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公开(公告)号:US20230114281A1
公开(公告)日:2023-04-13
申请号:US17805886
申请日:2022-06-08
Inventor: Gregory KISSLING , Denis VINCENT , Stéphane LAUPER , Bernard BERTHEVILLE
Abstract: An item produced in a cermet material including by weight between 85 and 94% of a ceramic phase and between 6 and 15% of a metal binder phase, the ceramic phase mostly including a tungsten carbide phase and optionally one or more phases of one or more secondary carbides selected from the elements Ti, Zr, Hf, V, Nb, Ta, Cr and Mo, the metal binder comprising Ag, Pd, Ru and Co. The invention generally relates to the method for manufacturing said item.
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公开(公告)号:US20200061954A1
公开(公告)日:2020-02-27
申请号:US16466071
申请日:2017-12-19
Inventor: Nicolas FRANCOIS , Gregory KISSLING , Stewes BOURBAN , Juliette MULLER , Jean-Luc BAZIN
IPC: B32B3/12 , B29C45/14 , B29C70/68 , G04B37/22 , C01B32/158
Abstract: The invention relates to a timepiece component made of composite material including at least one reinforcement and one matrix, the reinforcement having a three-dimensional honeycomb structure with a plurality of cells into which the matrix is injected.The invention also concerns a method for manufacturing such a timepiece component.
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公开(公告)号:US20240019814A1
公开(公告)日:2024-01-18
申请号:US18299371
申请日:2023-04-12
Inventor: Loïc OBERSON , Alexandre NETUSCHILL , Stéphane LAUPER , Gregory KISSLING , Stewes BOURBAN , Pierre SAURET
CPC classification number: G04B37/22 , G04D3/0053 , G04D3/0097
Abstract: A method for manufacturing a timepiece component including successive steps of: providing a timepiece component (1); breaking the timepiece component (1) into a plurality of pieces (10); depositing the pieces (10) on a support (2) and creating a desired pattern to be reassembled, the pattern having interstices (1) between the various pieces (10) of the timepiece component (1); transferring the support (2) into a mould adapted by hot forming and placing a preform (3) on the pieces (10) of the timepiece component; heating the whole to a temperature higher than the vitreous transition temperature of the preform (3) and applying a force on the preform to fill the interstices (11) and obtain a reassembled timepiece component (1′); cooling the whole below the vitreous transition temperature of the preform (3) to form the reassembled timepiece component (1′); recovering the reassembled timepiece component (1′) and machining it to the required dimensions.
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