http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-110481774-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_a51bfab800a84c5ea378dcb6ed308037 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C33-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U10-40 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C33-02 |
| filingDate | 2019-08-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_7265e2998a539e4d6656ad450d748af5 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_438aaecec8ed125517cfa7071c9f024b http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f0b760633ce5fdb8b3c861d492ecd6c7 |
| publicationDate | 2019-11-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-110481774-A |
| titleOfInvention | A flapping wing structure and flapping wing aircraft based on main aileron mode |
| abstract | The invention discloses a flapping wing structure based on the main aileron mode. The main aileron mechanism includes connecting rods, upper and lower main wing main rods, elbow joints, aileron main rods and several main and aileron skeletons; The close pivot joint is pivotally connected to the corresponding crank of the drive mechanism, and the close pivot joint is pivotally connected to the close pivot joint of the upper main wing main rod, and its far body pivot joint is pivotally connected to the close personal pivot joint of the lower main wing main pole; the upper main wing main pole The secondary close pivot point of the lower main wing is pivotally connected to the fuselage, and its remote pivot point is pivotally connected to the upper pivot point of the elbow joint; For the knuckle joint, the aileron frame is sequentially fixed on the aileron main rod, and the main airfoil frame is sequentially fixed on the upper main wing main rod or the lower main wing main rod. The invention adopts a two-stage structure of the main wing and the aileron, which improves the transmission efficiency and has a simple and reliable structure; the main wing part is folded relative to the aileron part, the air resistance is reduced most efficiently, and the power is maximized. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112278267-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2022134394-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112407277-A |
| priorityDate | 2019-08-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 21.