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Diverter Lip for SealProposed one-piece design change for cooling turbine rotor disks eliminates temperature differential that normally causes thermal stresses and cracks.
Document ID
19840000168
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Jackson, E. D., III (Rockwell International Corp.)
Johnson, D. (Rockwell International Corp.)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
MFS-19891
Report Number: MFS-19891
ISSN: 0145-319X
Accession Number
84B10168
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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