http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2009509828-A
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2027-268 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-26 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-12 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-20 |
| filingDate | 2006-09-26^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2009-03-12^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-2009509828-A |
| titleOfInvention | Engine suspension device provided between aircraft wing and engine |
| abstract | The present invention relates to an engine suspension system configured to be provided between an aircraft wing body and an engine. This suspension device comprises a high-rigidity structural part (8) and a front aerodynamic structural part (24) attached in a state fixed to the high-rigidity structural part (8) by suspension means. The front aerodynamic structural part includes an engine fan casing and is configured to be provided between the highly rigid structural part and the wing body. In the present invention, the suspension means comprises at least one length-adjustable connecting rod (32). One end of the connecting rod is attached to the highly rigid structural part (8) and the other end is attached to the front aerodynamic structural part. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2010536658-A |
| priorityDate | 2005-09-27^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
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