A rational method for optimizing shroud damping

ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996

Volumn 5, Issue , 1996, Pages

  Griffin, J H ^a   Labelle, R F ^b  

^a CARNEGIE MELLON UNIVERSITY   (United States)

^b Pratt and Whitney   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

INTERFACE STATES;

COMPUTER CODES; ENGINE TEST; FRICTION INTERFACES; OHIO STATE UNIVERSITY; RATIONAL METHODS; RESONANT RESPONSE; SHROUDED BLADES; VIBRATORY RESPONSE;

GAS TURBINES;

EID: 84930444443     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/96-GT-402     Document Type: Conference Paper

References (4)

1. Cameron, T. M., Griffin. J. H., Kielb, R. E., and Hoosac, T. M., "An Integrated Approach for Friction Damper Design." ASME Journal of Vibration. Acoustics, Stress and Reliability in Design Vol. 112, 1990, pp. 175-182.
2. Griffin. "A Review of Friction Damping of Turbine Blade Vibration," International Journal of Turbo and Jet Engines. Vol. 7. 1990, pp. 297-307.
3. Richardson. S. M. and Griffin. J. H. "The Guide Consortium: Government, Universities, and Industry Working Together to Develop New Technologies," Presented at the 1995 International Gas Turbine and Aeroengine Congress and Exposition.
4. Yang. B. D. and Menq. C.-H., "Modeling of Friction Contact and Its Application of the Design of Shroud Contact", accepted for presentation at the 1996 International Gas Turbine and Aeroengine Congress and Exposition