| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_24f54aefd7a75822ce9d6a7759e20068
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_6a687322ae9230458025fa328de1c211 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29K2105-0827
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29L2031-7096
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-40
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29L2031-003
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29B11-16
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29L2031-709
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T156-1002
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29L2031-3082
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T156-1051 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C1-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C70-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29D99-0003
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C70-342
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B29C70-304 |
| classificationIPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29K105-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29L31-30 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C70-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C70-06
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B29C39-10 |
| filingDate |
2004-09-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_598f1a009423d1e6539a250aa60fb9b1
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_641fcd435f8fdd858772f33098765758 |
| publicationDate |
2006-03-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
JP-2006069166-A |
| titleOfInvention |
Manufacturing method of fiber reinforced composite material annular structure and annular frame for aircraft fuselage comprising the structure |
| abstract |
PROBLEM TO BE SOLVED: To provide a method for manufacturing a fiber-reinforced composite material annular structure having rigidity corresponding to each of a web part and a flange part in a relatively short time and at a low cost, and an annular frame for an aircraft fuselage comprising the structure. . SOLUTION: (a) An annular basic preform 2 having a flat plate annular web portion 21 and a flange portion 22 substantially perpendicular to the web portion 21 is formed from reinforcing fibers, and (b) the annular basic portion. A flat plate-shaped reinforcing preform 3 made of reinforcing fibers is joined to the web portion 21 of the preform 2 and (c) a cylindrical reinforcing preform made of reinforcing fibers is attached to the flange portion 22 of the annular basic preform 2. 4 is a method in which an annular fiber preform 1 having a monolithic structure is formed by bonding 4, and the obtained annular fiber preform 1 is impregnated with a matrix resin and cured. [Selection] Figure 1 |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/TW-I391234-B
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2014065280-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2014065281-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10273829-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2010140205-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2015504984-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9988156-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8790566-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9662841-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-7193282-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2020044675-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2492049-C2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2009178863-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9481442-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2011102033-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2598936-C1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2014084812-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-2502733-A2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-20200031506-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2010537889-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10668672-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-3623141-A1 |
| priorityDate |
2004-09-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |