| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_d3744297f7a58cf47d29b37e14000e68 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2027-266 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-26 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26 |
| filingDate |
2007-06-25^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4afe822ade546b2322054c2a30c6e3e3
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c518ee21feffe734a5af8246bbbb97b3
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_fb7645cbdae60fb160656a6144ac0bb8 |
| publicationDate |
2008-12-26^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
FR-2917711-A1 |
| titleOfInvention |
SUSPENSION OF A TURBOMOTEUR TO THE STRUCTURE OF AN AIRCRAFT |
| abstract |
The present invention relates to the suspension of a turbine engine to the structure of an aircraft of the type comprising a beam (2) with fastening means to said structure and at least one connecting rod (4) hinged at one end to a trunnion ( 6) integral with the beam and the other on a fixed fitting of the turbine engine. This suspension is characterized in that the pin (6) is mounted on the beam by means of a flexible connection (7). According to a preferred embodiment, the flexible connection consists of two laminated cylinders (71, 72), elastomer and metal, prestressed. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3098194-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3050722-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10843806-B2 |
| priorityDate |
2007-06-25^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |