Integral Tuned Mass Absorber for Turbine Blades

TBMG-46499

09/01/2022

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.

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