http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2483000-C2

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_bab2564536aab165272a9a5f75808a21
classificationCPCAdditional http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2033-0233
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D15-163
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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D15-16
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D15-00
filingDate 2008-09-29^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2013-05-27^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_52cd49dbfa308fb98ddc371b35d28cca
publicationDate 2013-05-27^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber RU-2483000-C2
titleOfInvention Air intake piezoelectric anti-icing system
abstract FIELD: transport. n SUBSTANCE: invention relates to aircraft anti-icing systems. Aircraft nacelle comprises assembly of turbojet air intake leading edge 1, inner surface 9, outer surface 11, and anti-icing means including anti-icing coat 133 applied on part of outer surface 11. Bonding matrix of said coat 13 comprises, at least, one piezoelectric active element. Piezoelectric actuators comprise, at least, one piezoelectric active element 21 engaged with inner surface and electric power feeder 23. Said piezoelectric active element 21 comprises cylinder and vibrator. Anti-icing coat material represents polyurethane or fluoropolyurethane dyes, resins or plastics containing Teflon. Thickness e of anti-icing coat 13 makes 20 to 100 mcm. n EFFECT: efficient protection against icing. n 8 cl, 2 dwg
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priorityDate 2007-10-22^^<http://www.w3.org/2001/XMLSchema#date>
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