ENGINE WITH RELATED BATTERIES AND TURBINE AND TURBOMACHINE INCLUDING IT
A dual-disc blade wheel design with complementary cavities and optional ring support ensures durable axial retention of blades, addressing weight and bulk issues, while maintaining efficiency and performance in turbine applications.
FR3170533A1Pending Publication Date: 2026-06-26SAFRAN HELICOPTER ENGINES
Patent Information
- Authority / Receiving Office
- FR · FR
- Patent Type
- Applications
- Current Assignee / Owner
- SAFRAN HELICOPTER ENGINES
- Filing Date
- 2024-12-23
- Publication Date
- 2026-06-26
Smart Images
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Abstract
The invention relates to a turbine wheel (100) for a turbomachine, comprising blades (120) and a disk (110) supporting them. The disk is annular and extends circumferentially around a principal axis (X). Each blade comprises a foot (124) and a blade (122) extending from the foot. The disk (110) has at least one cavity (116) formed on its periphery, configured to receive the feet of the blades. The invention is characterized in that the disk comprises a first disk (110A) and a second disk (110B). The first disk (110A) and the second disk (110B) each have at least one first cavity (116A) and a second cavity (116B) formed on their peripheries. The first and second disks are joined such that a first cavity and a second cavity at least partially form a wheel disc cavity. Figure for the abbreviation: Figure 2
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