Missile wing high-temperature-resistant heat-insulating coating, preparation method thereof and missile wing
The invention relates to the field of high-temperature-resistant heat-insulating coatings, in particular to a missile wing high-temperature-resistant heat-insulating coating, a preparation method of the missile wing high-temperature-resistant heat-insulating coating and a missile wing. Comprising th...
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| creator | TAN GAOHUI CAI TANQIANG |
| description | The invention relates to the field of high-temperature-resistant heat-insulating coatings, in particular to a missile wing high-temperature-resistant heat-insulating coating, a preparation method of the missile wing high-temperature-resistant heat-insulating coating and a missile wing. Comprising the following components: 80-100 parts of boron-containing organic silicon resin, 25-40 parts of mesoporous silica hollow spheres, 8-15 parts of silanol-based POSS, 5-10 parts of organic bentonite, 1-2 parts of a silane coupling agent, 10-15 parts of low-melting-point glass powder, 1-3 parts of a dispersant, 3-5 parts of a light stabilizer, 5-10 parts of methyl isobutyl ketone and 150-180 parts of an organic solvent. The high-temperature-resistant heat-insulating coating has good high-temperature-resistant and heat-insulating performance, shows good wave absorbing performance and can improve the stealth performance of guided missiles.
本发明涉及耐高温隔热涂层领域，具体为一种弹翼耐高温隔热涂层及其制备方法、弹翼，以重量份数计，包括以下组份：含硼有机硅树脂80-100份、介孔二氧化硅空心球25-40份 |
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本发明涉及耐高温隔热涂层领域，具体为一种弹翼耐高温隔热涂层及其制备方法、弹翼，以重量份数计，包括以下组份：含硼有机硅树脂80-100份、介孔二氧化硅空心球25-40份</description><language>chi ; eng</language><subject>ADHESIVES ; AMMUNITION ; BLASTING ; CHEMICAL PAINT OR INK REMOVERS ; CHEMISTRY ; COATING COMPOSITIONS, e.g. PAINTS, VARNISHES ORLACQUERS ; CORRECTING FLUIDS ; DYES ; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION ; FILLING PASTES ; HEATING ; INKS ; LIGHTING ; MECHANICAL ENGINEERING ; METALLURGY ; MISCELLANEOUS APPLICATIONS OF MATERIALS ; MISCELLANEOUS COMPOSITIONS ; NATURAL RESINS ; PAINTS ; PASTES OR SOLIDS FOR COLOURING OR PRINTING ; POLISHES ; USE OF MATERIALS THEREFOR ; WEAPONS ; WOODSTAINS</subject><creationdate>2023</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230328&DB=EPODOC&CC=CN&NR=115851127A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230328&DB=EPODOC&CC=CN&NR=115851127A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TAN GAOHUI</creatorcontrib><creatorcontrib>CAI TANQIANG</creatorcontrib><title>Missile wing high-temperature-resistant heat-insulating coating, preparation method thereof and missile wing</title><description>The invention relates to the field of high-temperature-resistant heat-insulating coatings, in particular to a missile wing high-temperature-resistant heat-insulating coating, a preparation method of the missile wing high-temperature-resistant heat-insulating coating and a missile wing. Comprising the following components: 80-100 parts of boron-containing organic silicon resin, 25-40 parts of mesoporous silica hollow spheres, 8-15 parts of silanol-based POSS, 5-10 parts of organic bentonite, 1-2 parts of a silane coupling agent, 10-15 parts of low-melting-point glass powder, 1-3 parts of a dispersant, 3-5 parts of a light stabilizer, 5-10 parts of methyl isobutyl ketone and 150-180 parts of an organic solvent. The high-temperature-resistant heat-insulating coating has good high-temperature-resistant and heat-insulating performance, shows good wave absorbing performance and can improve the stealth performance of guided missiles.
本发明涉及耐高温隔热涂层领域，具体为一种弹翼耐高温隔热涂层及其制备方法、弹翼，以重量份数计，包括以下组份：含硼有机硅树脂80-100份、介孔二氧化硅空心球25-40份</description><subject>ADHESIVES</subject><subject>AMMUNITION</subject><subject>BLASTING</subject><subject>CHEMICAL PAINT OR INK REMOVERS</subject><subject>CHEMISTRY</subject><subject>COATING COMPOSITIONS, e.g. PAINTS, VARNISHES ORLACQUERS</subject><subject>CORRECTING FLUIDS</subject><subject>DYES</subject><subject>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</subject><subject>FILLING PASTES</subject><subject>HEATING</subject><subject>INKS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>METALLURGY</subject><subject>MISCELLANEOUS APPLICATIONS OF MATERIALS</subject><subject>MISCELLANEOUS COMPOSITIONS</subject><subject>NATURAL RESINS</subject><subject>PAINTS</subject><subject>PASTES OR SOLIDS FOR COLOURING OR PRINTING</subject><subject>POLISHES</subject><subject>USE OF MATERIALS THEREFOR</subject><subject>WEAPONS</subject><subject>WOODSTAINS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNzLsKwkAQRuE0FqK-w9i7xSpBWwmKjVb2YUj-ZBf2xu4EX98LFpZWp_k488pdbSnWgR42jGTsaJTAJ2SWKUNlFFuEg5ABi7KhTI7lTbv46YZSRuIXtzGQh5jYkxhkxIE49OR__stqNrArWH27qNbn0725KKTYoiTuECBtc9O6PtRab_fH3T_mCa_4QrA</recordid><startdate>20230328</startdate><enddate>20230328</enddate><creator>TAN GAOHUI</creator><creator>CAI TANQIANG</creator><scope>EVB</scope></search><sort><creationdate>20230328</creationdate><title>Missile wing high-temperature-resistant heat-insulating coating, preparation method thereof and missile wing</title><author>TAN GAOHUI ; CAI TANQIANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN115851127A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>ADHESIVES</topic><topic>AMMUNITION</topic><topic>BLASTING</topic><topic>CHEMICAL PAINT OR INK REMOVERS</topic><topic>CHEMISTRY</topic><topic>COATING COMPOSITIONS, e.g. PAINTS, VARNISHES ORLACQUERS</topic><topic>CORRECTING FLUIDS</topic><topic>DYES</topic><topic>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</topic><topic>FILLING PASTES</topic><topic>HEATING</topic><topic>INKS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>METALLURGY</topic><topic>MISCELLANEOUS APPLICATIONS OF MATERIALS</topic><topic>MISCELLANEOUS COMPOSITIONS</topic><topic>NATURAL RESINS</topic><topic>PAINTS</topic><topic>PASTES OR SOLIDS FOR COLOURING OR PRINTING</topic><topic>POLISHES</topic><topic>USE OF MATERIALS THEREFOR</topic><topic>WEAPONS</topic><topic>WOODSTAINS</topic><toplevel>online_resources</toplevel><creatorcontrib>TAN GAOHUI</creatorcontrib><creatorcontrib>CAI TANQIANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TAN GAOHUI</au><au>CAI TANQIANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Missile wing high-temperature-resistant heat-insulating coating, preparation method thereof and missile wing</title><date>2023-03-28</date><risdate>2023</risdate><abstract>The invention relates to the field of high-temperature-resistant heat-insulating coatings, in particular to a missile wing high-temperature-resistant heat-insulating coating, a preparation method of the missile wing high-temperature-resistant heat-insulating coating and a missile wing. Comprising the following components: 80-100 parts of boron-containing organic silicon resin, 25-40 parts of mesoporous silica hollow spheres, 8-15 parts of silanol-based POSS, 5-10 parts of organic bentonite, 1-2 parts of a silane coupling agent, 10-15 parts of low-melting-point glass powder, 1-3 parts of a dispersant, 3-5 parts of a light stabilizer, 5-10 parts of methyl isobutyl ketone and 150-180 parts of an organic solvent. The high-temperature-resistant heat-insulating coating has good high-temperature-resistant and heat-insulating performance, shows good wave absorbing performance and can improve the stealth performance of guided missiles.
本发明涉及耐高温隔热涂层领域，具体为一种弹翼耐高温隔热涂层及其制备方法、弹翼，以重量份数计，包括以下组份：含硼有机硅树脂80-100份、介孔二氧化硅空心球25-40份</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | ADHESIVES AMMUNITION BLASTING CHEMICAL PAINT OR INK REMOVERS CHEMISTRY COATING COMPOSITIONS, e.g. PAINTS, VARNISHES ORLACQUERS CORRECTING FLUIDS DYES EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION FILLING PASTES HEATING INKS LIGHTING MECHANICAL ENGINEERING METALLURGY MISCELLANEOUS APPLICATIONS OF MATERIALS MISCELLANEOUS COMPOSITIONS NATURAL RESINS PAINTS PASTES OR SOLIDS FOR COLOURING OR PRINTING POLISHES USE OF MATERIALS THEREFOR WEAPONS WOODSTAINS |
| title | Missile wing high-temperature-resistant heat-insulating coating, preparation method thereof and missile wing |
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