http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-2190741-B1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_bab2564536aab165272a9a5f75808a21 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D29-08 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D29-08 |
| filingDate | 2008-05-05^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2011-08-31^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c74dfc194540517f702fdafa2a6f5f27 |
| publicationDate | 2011-08-31^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | EP-2190741-B1 |
| titleOfInvention | Jet engine nacelle with dampers for half-shells |
| abstract | The present invention relates to a jet engine nacelle (1) comprising an aft section (8) formed from at least two half-shells (9) rotatably mounted such that they can each be deployed between a working position and a maintenance position under the action of a telescopic ram (11) and of a telescopic connecting rod (12) each respectively having a first end (13, 14) fastened in or on the jet engine and a second end (16, 17) fastened in the corresponding half-shell, characterized in that it comprises at least one damping member (19) arranged between each connecting rod and said half-shell, said damping member being designed such that it is in a prestressed state when the half-shell is in the working position. |
| priorityDate | 2007-08-20^^<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/compound/CID91778 http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419545405 |
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