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Rotating part i.e. fan, for turbine engine of aircraft, has blade with circumferential projection detected in continuity of adjacent platform forming sector, where projection participates in definition of inter-blade surface
Rotating part i.e. fan, for turbine engine of aircraft, has blade with circumferential projection detected in continuity of adjacent platform forming sector, where projection participates in definition of inter-blade surface
The part i.e. fan (1), has blades (6) fixedly jointed on a disk (4) and circumferentially spaced with one another, and platform forming sectors (10) fixedly formed on the disk between the blades. The platform forming sectors partially define an inter-blade surface (12) that is adapted by an annular flow of air traversing the part. Each blade has a circumferential projection (40) detected in a continuity of the adjacent platform forming sector. The circumferential projection equally participates in the definition of the inter-blade surface. An independent claim is also included for a method for manufacturing a rotating part.
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