http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-106288953-B

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filingDate 2016-11-07^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2017-10-03^^<http://www.w3.org/2001/XMLSchema#date>
publicationDate 2017-10-03^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-106288953-B
titleOfInvention A kind of light thermal-insulation ventilation unit for carrier rocket flat pad
abstract The invention discloses a kind of light thermal-insulation ventilation unit for carrier rocket flat pad, including air intake passage and return air channel, air intake passage includes air intake straight pipeline and air-intaking bent pipe road, the two ends of air intake straight pipeline are respectively equipped with the first plug, ventilating opening is offered on one side wall of air intake straight pipeline and the first seal closure is installed at ventilating opening, return air channel includes return air straight pipeline and return air curved pipe, the two ends of return air straight pipeline are respectively equipped with the second plug, ventilating opening is offered on one side wall of return air straight pipeline and the second seal closure is installed at ventilating opening, air intake straight pipeline, first seal closure, return air straight pipeline and the second seal closure are made using composite.The present invention has the advantages that strong simple in construction, lighter weight, heat-insulating property, good seal performance, bearing capacity are big, and with excellent Corrosion Protection and burn-out proof performance, can fully meet the requirement integrated to temperature adjustment function of generation information flat pad.
priorityDate 2016-11-07^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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