http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-103600550-B

Outgoing Links

Predicate Object
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B32B27-28
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filingDate 2013-10-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2015-08-05-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationDate 2015-08-05-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-103600550-B
titleOfInvention A kind of Aircraft engine hanger leading edge
abstract A kind of Aircraft engine hanger leading edge, comprise engine lifting bracket 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 water-soluble epoxy red ferric oxide primer, finish paint is organic silicone modified acrylate coating material; The build of priming paint and finish paint is respectively 21 microns and 50 microns; Described organic silicone modified acrylate coating material comprises: by weight, organosilicon modified crylic acid resin 55-65%, color filters 20-25%, nano-calcium carbonate 3%, nano zine oxide 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 lifting bracket leading edge according to engine lifting bracket leading edge 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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Total number of triples: 45.