Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_2f4b322f3fa77a2eb6b4d067b6585a40 |
classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C2009-005 |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C9-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C13-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C9-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D41-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C5-08 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C9-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C5-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D41-007 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C13-50 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C9-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C9-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C5-08 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C5-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C13-50 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C9-18 |
filingDate |
2020-03-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate |
2022-02-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6e747ddbbad10d7ac74e042049232ed5 |
publicationDate |
2022-02-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
US-11247767-B2 |
titleOfInvention |
Wireless autopilot system |
abstract |
A wireless autopilot system includes an aircraft attachment device having a mounting plate for securement onto a flight control surface of an aircraft, and a flight control device that is hingedly connected to the aircraft attachment device. The flight control device including an airfoil that is connected to the mounting plate, and a steering tab that is connected to the trailing edge of the airfoil. A main body extends outward from the airfoil to function as an anti-flutter counterbalance. A servomotor is connected to the steering tab by an elongated rigid rod, and a controller having a wireless transceiver for communicating with an application on an externally located processor enabled device. Changes in the position of the servomotor during flight are instructed by the application, and result in a change to the orientation of the aircraft. |
priorityDate |
2020-03-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |