http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-103722850-B

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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-16
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filingDate 2013-10-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2015-06-10-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b69573055eb3f6d041b8a14346c570ff
publicationDate 2015-06-10-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-103722850-B
titleOfInvention Engine hanging bracket front edge component of aircraft
abstract An engine hanging bracket front edge component of an aircraft comprises an engine hanging bracket front edge casing and an anti-icing coating located outside the casing, wherein the anti-icing coating comprises base coat and finishing coat, the base coat adopts alcohol-soluble inorganic zinc silicate base coat, and the finishing coat adopts an organic silicone modified acrylate coating; the dry film thickness of the base coat is 20 mu m, and the dry film thickness of the finishing coat is 36 mu m; and the organic silicone modified acrylate coating comprises components in percentage by weight as follows: 55%-65% of organic silicone modified acrylate resin, 20%-25% of color fillers, 3% of nano titanium dioxide, 3% of nano magnesium oxide, 1% of a flatting agent, 0.8% of a defoaming agent, 1.2% of a dispersing agent, 0.5% of a catalyst and 3%-5% of a solvent. The engine hanging bracket front edge component can effectively prevent an ice layer from forming on an engine hanging bracket front edge, and a formed ice layer falls off conveniently.
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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