TIMEPIECE COMPONENT CONTAINING A HIGH-ENTROPY ALLOY

Abstract
The invention concerns a timepiece component containing a high-entropy alloy, the high-entropy alloy containing between 4 and 13 main alloying elements forming a single solid solution, the high-entropy alloy having a concentration of each main alloying element comprised between 1 and 55 at. %.
Description
FIELD OF THE INVENTION

The present invention concerns a timepiece component containing a high-entropy alloy, and a method for fabricating such a timepiece component. The invention also concerns the use of a high-entropy alloy for fabricating a timepiece component.


PRIOR ART

Timepiece components, and especially mainsprings, are subjected to high stresses, particularly during fabrication processes, but also during use.


They must, in particular, offer high mechanical strength and high ductility. However, at present, timepiece components rarely simultaneously offer these antagonistic features.


SUMMARY OF THE INVENTION

It is an object of the invention to overcome the drawbacks of the state of the art by proposing a timepiece component offering higher mechanical strength and higher ductility.


To achieve this, there is proposed, according to a first aspect of the invention, a timepiece component containing a high-entropy alloy, the high-entropy alloy containing between 4 and 13 main alloying elements forming a single solid solution, the high-entropy alloy having a concentration of each main alloying element comprised between 1 and 55 at. %. Indeed, such a component has higher mechanical strength and higher ductility than those of the prior art.


Advantageously, the concentration of each main alloying element is comprised between 10 and 55 at. %.


According to different preferred embodiments:

    • the high-entropy alloy may satisfy the following formula: FeaMnbCocCrd where a, b, c et d are comprised between 1 and 55 at. %;
    • the high-entropy alloy may have the following formula: Fe50Mn30Co10Cr10;
    • the high-entropy alloy may satisfy the following formula: Fe80-xMnxCo10Cr10, where x is comprised between 25 and 79 at. %, and preferably x is comprised between 25 and 45 at. %;
    • the high-entropy alloy may satisfy the following formula: FeaMnbNieCocCrd where a, b, c, d and e are comprised between 1 and 55 at. %;
    • the high-entropy alloy may satisfy the following formula: Fe20Mn20Ni20Co20Cr20;
    • the high-entropy alloy may satisfy the following formula: Fe40Mn27Ni26Co5Cr2;
    • the high-entropy alloy may satisfy the following formula: TaaNbbHfcZrdCre where a, b, c, d and e are comprised between 1 and 55 at. %;
    • the high-entropy alloy may, in particular, satisfy the following formula: Ta20Nb20Hf20Zr20Ti20;
    • the high-entropy alloy may satisfy the following formula: AlaLibMgcScdTie where a, b, c, d and e are comprised between 1 and 55 at. %;
    • the high-entropy alloy may, in particular, satisfy the following formula: Al20Li20Mg10Sc20Ti30;
    • the high-entropy alloy may satisfy the following formula: AlaCobCrcCudFeeNif where a, b, c, d, e and f are comprised between 1 and 55 at. %.
    • the high-entropy alloy may satisfy the following formula: Cr18.2Fe18.2Co18.2Ni18.2Cu18.2Al9.0.


Advantageously, the high-entropy alloy may contain one or more interstitial elements from among the following: C, N, B. These interstitial elements further increase the mechanical strength of the alloy.


Advantageously, the high-entropy alloy may contain one or more structural hardening elements from among the following: Ti, Al, Be, Nb, preferably in a mass concentration comprised between 0.1 and 3%.


According to different embodiments, the timepiece component may be one of the following: a spring, a mainspring, a jumper spring, an impulse pin, a roller, pallets, a staff, a pallet lever, a pallet fork, a wheel, an escape wheel, an arbor, a pinion, an oscillating weight, a winding stem, a crown, a watch case, a bracelet link, a watch bezel, a bracelet clasp.


A second aspect of the invention also concerns the use of a high-entropy alloy for fabricating a timepiece component, the high-entropy alloy containing between 4 and 13 main alloying elements forming a single solid solution, the alloy having a concentration of each main alloying element comprised between 1 and 55 at. %.





BRIEF DESCRIPTION OF THE DRAWINGS

Other features and advantages of the present invention will appear more clearly in the following detailed description of preferred embodiments, given by way of non-liming examples with reference to the appended Figures, in which:



FIG. 1 schematically represents a mainspring according to one embodiment of the invention;



FIG. 2 schematically represents the steps of a method for fabricating a mainspring according to one embodiment of the invention.





DETAILED DESCRIPTION


FIG. 1 schematically represents a mainspring 1 according to one embodiment of the invention. This mainspring 1 is made of a high-entropy alloy.


In such a high-entropy alloy, the entropy of mixing is high and makes the single phase more thermodynamically stable than the mixing of several phases.


The mainspring is preferably made from the high-entropy alloy described in the publication ‘Metastable high-entropy dual-phase alloys overcome the strength-ductility trade-off’, Zhiming Li et al, Nature 534, 227-230 (9 Jun. 2016). This high-entropy alloy has the following formula: Fe80-xMnxCo10Cr10. x is preferably comprised between 25 and 79 at. %.


More precisely, according to a first embodiment, the mainspring may be made from a Fe35Mn45Co10Cr10 alloy. The mainspring produced in this manner has the advantage of combining high tensile strength and high ductility.


According to a second embodiment, the mainspring may be made from a Fe40Mn40Co10Cr10.alloy. The spring produced in this manner has the advantage of high tensile strength and high ductility. It also operates according to a TWIP (twinning induced plasticity) mechanism.


According to a third embodiment, the mainspring may be made from a Fe45Mn35Co10Cr10.alloy. The mainspring produced in this manner has the advantage of having even higher tensile strength and higher ductility. It also operates according to a TRIP (transformation induced plasticity) mechanism.


According to a fourth embodiment, the mainspring can be made from a Fe50Mn30Co10Cr10 alloy. The mainspring produced in this manner has the advantage of having even higher tensile strength and higher ductility. It operates according to a TRIP mechanism with the appearance of two phases, FCC and HCP, by a twinning mechanism.


The invention is not limited to fabrication of a mainspring. Indeed, other timepiece components could be fabricated from the high-entropy Fe80-xMnxCo10Cr10 alloy, such as a spring, a staff, an impulse pin, a balance, an arbor, a roller, pallets, a pallet lever, a pallet fork, an escape wheel, a shaft, a pinion, a an oscillating weight, a winding stem, a crown, a jumper spring, a watch case, a bracelet link, a watch bezel, a bracelet clasp . . . .



FIG. 2 schematically represents the steps of a method for fabricating the mainspring of FIG. 1.


This method includes a first step 101 of fabricating a high-entropy alloy ingot. To do so, the elements are mixed in pure or pre-alloy form, they are then melted, and the mixture is cast to form an ingot.


The method then includes a step 102 of hot forging the ingot.


The method then includes a hot lamination step 103.


The method then includes a cold lamination step 104.


The method then includes a wire drawing step 105.


The method then includes a cold lamination step 106.


Naturally, the invention is not limited to the embodiments described with reference to the Figures and variants could be envisaged without departing from the scope of the invention.


Thus, in the preceding examples, the Fe80-x MnxCo10Cr10 alloy was used. However, other high-entropy alloys could be used, such as, for example:

    • Fe20Mn20Ni20Co20Cr20,
    • Fe40Mn27Ni26Co5Cr2,
    • Ta20Nb20Hf20Zr20Ti20,
    • Al20Li20Mg10Sc20Ti30,
    • Cr18.2Fe18.2Co18.2Ni18.2Cu18.2Al9.0.

Claims
  • 1: A timepiece component, comprising: a high-entropy alloy,wherein the high-entropy alloy is formed of multiple metallic elements forming a single-phase structure, andthe high-entropy alloy satisfies formula FeaMnbCocCrd, or formula Fe80-xMnxCo10Cr10, or formula FeaMnbNieCocCrd, or formula TaaNbbHfcZrdCre, or formula AlaLibMgcScdTie, where a, b, c, d, e and f, when present, are each a value independently ranging from 1 to 55 at. %, and where x, when present, is a value ranging from 25 to 79 at. %.
  • 2: The timepiece component according to claim 1, wherein the high-entropy alloy satisfies formula: FeaMnbCOcCrd,wherein a, b, c and d are from 1 to 55 at. %.
  • 3: The timepiece component according to claim 1, wherein the high-entropy alloy satisfies formula: Fe80-xMnxCo10Cr10,wherein x is from 25 to 79 at. %.
  • 4: The timepiece component according to claim 1, wherein the high-entropy alloy satisfies formula: FeaMnbNieCocCrd,wherein a, b, c, d and e are from 1 to 55 at. %.
  • 5: The timepiece component according to claim 1, wherein the high-entropy alloy satisfies formula: TaaNbbHfcZrdCre,wherein a, b, c, d and e are from 1 to 55 at. %.
  • 6: The timepiece component according to claim 1, wherein the high-entropy alloy satisfies formula: AlaLibMgcScdTie,wherein a, b, c, d and e are from 1 to 55 at. %.
  • 7: The timepiece component according to claim 1, wherein the high-entropy alloy comprises one or more interstitial elements selected from the group consisting of C, N, and B.
  • 8: The timepiece component according to claim 1, wherein the high-entropy alloy comprises one or more structural hardening elements selected from the group consisting of Ti, Al, Be, and Nb.
Priority Claims (1)
Number Date Country Kind
16191867.7 Sep 2016 EP regional
CROSS REFERENCE TO RELATED APPLICATIONS

The present application is a continuation of U.S. Ser. No. 16/331,038, filed Mar. 6, 2019, pending, which is a 371 of PCT application no. PCT/EP2017/069219, filed Jul. 28, 2017, no inactive, and claims priority to European application EP16191867.7, filed Sep. 30, 2016.

Continuations (1)
Number Date Country
Parent 16331038 Mar 2019 US
Child 16775657 US