On a self-tuning impact vibration damper for rotating Turbomachinery

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Daffy, K P ^a   Bagley, R L ^b   Mehmed, O ^c  

^a OHIO AEROSPACE INSTITUTE   (United States)

^b UNIVERSITY OF TEXAS AT SAN ANTONIO   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FATIGUE OF MATERIALS; PROPULSION; TURBOMACHINERY;

CENTRIFUGAL LOADS; ENGINE ORDERS; IMPACT DAMPER; IMPACT VIBRATION; MASS MOTION; ROTOR COMPONENTS; SELFTUNING; TUNED-MASS DAMPERS;

DAMPING;

EID: 84896447106     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Brown, G. V. and North, C.M. 1987 "The Impact Damped Harmonic Oscillator in Free Decay", NASA TM 89897, ASME Vibrations Conference.
2. Duffy, K.P., Brown, G.V., and Mehmed, O. 1998 "Impact Damping of Rotating Cantilever Plates", 3rd National Turbine Engine High Cycle Fatigue Conference.
3. th National Turbine Engine High Cycle Fatigue Conference.
4. th National Turbine Engine High Cycle Fatigue Conference.
5. Hollkamp, J.J., Bagley, R.L., and Gordon, R.W. 1999 "A Centrifugal Pendulum Absorber for Rotating, Hollow Engine Blades", Journal of Sound and Vibration, v. 219 n. 3, pp. 539-549.
6. Sharif-Bakhtar, M. and Shaw, S.W. 1988 "The Dynamic Response of a Centrifugal Pendulum Vibration Absorber with Motion-Limiting Stops," Journal of Sound and Vibration, v. 126 n. 2, pp. 221-235.