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Development of welded metal bellows having minimum effective diameter changeA program of analysis, design, and fabrication was conducted to develop welded metal bellows having a minimum change in effective diameter for cryogenic turbomachinery face seal applications. Linear analysis of the principle types of bellows provided identification of concepts capable of meeting basic operation requirements. For the 6-inch (.152 m) mean diameter, 1.5-inch free length bellows studied, nonlinear analysis showed that opposed and nested toroidal bellows plates stiffened by means of alternating stiffener rings were capable of maintaining constant effective diameter within 0.3% and 0.1% respectively under the operating conditions of interest. Changes in effective diameter were due principally to bellows axial deflection with pressure differential having a lesser influence. Fabrication problems associated with joining the thin bellows plates to the relatively heavy stiffener rings were encountered and precluded assembly and testing of a bellows core. Fabrication problems are summarized and recommended fabrication methods for future effort are presented.
Document ID
19730013696
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Henschel, J. K.
(Sealol, Inc. Providence, RI, United States)
Stevens, J. B.
(Sealol, Inc. Providence, RI, United States)
Harvey, A. C.
(Foster-Miller Assoc., Inc.)
Howland, J. S.
(Foster-Miller Assoc., Inc.)
Rhee, S. S.
(Foster-Miller Assoc., Inc.)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-121117
Report Number: NASA-CR-121117
Accession Number
73N22423
Funding Number(s)
CONTRACT_GRANT: NAS3-12004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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