http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9718532-B2
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_3c661150bbace93394332abb390d97eb |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T70-5236 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B63B2035-009 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T70-583 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C2003-142 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-12 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C3-26 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B63H9-0607 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B63H9-061 |
| classificationIPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C3-14 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B63H9-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C3-26 |
| filingDate | 2013-11-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2017-08-01-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ba2f0929e0a6e80246076f5a608b81f4 |
| publicationDate | 2017-08-01-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | US-9718532-B2 |
| titleOfInvention | Wing and application thereof |
| abstract | The present disclosure relates to a wing. More specifically, aspects of the invention relate to a variable shaped wing movable incrementally between a neutral configuration and a deformed configuration, wherein the wing takes a reflexed camber aerofoil section shape in the deformed configuration. The wing includes a first aerofoil segment and a second aerofoil segment having ends connected or fixed to one another at opposing neutral leading and trailing edges and spaced apart from one another along their lengths across a neutral mean camber line extending between the neutral leading and trailing edges to form a neutral aerofoil section of the wing. One or more actuators deform the wing between the neutral aerofoil section and a reflexed camber aerofoil section, with the first and second aerofoil segments being resilient to bias the wing towards an initial at rest aerofoil section. |
| priorityDate | 2012-11-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 25.