MODULE FOR AN AIRCRAFT TURBOMACHINE
The turbomachine module integrates a frame and lattice structure for efficient additive manufacturing, addressing housing optimization challenges by reducing mass and improving mechanical and thermal performance.
Patent Information
- Application Number
- FR2024010228
- Authority / Receiving Office
- FR · FR
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2024-09-25
- Publication Date
- 2026-03-27
AI Technical Summary
Existing turbomachine modules face challenges in optimizing housing design for compactness and robustness, particularly in additive manufacturing, leading to complex shapes and excessive mass, which are time-consuming and not well-suited for efficient production.
A turbomachine module design utilizing a frame and lattice of intersecting ribs formed by additive manufacturing, integrating equipment housings and connecting elements, allowing precise modeling and reduced material usage, enhancing mechanical resistance and thermal management.
The design achieves faster modeling, reduced mass, improved mechanical resistance, better thermal control, and efficient additive manufacturing, while maintaining compactness and structural integrity.