Process for manufacturing toothed parts hardened by nitriding, in particular parts for aircraft turbomachines

The method of austenitization, quenching, intermediate tempering, and staged nitriding addresses the challenge of achieving high surface hardness in steel parts for turbomachines by maintaining core hardness and reducing production time, suitable for industrial-scale production.

FR3159176A1Pending Publication Date: 2025-08-15SAFRAN SA +1
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Patent Information

Application Number
FR2024001231
Authority / Receiving Office
FR · FR
Patent Type
Applications
Current Assignee / Owner
Filing Date
2024-02-08
Publication Date
2025-08-15

AI Technical Summary

Technical Problem

Existing nitriding processes for steel parts, particularly for aircraft turbomachines, face challenges in achieving high surface hardness while maintaining core hardness, and are inefficient for mass production due to long treatment times and tempering effects that reduce overall hardness.

Method used

A method involving austenitization, quenching, low-temperature intermediate tempering, wire electroerosion tooth cutting, and staged nitriding at varying temperatures and potentials to form hardened layers without compromising core hardness, including low-temperature and high-temperature nitriding steps.

Benefits of technology

Enables the production of toothed parts with high surface hardness suitable for mechanical transmission without reducing core hardness, compatible with industrial-scale production times and avoiding the need for post-nitriding layer removal.

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Abstract

A method (1) is proposed for manufacturing a toothed part from a nitriding steel part comprising the following successive steps: a step of heat treatment (2) of the steel part at a first austenitization temperature of the steel and quenching (3) of the part, a step of intermediate tempering (4) of the steel part up to a second temperature lower than 350 °C, a step of cutting teeth (5) in a surface of the part by wire electroerosion, a step of nitriding (7, 8) the part at a third temperature higher than the second temperature and lower than the first temperature. Figure for abstract: Fig. 1
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Description

Title of the invention: Method for manufacturing toothed parts hardened by nitriding, in particular parts for aircraft turbomachines Technical field

[0001] The present disclosure relates generally to the field of metallurgy. It relates more specifically to processes for manufacturing steel parts comprising heat treatment of steel parts by nitriding. It advantageously finds application for the manufacture of power transmission parts, such as, for example, pinion teeth, crowns or bearings used in aircraft turbomachines. STATE OF THE ART

[0002] In order to increase the mechanical hardness on the surface of a steel part, it is common to use heat treatment processes called "nitriding", during which nitrogen atoms are diffused into the surface to be treated, in particular by applying a nitrogen-rich gaseous environment around the part. The gases, which generally include ammonia, are adsorbed by the surface, and precipitate in the form of iron nitrides on the surface, forming a surface layer called the combination layer or "white" layer. The excess nitrogen will then diffuse into the matrix of the steel and precipitate in the form of nitrides with certain alloying elements (for example chromium, vanadium or molybdenum), forming a diffusion layer. The combination of these two layers forms a hardened layer which increases the hardness of the treated surface.It is generally desirable to remove the combination layer following nitriding, as this layer is too fragile for certain applications, particularly when surface loading of the part is planned.

[0003] A metal part is often subjected to nitriding taking place at temperatures of the order of 480 to 580°C after other heat treatment steps, namely: - a heat treatment called austenitization which results in a homogeneous and entirely austenitic microstructure - quenching, i.e. a rapid drop in the temperature of the part, which transforms at least part of the austenite obtained following heating into martensite, the hardness of which is particularly high, - tempering, which consists of a heat treatment at a temperature typically between 600 and 620°C which softens the effects of quenching by increasing the ductility and toughness of the part while removing the residual stresses of thermal origin resulting from quenching.

[0004] Such methods make it possible to effectively treat the surface of a part, however the time required to implement the nitriding step increases considerably when it is desired to treat a deeper part of the part, which can reach several hundred hours depending on the depth of the treatment. This makes it incompatible with mass production of parts.

[0005] In addition to the industrial and technical difficulties associated with such treatment times in themselves, maintaining the part at a high temperature for a long time during the nitriding step produces the same effects as a tempering step, i.e. a reduction in the hardness of the part, not only in its surface but also in the core of the part. Thus, the greater the depth that one wishes to treat by nitriding, the longer the nitriding step, so that the reduction in hardness in the core of the part becomes significant if the nitriding temperature is high.

[0006] French patent FR 3 082 529 B1 discloses a nitriding treatment process in which the tempering step carried out between the quenching step and the nitriding step is a low-temperature tempering step, or "stress relief". This step, like the tempering step of usual nitriding processes, consists of a rise in temperature then a slow cooling of the part, however the maximum temperature reached is less than 350°C so that the hardness of the part after stress relief in the process of patent FR 3 082 529 B1 is greater than its hardness after tempering in a usual treatment process. After the stress relief step of the patent, the part is in a so-called "tempered-stressed" state, by comparison with the "tempered-tempered" state of a part following the tempering step of usual nitriding processes.The nitriding step according to this patent is therefore carried out on a part with higher hardness, and can take place at a high temperature, the drop in hardness which occurs in the core of the part during the nitriding step becoming acceptable with regard to the target hardness which one wishes to achieve.

[0007] For the specific case of transmission parts, this nitriding process on the part in the "stressed hardened" state gives the part a higher surface hardness than that of a part treated by means of a usual nitriding process (approximately 500 to 600 HV compared to approximately 400 HV respectively), so that it becomes difficult to cut teeth in the part by conventional machining. EXPOSED

[0008] An aim of the present disclosure is therefore to enable the manufacture of a toothed part, such as a mechanical transmission part, which has a high surface hardness without compromising the hardness at the core of the part, by means of a nitriding process whose implementation time is limited.

[0009] To this end, according to a first aspect, a method of manufacturing a toothed part from a nitriding steel part is proposed, comprising the following successive steps:

[0010] a step of heat treatment of the steel part at a first austenitization temperature of the steel and quenching of the part,

[0011] an intermediate tempering step of the steel part up to a second temperature below 350°C,

[0012] a step of cutting teeth in a surface of the part by wire electroerosion,

[0013] a step of nitriding the part at a third temperature higher than the second temperature and lower than the first temperature.

[0014] Thus, the proposed method allows the manufacture of a steel toothed part having a high hardness while maintaining a process implementation time compatible with the production of parts on an industrial scale.

[0015] According to one implementation, the method comprises, after cutting the teeth, a step of grinding the surface of the part by removing material.

[0016] According to one implementation of the method, the nitriding of the part successively comprises:

[0017] a low temperature nitriding step carried out at a temperature greater than or equal to 450°C and less than or equal to 500°C,

[0018] a high temperature nitriding step carried out at a temperature greater than or equal to 520°C and less than or equal to 550°C.

[0019] According to one implementation of the method, the low-temperature nitriding comprises maintaining the steel part in an atmosphere containing gaseous ammonia and gaseous hydrogen, successively for a first time range at a nitriding potential KN ] greater than 3, and for a second time range at a nitriding potential KN 2 greater than a transition nitriding potential at which a formation of phase iron nitride y' takes place,

[0020] the nitriding potential being defined by the equation

[0021] _ ^Hy).

[0022] where p(NH3)i is the partial pressure of ammonia in Pascals and p(H2)i is the partial pressure of hydrogen in Pascals during the i-th time range, and

[0023] i = 1 or 2.

[0024] According to one implementation of the method, the first time range corresponds substantially to 25% of a duration of the low temperature nitriding, and the second time range corresponds substantially to 75% of a duration of the low temperature nitriding.

[0025] According to one implementation of the method, high temperature nitriding comprises the

[0026]

[0027]

[0028]

[0029]

[0030]

[0031]

[0032]

[0033]

[0034]

[0035]

[0036] maintaining the steel part in an atmosphere containing ammonia and hydrogen gas, successively for a third time range at a nitriding potential KN 3 and for a fourth time range at a nitriding potential KN_4 strictly lower than the nitriding potential KN 3, the nitriding potential being defined by the equation K N_i- wherep(NH3)i is the partial pressure of ammonia in Pascals andp(H2)i is the partial pressure of hydrogen in Pascals during the i-th time range, and i = 3 or 4. According to one implementation of the process, high temperature nitriding is carried out for a duration greater than or equal to 100 hours and less than or equal to 300 hours. According to one implementation of the process, the intermediate tempering is carried out at a temperature greater than or equal to 180°C and less than or equal to 300°C. Furthermore, a turbomachine is proposed comprising a toothed part obtained by implementing the method defined above, the toothed part being in particular a mechanical transmission part. DESCRIPTION OF FIGURES Other characteristics, aims and advantages of the invention will emerge from the following description, which is purely illustrative and non-limiting, and which must be read in conjunction with the appended drawings in which: [Fig.l] illustrates a method of manufacturing a toothed part according to the present disclosure. Throughout the figures, similar elements have identical references. DETAILED DESCRIPTION A method 1 for manufacturing a toothed part from a nitriding steel part is illustrated in [Fig.l]. The method is suitable for the treatment of any nitriding steel part, typically a low-alloy steel containing elements allowing the formation of nitrides, such as chromium, molybdenum, vanadium or aluminum. The steel has a carbon content which may preferably be from 0.15 to 0.8% by mass. The method allows in particular the manufacture of toothed parts for the aeronautical industry, such as pinions or teeth, which ensure the transmission of mechanical forces or which must more generally withstand the mechanical stresses to which they are subjected, these stresses being concentrated essentially on the surface and near the surface,

[0037] The manufacturing method 1 comprises a first step 2 of heat treatment of the part at an austenitization temperature of the steel, at which the steel has a fully austenitic microstructure. An austenitization temperature corresponds to a temperature which allows the transformation of alpha iron into gamma iron. It can be determined for a given steel from the phase transformation diagrams. The heating step 2 can in particular be carried out up to a temperature greater than or equal to 900°C, for example in the range of temperatures greater than or equal to 920°C and less than or equal to 940°C. The duration of the heating is such that it allows the carbides (carbon and alloying elements) to be dissolved and homogenized in the austenitic matrix. It can be for example between 30 minutes and 1 hour 30 minutes.

[0038] Heat treatment step 2, commonly called the austenitization step, is a step well known to those skilled in the art who will be able to determine the operating conditions for a given steel in order to give the steel initial hardness properties.

[0039] Heat treatment step 2 is followed by a quenching step 3, which is rapid cooling, carried out for example at a sufficiently high cooling rate, given by the TRC diagram of the steel in question, to allow the complete transformation of austenite into martensite, a crystallographic phase exhibiting particularly high hardness.

[0040] The quenching step 3 is a step well known to those skilled in the art, which will therefore not be detailed in the present application.

[0041] The method 1 comprises, subsequent to the quenching step 3, a low-temperature intermediate tempering step 4. This tempering is carried out up to a temperature below 350°C, for example greater than or equal to 150°C and less than or equal to 350°C, preferably greater than or equal to 180°C and less than or equal to 300°C. This low-temperature tempering allows relaxation of the part, i.e. relaxation of part of the residual stresses resulting from the quenching and a slight softening of the material allowing it to be machined without risking the appearance of cracks. The hardness of the core of the part always remains quite high compared to parts having undergone “conventional” tempering at higher temperatures of the order of 570-620°C.

[0042] Following the intermediate tempering step 4, a step of cutting teeth 5 is carried out in the part, so as to obtain a toothed part. This may in particular be a transmission part, such as a gear for a reducer. The cutting of teeth 5 is carried out by wire electroerosion. Electroerosion methods consist of eroding a conductive part to give it a predetermined shape by applying electrical discharges. For wire electroerosion, a live metal wire and the workpiece are immersed in an insulating liquid. An electric arc is formed between the part to be treated, which forms a first electrode, and the wire under tension, which forms a second electrode - the two electrodes generally not touching (although infrequent contacts can occur without negative consequences on the result obtained). The wire is typically arranged between two coils, so as to allow unwinding of the wire during the implementation of the EDM, so as to change the active part of the wire continuously. The wire is guided so as to erode the part by forming small craters in it, the size of the craters depending on the parameters of the EDM (tension in the wire, width of the wire, etc.). The EDM allows the cutting of teeth 5 in the steel part after the intermediate tempering 4, despite the high hardness of the surface of such a part in the "hardened relaxed" state which can be up to approximately 600HV, in comparison with the parts in the "hardened tempered" state of the state of the art, whose surface is less hard.

[0043] The cutting of teeth 5 is followed by a nitriding step 7, 8 during which the steel part is placed in an atmosphere containing a gas with a high nitrogen content, typically ammonia, which releases nitrogen to the surface of the steel during its adsorption (by catalytic cracking with iron oxide). A surface layer, called a combination layer, then forms on the surface of the steel due to the formation of iron nitrides. Then, the nitrogen diffuses into the matrix of the steel and metal nitrides are formed with certain alloying elements of the steel (for example chromium, vanadium or molybdenum) at the grain boundaries, thus forming a so-called "diffusion" layer. This diffusion layer comprises nitrides formed by the nitrogen atoms in contact with the metals contained in the steel, which give it increased hardness compared to the surface of the part before nitriding.The assembly formed by the diffusion layer and the combination layer forms a hardened layer, which increases the surface hardness of the part. The duration of the nitriding step 7, 8 depends on the depth to which the part is to be treated.

[0044] Preceding nitriding 7, 8 with low-temperature intermediate tempering 4 makes it possible to obtain, between these two steps, a part whose hardness is greater than that of a part which would have been treated with high-temperature tempering, in particular with regard to the hardness at the core of the part. Thus, the drop in hardness which inevitably occurs at the core of the part during nitriding, and which is all the more significant when the nitriding step is carried out at high temperature or for a long time, becomes acceptable: for a part treated by means of low-temperature tempering, the hardness of the core at the start of nitriding is sufficiently high so that the hardness of the core at the end of nitriding remains above a desired threshold.In other words, the low temperature tempering preceding nitriding makes it possible to compensate for the drop in hardness associated with a high nitriding temperature, this high temperature being in itself advantageous because it makes it possible to accelerate the . diffusion. It is therefore possible to increase the surface hardness of the part by means of a relatively long nitriding without compromising the hardness at the core of the part, or alternatively, and in accordance with the Hollomon-Jaffe law, to reduce the treatment time required while maintaining comparable hardness over the same depth, because the nitriding can then be carried out at a higher temperature.

[0045] According to one embodiment, a grinding step 6 is implemented following the tooth cutting step 5. The grinding step 6 is preferably implemented before the nitriding 7, 8 so as to be carried out when the surface hardness of the part has not yet reached its post-nitriding value, but can possibly be carried out after the nitriding 7, 8. The cutting of teeth 5 by electroerosion can disturb the metallurgical structure on the surface of the part over a few hundred microns, and in particular increase the geometric irregularity of the surface of the part. Such a grinding step 6 therefore makes it possible to obtain a part surface which has dimensions included within predefined tolerances.

[0046] According to one embodiment, the nitriding 7, 8 is carried out in two separate steps. A first low-temperature nitriding step 7 is implemented at a temperature greater than or equal to 450°C and less than or equal to 500°C. The duration of this stage is set according to the depth of the part that it is desired to treat, as well as according to the thickness of the surface that must be removed during the grinding 6. The low-temperature nitriding 7 makes it possible to generate small-sized metal nitrides in the surface of the part so as to increase its hardness, the so-called “white layer” or “combination layer” containing the nitrides and of very low thickness being formed in the extreme surface of the part. The low-temperature nitriding 7 is followed by a high-temperature nitriding step 8, implemented at a temperature greater than or equal to 520°C and less than or equal to 550°C.The duration of this step depends on the nitriding temperature, the depth of the part to be treated, and the desired surface and core hardness of the part, and may in particular be between 100 and 300 hours. The high-temperature nitriding temperature 8 may be chosen so as to be significantly lower than the temperature at which the first austenite grains appear in the part, so as not to compromise the beneficial effect of the increase in surface hardness obtained during quenching 3. Indeed, nitriding carried out in the austenitic range would generate nitrogen ferrite, which is particularly brittle. High-temperature nitriding 8 allows the diffusion of the nitrogen atoms contained in the white layer towards the interior of the part, so as to form a layer called the "diffusion layer", adjacent to the white layer.The division of the nitriding step into two steps of low temperature 7 and high temperature 8 nitriding allows a good compromise between, on the one hand, the nitriding duration, and on the other hand the performances. mechanical properties of the treated part. Indeed, the inventors have found that nitriding carried out entirely at high temperature, for example at 550°C, negatively affects the hardness at the core of the part, despite the use of a low-temperature intermediate tempering 4, while nitriding carried out entirely at low temperature, for example at 450°C, must be carried out for unacceptable durations for the efficient production of transmission parts.

[0047] In a known manner, a nitriding step is characterized by a quantity called nitriding potential, defined by the equation:

[0048] V Pte / 2

[0049] where p(NH3) is the partial pressure of ammonia and p(H2) the partial pressure of hydrogen, both expressed in Pascals. This quantity effectively reflects the nitriding nature of an atmosphere.

[0050] According to one embodiment, the low-temperature nitriding step 7 is itself carried out in two successive sub-steps, both carried out at a temperature in the range of 450 - 500 °C but at different nitriding potentials KN. The first low-temperature nitriding sub-step 7 is carried out at a nitriding potential KN ] greater than 3, while the second low-temperature nitriding sub-step 7, which follows the first sub-step, is carried out at a nitriding potential KN 2 greater than a transition nitriding potential, at which the formation of y'-phase iron nitrides begins, i.e. of chemical formula Fe3N4. The first low-temperature nitriding sub-step 7 makes it possible, thanks to its high nitriding potential, to ensure the formation of a white layer of sufficient thickness to be able to act as a reservoir of nitrogen atoms during the remainder of the nitriding.During the second sub-step, the growth of nitrides in the white layer is significantly less important than during the first sub-step due to the lower nitriding potential KN. This makes it possible to reduce the growth kinetics of the combination layer, or even to consume it in order to avoid a rectification step of this layer which is too important at the end of manufacturing.

[0051] As regards the duration of the sub-steps, the first low-temperature nitriding sub-step 7 may for example be implemented during the first quarter of the low-temperature nitriding step 7 while the second low-temperature nitriding sub-step 7 may be implemented during the last three-quarters of the low-temperature nitriding step 7.

[0052] For high temperature nitriding 8 carried out in depth, the white layer can reach a few tens of micrometers at the extreme surface, the thickness of the white layer evolving with the depth of nitriding. However, the white layer is very hard, being able to reach 1000 HV, and very fragile. This makes it unusable when the surface of the part is intended to be mechanically loaded, which is the case for mechanical transmission parts. In state-of-the-art nitriding processes carried out at high temperature, it is therefore necessary to remove this white layer after the heat treatment of the part by nitriding, which can be complex and expensive depending on the geometry of the affected area. In addition, during nitriding, the white layer and the diffusion layer have different expansion coefficients, so that significant heating of the part occurring during high-temperature nitriding 8 can lead to crazing of the part.

[0053] One way to overcome this problem is to vary the nitriding potential KN during the high-temperature nitriding step 8. For example, the high-temperature nitriding 8 may comprise a first sub-step, at a nitriding potential KN 3 and a second sub-step at a nitriding potential KN_4 lower than the potential KN 3, so as to maintain a sufficient nitrogen reserve in the combination layer to ensure the diffusion of nitrogen into the diffusion layer and to allow the growth of the diffusion layer while limiting the growth of the combination layer by formation of iron nitride. The first sub-step may last most of the time allocated to the high-temperature nitriding 8, while the second sub-step may be shorter, for example a few hours or a few tens of hours.The first high-temperature nitriding sub-step 8 allows both a continuation of the adsorption of nitrogen atoms by the surface initiated during the low-temperature nitriding 7, as well as a start of diffusion of the nitrogen atoms from the white layer towards the diffusion layer, while the second high-temperature nitriding sub-step 8, which is carried out at a very low nitriding potential KN_4, largely consumes the white layer by diffusion of the nitrogen towards the diffusion layer. Thus, the presence of a white layer at the end of the high-temperature nitriding 8 is eliminated, so that a step of removing such a layer is not necessary.

[0054] Decarburization of the surface may take place during high temperature nitriding 8. A second grinding may be carried out to treat the affected areas, so as to prevent a reduction in the hardness and mechanical strength of these areas.

[0055] According to another aspect, the present disclosure relates to a turbomachine comprising a toothed part, in particular a mechanical transmission part, for example a reducer, the toothed part being obtained by implementing the method for manufacturing a toothed part described previously.

Claims

Claims

1. Method (1) for manufacturing a toothed part from a nitriding steel part comprising the following successive steps: a step of heat treatment (2) of the steel part at a first austenitization temperature of the steel and quenching (3) of the part, a step of intermediate tempering (4) of the steel part up to a second temperature lower than 350°C, a step of cutting teeth (5) in a surface of the part by wire electroerosion, a step of nitriding (7, 8) the part at a third temperature higher than the second temperature and lower than the first temperature.

2. Manufacturing method according to the preceding claim, comprising, after cutting the teeth (5), a step of grinding (6) the surface of the part by removing material.

3. Manufacturing method according to any one of claims 1 and 2, wherein the nitriding of the part successively comprises: a low temperature nitriding step (7) carried out at a temperature greater than or equal to 450°C and less than or equal to 500°C, a high temperature nitriding step (8) carried out at a temperature greater than or equal to 520°C and less than or equal to 550°C.

4. Manufacturing method according to the preceding claim, wherein the low temperature nitriding (7) comprises maintaining the steel part in an atmosphere containing gaseous ammonia (NH3) and gaseous hydrogen (H2), successively during a first time range at a nitriding potential KNj greater than 3, and during a second time range at a nitriding potential KN 2 greater than a transition nitriding potential at which a formation of y' phase iron nitride (Fe3N4) takes place, the nitriding potential being defined by the equation where p(NH3)i is the partial pressure of ammonia in Pascals and p(H2)i is the partial pressure of hydrogen in Pascals during the i-th time range, and i = 1 or 2.

5. Manufacturing method according to the preceding claim, wherein the first time range corresponds substantially to 25% of a duration of the low temperature nitriding (7), and the second time range corresponds substantially to 75% of a duration of the low temperature nitriding (7).

6. A manufacturing method according to any one of claims 3 to 5, wherein the high-temperature nitriding (8) comprises maintaining the steel part in an atmosphere containing gaseous ammonia (NH3) and hydrogen (H2), successively for a third time range at a nitriding potential KN 3 and for a fourth time range at a nitriding potential KN_4 strictly lower than the nitriding potential KN 3, the nitriding potential being defined by the equation / X^. 'v-'“ mr where p(NH3)t is the partial pressure of ammonia in Pascals and p(H2)i is the partial pressure of hydrogen in Pascals during the i-th time range, and i = 3 or 4.

7. A manufacturing method according to any one of claims 3 to 6, wherein the high-temperature nitriding (8) is carried out for a period greater than or equal to 100 hours and less than or equal to 300 hours.

8. Manufacturing method according to any one of claims 1 to 7, wherein the intermediate tempering (4) is carried out at a temperature greater than or equal to 180°C and less than or equal to 300°C.

9. Turbomachine comprising a toothed part obtained by implementing the method according to any one of claims 1 to 8, the toothed part being in particular a mechanical transmission part.

Citation Information

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