| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_f11ac5ada799060f8c2e97b1ee47b80d |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C2003-445 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C3-48
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C3-38 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C3-48 |
| filingDate |
2013-09-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_98bd3e274a94d49340eaf68f19252a50
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_3f76de506a0de891545b274b0e53cce4
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a4aedc450b4191ac5c9580cf21009565
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_99c60cb06438d0b8061bb13d5ba50344
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9ed11524eb94871456a8ba9c827204cc
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c277712dc4eb43141b9180e0c639a66b
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_db80175d4ef21e659978b294476122f6
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_205c9a2bd730342f953011c59e730fd1 |
| publicationDate |
2014-03-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
WO-2014041221-A1 |
| titleOfInvention |
Deformable wing including a mobile upper surface |
| abstract |
The invention relates to a deformable aircraft wing (1) including a mobile upper surface, comprising a double skin (7) on the upper surface of the wing (1), one of the aforementioned skins (7) corresponding to the leading edge (2), while the other corresponds to the trailing edge (3). The skins (7) overlap in the central zone of the wing such that they can move in relation to one another and they extend in the direction of the chord of the profile of the wing (1). The wing (1) comprises actuators (8) which are positioned on the main spars of the wing (5) and which exert a reaction force against the spars (5) when they exert the force necessary to deform the wing (1), moving the skins (7) in the direction of the chord of the profile until the low-speed flight, take-off and landing configuration is obtained. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2020115032-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2574491-C2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10654557-B2 |
| priorityDate |
2012-09-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |