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Development of the sonic pump levitationA prototype levitating/positioning device termed the Sonic Pump Levitator was designed, built and successfully tested in full gravity and in the reduced gravity of the parabolic flight regime of the KC-135. Positioning is achieved by timely and appropriate application of gas momentum from one or more of six sonic pumps. The sonic pumps, which are arranged orthogonally in opposed pairs about the levitation region, are activated by an electro-optical, computer controlled, feedback system. The sonic pump is a transducer which is capable of converting sound energy into a directed flow of gas. It consists of a loudspeaker whose face is sealed by a closure perforated by one or more orifices. The diaphragm of the loudspeaker is the only moving part of the sonic pump, no valves being needed. This very low inertia electromechanical device was developed to provide the short response time necessary to keep pace with the demands of computerized position keeping.
Document ID
19840024678
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dunn, S. A.
(Sedun, Inc., Madison Wisc., United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-161963
NAS 1.26:161963
Report Number: NASA-CR-161963
Report Number: NAS 1.26:161963
Accession Number
84N32749
Funding Number(s)
CONTRACT_GRANT: NAS8-33513
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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