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Blade tip rubbing stress predictionA linear analysis was performed to determine the dynamic response of a turbine blade to intermittent rubbing against a tip seal. The response analysis consisted of a parametric study where the rubbing friction force was assumed to vary as a half sine wave over a preselected contact arc. The length of the contact arc, as well as the pump speed, was varied to determine the effects of each. Results show that for a given contact arc there are distinct critical speeds at which the blade response becomes a maximum.
Document ID
19900019299
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brusher, Gerald A.
(Rockwell International Corp. Canoga Park, CA, United States)
Davis, Gary A.
(Rockwell International Corp. Canoga Park, CA, United States)
Shea, Daniel M.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1988
Publication Information
Publication: NASA, Marshall Space Flight Center, Advanced Earth-to-Orbit Propulsion Technology 1988, Volume 1
Subject Category
Aircraft Propulsion And Power
Accession Number
90N28615
Funding Number(s)
CONTRACT_GRANT: NAS8-36361
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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