METHOD FOR MANUFACTURING A CASING FOR AN AIRCRAFT TURBINE ENGINE

    公开(公告)号:US20250122813A1

    公开(公告)日:2025-04-17

    申请号:US18692544

    申请日:2022-09-14

    Abstract: A method for producing casing for an aircraft turbine engine includes a first step of manufacturing an annular shell having an axis A made of a composite material in a mold that includes an annular cavity that receives the preform. A resin is injected into the cavity and subsequently polymerized. During a second step, at least one axial abutment means is arranged inside the shell, and during a third step, the annular cartridge made of an abradable material is arranged inside the annular shell in contact with the axial abutment means. A fourth step includes bonding the annular cartridge to the first inner annular surface. The first and second steps are simultaneous, and the at least one axial abutment means is molded with the preform in the mold.

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