MODULE FOR AN AIRCRAFT TURBOMACHINE

FR3166662A1Pending Publication Date: 2026-03-27SAFRAN SA +1
4 Cites -1 Cited by

Patent Information

Authority / Receiving Office
FR · FR
Patent Type
Applications
Current Assignee / Owner
Filing Date
2024-09-25
Publication Date
2026-03-27

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Abstract

Module (10) for an aircraft turbomachine, this module (10) comprising a housing (16) and several components located in several housings (12) of the housing (16) and connected to each other by connecting elements (14), characterized in that the housing (16) is formed by additive manufacturing and comprises in a single block: - a frame (18) delimiting the housing (16), and - a lattice (20) of intersecting ribs located within the frame (18) and connected to the frame (18), the housings (12) and the connecting elements (14) being located within the frame (18) and encompassed within the lattice of ribs (20), which is connected to at least some housings (12) and / or connecting elements (14) to ensure their retention. Abbreviated figure: Figure 3
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Citation Information

Patent Citations

  • Cell structure including reinforcement pattern

    CN114382594A

  • Improved part manufacturing process using additive manufacturing

    FR3118892A1

  • Turbulating cooling structures

    US20160023272A1

  • Electric machine having a containment band

    US20220231556A1