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Optical fiber data transfer systemThis Phase 2 effort applies the results of Phase 1 to design and fabricate an optical slip ring system for a helicopter rotor blade/wind tunnel application. In this application, there are two assemblies: one on the rotating portion of the mechanical system, one on the stationary portion. The assembly on the rotating portion digitizes and encodes 128 transducer signals from various parts of the blade, and optically transfers data across the noncontacting coupling. Two complete identical independent channels are provided. On the stationary side, the signals are decoded and one channel is transmitted in digital form to a computer for recording and analysis. The second channel reconstructs the analog transducer signals for real time observation. In the opposite direction, eight signal channels enable control signals to be passed from the stationary to the rotating part of the system. Power to the rotor mounted electronics is supplied via power slip rings. The advantages of the optical over the traditional electro-mechanical slip ring method of data transfer across a rotating joint are long life, low-maintenance, immunity to crosstalk, and wider bandwidth. Successful completion of this effort demonstrated that this method is practical and reliable, and can be implemented under difficult conditions of available space, power, environment, and stringent performance and equipment life requirements.
Document ID
19890005005
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mcmillan, S. H.
(Schwartz Electro-Optics, Inc. Orlando, FL, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1988
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA-CR-181704
NAS 1.26:181704
Report Number: NASA-CR-181704
Report Number: NAS 1.26:181704
Accession Number
89N14376
Funding Number(s)
CONTRACT_GRANT: NAS1-18331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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