http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-2987347-A1

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classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-26
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filingDate 2012-02-28^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1371451c83bc85087f54c20867e60226
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publicationDate 2013-08-30^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber FR-2987347-A1
titleOfInvention CUTTING PIECE FOR A REAR SUSPENSION OF A TURBOMOTEUR TO AN AIRCRAFT PYLON AND SUSPENSION COMPRISING SUCH AN ATTACHMENT PIECE.
abstract According to the invention, the attachment piece (19) for the rear suspension (3B) of a turbine engine (1) to an aircraft pylon (2) and intended to be fixed on an inter-turbine casing (5) the turbine engine (1), arranged between a high-pressure turbine casing (6) and a low-pressure turbine casing (7), is remarkable in that it comprises a portion of frustoconical ferrule (20) of angular sector (alpha) predetermined.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/GB-2551632-B
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3075175-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-111511644-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9784135-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2019122634-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11440670-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10843806-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2022248791-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-3123323-A1
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