• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention relates to a method for heat treatment of a powder-form preform (3) comprising a titanium-based alloy, the method comprising the heat treatment of the preform in an oven (1) at a pre-defined temperature, the preform being on a support (6) during heat treatment. The support (6) comprises a titanium-based alloy whose titanium mass content is greater than or equal to 45%, or a zirconium-based alloy whose mass content of zirconium is greater than or equal to 95%, the material forming the support having a melting temperature higher than the predefined temperature of the heat treatment, and in that an anti-diffusion barrier (7) is disposed between the preform (3) and the support (6) to prevent the weld from the preform on the support.
    公开号:FR3038622A1
    申请号:FR1556375
    申请日:2015-07-06
    公开日:2017-01-13
    发明作者:Guillaume Fribourg；Jean-Claude Bihr；Clement Gillot
    申请人:SNECMA SAS；Alliance Systems Inc；
    IPC主号:
    专利说明:

    Background of the invention
    The present invention relates to the general field of heat treatments of powder preforms. The invention applies more particularly, but not exclusively, to the sintering of preforms of three-dimensional parts obtained by shaping a titanium-based alloy powder.
    It is now common to use methods for manufacturing three-dimensional pieces of metal (or metal alloy) or ceramic implementing a powder shaping step in order to obtain a preform (for example using a powder injection molding technique (PIM or MIM) using a binder, hot isostatic pressing, or "tape casting"), followed by a step of sintering the preform.
    The sintering of the preform consists of a heat treatment at high temperature (typically the sintering temperature is between 70% and 99% of the melting temperature of the material forming the powder of the preform, or even greater than this melting temperature in the case of a liquid phase sintering), intended to densify the powder in order to obtain a consolidated monobloc part.
    For titanium-based alloys (eg TiAl6V4, TiAl-48-2-2, etc.), which are particularly sensitive to oxidation, the sintering conditions must be carefully controlled to minimize contamination of the alloys. the finished part in oxygen. Indeed, the presence of oxygen in the finished part significantly deteriorates its properties and mechanical strength.
    In the sintering conditions generally used for these titanium-based alloys, especially a sintering temperature greater than 1100 ° C., the contamination of the finished parts is relatively significant following the sintering. Sources of oxygen that can potentially contaminate the part during sintering have been identified among the following: - traces of oxygen contained in the atmosphere of the furnace enclosure, - moisture of the furnace, and - oxygen present in the sintering tools (such as the tray supporting the preform or the oven itself).
    It is known to use "getters" of oxygen or oxygen traps, for example in the form of metal chips arranged around the preform, which absorb oxygen by oxidizing.
    However, these oxygen traps do not provide a satisfactory level of oxygen contamination on the aforementioned alloys, resulting in insufficient mechanical strength of the final part.
    Object and summary of the invention
    The main purpose of the present invention is therefore to overcome such drawbacks by proposing a method of heat treatment of a powder piece preform comprising a titanium-based alloy, the process comprising the heat treatment of the preform in an oven at a temperature of predefined temperature, the preform being on a support during the heat treatment. The method is characterized in that the support comprises a titanium-based alloy whose titanium mass content is greater than or equal to 45%, or a zirconium-based alloy whose zirconium content by mass is greater than or equal to 95% the support material having a melting temperature above the predefined temperature of the heat treatment, and in that an anti-diffusion barrier is disposed between the preform and the support to prevent the preform from being welded to the support .
    The process according to the invention is notably remarkable in that the support on which the preform is placed makes it possible to reduce the oxygen contamination of the final part following the heat treatment (this heat treatment can be sintering).
    First of all, since the support comprises a high titanium mass content alloy (typically more than 45%) or a high zirconium mass content alloy (typically more than 95%), it can absorb traces of oxygen in the atmosphere present in the furnace enclosure. Indeed, titanium or zirconium can easily absorb the surrounding oxygen by oxidizing.
    In addition, the support makes it possible to absorb the oxygen that may have already contaminated the preform. Indeed, titanium and zirconium are more reductive than the titanium oxide (T1O2) formed during the oxidation of titanium present in the preform. Thus, the support acts as an oxygen trap for the oxygen present in the preform.
    In the prior art, during the sintering of titanium-based alloy powder preforms, the preform is typically disposed on a ceramic tray (for example, zirconia, alumina or yttrine). It has been observed that the ceramic tray is progressively degraded after several sintering cycles. An oxidation-reduction reaction occurs between the ceramic tray and the workpiece, resulting in the reduction of the ceramic of the tray, and the enrichment of the oxygen part.
    With the method according to the invention, as the preform is disposed on the support it is not in contact with other tools present in the oven (such as a sole, or a ceramic tray such as those presented above), which advantageously prevents these tools from contaminating the preform. In other words, the support acts as a barrier or buffer for oxygen between these tools and the preform.
    Finally, since the support consists of a material having a melting point higher than the predetermined temperature of the heat treatment (for example the temperature of a sintering stage), the plate is plastically deformable, that is to say that it undergoes in particular no irreversible modifications of its structure when it is brought to this temperature. Thus, it can be reused for several heat treatment cycles without deforming.
    In some embodiments, the support comprises a titanium-based alloy whose titanium mass content is greater than or equal to 90%, more preferably greater than or equal to 99%. For example, the support may comprise a titanium-based alloy selected from the following: T40, T60, TIA6V4, TiAI-48-2-2.
    Alternatively, the support may comprise a zirconium-based alloy selected from Zircaloy-2, Zircaloy-4.
    Preferably, the support has a thickness of between 0.1 mm and 20 mm.
    Also preferably, the anti-diffusion barrier comprises alumina or yttrium oxide (Yttrine).
    More preferably, the plate is etched. By "stripped" is meant any treatment intended to erode the upper surface of the support intended to support the preform, such as for example: by polishing, by milling, by sandblasting ... This treatment makes it possible to eliminate the oxide layer which can form on the support when it is in the presence of oxygen (the oxygen of the air for example), but also to increase the reactive surface to capture the oxygen during the heat treatment.
    The heat treatment of the preform may be a sintering of the preform, the preset temperature of the heat treatment being the temperature of a sintering stage.
    BRIEF DESCRIPTION OF THE DRAWINGS Other features and advantages of the present invention will emerge from the description given below, with reference to the accompanying drawings which illustrate an embodiment having no limiting character. In the figure: - Figure 1 is a schematic sectional view of a support according to the invention positioned in the enclosure of an oven and surmounted by a preform intended to be heat treated.
    DETAILED DESCRIPTION OF THE INVENTION The invention will now be described in its application to the sintering of a titanium-based alloy powder piece preform in order to reduce the oxygen contamination of the sintered workpiece.
    It should be noted that the invention is not limited only to the sintering of powder preforms, but can also be implemented in any type of heat treatment requiring protection against oxidation, for example debinding a blank of powder mixed with a binder.
    FIG. 1 very schematically illustrates the enclosure 2 of a furnace 1, used to carry out the high temperature sintering of a preform 3.
    The preform 3 is made by shaping a powder of a titanium-based alloy. For example, titanium based alloys such as: TiAl6V4, Ti-17, Ti-6242, Ti-5553, TiAl-48-2-2, TNMB1, and the like can be used.
    In a manner known per se, the shaping of the powder to make the preform 3 can be done using a method of the type MIM ("Metal Injection Molding"), HIP ("Hot Isostatic Pressing"), by casting powder, by film casting ("Tape Casting"), extrusion, etc.
    In the chamber 2 is a sole 4 disposed in the enclosure, which can also be integrated in the oven. This sole 4 may consist of a molybdenum alloy plate (for example of the TZM type) or graphite. Note that in practice several soles 4 may be present in the sintering chamber. For reasons of simplification, only one sole 4 has been shown.
    A tray 5 of ceramic material may possibly overcome the hearth 4 of the oven. This ceramic tray 5 may for example comprise zirconia (ZrO 2), alumina (Al 2 O 3) or ITttrine (Y 2 O 3).
    According to the invention, a support 6 is arranged on the ceramic plate 5. This support 6, here taking the form of a support plate 6, consists of a metal or a metal alloy which has reducing properties with respect to titanium dioxide (TiO 2) in particular. The support plate 6 then acts as an oxygen trap, not only for the oxygen present in the atmosphere of the chamber 2, but also for the oxygen present in the preform 3 which will be positioned on the support plate 6 and the tools present in the oven. In addition, this support plate 6 also acts as a barrier for the oxygen present in the ceramic tray 5 and the sole 4, which can no longer reach the preform 3 during sintering.
    It is preferable that the support plate 6 covers as much as possible the ceramic tray 5 or the hearth 4, in order to limit the contamination of oxygen coming from these tools. Advantageously, the support plate 6 covers the base of the chamber 2 of the oven 1. The thickness e of the support plate 6 may for example be between 0.1 mm and 20 mm.
    Materials which have the required reducing properties may be chosen for example from titanium-based alloys or zirconium-based alloys which have mass contents of these sufficiently high elements.
    A titanium-based alloy for the support plate 6 according to the invention preferably has a titanium mass content greater than or equal to 45%, more preferably a titanium content by mass greater than or equal to 90%, or even more preferably a content of mass of titanium greater than or equal to 99%. For example, such an alloy may be selected from the following known alloys: T40, T60, TiAl6V4, TiAl-48-2-2.
    As a variant, a zirconium-based alloy for the support plate 6 according to the invention preferably has a zirconium content greater than or equal to 95%. For example, such an alloy may be selected from the following known alloys: Zircaloy-2, Zircaloy-4.
    In addition, the support plate 6 is preferably virtually plastically deformable at the heat treatment temperatures envisaged, which means that its mechanical properties and its shape are not affected by the temperatures to which it will be subjected. In other words, the support plate 6 must be dimensionally stable, it may however undergo slight deformations due to the mass of the part that it supports.
    In practice, the melting temperature of the material constituting the support plate 6 is greater than the highest temperature at which it will be subjected during the heat treatment. In the case of sintering a titanium-based alloy powder preform, the sintering temperature is generally greater than 1100 ° C. Thus, it will be necessary for example that the melting temperature of the material constituting the support plate 6 is at least greater than 1100 ° C.
    It is advantageous to strip the support plate 6 before positioning it in the oven 1. To do this, it can be polished, milled or sanded. This pickling treatment makes it possible to remove any oxide layer that may have formed on the support plate 6 in the open air. In addition, the etching also makes it possible to increase the reactive surface of the support plate 6 to improve the oxygen scavenging.
    The support plate 6 is covered at least in part with an anti-diffusion barrier 7 (for example based on alumina or yttrine), in order to prevent the preform 3 which is then positioned on the support plate 6 adheres with it because of the diffusion of the metallic elements (by a welding-diffusion phenomenon). The antidiffusion barrier is thus disposed between the support plate 6 and the preform 3. The deposition of the diffusion barrier 7 can be done directly by applying a layer of powder by brush or spray from a solution.
    It should also be noted that an anti-diffusion barrier similar to that described above may be arranged between the ceramic plate 5 and the support plate 6 (or between the sole plate 4 and the support plate 6, if appropriate) in order to avoid that they adhere to each other.
    Once all the tools and the preform are positioned in the furnace, sintering of the preform 3 can be carried out. The operating conditions for sintering a titanium-based alloy powder preform are known to those skilled in the art. art and will not be described in more detail here.
    Example
    The sintering of a powder aerospace turbine engine turbine blade preform is carried out, shaped by a metal injection molding (MIM) process. The powder used comprises a titanium-based alloy of the TiAl-48-2-2 type.
    The support plate 6 used in this example comprises a titanium-based alloy of the T1AI6V4 type, and was covered with an anti-diffusion yttrium oxide (Yttrine) barrier by spray from a solution.
    The sintering of the preform is carried out at a temperature of between 1380 ° C. and 1445 ° C. for a period of between 2 hours and 10 hours under a neutral atmosphere of argon.
    The oxygen content in the final piece after sintering (measured according to EN10276) is in the order of 1300 ppm. By way of comparison, when the preform is sintered under the same conditions without using a plate according to the invention, the oxygen content in the part reaches 4500 ppm. Thus, in this example, the use of a plate according to the invention allows to divide the oxygen contamination in the final piece by a factor of 3.5.
    权利要求:
    Claims (9)
    [1" id="c-fr-0001]
    A method of heat treating a powder-form preform (3) comprising a titanium-based alloy, the method comprising heat-treating the preform in an oven (1) at a predetermined temperature, the preform being on a support (6) during the heat treatment, characterized in that the support (6) comprises a titanium-based alloy whose titanium mass content is greater than or equal to 45%, or a zirconium-based alloy whose mass content zirconium is greater than or equal to 95%, the support-forming material having a melting point higher than the predefined temperature of the heat treatment, and in that an anti-diffusion barrier (7) is arranged between the preform (3) and the support (6) to prevent soldering of the preform on the support.
    [2" id="c-fr-0002]
    2. Method according to claim 1, characterized in that the support (6) comprises a titanium-based alloy whose mass content of titanium is greater than or equal to 90%.
    [3" id="c-fr-0003]
    3. Method according to any one of claims 1 and 2, characterized in that the support (6) comprises a titanium-based alloy whose mass content of titanium is greater than or equal to 99%.
    [4" id="c-fr-0004]
    4. Method according to any one of claims 1 to 3, characterized in that the carrier (6) comprises a titanium alloy selected from the following: T40, T60, TAI6V4, TiAI-48-2-2.
    [5" id="c-fr-0005]
    5. Method according to claim 1, characterized in that the support (6) comprises a zirconium-based alloy selected from the following: Zircaloy-2, Zircaloy-4.
    [6" id="c-fr-0006]
    6. Method according to any one of claims 1 to 5, characterized in that the support has a thickness (e) of between 0.1 mm and 20 mm.
    [7" id="c-fr-0007]
    7. Method according to any one of claims 1 to 6, characterized in that the anti-diffusion barrier (7) comprises alumina or yttrium oxide.
    [8" id="c-fr-0008]
    8. Method according to any one of claims 1 to 7, characterized in that the carrier (6) is etched.
    [9" id="c-fr-0009]
    9. Method according to any one of claims 1 to 8, characterized in that the heat treatment of the preform (3) is a sintering of the preform, the preset temperature of the heat treatment being the temperature of a sintering bearing.
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    引用文献:
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    法律状态:
    2016-08-04| PLFP| Fee payment|Year of fee payment: 2 |
    2017-01-13| PLSC| Publication of the preliminary search report|Effective date: 20170113 |
    2017-05-02| PLFP| Fee payment|Year of fee payment: 3 |
    2018-06-21| PLFP| Fee payment|Year of fee payment: 4 |
    2018-09-14| CD| Change of name or company name|Owner name: ALLIANCE, FR Effective date: 20180809 Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20180809 |
    2020-06-23| PLFP| Fee payment|Year of fee payment: 6 |
    2021-06-23| PLFP| Fee payment|Year of fee payment: 7 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1556375A|FR3038622B1|2015-07-06|2015-07-06|METHOD FOR THERMALLY PROCESSING TITANIUM ALLOY POWDER PREFORM|FR1556375A| FR3038622B1|2015-07-06|2015-07-06|METHOD FOR THERMALLY PROCESSING TITANIUM ALLOY POWDER PREFORM|
    BR112018000280-1A| BR112018000280A2|2015-07-06|2016-07-06|PROCESS FOR THERMAL TREATMENT OF A PREFORM.|
    EP16750926.4A| EP3320287B1|2015-07-06|2016-07-06|Method for heat treating a preform made of titanium alloy powder|
    CN201680050001.4A| CN108291776B|2015-07-06|2016-07-06|Method for heat treating preforms made from titanium alloy powder|
    JP2018520029A| JP6987751B2|2015-07-06|2016-07-06|Methods for heat treating preforms made of titanium alloy powder|
    PCT/FR2016/051710| WO2017006053A1|2015-07-06|2016-07-06|Method for heat treating a preform made of titanium alloy powder|
    RU2018104320A| RU2711395C2|2015-07-06|2016-07-06|Method of heat treatment of workpiece from titanium alloy powder|
    CA2991283A| CA2991283A1|2015-07-06|2016-07-06|Method for heat treating a preform made of titanium alloy powder|
    US15/741,844| US10967430B2|2015-07-06|2016-07-06|Method for heat treating a preform made of titanium alloy powder|
    US17/193,628| US20210187609A1|2015-07-06|2021-03-05|Method for heat treating a preform made of titanium alloy powder|
    JP2021109889A| JP2021179011A|2015-07-06|2021-07-01|Method for heat-treating preform made of titanium alloy powder|
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