http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8870159-B2

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filingDate 2010-07-22-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2014-10-28-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_409af4acd8e0a017fe208906ff4476e2
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publicationDate 2014-10-28-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-8870159-B2
titleOfInvention Aerodynamic chopper for gas flow pulsing
abstract This supersonic pulse flow device is intended to provide a technical solution in a number of fields where the injection of a flow must be pulsed as required by the process or in order to limit the power consumption and size of the pumping means. In the case of flows achieved by means of a Laval nozzle, it is possible to generate a uniform supersonic jet at very low temperature (currently up to 20 K), which is stable over hydrodynamic periods of time between 150 and 1000 microseconds. This device is aimed as solving problems relating to the use of aerodynamic tools in research and development and in industrial processes.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2019321790-A1
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Total number of triples: 25.