http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102007008942-A1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_5f2b4f3cb7d30e6f6ec9389ca927205f |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-52 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-52 |
| filingDate | 2007-02-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_27edc2b3c49ac8f721a48598affd52db http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9905db20335c8743f768794094185b8c |
| publicationDate | 2008-09-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | DE-102007008942-A1 |
| titleOfInvention | Injection head for the combustion chamber of a rocket engine |
| abstract | ThenThe invention relates to an injection head (1) for the combustion chamber (2) of anRocket engine, which has a footprint that exceeds a numbernis arranged distributed on injection elements (5). There are eachnfrom an outlet (6) of the injection elements (5) fuel componentsninto the combustion chamber (2) injectable, so that by mixingnand combustion of the fuel components in the combustion chamber (2)nhot gasnwhich is capable of generating thrust at a high speednis acceleratable. The base areanof the injection head (1) has a contoured shape, whereinnby the contoured shape the emergence of zones with reducednPressure, in particular between immediately adjacent outlets (6),nprevented or at least reduced. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2453722-C2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2572261-C2 |
| priorityDate | 2007-02-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 20.