http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-3155888-U
Outgoing Links
| Predicate | Object |
|---|---|
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C21-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D37-00 |
| filingDate | 2009-04-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2009-12-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2009-12-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-3155888-U |
| titleOfInvention | Combination of aircraft and helium injecting and discharging equipment aimed at reducing fuel consumption and CO2 emissions |
| abstract | An aircraft capable of reducing fuel consumption by adopting a fuselage shape capable of reducing air resistance during take-off and providing an inlet / outlet for injecting and exhausting helium. A fuselage with a fixed main wing including an auxiliary wing, a tail with a nose and an elevator, a tail with a vertical tail including a rudder, and a jet engine fixed to the tail or the main wing or the nose. Or, in an aircraft composed of a propeller and a propeller engine, a fuel tank, a take-off and landing leg, and a steering control device that controls flight of the aircraft, the apex and front position from the nose 1 to the aft 7 direction Protruding blade 18 is sharply sharpened, and at the time of take-off, the air and airflow to the aircraft above the aircraft is cut to the left and right, reducing the upward air resistance to the aircraft as the aircraft rises, and generated by the main wing Increases the lifted power and enables the fuel consumption during take-off to be reduced. [Selection] Figure 1 |
| priorityDate | 2009-04-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 15.