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Emitted vibration measurement device and methodThis invention is directed to a method and apparatus for measuring emitted vibrational forces produced by a reaction wheel assembly due to imbalances, misalignment, bearing defects and the like. The apparatus includes a low mass carriage supported on a large mass base. The carriage is in the form of an octagonal frame having an opening which is adapted for receiving the reaction wheel assembly supported thereon by means of a mounting ring. The carriage is supported on the base by means of air bearings which support the carriage in a generally frictionless manner when supplied with compressed air from a source. A plurality of carriage brackets and a plurality of base blocks provided for physical coupling of the base and carriage. The sensing axes of the load cells are arranged generally parallel to the base and connected between the base and carriage such that all of the vibrational forces emitted by the reaction wheel assembly are effectively transmitted through the sensing axes of the load cells. In this manner, a highly reliable and accurate measurment of the vibrational forces of the reaction wheel assembly can be had. The output signals from the load cells are subjected to a dynamical analyzer which analyzes and identifies the rotor and spin bearing components which are causing the vibrational forces.
Document ID
19870005237
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Gisler, G. L.
(Sperry Corp., Phoenix Ariz., United States)
Date Acquired
August 13, 2013
Publication Date
October 28, 1986
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Number: US-PATENT-4,619,142
Patent Application Number: US-PATENT-APPL-SN-657310
Patent Number: NASA-CASE-MFS-25981-1
Accession Number
87N14670
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,619,142|NASA-CASE-MFS-25981-1
Patent Application
US-PATENT-APPL-SN-657310
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