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
Smart Images

Figure 00000000_0000_ABST
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
Need to check novelty before this filing date? Find Prior Art
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