http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-110087866-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_129e393582e6bdf4029baf2206522f45 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C44-12 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C44-128 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C43-006 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C70-681 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C70-745 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C44-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C39-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C70-68 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C39-38 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C39-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C44-04 |
| classificationIPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29K105-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29L9-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29K105-06 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C39-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C39-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C70-68 |
| filingDate | 2017-12-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d118243da3cb4d4cae2f8575d0e51239 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_8b266d985cb0899781b7b296fa8edcc9 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_babc1644ae4835103781c924754c83d4 |
| publicationDate | 2019-08-02-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-110087866-A |
| titleOfInvention | Manufacturing method of composite structure and manufacturing method of integrated composite structure |
| abstract | The present invention provides a method for producing a composite structure capable of easily forming a complex shape without requiring high cost, and capable of producing a composite structure excellent in light weight and mechanical properties. The method for manufacturing a composite structure according to the present invention is a method for manufacturing a composite structure in which a first member and a structure of a second member are integrated, characterized by comprising the following steps: an arranging step; A structure precursor having a resin and reinforcing fibers is disposed in the mold composed of the first member; in a heating step, the structure precursor is heated until the storage elastic modulus (G') of the structure precursor becomes less than 1.2 A temperature of ×10 8 Pa or higher; a forming step of expanding the above-mentioned structural body precursor by heating, and making it a structure of the second member to be brought into close contact with the first member to obtain a composite structure; and a cooling step, the In the cooling of the composite structure, the flexural modulus of the first member at the temperature of the heating step is 5 GPa or more, and the structure of the second member includes a resin, reinforcing fibers, and voids. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-115430825-A |
| priorityDate | 2016-12-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 40.