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Elastomer mounted rotors - An alternative for smoother running turbomachineryThis paper describes the design of elastomeric bearing supports for a rotor built to simulate the power turbine of an advanced gas turbine engine which traverses two bending critical speeds. The elastomer dampers were constructed so as to minimize rotor dynamic response at the critical speeds. Results are presented of unbalance response tests performed with two different elastomer materials. These results showed that the resonances on the elastomer-mounted rotor were well damped for both elastomer materials and showed linear response to the unbalance weights used for response testing. Additional tests were performed using solid steel supports at either end (hand-mounted), which resulted in drastically increased sensitivity and nonlinear response, and with steel supports in one end of the rotor and the elastomer at the other, which yielded results which were between the soft- and hard-mounted cases. It is concluded that elastomeric supports are a viable alternative to other methods of mounting flexible rotors, that damping was well in excess of predictions and that elastomeric supports are tolerant of small rotor misalignments.
Document ID
19790048401
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tecza, J. A.
(Mechanical Technology, Inc. Latham, NY, United States)
Jones, S. W.
(Mechanical Technology, Inc. Latham, NY, United States)
Smalley, A. J.
(Mechanical Technology Inc. Latham, N.Y., United States)
Cunningham, R. E.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Darlow, M. S.
(Mechanical Technology, Inc. Latham, NY, United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Subject Category
Mechanical Engineering
Report/Patent Number
ASME PAPER 79-GT-149
Meeting Information
Meeting: American Society of Mechanical Engineers, Gas Turbine Conference and Exhibit and Solar Energy Conference
Location: San Diego, CA
Start Date: March 12, 1979
End Date: March 15, 1979
Sponsors: American Society of Mechanical Engineers
Accession Number
79A32414
Distribution Limits
Public
Copyright
Other

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