NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
An investigation of angular stiffness and damping coefficients of an axial spline coupling in high-speed rotating machineryThis paper provided an opportunity to quantify the angular stiffness and equivalent viscous damping coefficients of an axial spline coupling used in high-speed turbomachinery. A unique test methodology and data reduction procedures were developed. The bending moments and angular deflections transmitted across an axial spline coupling were measured while a nonrotating shaft was excited by an external shaker. A rotor dynamics computer program was used to simulate the test conditions and to correlate the angular stiffness and damping coefficients. In addition, sensitivity analyses were performed to show that the accuracy of the dynamic coefficients do not rely on the accuracy of the data reduction procedures.
Document ID
19940029686
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ku, C.-P. Roger
(Mechanical Technology, Inc. Latham, NY, United States)
Walton, James F., Jr.
(Mechanical Technology, Inc. Latham, NY, United States)
Lund, Jorgen W.
(Mechanical Technology, Inc. Latham, NY, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Publication Information
Publication: NASA. Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1993
Subject Category
Mechanical Engineering
Accession Number
94N34192
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available