EP0018263A1 - Process for chromizing steel articles, and chromized steel articles - Google Patents

Process for chromizing steel articles, and chromized steel articles Download PDF

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Publication number
EP0018263A1
EP0018263A1 EP80400451A EP80400451A EP0018263A1 EP 0018263 A1 EP0018263 A1 EP 0018263A1 EP 80400451 A EP80400451 A EP 80400451A EP 80400451 A EP80400451 A EP 80400451A EP 0018263 A1 EP0018263 A1 EP 0018263A1
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Prior art keywords
nitrogen
metal part
depth
chromium
chromized
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Granted
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EP80400451A
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German (de)
French (fr)
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EP0018263B1 (en
Inventor
André Robert Faure
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Atto Confirmatorio E Ricognitivo Di Licenza Esclus
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Aubert and Duval SA
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Priority to AT80400451T priority Critical patent/ATE3883T1/en
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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C12/00Solid state diffusion of at least one non-metal element other than silicon and at least one metal element or silicon into metallic material surfaces
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/02Pretreatment of the material to be coated
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12576Boride, carbide or nitride component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12806Refractory [Group IVB, VB, or VIB] metal-base component
    • Y10T428/12826Group VIB metal-base component
    • Y10T428/12847Cr-base component
    • Y10T428/12854Next to Co-, Fe-, or Ni-base component

Definitions

  • the present invention relates to a method for chromizing metal parts such as steel parts, of the type in which chromium is diffused in order to obtain a surface layer of chromium and in which the chromium supply is obtained by gas phase decomposition of chromium halides, the decomposition of the halide and the diffusion of chromium in the steel being carried out simultaneously by heating the parts to temperatures not exceeding 1300 ° C., in the halide atmosphere, the actual chromizing operation being preceded by a surface nitrogen addition operation.
  • the actual chromization is known, for example, from the works of Doctor GALMICHE and from the ONERA patents n ° 1.012.401 and their two additions 60.539 and 60.686.
  • the object of the present invention is to propose a hard chromization process of the aforementioned type and making it possible to produce steel parts having a hard chromized surface layer comprising carbo-nitrides, a layer having a thickness greater than at least 20 microns, preferably 30 microns, and a fine grain undercoat with little or no decar burée.
  • This object is achieved by the fact that prior to the actual chromizing operation, the introduction of nitrogen into the surface layer of the metal part is made so that the nitrogenous surface layer has a content greater than 0.8 % nitrogen over a depth or thickness at least equal to 0.5 mm.
  • hard chromized layers comprising carbo-nitrides instead of separate carbides and / or separate nitrides, these layers being of a thickness greater than at least 20 microns and having a high resistance to wear.
  • the presence of nitrogen in the surface layers of the steel parts makes it possible to achieve a different balance of the chromium and carbon elements with respect to the base steel during the chromization reaction, this different balance thus allowing to obtain much deeper chromized surface layers without producing significantly decarburized undercoats and without enlarging the grain in undercoat.
  • the surface introduction of nitrogen can be carried out by heating the workpiece to a temperature between 400 and 800 ° C. and in any case at a temperature below the lower critical point of the treated steel, and for the periods between 12 and 150 hours in a nitrogen generating medium which, by way of example may consist of molten nitrous salts, ammonia or nitrogen gases, ionized or not.
  • nitrogenous surface layers previously containing more than 0.8% nitrogen over a depth at least equal to 0.5 mm.
  • nitrogenous surface layers are prepared having a nitrogen content of between 1 and 2% over a depth of 0.5 to 1.0 mm.
  • Such satisfactory nitrogenous layers can be obtained by treatment cycles in an ammonia atmosphere of 24 hours at 700 ° C or 90 hours at 560 ° C.
  • the chromium halide atmosphere conforms to the already known technique
  • the temperature and holding time parameters can be conformed to the already known technique, but they can also be modified according to the prior introduction of nitrogen; compared to what they would be on the same non "activated" steel according to the present invention.
  • the chromization temperatures can be reduced in order to limit the magnification of the grains of the undercoat.
  • the steel parts can preferably undergo a regenerative heat treatment in order to reduce the grain sizes and improve the resilience of the base steel.
  • the comparison drawing shows the comparison of the chromized layers obtained on the same steel grade 32 CDV 13 (AFNOR) by known chromization techniques without or with prior activation by nitrogen and in the three cases followed by a heat treatment of grain regeneration by heating under vacuum, quenching and tempering.
  • AFNOR chromization technique
  • FIG. 1 is a micro-hardness diagram showing for the steel grade 32 CDV 13 (AFNOR) three examples of chromized steel parts and, FIGS. 2 to 4 show micro-photos of the surface layer and of the adjacent underlay of these three examples of chromized steel parts, the enlargement factor being in all three cases of 200.
  • AFNOR steel grade 32 CDV 13
  • the hardness of different levels of the steel parts is indicated on the ordinate, hardness measured in Vickers points and on the abscissa the thickness or depth of the layers in microns from the surface of the part of steel considered.
  • the curve a in solid lines represents the hardness of a piece of steel in Vickers degrees as a function of the depth of the level considered.
  • This piece of steel, the transverse structure of which is illustrated in FIG. 2 has not been previously activated by nitrogen, but only one chromium-plating operation for 12 hours at 940 ° C.
  • the chromized surface layer 1 has a depth or thickness of 12 microns and has a Vickers hardness greater than 1,500 points and reaching more than 1,800 points.
  • a sub-layer 2 whose Vickers hardness decreases rapidly to a minimum value of 260 and then slowly rises to Vickers hardness at the heart of the hardness steel part which is of the order of 350 and is reached at a depth of 77 microns.
  • this sublayer or decarburization zone 2 is of the order of 65 microns which is more than 5 times the thickness of the chromized surface layer 1 and the minimum hardness of the sublayer 2 is only about 3/4 of the Vickers hardness at the heart of the steel part.
  • the decrease in the hardness of the underlay compared to that of the core of the steel part clearly shows the extent of the decarburized zone and the harmful influence of the inevitable carbon pumping during the known chromization operation. It can also be seen from FIG. 2 that the size of the grain in the sub-layer is significant (Afnor index 4).
  • Curve b of FIG. 1 shows the hardness of a piece of steel of the same aforementioned grade without activation with nitrogen, subjected to a chromization operation also for 12 hours, but at a higher temperature, namely 980 ° C.
  • This increase in temperature brings the depth of the chromized surface layer 1 to 16 microns, but on the other hand the corresponding structure illustrated in FIG. 3 shows an even larger and unfavorable grain size (Afnor index 3) than that of the structure.
  • the diagram of microhardness shows at the bottom of curve b between a depth of 16 microns and 85 microns (sublayer 2) an even deeper and more intense decarburization zone (minimum Vickers hardness 240 points) than that of the example in the curve a and of FIG. 2.
  • the Vickers hardness of the undercoat 2 is of the order of 2/3 of the Vickers hardness at the heart of the steel part and the undercoat 2 with its decarburized zone a a thickness at least four times greater than that of the chromized surface layer 1.
  • Curve c of FIG. 1 corresponds to a piece of steel having undergone prior activation by the surface introduction of nitrogen in accordance with the present invention (treatment cycle of 90 hours at 560 ° C.).
  • This curve c in FIG. 1 shows the Vickers hardness of a piece of steel of the same grade as the previous examples, but is obtained after the same chromization cycle as the example of curve a, that is 12 hours at 940 ° C.
  • the chromized layer 1 has a depth of 50 microns.
  • the structure; illustrated by FIG. 4 also shows the fineness of the grain obtained in the sub-layer 2 over a depth of 1 mm and the diagram of microduretures (FIG. 1) shows for curve c a much less thick decarburization zone (20 to 30 microns ) and less intense (minimum Vickers hardness around 330 points) than in the two previous examples.
  • the thickness of the decarburized zone is very small, is less than that of the chromized layer 1 and is only approximately equal to half that of said chromized layer 1.
  • the hardness of the decarburized zone of the underlayer 2 it is at least equal to about 95% of the hardness of the core of the steel piece.
  • the loss of hardness in the underlayment compared to the base steel at The core of the steel part is inside 25 Vickers points and affects a weakly decarburized area with a thickness of less than 25 microns.
  • grain fineness which is at least equal to or greater than the Afnor6 index (index 7) over a thickness at least equal to 0.5 mm (1 mm) .
  • carbon-containing steel intended for hard chromium plating has a surface layer containing at least 0.8% nitrogen over a depth greater than 0.5 mm. It has been found that to the extent that the nitrogen content of the surface layer before chromization exceeds 0.8% over a depth of 0.5 mm, there is found after said chromization in the sublayer a higher residual nitrogen content at 0.4% over a depth greater than 0.5 mm, this nitrogen content preventing significant decarburization and a significant enlargement of the grain of the undercoat.
  • the nitrogen content of the surface layer of the steel is, before chromization, greater than 0.8% over a depth greater than 0.5 mm, after said chromization is found in the chromized surface layer the presence of chromium carbonitrides with a nitrogen content greater than 2%.
  • the invention relates not only to the new hard chromization process, but also to the pieces of steel treated with nitrogen with a view to chromization as well as to the pieces of steel chromized according to the present process and having a chromized surface layer. hard with a depth of at least 20 microns and a Vickers hardness of at least 1200 points.

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
  • Heat Treatment Of Steel (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

The invention relates to a method for chromizing metallic pieces such as steel pieces and to chromized metallic pieces obtained thereby, said metallic pieces, particularly steel, comprising a chromized surface layer with a hardness at least equal to 1200 Vickers degrees and a thickness at least equal to 12 microns as well as an adjacent sub-layer with a hardness less than that of the core of said piece. The chromized surface layer has a depth preferably at least equal to 20 microns, more preferably 30 microns, and the hardness of the sublayer presents a maximum variation of 25 Vickers degrees with respect to that of the core of said piece.

Description

La présente invention concerne un procédé de chromisation de pièces métalliques telles que des pièces d'acier, du type selon lequel on fait diffuser du chrome en vue d'obtenir une couche superficielle de chrome et selon lequel l'apport de chrome est obtenu par la décomposition en phase gazeuse d'halogénures de chrome, la décomposition de l'halogénure et la diffusion du chrome dans l'acier étant réalisée simultanément en chauffant les pièces à des températures ne dépassant pas 1300°C, dans l'atmosphère d'halogénure, l'opération de chromisation proprement dite étant précédée d'une opération d'apport superficiel d'azote.The present invention relates to a method for chromizing metal parts such as steel parts, of the type in which chromium is diffused in order to obtain a surface layer of chromium and in which the chromium supply is obtained by gas phase decomposition of chromium halides, the decomposition of the halide and the diffusion of chromium in the steel being carried out simultaneously by heating the parts to temperatures not exceeding 1300 ° C., in the halide atmosphere, the actual chromizing operation being preceded by a surface nitrogen addition operation.

La chromisation proprement dite est connue, par exemple, par les travaux du Docteur GALMICHE et par les brevets ONERA n° 1.012.401 et leurs deux additions 60.539 et 60.686.The actual chromization is known, for example, from the works of Doctor GALMICHE and from the ONERA patents n ° 1.012.401 and their two additions 60.539 and 60.686.

L'application de ces procédés de traitement connus à la surface d'acier doux conduit à l'obtention de couches superficielles à forte teneur en chrome qui ont l'avantage d'être inoxydables mais ne présentent pas de duretés élevées. Il s'agit là de la chromisation "douce" qui trouve ses applications dans le domaine de l'inoxydabilité.The application of these known treatment methods to the surface of mild steel leads to the production of surface layers with a high chromium content which have the advantage of being stainless but do not exhibit high hardnesses. This is "soft" chromization which finds its applications in the field of oxidisability.

Grâce à ce type de procédé de chromisation, on obtient sans difficulté des couches de plus en plus profondes ou épaisses par simple augmentation de la durée du cycle de traitement donc du temps de diffusion du chrome.Thanks to this type of chromization process, it is easy to obtain increasingly deep or thick layers by simply increasing the duration of the treatment cycle and therefore the diffusion time of the chromium.

L'application de ces mêmes traitements connus à la surface d'aciers contenant du carbone conduit également à l'obtention de couches superficielles à forte teneur en chrome. Mais cette fois, dans la couche superficielle, le chrome se combine également au carbone pour donner des carbures de chrome qui confèrent à la couche superficielle une grande dureté en plus de son inoxydabilité. Il s'agit là de la chromisation dure qui trouve ses applications dans le domaine des aciers devant présenter une résistance à l'usure combinée éventuellement à l'inoxydabilité desdits aciers.The application of these same known treatments to the surface of steels containing carbon con also results in the production of surface layers with a high chromium content. But this time, in the surface layer, chromium also combines with carbon to give chromium carbides which give the surface layer great hardness in addition to its stainlessness. This is hard chromium plating which finds its applications in the field of steels which must have a resistance to wear possibly combined with the oxidisability of said steels.

Mais dans ce type de chromisation dure si l'on cherche à obtenir comme précédemment des couches de plus en plus profondes en augmentant simplement la durée du cycle de traitement on rencontre les écueils suivants :

  • a) l'affinité chrome-carbone étant très grande, il se forme dès les premières heures du cycle de traitement, une couche de carbure de chrome stable qui forme rapidement une sorte d'écran gênant fortement ou empêchant l'absorption du chrome par l'acier et par conséquent l'augmentation du temps de traitement n'accroît pratiquement plus la profondeur de diffusion du chrome, c'est-à-dire l'épaisseur de la couche chromisée.
  • b) la vitesse de diffusion du carbone dans l'acier étant plus grande que celle du chrome, on constate au contraire que l'augmentation du temps de traitement provoque un "pompage" du carbone de l'acier de base par le chrome superficiel, aboutissant ainsi à la formation d'une couche d'acier décarburée immédiatement sous la couche chromisée. La présence de cette sous-couche décarburée est souvent une gêne pour la tenue mécanique des couches superficielles fortement sollicitées, car la résistance mécanique de l'acier décarburé est très amoindrie.
  • c) la profondeur de diffusion pourrait être accrue par l'augmentation de la température de chromisation, si l'on n'était alors pas limité par le problème du grossissement du grain de l'acier sous jacent, qui a pour inconvénient de fragiliser la sous-couche ce qui peut être néfaste dans certaines applications dans lesquelles les pièces chromisées sont soumises à de fortes sollicitations mécaniques.
But in this type of hard chromization if one seeks to obtain as previously increasingly deeper layers by simply increasing the duration of the treatment cycle one meets the following pitfalls:
  • a) since the chromium-carbon affinity is very high, a stable layer of chromium carbide is formed from the first hours of the treatment cycle, which quickly forms a sort of screen which greatly hinders or prevents the absorption of chromium by steel and therefore increasing the processing time practically no longer increases the depth of diffusion of chromium, that is to say the thickness of the chromized layer.
  • b) the rate of diffusion of the carbon in the steel being greater than that of the chromium, it is noted on the contrary that the increase in the treatment time causes a "pumping" of the carbon of the base steel by the surface chromium, thus resulting in the formation of a layer of decarburized steel immediately below the chromized layer. The presence of this decarburized sub-layer is often a hindrance for the mechanical strength of the highly stressed surface layers, since the mechanical resistance of the decarburized steel is very much reduced.
  • c) the diffusion depth could be increased by increasing the chromization temperature, if one were not then limited by the problem of the magnification of the grain of the underlying steel, which has the disadvantage of weakening the undercoat which can be harmful in certain applications in which the chromized parts are subjected to strong mechanical stresses.

Dans l'état actuel de la technique et dans le domaine de la chromisation dure, il est ainsi très difficile de dépasser des profondeurs d'une quinzaine de microns, pour la couche superficielle effectivement durcie au-delà d'une dureté de l'ordre de 1200, de préférence 1400 points Vickers. Cette limite minimale de dureté dépend d'ailleurs de la composition chimique effective de l'acier à traiter.In the current state of the art and in the field of hard chromization, it is therefore very difficult to exceed depths of about fifteen microns, for the surface layer actually hardened beyond a hardness of the order 1200, preferably 1400 Vickers points. This minimum hardness limit also depends on the effective chemical composition of the steel to be treated.

On a déjà proposé de prévoir un apport superficiel en azote avant l'opération de chromisation (voir par exemple brevet français 1.410.647 ou le brevet US correspondant 3,282,746). Les conditions de ce traitement préalable (température supérieure à la température critique et durée inférieure à deux heures - présence de carbone dans les gaz de traitement) ne permettent pas d'obtenir une couche superficielle chromisée dure d'une épaisseur supérieure à 20 microns. En outre, selon le procédé connu, les nitrures présents dans la couche superficielle restent isolés sous forme d'une bande intermédiaire.It has already been proposed to provide a surface nitrogen supply before the chromizing operation (see for example French patent 1,410,647 or the corresponding US patent 3,282,746). The conditions of this preliminary treatment (temperature above the critical temperature and duration less than two hours - presence of carbon in the treatment gases) do not make it possible to obtain a hard chromized surface layer with a thickness greater than 20 microns. In addition, according to the known method, the nitrides present in the surface layer remain isolated in the form of an intermediate strip.

Le but de la présente invention est de proposer un procédé de chromisation dure du type susmentionné et permettant de réaliser des pièces d'acier possédant une couche superficielle chromisée dure comportant des carbo-nitrures, couche d'une épaisseur supérieure à au moins 20 microns, de préférence 30 microns, et une sous-couche à grains fins et peu ou pas décarburée.The object of the present invention is to propose a hard chromization process of the aforementioned type and making it possible to produce steel parts having a hard chromized surface layer comprising carbo-nitrides, a layer having a thickness greater than at least 20 microns, preferably 30 microns, and a fine grain undercoat with little or no decar burée.

Ce but est atteint du fait que préalablement à l'opération de chromisation proprement dite, l'introduction de l'azote dans la couche superficielle de la pièce métallique est faite de telle sorte que la couche superficielle azotée présente une teneur supérieure à 0,8 % d'azote sur une profondeur ou épaisseur au moins égale à 0,5 mm.This object is achieved by the fact that prior to the actual chromizing operation, the introduction of nitrogen into the surface layer of the metal part is made so that the nitrogenous surface layer has a content greater than 0.8 % nitrogen over a depth or thickness at least equal to 0.5 mm.

Grâce à l'invention, on obtient alors après l'opération de chromisation proprement dite des couches chromisées dures comportant des carbo-nitrures au lieu de carbures séparés et/ou de nitrures séparés, cescouches étant d'une épaisseur supérieure à au moins 20 microns et présentant une résistance élevée à l'usure.Thanks to the invention, there are then obtained after the actual chromization operation hard chromized layers comprising carbo-nitrides instead of separate carbides and / or separate nitrides, these layers being of a thickness greater than at least 20 microns and having a high resistance to wear.

L'expérience de la Demanderesse a conduit à mettre en évidence l'influence bénéfique de l'azote

  • - d'une part, sur l'affinité chrome-carbone et par conséquent sur la vitesse de formation du carbure de chrome conduisant même, pour une teneur suffisante en azote, à la formation de carbonitrures de chrome au lieu de carbures de chrome et,
  • - d'autre part, sur les vitesses respectives de diffusion du carbone et du chrome dans l'acier et,
  • - par ailleurs, sur la cinétique de grossissement du grain de l'acier.
The Applicant's experience has led to highlight the beneficial influence of nitrogen
  • - on the one hand, on the chromium-carbon affinity and therefore on the rate of formation of chromium carbide leading even, for a sufficient nitrogen content, to the formation of chromium carbonitrides instead of chromium carbides and,
  • - on the other hand, on the respective diffusion rates of carbon and chromium in the steel and,
  • - moreover, on the magnification kinetics of the steel grain.

Il en résulte que la présence d'azote dans les couches superficielles des pièces d'acier permet de réaliser un équilibre différent des éléments chrome et carbone vis à vis de l'acier de base lors de la réaction de chromisation, cet équilibre différent permettant ainsi d'obtenir des couches superficielles chromisées beaucoup plus profondes sans produire de sous-couches notablement décarburées et sans grossir le grain en sous-couche.As a result, the presence of nitrogen in the surface layers of the steel parts makes it possible to achieve a different balance of the chromium and carbon elements with respect to the base steel during the chromization reaction, this different balance thus allowing to obtain much deeper chromized surface layers without producing significantly decarburized undercoats and without enlarging the grain in undercoat.

L'introduction de l'azote dans les couches superficielles des pièces d'acier à chromiser conduit à une sorte d'activation desdites couches.The introduction of nitrogen into the surface layers of the pieces of steel to be chromized leads to a sort of activation of said layers.

L'introduction superficielle d'azote peut se réaliser en chauffant la pièce à traiter à une température comprise entre 400 et 8000C et de toute façon à une température inférieure au point critique inférieur de l'acier traité, et pendant les durées comprises entre 12 et 150 heures dans un milieu générateur d'azote qui, à titre d'exemple peut être constitué par des sels nitreux fondus, des gaz d'ammoniac ou d'azote, ionisés ou non.The surface introduction of nitrogen can be carried out by heating the workpiece to a temperature between 400 and 800 ° C. and in any case at a temperature below the lower critical point of the treated steel, and for the periods between 12 and 150 hours in a nitrogen generating medium which, by way of example may consist of molten nitrous salts, ammonia or nitrogen gases, ionized or not.

Cette technique est assez analogue aux techniques classiques de nitruration mais toutefois les températures et les durées de chauffage optimales doivent être choisies en fonction des nuances d'acier considérées et surtout en fonction de l'effet ultérieur escompté lors de la phase finale de chromisation.This technique is quite analogous to conventional nitriding techniques but, however, the optimum temperatures and heating times must be chosen according to the steel grades considered and especially according to the expected later effect during the final chromization phase.

En effet, des introductions superficielles trop pauvres en azote n'auraient pas d'action suffisante ni sur la profondeur de la couche chromisée, ni sur la formation des carbonitrures de chrome et des introductions d'azote trop superficielles pourraient effectivement agir favorablement sur la profondeur de la couche chromisée proprement dite mais n'auraient pas l'action escomptée sur la décarburation et la grosseur de grain de la sous-couche.Indeed, surface introductions that are too poor in nitrogen would not have sufficient action either on the depth of the chromized layer, or on the formation of chromium carbonitrides, and too superficial nitrogen introductions could effectively act on the depth. of the chromized layer proper but would not have the expected action on the decarburization and the grain size of the undercoat.

Il importe donc de préparer des couches superficielles azotées comportant préalablement une teneur supérieure à 0,8 % d'azote sur une profondeur au moins égale à 0,5 mm. De préférence, on prépare des couches superficielles azotées ayant une teneur d'azote comprise entre 1 et 2 % sur une profondeur de 0,5 à 1,0 mm. Sur un acier du type 32 CDV 13 de telles couches azotées satisfaisantes peuvent être obtenues par des cycles de traitement en atmosphère d'ammoniac de 24 heures à 700°C ou 90 heures à 560°C.It is therefore important to prepare nitrogenous surface layers previously containing more than 0.8% nitrogen over a depth at least equal to 0.5 mm. Preferably, nitrogenous surface layers are prepared having a nitrogen content of between 1 and 2% over a depth of 0.5 to 1.0 mm. On a steel of type 32 CDV 13 such satisfactory nitrogenous layers can be obtained by treatment cycles in an ammonia atmosphere of 24 hours at 700 ° C or 90 hours at 560 ° C.

Cette introduction de l'azote peut être réalisée :

  • - soit par une opération conduite dans une installation séparée et préalablement à l'opération de chromisation proprement dite, avec un refroidissement de la pièce à traiter entre l'introduction superficielle d'azote et ladite opération de chromisation,
  • - soit dans l'installation de chromisation proprement dite, lors d'une phase initiale destinée seulement à l'introduction d'azote et suivie du cycle de chromisation proprement dit.
This introduction of nitrogen can be carried out:
  • either by an operation carried out in a separate installation and prior to the actual chromization operation, with cooling of the part to be treated between the surface introduction of nitrogen and said chromization operation,
  • - or in the actual chromization installation, during an initial phase intended only for the introduction of nitrogen and followed by the actual chromization cycle.

Lors de la phase finale de chromisation, l'atmosphère d'halogénure de chrome est conforme à la technique déjà connue, les paramètres de température et de durée de maintien peuvent être conformés à la technique déjà connue, mais ils peuvent aussi être modifiés en fonction de l'introduction préalable d'azote ; par rapport à ce qu'ils seraient sur le même acier non "activé" conformément à la présente invention. En particulier, les températures de chromisation peuvent être réduites afin de limiter le grossissement des grains de la sous-couche.During the final chromization phase, the chromium halide atmosphere conforms to the already known technique, the temperature and holding time parameters can be conformed to the already known technique, but they can also be modified according to the prior introduction of nitrogen; compared to what they would be on the same non "activated" steel according to the present invention. In particular, the chromization temperatures can be reduced in order to limit the magnification of the grains of the undercoat.

Il convient en effet de distinguer deux mécanismes différents tous deux bénéfiques à la finesse ou petitesse des grains :

  • 1) Dans la sous-couche proche, et de façon plus précise sous une profondeur de l'ordre du millimètre, la présence effective d'azote a pour effet direct l'obtention d'un grain beaucoup plus fin pour une température égale de chromisation.
  • 2) Dans la sous-couche profonde et de façon plus précise dans tout le coeur des pièces d'acier il n'y a pas présence d'azote et le grossissement des grains pourrait s'effectuer comme dans une opération de chromisation connue. Cependant, dans la mesure où l'invention permet de pratiquer la chromisation à température plus basse, cela a pour effet indirect de provoquer un grossissement de grain plus faible.
It is indeed necessary to distinguish two different mechanisms both beneficial to the fineness or smallness of the grains:
  • 1) In the near sub-layer, and more precisely under a depth of the order of a millimeter, the effective presence of nitrogen has the direct effect of obtaining a much finer grain for an equal chromization temperature. .
  • 2) In the deep sub-layer and more precisely throughout the core of the steel parts there is no presence of nitrogen and the magnification of the grains could be carried out as in a known chromization operation. However, insofar as the invention makes it possible to practice chromization at a lower temperature, this has the indirect effect of causing a lower magnification of the grain.

Après chromisation, les pièces d'acier peuvent préférablement subir un traitement thermique de régénération en vue de réduire les grosseurs de grain et améliorer les résiliences de l'acier de base.After chromization, the steel parts can preferably undergo a regenerative heat treatment in order to reduce the grain sizes and improve the resilience of the base steel.

A titre d'exemple, on indique sur le dessin annexé la comparaison des couches chromisées obtenues sur une même nuance d'acier 32 CDV 13 (AFNOR) par les techniques de chromisation connues sans ou avec activation préalable par l'azote et dans les trois cas suivies d'un traitement thermique de.régénération du grain par chauffage sous vide, trempe et revenu.By way of example, the comparison drawing shows the comparison of the chromized layers obtained on the same steel grade 32 CDV 13 (AFNOR) by known chromization techniques without or with prior activation by nitrogen and in the three cases followed by a heat treatment of grain regeneration by heating under vacuum, quenching and tempering.

Sur le dessin annexé, la figure 1 est un diagramme de microduretés montrant pour la nuance d'acier 32 CDV 13 (AFNOR) trois exemples de pièces d'acier chromisées et, les figures 2 à 4 montrent des micro- photos de la couche superficielle et de la sous-couche adjacente de ces trois exemples de pièces d'acier chromisées, le facteur d'agrandissement étant dans les trois cas de 200.In the appended drawing, FIG. 1 is a micro-hardness diagram showing for the steel grade 32 CDV 13 (AFNOR) three examples of chromized steel parts and, FIGS. 2 to 4 show micro-photos of the surface layer and of the adjacent underlay of these three examples of chromized steel parts, the enlargement factor being in all three cases of 200.

Sur la figure 1, on a indiqué sur l'ordonnée la dureté de différents niveaux des pièces d'acier, dureté mesurée en points Vickers et sur l'abscisse l'épaisseur ou profondeur des couches en microns à partir de la surface de la pièce d'acier considérée.In FIG. 1, the hardness of different levels of the steel parts is indicated on the ordinate, hardness measured in Vickers points and on the abscissa the thickness or depth of the layers in microns from the surface of the part of steel considered.

Sur cette figure 1, la courbe a en trait plein représente la dureté d'une pièce d'acier en degrés Vickers en fonction de la profondeur du niveau considéré. Cette pièce d'acier dont la structure transversale est illustrée sur la figure 2 n'a pas subi d'activation préalable par l'azote, mais seulement une opération de chromisation de 12 heures à 940°C.In this FIG. 1, the curve a in solid lines represents the hardness of a piece of steel in Vickers degrees as a function of the depth of the level considered. This piece of steel, the transverse structure of which is illustrated in FIG. 2, has not been previously activated by nitrogen, but only one chromium-plating operation for 12 hours at 940 ° C.

On constate que la couche superficielle chromisée 1 a une profondeur ou épaisseur de 12 microns et présente une dureté Vickers supérieure à 1 500 points et atteignant plus de 1800 points. Dès que l'on sort de la couche superficielle chromisée 1 vers le coeur de la pièce d'acier, on pénètre dans une sous-couche2 dont la dureté Vickers diminue rapidement jusqu'à une valeur minimale de 260 pour remonter ensuite lentement jusqu'à la dureté Vickers au coeur de la pièce d'acier dureté qui est d'une valeur de l'ordre de 350 et est atteinte à une profondeur de 77 microns. L'épaisseur de cette sous-couche ou zone de décarburation 2 est de l'ordre de 65 microns ce qui est plus de 5 fois l'épaisseur de la couche superficielle chromisée 1 et la dureté minimale de la sous-couche 2 n'est qu'environ 3/4 de la dureté Vickers au coeur de la pièce d'acier. La diminution de la dureté de la sous-couche par rapport à celle du coeur de la pièce d'acier montre clairement l'étendue de la zone décarburée et l'influence néfaste du pompage de carbone inévitable pendant l'opération de chromisation connue. On constate aussi d'après la figure 2 que la grosseur de grain en sous-couche est importante (indice Afnor 4).It can be seen that the chromized surface layer 1 has a depth or thickness of 12 microns and has a Vickers hardness greater than 1,500 points and reaching more than 1,800 points. As soon as one leaves the chromized surface layer 1 towards the core of the steel part, one enters a sub-layer 2 whose Vickers hardness decreases rapidly to a minimum value of 260 and then slowly rises to Vickers hardness at the heart of the hardness steel part which is of the order of 350 and is reached at a depth of 77 microns. The thickness of this sublayer or decarburization zone 2 is of the order of 65 microns which is more than 5 times the thickness of the chromized surface layer 1 and the minimum hardness of the sublayer 2 is only about 3/4 of the Vickers hardness at the heart of the steel part. The decrease in the hardness of the underlay compared to that of the core of the steel part clearly shows the extent of the decarburized zone and the harmful influence of the inevitable carbon pumping during the known chromization operation. It can also be seen from FIG. 2 that the size of the grain in the sub-layer is significant (Afnor index 4).

La courbe b de la figure 1 montre la dureté d'une pièce d'acier de la même nuance précitée sans activation à l'azote, soumise à une opération de chromisation également pendant 12 heures, mais à une température plus élevée, à savoir 980°C. Cette augmentation de température porte à 16 microns la profondeur de la couche superficielle chromisée 1, mais en contre partie la structure correspondante illustrée par la figure 3 montre une grosseur de grain encore plus importante-et défavorable (indice Afnor 3) que celle de la structure représentée sur la figure 2 et le diagramme de microduretés montre en bas de la courbe b entre une profondeur de 16 microns et de 85 microns (sous-couche 2) une zone de décarburation encore plus profonde et plus intense (dureté minimale Vickers 240 points)que celle de l'exemple de la courbe a et de la figure 2. Ici la dureté Vickers de la sous-couche 2 est de l'ordre des 2/3 de la dureté Vickers au coeur de la pièce d'acier et la sous-couche 2 avec sa zone décarburée a une épaisseur au moins quatre fois supérieure à celle de la couche superficielle chromisée 1.Curve b of FIG. 1 shows the hardness of a piece of steel of the same aforementioned grade without activation with nitrogen, subjected to a chromization operation also for 12 hours, but at a higher temperature, namely 980 ° C. This increase in temperature brings the depth of the chromized surface layer 1 to 16 microns, but on the other hand the corresponding structure illustrated in FIG. 3 shows an even larger and unfavorable grain size (Afnor index 3) than that of the structure. shown in Figure 2 and the diagram of microhardness shows at the bottom of curve b between a depth of 16 microns and 85 microns (sublayer 2) an even deeper and more intense decarburization zone (minimum Vickers hardness 240 points) than that of the example in the curve a and of FIG. 2. Here the Vickers hardness of the undercoat 2 is of the order of 2/3 of the Vickers hardness at the heart of the steel part and the undercoat 2 with its decarburized zone a a thickness at least four times greater than that of the chromized surface layer 1.

La courbe c de la figure 1 correspond à une pièce d'acier ayant subi l'activation préalable par l'introduction superficielle d'azote conformément à la présente invention (cycle de traitement de 90 heures à 560°C). Cette courbe c de la figure 1 montre la dureté Vickers d'une pièce d'acier de la même nuance que les exemples précédents, mais est obtenue après le même cycle de chromisation que l'exemple de la courbe a, soit 12 heures à 940°C. Comme on peut le voir sur les figures 1 et 4, la couche chromisée 1 présente une profondeur de 50 microns. La structure; illustrée par la figure 4 montre en plus la finesse du grain obtenu dans la sous-couche 2 sur une profondeur de 1mm et le diagramme des microduretés (figure 1) montre pour la courbe c une zone de décarburation beaucoup moins épaisse (20 à 30 microns) et moins intense (dureté Vickers minimale environ 330 points) que sur les deux exemples précédents.Curve c of FIG. 1 corresponds to a piece of steel having undergone prior activation by the surface introduction of nitrogen in accordance with the present invention (treatment cycle of 90 hours at 560 ° C.). This curve c in FIG. 1 shows the Vickers hardness of a piece of steel of the same grade as the previous examples, but is obtained after the same chromization cycle as the example of curve a, that is 12 hours at 940 ° C. As can be seen in Figures 1 and 4, the chromized layer 1 has a depth of 50 microns. The structure; illustrated by FIG. 4 also shows the fineness of the grain obtained in the sub-layer 2 over a depth of 1 mm and the diagram of microduretures (FIG. 1) shows for curve c a much less thick decarburization zone (20 to 30 microns ) and less intense (minimum Vickers hardness around 330 points) than in the two previous examples.

On remarque que, dans le cas de l'exemple selon l'invention, l'épaisseur de la zone décarburée est très faible, est inférieure à celle de la couche chromisée 1 et n'est qu'environ égale à la moitié de celle de ladite couche chromisée 1. Quant à la dureté de la zone décarburée de la sous-couche 2, elle est au moins égale à environ 95 % de la dureté du coeur de la pièce d'acier. Autrement dit, la perte de dureté dans la sous-couche par rapport à l'acier de base au coeur de la pièce d'acier est intérieure à 25 points Vickers et affecte une zone faiblement décarburée d'une épaisseur inférieure à 25 microns. On a ici une très bonne finesse de grain dans la sous-couche 2, finesse de grain qui est au moins égale ou supérieure à l'indice Afnor6(indice 7) sur une épaisseur au moins égale à 0,5 mm (1 mm).It is noted that, in the case of the example according to the invention, the thickness of the decarburized zone is very small, is less than that of the chromized layer 1 and is only approximately equal to half that of said chromized layer 1. As for the hardness of the decarburized zone of the underlayer 2, it is at least equal to about 95% of the hardness of the core of the steel piece. In other words, the loss of hardness in the underlayment compared to the base steel at The core of the steel part is inside 25 Vickers points and affects a weakly decarburized area with a thickness of less than 25 microns. Here we have a very good grain fineness in the sublayer 2, grain fineness which is at least equal to or greater than the Afnor6 index (index 7) over a thickness at least equal to 0.5 mm (1 mm) .

Comme précédemment mentionné, il importe que l'acier contenant du carbone et destiné à la chromisation dure ait une couche superficielle contenant au moins 0,8 % d'azote sur une profondeur supérieure à 0,5 mm. On a constaté que dans la mesure où la teneur en azote de la couche superficielle avant chromisation dépasse 0,8 % sur une profondeur de 0,5 mm, on retrouve après la dite chromisation dans la sous-couche une teneur d'azote résiduel supérieure à 0,4 % sur une profondeur supérieure à 0,5 mm, cette teneur en azote empêchant une décarburation importante et un grossissement notable du grain de la sous-couche.As previously mentioned, it is important that carbon-containing steel intended for hard chromium plating has a surface layer containing at least 0.8% nitrogen over a depth greater than 0.5 mm. It has been found that to the extent that the nitrogen content of the surface layer before chromization exceeds 0.8% over a depth of 0.5 mm, there is found after said chromization in the sublayer a higher residual nitrogen content at 0.4% over a depth greater than 0.5 mm, this nitrogen content preventing significant decarburization and a significant enlargement of the grain of the undercoat.

En outre, lorsque la teneur en azote de la couche superficielle de l'acier est, avant la chromisation, supérieure à 0,8 % sur une profondeur supérieure à 0,5 mm on retrouve après ladite chromisation dans la couche superficielle chromisée la présence de carbonitrures de chrome dont la teneur en azote est supérieure à 2 %.In addition, when the nitrogen content of the surface layer of the steel is, before chromization, greater than 0.8% over a depth greater than 0.5 mm, after said chromization is found in the chromized surface layer the presence of chromium carbonitrides with a nitrogen content greater than 2%.

On retrouve d'ailleurs dans tous les cas une sous-couche qui sur une épaisseur au moins égale à 1 mm présente un grain fin d'indice Afnor égal ou supérieur à 7.We also find in all cases an undercoat which over a thickness at least equal to 1 mm has a fine grain of Afnor index equal to or greater than 7.

L'invention vise non seulement le nouveau procé- dé de chromisation dure, mais aussi les pièces d'acier traitées à l'azote en vue de la chromisation ainsi que les pièces d'acier chromisées selon le présent procédé et possédant une couche superficielle chromisées dures d'une profondeur au moins égale à 20 microns et ayant une dureté Vickers au moins égale à 1200 points.The invention relates not only to the new hard chromization process, but also to the pieces of steel treated with nitrogen with a view to chromization as well as to the pieces of steel chromized according to the present process and having a chromized surface layer. hard with a depth of at least 20 microns and a Vickers hardness of at least 1200 points.

Claims (12)

1. Procédé de chromisation de pièces métalliques telles que des pièces d'acier, du type selon lequel on fait diffuser du chrome à la surface de pièces métalliques en vue d'obtenir une couche superficielle de chrome et selon lequel l'apport de chrome est obtenu par la décomposition en phase gazeuse d'halogénures de chrome, la décomposition de l'halogénure et la diffusion du chrome dans l'acier étant réalisées simultanément en chauffant lesdites pièces à des températures ne dépassant pas 1300°C dans l'atmosphère d'halogénure, cette opération de chromisation proprement dite étant précédée d'une opération d'apport superficiel d'azote, caractérisé en ce que l'introduction de l'azote dans la couche superficielle de la pièce métallique est faite de telle sorte que la couche superficielle azotée présente une teneur supérieure à 0,8 % d'azote sur une profondeur ou épaisseur au moins égale à 0,5 mm.1. A method for chromizing metal parts such as steel parts, of the type in which chromium is made to diffuse on the surface of metal parts in order to obtain a surface layer of chromium and in which the addition of chromium is obtained by the gas phase decomposition of chromium halides, the decomposition of the halide and the diffusion of chromium in the steel being carried out simultaneously by heating said parts to temperatures not exceeding 1300 ° C. in the atmosphere of halide, this chromisation operation proper being preceded by a surface nitrogen supply operation, characterized in that the introduction of nitrogen into the surface layer of the metal part is made so that the surface layer nitrogen has a content greater than 0.8% nitrogen over a depth or thickness at least equal to 0.5 mm. 2. Procédé selon la revendication 1, caractérisé en ce que l'introduction superficielle d'azote est réalisée par le chauffage de la pièce métallique à traiter à une température comprise entre 400°C et 800°C et de toute façon à une température inférieure au point critique inférieur de la pièce métallique traitée, dans un milieu générateur d'azote.2. Method according to claim 1, characterized in that the surface introduction of nitrogen is carried out by heating the metal part to be treated at a temperature between 400 ° C and 800 ° C and in any case at a lower temperature at the lower critical point of the treated metal part, in a nitrogen generating medium. 3. Procédé selon l'une des revendications 1 et2, caractérisé en ce que la durée du cycle d'introduction d'azote est comprise entre 12 et 150 heures.3. Method according to one of claims 1 and2, characterized in that the duration of the nitrogen introduction cycle is between 12 and 150 hours. 4. Procédé selon l'une des revendications 1 à 3, caractérisé en ce que l'introduction superficielle d'azote dans la pièce métallique est immédiatement suivie de l'opération de chromisation proprement dite.4. Method according to one of claims 1 to 3, characterized in that the surface introduction of nitrogen into the metal part is immediately followed by the actual chromization operation. 5. Procédé selon l'une des revendications 1 à 3, caractérisé en ce qu'après le cycle d'introduction superficielle d'azote on laisse refroidir la pièce métallique azotée avant de la soumettre à l'opération de chromisation proprement dite.5. Method according to one of claims 1 to 3, characterized in that after the surface nitrogen introduction cycle is allowed to cool the nitrogenous metal piece before subjecting it to the actual chromization operation. 6. Pièce métallique, notamment d'acier, comportant une couche superficielle chromisée d'une dureté au moins égale à 1200 points Vickers et d'une profondeur au moins égale à 12 microns ainsi qu'une sous-couche adjacente d'une dureté inférieure à celle du coeur de ladite pièce, caractérisée en ce que la couche superficielle chromisée présente des carbonitrures et a une profondeur au moins égale à 20 microns, de préférence 30 microns, et que la dureté de la sous-couche présente un écart maximum de 25 points Vickers par rapport à celle du coeur de ladite pièce.6. Metal part, in particular steel, comprising a chromized surface layer with a hardness at least equal to 1200 Vickers points and a depth at least equal to 12 microns as well as an adjacent undercoat of lower hardness to that of the core of said part, characterized in that the chromized surface layer has carbonitrides and has a depth at least equal to 20 microns, preferably 30 microns, and that the hardness of the underlay has a maximum deviation of 25 Vickers points relative to that of the heart of said piece. 7. Pièce métallique selon la revendication 6, caractérisée en ce que la présence des carbonitrures de chrome dans la couche superficielle chromisée correspond à une teneur minimale en azote au moins égale à 2 %.7. Metal part according to claim 6, characterized in that the presence of chromium carbonitrides in the chromized surface layer corresponds to a minimum nitrogen content at least equal to 2%. 8. Pièce métallique selon la revendication 6, et présentant une sous-couche ayant une zone décarburée, caractérisée en ce que l'épaisseur de la zone décarburée est inférieure à la profondeur de la couche superficielle chromisée.8. Metal part according to claim 6, and having a sub-layer having a decarburized zone, characterized in that the thickness of the decarburized zone is less than the depth of the chromized surface layer. 9. Pièce métallique selon la revendication 8, caractérisée en ce que la zone décarburée a une profondeur ou épaisseur inférieure à 30 microns.9. Metal part according to claim 8, characterized in that the decarburized zone has a depth or thickness less than 30 microns. 10. Pièce métallique selon l'une des revendications 6 à 9, caractérisée en ce que la sous-couche présente du grain fin d'indice Afnor égal ou supérieur à 6 sur une épaisseur ou profondeur au moins égale à 0,5 mm.10. Metal part according to one of claims 6 to 9, characterized in that the sub-layer has fine grain of Afnor index equal to or greater than 6 over a thickness or depth at least equal to 0.5 mm. 11. Pièce métallique selon l'une des revendications 6 à 10, caractérisée en ce que la teneur.en azote résiduel de la sous-couche est supérieure à 0,4 %.11. Metal part according to one of claims 6 to 10, characterized in that the residual nitrogen content.in the sublayer is greater than 0.4%. 12. Pièce métallique selon la revendication 11, caractérisée en ce que la sous-couche présente de l'azote résiduel sur une épaisseur ou profondeur supérieure à 0,5 mm.12. Metal part according to claim 11, characterized in that the sub-layer has residual nitrogen over a thickness or depth greater than 0.5 mm.
EP80400451A 1979-04-20 1980-04-03 Process for chromizing steel articles, and chromized steel articles Expired EP0018263B1 (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1986007614A1 (en) * 1985-06-17 1986-12-31 Kabushiki Kaisha Toyota Chuo Kenkyusho Method of treating the surface of iron alloy materials
EP1904661A1 (en) * 2005-07-21 2008-04-02 Hard Technologies Pty Ltd Duplex surface treatment of metal objects

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4578319A (en) * 1984-05-08 1986-03-25 Toyo Kohan Co., Ltd. Surface treated steel sheet having an excellent weldability and its production method
JP2584217B2 (en) * 1986-11-18 1997-02-26 株式会社豊田中央研究所 Surface treatment method
US5123972A (en) * 1990-04-30 1992-06-23 Dana Corporation Hardened insert and brake shoe for backstopping clutch
SA05260056B1 (en) 1991-03-08 2008-03-26 شيفرون فيليبس كيميكال كمبني ال بي Hydrocarbon processing device
US6274113B1 (en) 1994-01-04 2001-08-14 Chevron Phillips Chemical Company Lp Increasing production in hydrocarbon conversion processes
US6258256B1 (en) 1994-01-04 2001-07-10 Chevron Phillips Chemical Company Lp Cracking processes
US5575902A (en) * 1994-01-04 1996-11-19 Chevron Chemical Company Cracking processes
US6419986B1 (en) 1997-01-10 2002-07-16 Chevron Phillips Chemical Company Ip Method for removing reactive metal from a reactor system
US6197125B1 (en) * 1999-12-13 2001-03-06 Mcdermott Technology, Inc. Modification of diffusion coating grain structure by nitriding
CN115058684B (en) * 2022-06-29 2024-02-09 中国航发动力股份有限公司 Preparation method of chromium hardening layer of high-carbon tool steel

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3205153A (en) * 1962-05-21 1965-09-07 Chandler Evans Inc Process and product of chrome plating nitrided steel
FR1410647A (en) * 1964-10-05 1965-09-10 Formsprag Co Process for hardening rubbing surfaces and new industrial products obtained
US3256818A (en) * 1955-11-26 1966-06-21 Berghaus Bernhard Method of reducing barrel wear
FR95448E (en) * 1967-06-27 1970-11-06 Ct Stephanois De Rech Mecaniqu Surface treatment for mechanical parts.
FR2031373A1 (en) * 1969-02-17 1970-11-20 Petignat Maurice Surface-hardening of oxidn resistant austen - itic steel parts
EP0010484A1 (en) * 1978-10-25 1980-04-30 Creusot-Loire Improvement in the chromising of steel in the gaseous phase

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2437249A (en) * 1946-04-17 1948-03-09 Nitralloy Corp Method of nitriding
FR1012401A (en) * 1949-08-05 1952-07-09 Onera (Off Nat Aerospatiale) Improvements to the processes for forming surface diffusion alloys, especially chromium
FR60539E (en) * 1949-12-06 1954-11-09 Nat D Etudes & De Rech S Aeron Improvements to the processes for forming surface diffusion alloys, especially chromium
FR60686E (en) * 1950-06-27 1954-11-22 Onera (Off Nat Aerospatiale) Improvements to the processes for forming surface diffusion alloys, especially chromium
US3152007A (en) * 1961-04-13 1964-10-06 Diamond Alkali Co Process for chromizing ferrous metal objects
US3222212A (en) * 1962-11-29 1965-12-07 Alloy Surfaces Co Inc Process for chromizing
US3282746A (en) * 1963-11-18 1966-11-01 Formsprag Co Method of hardening wear surfaces and product
US3414428A (en) * 1964-10-20 1968-12-03 Allied Chem Chromizing compositions and methods and continuous production of chromium halides for chromizing
FR1555534A (en) * 1967-06-27 1969-01-31
US3892597A (en) * 1972-04-13 1975-07-01 Midland Ross Corp Method of nitriding
US4042426A (en) * 1975-03-10 1977-08-16 National Steel Corporation Chromized steel substrate

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3256818A (en) * 1955-11-26 1966-06-21 Berghaus Bernhard Method of reducing barrel wear
US3205153A (en) * 1962-05-21 1965-09-07 Chandler Evans Inc Process and product of chrome plating nitrided steel
FR1410647A (en) * 1964-10-05 1965-09-10 Formsprag Co Process for hardening rubbing surfaces and new industrial products obtained
FR95448E (en) * 1967-06-27 1970-11-06 Ct Stephanois De Rech Mecaniqu Surface treatment for mechanical parts.
FR2031373A1 (en) * 1969-02-17 1970-11-20 Petignat Maurice Surface-hardening of oxidn resistant austen - itic steel parts
EP0010484A1 (en) * 1978-10-25 1980-04-30 Creusot-Loire Improvement in the chromising of steel in the gaseous phase

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
SOVIET INVENTIONS ILLUSTRATED, juin 1966, Derwent Publications Ltd., Metallurgy (7), page 8, Londres GB, & SU - A - 176 152 (YU.N. GRIBOEDOV), (17-06-1964). *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1986007614A1 (en) * 1985-06-17 1986-12-31 Kabushiki Kaisha Toyota Chuo Kenkyusho Method of treating the surface of iron alloy materials
EP1904661A1 (en) * 2005-07-21 2008-04-02 Hard Technologies Pty Ltd Duplex surface treatment of metal objects
EP1904661A4 (en) * 2005-07-21 2010-12-29 Hard Technologies Pty Ltd Duplex surface treatment of metal objects
US8317926B2 (en) 2005-07-21 2012-11-27 Hard Technologies Pty Ltd. Duplex surface treatment of metal objects

Also Published As

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FR2454471B1 (en) 1983-12-23
US4481264A (en) 1984-11-06
FR2454471A1 (en) 1980-11-14
ATE3883T1 (en) 1983-07-15
EP0018263B1 (en) 1983-06-22
DE3063830D1 (en) 1983-07-28

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