http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-210882660-U
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_917878769458a5412113ca874f0cc114 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C25-26 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C25-62 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C3-56 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D45-04 |
| filingDate | 2019-11-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2020-06-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c5f67bc6fdf3d2f47388aeee10fc47d5 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b477ad292f67c4b20d9dd0fa3df584ec |
| publicationDate | 2020-06-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-210882660-U |
| titleOfInvention | Protection type unmanned aerial vehicle |
| abstract | The utility model discloses a protection type unmanned aerial vehicle, which comprises a fuselage, flexible wing, landing gear and fin, flexible wing sets up in the fuselage both sides, the fin sets up in the fuselage afterbody, the landing gear sets up in the fuselage lower part, the fuselage lower part still is provided with first rubber layer and air bag, first rubber layer middle part is provided with first well kenozooecium, air bag sets up in first well kenozooecium, landing gear includes the gyro wheel, wheel fork and bracing piece, gyro wheel and wheel fork swing joint, the bracing piece sets up in wheel fork upper portion, the bracing piece outside is provided with the sleeve pipe, the intraductal limiting plate that is provided with of cover, the free end of bracing piece runs through the limiting plate, pass through spring coupling between limiting plate and the wheel fork, the spring cup joints in the bracing. This unmanned aerial vehicle can effectively solve the problem that the trouble that exists of current unmanned aerial vehicle falls the back and can't carry out the self-protection and fall after falling the surface of water and sink, causes the problem of equipment damage. |
| priorityDate | 2019-11-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 21.