NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Electromagnetic dampers for cryogenic applicationsCryogenic turbomachinery of the type used to pump high-pressure liquid hydrogen at -423 F and liquid oxygen at -297 F to the main engines of the Space Shuttle are subjected to lateral rotor vibrations from unbalance forces and transient loads. Conventional dampers which utilize viscous fluids such as lubricating oil cannot be used in turbopumps because the bearing components are filled with either liquid hydrogen or liquid oxygen, which have viscosity comparable to air and, therefore, are not effective in viscous dampers. Electromagentic dampers are currently being explored as a means of providing damping in cryogenic turbopumps because their damping effectiveness increases as temperature decreases and because they are compatible with the liquid hydrogen or liquid oxygen in the turbopumps.
Document ID
19880013847
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brown, Gerald V.
(Army Aviation Systems Command Cleveland, OH, United States)
Dirusso, Eliseo
(Army Aviation Systems Command Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Publication Information
Publication: NASA, Lewis Research Center, Lewis Structures Technology, 1988. Volume 1: Structural Dynamics
Subject Category
Mechanical Engineering
Accession Number
88N23231
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available