http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-213677189-U
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_4735defcb28939997ecf240a6a828818 |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-40 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D41-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-12 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C7-00 |
| filingDate | 2020-10-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2021-07-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_8e3b76afb65439c661bc2c648e079e43 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_71f7075f3e2c3894850319603b769b99 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2b697129bfa609cf13675176de488337 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_eec9eda36d994599ed49614317798ec1 |
| publicationDate | 2021-07-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-213677189-U |
| titleOfInvention | Aircraft power supply system based on micro-combustion engine |
| abstract | The utility model discloses an aircraft power supply system based on little combustion engine, including nacelle and setting at inside little burning generator, controller, oil storage tank and the converter unit of nacelle, the nacelle include the support and wrap up at the outside covering of support, the middle part of nacelle is the straight section of cylinder, the windward side and the lee side of nacelle are provided with slick and sly transitional radome fairing. The oil storage tank comprises a front oil storage tank and a rear oil storage tank, and the front oil storage tank and the rear oil storage tank are communicated through a pipeline and a valve. The utility model is designed according to the requirement of aircraft power supply, and realizes the aircraft power supply based on a micro-combustion generator and a converter technology; the nacelle adopts a support and a skin structure of a frame beam bearing structure, the weight is reduced to the maximum extent, meanwhile, the windward side and the leeward side of the nacelle adopt fairing structures with pneumatic shapes, the air resistance is further reduced, and the gravity center position of the nacelle under the conditions of flat flight and an attack angle of 10 degrees meets the design requirements of an aircraft. |
| priorityDate | 2020-10-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
| Predicate | Subject |
|---|---|
| isDiscussedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID15320824 http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID449015670 |
Total number of triples: 19.