http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2629482-C1

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http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C39-02
filingDate 2016-03-29-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2017-08-29-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e8f6158e497f368bfd5224efefb98891
publicationDate 2017-08-29-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber RU-2629482-C1
titleOfInvention Unmanned combined helicopter
abstract FIELD: aviation. n SUBSTANCE: unmanned combined helicopter has two propellers in the rotary annulas ducts mounted on the sides of the bearing centerwings-compartment, in which the engines and the main reducer are located with the shafts laid inside the wing. The centerwing is made on a two-beam scheme with the propulsion bearing system and the concept of distributed traction of different-sized propellers (DTDP), arranged along the DTDP-X2+2 scheme, which includes, along with two smaller propellers in the rotary annulas ducts, different-sized propellers placed on pylon-sector, mounted on the centrowing wing above the mass center. The pylon is equipped with a reducer of crisscross propellers with an upper arrangement of V-shaped output shafts having an angle between their rotation axes equal to 30°. n EFFECT: simplification of longitudinal balancing with hovering and improvement of lateral-longitudinal controllability. n 1 dwg,1 tbl
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priorityDate 2016-03-29-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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Total number of triples: 22.