http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2019503941-A
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U70-83 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U10-13 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U50-15 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U50-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U2201-00 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U10-13 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C39-001 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C29-0025 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C39-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U70-83 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U50-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U50-15 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-20 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-82 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C39-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C39-024 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C15-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C15-02 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-20 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C39-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C27-08 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C29-00 |
| filingDate | 2016-12-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2019-02-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-2019503941-A |
| titleOfInvention | Vertical take-off and landing aircraft and its operation process |
| abstract | The present invention relates to an aircraft with vertical takeoff and landing and a method of operating the same. An aircraft with heavy aircraft type vertical takeoff and landing according to the present invention is a circularly symmetric aerodynamic carrier body (1), which is located on an aerodynamic contour rope and supports the components of the aircraft A carrier body and at least four vertical intubation propellers (3a), (3b), (3c), (3d), arranged symmetrically with the central vertical axis of the carrier body (1), It is also arranged symmetrically with respect to the preset flight axis and the horizontal axis of the carrier body (1), and the propellers (3a) and (3c) have the same direction of rotation opposite to the rotation of the propellers (3b) and (3d). A vertical intubation propeller and at least two horizontal intubation propellers (4) having opposing rotational directions and located inside or outside the carrier body, and a preset flight axis and both Horizontal intubation propellers and directional nozzles (5), installed in parallel to each other, one for each horizontal propeller (4), and supplied to the jet of the horizontal intubation propeller (4) by the power source (6) Directional nozzle and electronic control and flight management module (designed to provide vector orientation and supply the necessary power to operate all installed engines and all electrical and electronic equipment) 7) and a landing gear (9) intended to promote contact between the aircraft and the ground. [Selection] Figure 3 |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-102219922-B1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2020037377-A |
| priorityDate | 2015-12-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 39.