http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-111522047-B
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01K7-22 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01T7-005 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01T1-00 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01T7-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01K7-22 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01T1-00 |
| filingDate | 2020-03-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2022-01-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2022-01-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-111522047-B |
| titleOfInvention | Space-borne space photoelectric conversion module and photoelectric detection device |
| abstract | The invention provides a space-borne space photoelectric conversion module and a photoelectric detection device, wherein the photoelectric detection device comprises an array formed by photoelectric detection units, each photoelectric detection unit comprises a crystal module and a photoelectric conversion module, each photoelectric conversion module comprises a photoelectric converter, an electronics reading circuit board and a protection structure, each protection structure comprises an inner bushing, a magnetic shielding device and an outer bushing, the inner bushing and the outer bushing are made of magnesium-aluminum alloy materials, and the magnetic shielding devices are made of permalloy sheets. According to the invention, through structural improvement, the crystal module/the photoelectric conversion module are relatively independent, the problem of convenience in replacement of the satellite-borne crystal and the photoelectric conversion module can be solved, the inheritance of aerospace products is improved, the development period is shortened, the detection device can meet the requirement of the launching environment through the examination of the space mechanics environment, and the structural quality of equipment is effectively reduced through the integrated compact design on the premise of ensuring the structural strength. |
| priorityDate | 2020-03-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 23.