NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Turbomachinery shaft insertAn insert is presented for a hollow rotatable shaft on the end of which an impeller is mounted, the insert having a first cylindrical portion receivable within the end of the shaft. The insert includes a radially extending portion adjacent the end of the shaft having an annular wall including radially inner and outer surfaces for engaging tightly similar surfaces in a recess formed in the impeller to provide inner and outer pilot surfaces. The insert also includes a tubular extension which is received within a bore in the impeller, the tubular extension having spaced longitudinally extending slits for permitting the extension together with radially extending hook-like tongues thereon to be received within radial slots in the bore of the impeller to lock the impeller to the insert.
Document ID
19890019471
Acquisition Source
Legacy CDMS
Document Type
Other - Patent Application
Authors
Vonpragenau, George L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
May 26, 1989
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.71:MFS-28345-2
Report Number: NAS 1.71:MFS-28345-2
Patent Number: NASA-CASE-MFS-28345-2
Patent Application Number: US-PATENT-APPL-SN-358028
Accession Number
89N28842
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MFS-28345-2
Patent Application
US-PATENT-APPL-SN-358028
No Preview Available