained and use of the method. | |
FR2744383A1 (en) | Method of threading shaft | |
EP0250312B1 (en) | Method of making pinions of which the tooth-driving surfaces form a sharp-edged angle | |
FR2756757A1 (en) | PROCESS FOR MANUFACTURING A SHAPED METAL BOX AND FOOD METAL BOX OBTAINED BY THIS PROCESS | |
EP0845315A1 (en) | Method of forming a neck of a food container such as a metal beverage can | |
EP4499329A1 (en) | Method and unit for manufacturing an elongate intermediate part by hot forging | |
US5065605A (en) | Method of forming shaped configuration at end of long element | |
WO2025012554A1 (en) | Method for manufacturing an upset-forged part and assembly for implementing the method | |
JPS5924547A (en) | Processing method for outer diameter shape of cylindrical parts | |
FR2816011A1 (en) | Starter, for vehicle, is fitted with pinion, which is manufactured in two parts. | |
FR2736694A1 (en) | Fabrication process for cone synchroniser for use in vehicle gearboxes | |
FR2505213A1 (en) | METHOD FOR MANUFACTURING PARTS PROVIDED WITH ANNULAR WAVES AND PARTS MANUFACTURED ACCORDING TO SAID PROCESS |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19890227 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): DE FR GB |
|
17Q | First examination report despatched |
Effective date: 19910328 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MO |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 19940204 |
|
REF | Corresponds to: |
Ref document number: 68912620 Country of ref document: DE Date of ref document: 19940310 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: TP Ref country code: FR Ref legal event code: CD |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20040122 Year of fee payment: 16 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20040128 Year of fee payment: 16 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20040212 Year of fee payment: 16 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20050201 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20050901 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20050201 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20051031 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20051031 |