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Cryogenic gyroscope housingA cryogenic gyroscope housing having gas spin-up means provided in annular discs inserted between housing shells is described. A circumferential recess in the inner edges of the discs at their juncture serves as the gas spin-up channel, and recesses in the discs at their junctures with the shells form suction channels. The discs also have inlet and outlet ports communicating with the spin-up channel and exhaust slots communicating with the suction channels. Mating surfaces of the discs and housing shells are held in position by optical contact at the equational plane of the housing. Suspension electrodes and thin-film readout loops are disposed in shells. A centering band and clamp rings provide for proper alinement and placement of parts in formation of optical contact joints.
Document ID
19740010210
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Angele, W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
October 9, 1973
Subject Category
General
Report/Patent Number
Patent Number: US-PATENT-3,763,708
Patent Number: NASA-CASE-MFS-21136-1
Patent Application Number: US-PATENT-APPL-SN-262430
Accession Number
74N18323
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,763,708|NASA-CASE-MFS-21136-1
Patent Application
US-PATENT-APPL-SN-262430
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