http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-2958624-A1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_4e3c804fb60c8285b549597da004115a |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D29-04 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C9-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26 |
| filingDate | 2010-04-08^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_3852cd48daa04ddbe493624b30b80d73 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_7bbcf5f350badafc398b73441a961be9 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1fd0e52d7388e009559ef438ef9edcd7 |
| publicationDate | 2011-10-14^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | FR-2958624-A1 |
| titleOfInvention | AIRCRAFT TURBOHOMOTING MACHINE, COMPRISING AN INCOMING MOBILE REAR FLAP |
| abstract | The invention relates to an engine assembly for an aircraft, comprising a propeller turbine engine and an attachment pylon (14) intended to be laterally attached to a rear part of the aircraft structure, the mast having a surface aerodynamic profile (20) incorporating a trailing edge (21), the latter being arranged upstream of the turbine engine propeller. According to the invention, the mast comprises a movable rear flap (24) defining at least partly the trailing edge (21), and control means (34) of the flap designed to drive the latter in incidence, according to a law depending on the impact of the aircraft. |
| priorityDate | 2010-04-08^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
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