发明名称 Redundant front suspension for a turbo engine
摘要 The suspension, comprises a base support (4) fixed to the pylon (2) and connected to an intermediate engine housing, incorporates an auxiliary system which operates only in the event of main suspension failure. The auxiliary system comprises a first support (20) fixed to the pylon (2) and equipped with vertical fastening (30) and a horizontal plate (21), and a second support (40) fixed to the intermediate engine housing and having a vertical plate and a peg (45). The vertical fastening (30) comprises two lugs which fit on either side of the vertical plate on the second support and are bolted to it with a clearance, while the peg (45) on the second support projects through a hole (22) in the forward end of the first support's horizontal plate.
申请公布号 EP0844174(A1) 申请公布日期 1998.05.27
申请号 EP19970402790 申请日期 1997.11.20
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A." 发明人 DEMOUZON, FRANCIS MICHEL;FER, RENE PIERRE;HUET, PATRICK JEAN ALIBERT;MARNAS, LAURENT
分类号 B64D27/18;B64D27/26;(IPC1-7):B64D27/26 主分类号 B64D27/18
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