A vibration damper comprising a peg between outer platforms of adjacent composite-material blades of a turbine engine rotor wheel

A vibration damper between outer platforms of adjacent composite-material blades of a turbine engine rotor wheel, the damper including a peg having a substantially spherical portion at each of its two ends, and two hollow inserts for being received in tangential cavities that are provided facing eac...

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Bibliographische Detailangaben
Hauptverfasser: PATRICK JOSEPH MARIE GIRARD, THIERRY FACHAT, CLéMENT ROUSSILLE, STéPHANE PIERRE GUILLAUME BLANCHARD
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A vibration damper between outer platforms of adjacent composite-material blades of a turbine engine rotor wheel, the damper including a peg having a substantially spherical portion at each of its two ends, and two hollow inserts for being received in tangential cavities that are provided facing each other in outer platforms of two adjacent composite-material blades of a turbine engine rotor wheel, each spherical portion of the peg coming to bear with point contact against the inside of one of the inserts.