Flexible damper for turbine blades

A flexible damper (24) for turbine blades (10) includes a plurality of segments (32) positioned together in a substantially linear pattern, each segment (32) having a first side (46), a second side (48), a top side (50), a bottom side (52), a length (56), a width (54), and a thickness (58).

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Bibliographische Detailangaben
Hauptverfasser: Martin, Jr., Nicholas F, Wiebe, David J
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:A flexible damper (24) for turbine blades (10) includes a plurality of segments (32) positioned together in a substantially linear pattern, each segment (32) having a first side (46), a second side (48), a top side (50), a bottom side (52), a length (56), a width (54), and a thickness (58).