http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-0844174-A1

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filingDate 1997-11-20^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_0ba7e2f3426ad6fa9942f2d1788aac68
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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).
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priorityDate 1996-11-21^^<http://www.w3.org/2001/XMLSchema#date>
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