| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_b5dea06875d24beb15796be434afd892 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2237-765
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2237-84
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2237-38
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2235-77
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2235-96
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2235-5248
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2235-5244
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T428-30
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2237-365
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2237-704
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2235-614 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B32B18-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B35-571
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B35-80
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B35-62873 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C04B35-80
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C23C16-00 |
| filingDate |
2002-01-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
2007-08-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_8b978abd7bb1c4eb8de7421139b54e29
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_06aaa0091a4f98d4c485689f605f9aef
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ea69ff50f0c3cec54ebbada71e55db01 |
| publicationDate |
2007-08-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-7252860-B2 |
| titleOfInvention |
Process for producing a high temperature stable fiber reinforced ceramic |
| abstract |
A process is disclosed for producing a high temperature stable fiber composite ceramic by chemical vapor infiltration (CVI) with a silicon carbide precursor in a suitable carrier gas on carbon fiber preforms or silicon carbide fiber preforms. This process is characterized by the use of a process pressure of ≧0.6 bar absolute and a process temperature of ≧1100° C. Also disclosed are structural component parts, particularly for aircraft and spacecraft engineering, which are commonly exposed to high thermal and mechanical loading and which have been produced by the above process. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8728473-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9708226-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-106588060-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9512044-B2 |
| priorityDate |
2001-01-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |