http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-107701312-B
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-32 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-22 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-16 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-04 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-16 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C3-22 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-32 |
| filingDate | 2017-11-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2020-11-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2020-11-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-107701312-B |
| titleOfInvention | Hypersonic engine |
| abstract | The invention discloses a hypersonic engine which comprises an air inlet channel, an air compressor, a combustion chamber and a spray pipe, wherein airflow enters the air compressor through the air inlet channel, is compressed and then enters the combustion chamber, and is discharged through the spray pipe after combustion, a gas precooler is arranged between the air inlet channel and the air compressor, the inlet of the gas precooler is connected with a fuel pump, the outlet of the gas precooler is connected to the combustion chamber, a turbine is not arranged in the engine, and the air compressor is driven by a motor to work. The invention cancels a turbine of an engine and a corresponding cooling system, uses plasma thermal jet to generate electricity, and uses the motor to drive the compressor, thereby solving the problem that the front total temperature of the turbine is limited at present; a plurality of motors are used for realizing a multi-rotating shaft scheme so as to replace the traditional hollow shaft scheme. |
| priorityDate | 2017-11-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 29.