Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_558b57c8c61df7eb6dde16dab37f4ab4 |
classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2027-268 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-40 |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-20 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-18 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26 |
filingDate |
2010-12-27^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9b7ef371763f75c815af9c4d29987462 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_29970bba0a2ff56840f8a1544af09d8f |
publicationDate |
2012-06-29^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
FR-2969578-A1 |
titleOfInvention |
DEVICE FOR SUSPENDING A TURBOJET ENGINE |
abstract |
Suspension of a turbojet engine by articulated tie rods. A fastener comprises a support (37) comprising three branches (40, 41, 42) provided with passageways traversed by an axis (39), this axis being oriented generally parallel to a tangential direction of the casing and being articulated by ball (47) to the central branch (40) of the support. |
isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3079212-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2018031548-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-3792182-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3100530-A1 |
priorityDate |
2010-12-27^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |