ASSEMBLY INCLUDING A BLADE AND A BLADE RETAINING SYSTEM
The blade retention system with a pivot and movable jaw dovetail joint distributes stress, addressing stress concentration issues in composite blades, enhancing mechanical strength and reducing mass while maintaining aerodynamic performance.
Patent Information
- Authority / Receiving Office
- FR · FR
- Patent Type
- Patents
- Current Assignee / Owner
- SAFRAN AIRCRAFT ENGINES SAS
- Filing Date
- 2023-09-22
- Publication Date
- 2026-05-22
AI Technical Summary
Existing blade retention systems for large-dimension composite material blades in turbomachinery experience significant stress concentrations, particularly at the flange radius and lateral parts, leading to reduced lifespan due to antisymmetric loading and potential damage modes.
A blade retention system featuring a pivot with a groove and a movable jaw forming a dovetail joint, along with screws oriented parallel to the axis, distributes stress and prevents local concentration by allowing the foot to be tightly held between inclined planes, using a trapezoidal movable jaw and a groove configuration.
The system effectively diffuses stress, reduces mass, and enhances mechanical strength while maintaining aerodynamic performance, preventing damage and extending the lifespan of composite blades.
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