http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-115217669-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c094c8526b300120081f9f27c0ba8f7c |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K1-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D15-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D25-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-02 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D5-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D15-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C3-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K1-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D25-24 |
| filingDate | 2022-07-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2845bd8ef7dff077ac058b5b73d8c24f http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5204262b26edb0c202b731425c8ee603 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_56724222f47b32131a909201f9f62a49 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6603c1a415d78e63e13e9af379358f57 |
| publicationDate | 2022-10-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-115217669-A |
| titleOfInvention | A space turbine power generation system with a Rafael oblique cut nozzle and an air flotation structure |
| abstract | The invention discloses a space turbine power generation system with a Rafael oblique cut nozzle and an air flotation structure, and relates to the field of space spacecraft energy, comprising a high-pressure gas cylinder, a fuel storage tank, an oxidant storage tank, a gas generator, a turbine, Planetary gear box, generator and rectifier, fuel storage tank and oxidant storage tank are respectively connected with high pressure gas cylinders through air conduits, high pressure gas cylinders are connected with turbine air inlets through conduits, and fuel storage tanks are connected with fuel inlets of generators through conduits , the fuel outlet of the generator is connected with the fuel inlet of the planetary gear box through the conduit, the oxidant storage tank is connected with the feed port of the gas generator through the conduit, the fuel outlet of the planetary gear box is connected with the feed port of the gas generator, and the gas is generated. The outlet of the generator is connected to the air inlet of the turbine, and the terminal of the generator is connected to the terminal of the rectifier. The invention solves the lubrication problem of the bearing under the condition of high rotational speed of the air-inlet micro-turbine, and has the characteristics of stable operation, high reliability and long service life. |
| priorityDate | 2022-07-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 28.