http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CA-2731960-C
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_4e3c804fb60c8285b549597da004115a |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D31-12 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F16F15-20 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D31-12 |
| filingDate | 2009-07-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2016-08-09-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_32087fa3394d0fd72c6f3b02763deb8e http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6f1d28ebc27cce7d3c1b493f28260017 |
| publicationDate | 2016-08-09-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CA-2731960-C |
| titleOfInvention | Aircraft including at least one engine having counter-rotating rotors |
| abstract | The aircraft (50) comprises at least one motor (56) with counter-rotating rotors, the engine or at least one of the engines with unbalance associated with at least one ellipse (70). The aircraft comprises means able to control the motor or at least one of motors so that, at a given engine speed, the major axis (68) of the ellipse or at least one of the ellipses extends into a direction for which vibrations generated by the engine (s) have a minimum intensity at at least one location predetermined, in particular in a predetermined zone, of the aircraft. |
| priorityDate | 2008-07-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 19.