http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2018508003-A
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C09K2200-0682 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F16B37-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C09K2003-1062 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F16B33-004 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B05D3-065 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08G59-4064 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-226 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C09K3-1012 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B05D5-00 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C09K3-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F16J15-14 |
| filingDate | 2016-02-12-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2018-03-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-2018508003-A |
| titleOfInvention | Method for applying sulfur-containing sealing compounds, apparatus used therefor, aerospace aircraft treated thereby, and use thereof |
| abstract | Disclosed is a method for applying a sulfur-containing sealing compound, an apparatus used therefor, an aerospace vehicle processed thereby, and a method of using the same. The present invention relates to a sulfur-containing SCOD sealing compound, wherein at least one application site, in particular an aerospace component, is at least protruded from the surface using at least one nozzle element and at least one irradiation unit. A method for sealing, covering and / or aerodynamically smoothing one connecting element and / or sealing, covering and / or aerodynamically smoothing a surface with gaps or a non-planar connection site Regarding the method. This is because i) the nozzle element contains a mixed sealing compound and is guided and / or mounted on a connecting element protruding from the surface, a gap and / or a non-planar connection site, ii) a connection protruding from the surface Elements, gaps or uneven connection sites are completely covered with a sealing compound, said sealing compound forming a sealing compound coating, which is essentially a SCOD sealing compound cap, coating and / or mound or beaded front Iii) the nozzle element or at least part is lifted from the surface with the sealing compound coating if necessary, and iv) the curing of the sealing compound is the energy input and latent catalyst of at least one irradiation unit Starting with the release of or directly activating at least one reaction component Brought about by, wherein the mixed sealing compound is cured subsequently cured and / or further. The invention also relates to a corresponding device, a spacecraft to be treated in this way and the use of said method and device. |
| priorityDate | 2015-02-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 83.