MODULAR TRAY FOR THE POWDER BED ADDITIVE MANUFACTURING OF A PART WITH AN AXIS OF REVOLUTION
20230173584 · 2023-06-08
Assignee
Inventors
- Arnaud Georges NIFENECKER (Moissy-Cramayel, FR)
- Jérémi Christophe Benjamin ADOR (Moissy-Cramayel, FR)
- Frédéric AYCAGUER (Moissy-Cramayel, FR)
- Frédéric Jacques DUFAU (Moissy-Cramayel, FR)
- Gilles Gaston Jacques GOUIN (Moissy-Cramayel, FR)
- Jean-Pierre WILMES (Izernore, FR)
- Werner ARGUEL (Izernore, FR)
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B29C64/30
PERFORMING OPERATIONS; TRANSPORTING
B33Y30/00
PERFORMING OPERATIONS; TRANSPORTING
B22F12/82
PERFORMING OPERATIONS; TRANSPORTING
B29C64/40
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y40/20
PERFORMING OPERATIONS; TRANSPORTING
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/47
PERFORMING OPERATIONS; TRANSPORTING
B29C64/153
PERFORMING OPERATIONS; TRANSPORTING
Y02P10/25
GENERAL 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
B22F2003/247
PERFORMING OPERATIONS; TRANSPORTING
International classification
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B22F12/82
PERFORMING OPERATIONS; TRANSPORTING
B33Y30/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y40/20
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/47
PERFORMING OPERATIONS; TRANSPORTING
B29C64/153
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A modular tray, for the additive manufacturing of a part with an axis of revolution on a powder bed, includes: a shaft-mounted circular module including a shaft provided with a circular tray at one of the ends thereof, the shaft and the circular tray being concentric; and a main support module including, in one face, a cavity configured for receiving the shaft-mounted circular module, the shaft being completely inserted in the cavity. The assembly of the shaft-mounted circular module and of the main support module define a planar top surface that is at least partly formed by the circular tray of the shaft-mounted circular module.
Claims
1-8. (canceled)
9. A modular tray for an additive manufacturing of a part with an axis of revolution on a powder bed, the modular tray comprising: a shaft-mounted circular module comprising a shaft provided with two ends and with a circular tray at one of the two ends, the shaft and the circular tray being concentric; and a main support module including, in one face, a cavity configured for receiving the shaft-mounted circular module, the shaft being completely inserted in the cavity, wherein an assembly of the shaft-mounted circular module and of the main support module defines a planar top surface that is at least partly formed by the circular tray of the shaft-mounted circular module, and wherein the shaft of the shaft-mounted circular module is a preform of one end of the part to be manufactured.
10. The modular tray according to claim 9, further comprising an annular module, wherein the main support module further includes an annular cavity configured for receiving the annular module, the annular cavity and the cavity of the shaft-mounted circular module being concentric, and the annular module, once assembled with the shaft-mounted circular module and with the main support module, forming a portion of the planar top surface of the assembly.
11. The modular tray according to claim 9, wherein the shaft-mounted circular module is machined by turning.
12. A method for manufacturing a part with an axis of revolution, comprising: producing, by localized melting or localized sintering of a powder on a modular tray according to claim 1, a blank with an axis of revolution and at least one element supporting the blank, the melted or sintered powder and the modular tray being in contact solely: on the circular tray of the shaft-mounted circular module, thus forming a portion of the part and an optional element supporting the part; and optionally on the annular module, thus forming an optional other element supporting the part; the axis of revolution of the blank being coaxial with the axis of the shaft of the shaft-mounted circular module; removing, from the main support module, an assembly formed by the blank, the shaft-mounted circular module and the optional annular module; removing of powder from the assembly; placing the assembly on a device lathe for machining by turning; machining by turning of a first portion of the blank; if the assembly includes an annular module, separating of the blank from said annular module by cutting by turning, the cutting being implemented on the support element connecting the blank to the annular module along a cutting plane perpendicular to the axis of revolution of the blank; machining by turning of a second portion of the blank, by which: the optional support element remaining at the end of the separation step is completely eliminated; the optional support element connecting the blank to the shaft-mounted circular module is completely eliminated; and the shaft-mounted circular module is partially eliminated, the non-eliminated portion of said shaft-mounted circular module being integrated in the blank; the steps of machining by turning and the optional step of separating by turning being implemented by rotating the blank about the axis of the shaft of the shaft-mounted circular module; by which the part with an axis of revolution is obtained.
13. The manufacturing method according to claim 12, wherein the shaft of the shaft-mounted circular module is pre-machined so as to form a preform of one end of the part to be produced.
14. The manufacturing method according to claim 12, wherein the shaft-mounted circular module is produced from the same material as that of the part to be produced.
15. The manufacturing method according to claim 12, further comprising at least one step of hardening heat treatment of the part, the step being implemented between the steps of removing powder from the assembly and of placing the assembly on a device lathe for machining by turning, and/or after the step of machining by turning of the second portion of the blank.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0042] The invention will be best understood and other details, features and advantages of the invention will emerge from the reading of the description made by way of non-limitative example with reference to the accompanying drawings, which illustrate:
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DETAILED DESCRIPTION OF EMBODIMENTS
[0059] According to the invention, the additive manufacturing tray is formed from one or more removable modules, placed in cavities in a face of a main support module so as to define a planar surface on which the powder bed will be able to be spread; the powder will be melted or sintered only on these removable modules so that once the part has been formed, the assembly formed by the part and the removable modules will be able to be mounted—after removal of powder—on a lathe and thus insert the operation of separating the part and removable modules from the tray among the operations of turning the blank and finishing the part.
[0060] As illustrated in
[0061] As illustrated in
[0062] Preferably, the shaft is pre-machined so as to be a preform of one end of the part to be produced. In a first example illustrated in
[0063] The modular tray 12 may also include an annular module 18, intended to come to be housed in an annular cavity 19 (annular groove) present in the top face of the main support module 16 (
[0064] In
[0065] We shall now describe the manufacture of a part with an axis of revolution according to a first embodiment of the method according to the invention using the modular tray as illustrated in
[0066] The shaft-mounted circular module 13 and the annular module 18 are placed in their respective cavities 17 and 19 of the main support module 16 (
[0067] The manufacture of the blank 20 by selective melting or selective sintering of a powder is next proceeded with (
[0068] In the step of producing the blank 20 and the support element 7 on the modular tray 12, the part and the support element are for example constructed layer by layer by selective melting or selective sintering of the powder 21 by means of a laser beam 22, the powder 21 having a mean granulometry of between 10 and 50 μm, or by means of a beam 22 of electrons, the powder 21 having a mean granulometry of between 50 and 100 μm.
[0069] In this example embodiment (
[0070] Once the part is finished, it is removed from the main support module 16, the part being integral with the shaft-mounted circular module 13 and the annular module 18 (hereinafter referred to as removable modules) (
[0071] Then the part has the powder removed from it (
[0072] Then the assembly formed by the blank and the removable modules is installed on a lathe and the turning of a first portion of the part (here referred to as the front face of the part) is proceeded with (
[0073] The blank is next separated from the annular module 18 by cutting along a cutting plane C perpendicular to the axis of revolution of the part (which is also the axis of rotation of the lathe and the axis of the shaft 14) at the support element 7 (
[0074] It should be noted that it is possible to implement one or more heat treatments of the part during manufacture thereof. For example, once the powder removal has been implemented (
[0075] These same steps of the method according to the invention can also be implemented according to a second embodiment by using the modular tray as illustrated in
[0076] Whereas in a first embodiment (
[0077] We have compared the mass of powder lasered, as well as the lasering time necessary for producing the same part with an axis of revolution manufactured by the conventional technique requiring all the support elements described in
TABLE-US-00001 TABLE comparison between the conventional technique and two embodiments according to the invention. Technique used Mass lasered (kg) Lasering time (h) Conventional 6.115 112 Embodiment 1 4.496 82 Embodiment 2 3.821 70
[0078] To manufacture the part by additive manufacturing on a powder bed using a conventional tray, there will be a need for three types of support element (namely the support element 7 for supporting the web 4 and for supporting the outer ring 5, the support element 9 for supporting the outer hub 3 and the support element 10 for supporting the support element 7).
[0079] By using the modular tray (
[0080] By using the modular tray (
[0081] Thus it is found that embodiment 1 affords a saving of 27% on the lasered mass and on the lasering time compared with the conventional technique; as for embodiment 2, this affords a saving of 38% on the lasered mass and on the lasering time.