http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-103600541-B

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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B05D7-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08F283-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C09D7-12
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filingDate 2013-10-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2015-09-23-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationDate 2015-09-23-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-103600541-B
titleOfInvention A kind of front edge of engine air inlet duct of aircraft assembly
abstract A kind of front edge of engine air inlet duct of aircraft assembly, comprise engine inlets leading edge housing and the ice-phobic coating being positioned at hull outside, this ice-phobic coating comprises priming paint and finish paint, and described priming paint is alcohol insoluble inorganic zinc rich primer, finish paint is organic silicone modified acrylate coating material; The build of priming paint and finish paint is respectively 17 microns and 31 microns; Described organic silicone modified acrylate coating material comprises: by weight, organosilicon modified crylic acid resin 55-65%, color filters 20-25%, nano titanium oxide 3%, nano-calcium carbonate 3%, levelling agent 1%, defoamer 0.8%, dispersant 1.2%, catalyst 0.5%, solvent 3-5%.Effectively can reduce the formation of ice sheet in engine inlets leading edge according to engine inlets leading edge assemblies of the present invention, and be conducive to coming off of the ice sheet formed.
priorityDate 2013-10-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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