| Predicate |
Object |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T428-30
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2237-704
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/C04B2237-365
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2237-38
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2237-84
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2237-765
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2235-614
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2235-5248
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2235-5244 |
| 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/C04B35-62873
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B35-80 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C04B35-80 |
| filingDate |
2002-01-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_25628a90acd095692a023dbf0509ef87
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c10351265afb7989a1ddf0f0868e61ff
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ff6a0802a30451794a6c5b2e0cfefb81 |
| publicationDate |
2002-09-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-2002132046-A1 |
| 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-2006228474-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-100371302-C |
| priorityDate |
2001-01-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |