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/B64D2027-266 |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-26 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-18 |
filingDate |
1997-11-20^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_0ba7e2f3426ad6fa9942f2d1788aac68 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_127e7cbbaaa7dcc0dcede8da58718efb http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a0a78a8662ca8f30ca90bcb52aba9b19 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1895231152ea9a1308cc63d59a4f2456 |
publicationDate |
1998-05-27^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
EP-0844174-A1 |
titleOfInvention |
Redundant front suspension for a turbo engine |
abstract |
The invention relates to a redundant front suspension of a turbomachine on a mast (2) carried by an aircraft. The normal front suspension comprises a base part (4) fixed to the mast and having a suspension axis (5) cooperating with the intermediate casing of the engine. Thrust take-up bars (6, 7) connect the intermediate casing to the base part (4). The suspension device comprises a first support (20) fixed to the mast (2) and a second support (40) fixed to the intermediate casing each having a vertical yoke (30). These vertical yokes support a pin (33) arranged with play in one of the yokes. The second support (40) comprises a finger (45) which lodges with clearance in a bore (22) of a horizontal yoke (21) of the first support. The finger (45) and the horizontal yoke (21) take up the transverse forces in the event of rupture of the normal suspension. The vertical yokes take up the longitudinal and vertical forces in the event of failure of the normal suspension or of a thrust take-up bar (6, 7). |
isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2007033995-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2009510303-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2016042264-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3131734-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10081433-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3025782-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-4729623-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10486819-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-7963480-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-2891243-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-107074370-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-107074370-B http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2009509826-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3027873-A1 |
priorityDate |
1996-11-21^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |