http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CA-2841167-A1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_bab2564536aab165272a9a5f75808a21 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K1-72 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K3-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K1-625 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K1-72 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K1-62 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K3-06 |
| filingDate | 2012-07-17^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_69fba2134f0005b4d79c6653b5ad2405 |
| publicationDate | 2013-02-07^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CA-2841167-A1 |
| titleOfInvention | Aircraft propulsion unit including at least one turbojet engine and a nacelle |
| abstract | This nacelle for a double-flow turbojet comprises a cold air stream (16) having a non-constant cross-section on the periphery of the nacelle so that at least one flap (34) is offset radially with respect to the central axis of the turbojet, relative to the flaps (34) adjacent. The drive system flaps (34) offset radially is adapted to ensure a kinematic offset of said flaps (34) relative to the kinematics flaps (34) mounted on the rest of the periphery of the vein. |
| priorityDate | 2011-07-29^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
| Predicate | Subject |
|---|---|
| isDiscussedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419545405 http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID91778 |
Showing number of triples: 1 to 17 of 17.