Propulsion unit for an aircraft
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- SAFRAN AIRCRAFT ENGINES SAS
- Filing Date
- 2024-11-25
- Publication Date
- 2026-06-19
AI Technical Summary
In the prior art, fluid connection devices for aircraft propulsion units are bulky, costly, space-consuming, and uneconomical due to the use of flexible hoses, and they are also difficult to adapt to relative movement between movable and fixed surfaces.
The system employs rigid fluid flow pipes and interlocking connectors, achieving self-sealing of the fluid connection device through a convex-concave fit. This adapts to the relative movement of the movable surface relative to the fixed surface, ensuring the opening and closing of the fluid channel at different positions.
This enables fluid connection devices to adapt to the movement of movable surfaces relative to fixed surfaces without occupying additional space, reducing weight and cost while improving system flexibility and efficiency.
Smart Images

Figure CN122249634A_ABST