Integral Tuned Mass Absorber for Turbine Blades

TBMG-46499

9/1/2022

Abstract
Content

A novel turbine blade design and manufacturing approach developed by NASA provides a significant reduction in turbine blade resonant vibration. This innovation addresses the unique resonance vibration challenges of conventionally machined turbine bladed discs, or blisks. Additive manufacturing is used to make this unique structure.

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Citation
"Integral Tuned Mass Absorber for Turbine Blades," Mobility Engineering, September 1, 2022.
Additional Details
Publisher
Published
9/1/2022
Product Code
TBMG-46499
Content Type
Magazine Article
Language
English