http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CA-2995699-A1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_9cbbaf2c3314ee557a571acf8872ab83 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C13-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U10-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-82 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C27-57 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G05D1-0077 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G05D1-101 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D47-00 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C13-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G05D1-10 |
| filingDate | 2018-02-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_623d3f33165cc6e1fb1c08cbeedda4e6 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c4c0be8614bbc3eff18c9e4a27a86f31 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9844bd49afdead179b75be357f2d4884 |
| publicationDate | 2018-09-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CA-2995699-A1 |
| titleOfInvention | Automatic pilot device for a rotary-wing aircraft and rotary-wing aircraft including such a device |
| abstract | This autopilot device comprises at least one set of steering automatic actuator (22) comprising at least two primary actuators (24, 26, 28), at least one or each of the primary actuators (24, 26, 28) incorporating a calculation unit (40) Electronic configured for: communicate with a measurement system (14) configured to generate signals and / or a control station (12) configured to generate signals of command based on the actions of a crew, and - calculate, as a function of the measurement signals and / or the command, a control setpoint for the primary actuator (24, 26, 28) incorporating this calculation unit and / or a control setpoint for at least one or each other actuator primary (24, 26, 28) of the autopilot assembly (22), for controlling the aircraft by the autopilot device. |
| priorityDate | 2017-03-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 26.