发明名称 FAILS-SAFE JET ENGINE JOINT
摘要 <p>A suspension system including a front suspension plane located at an intermediate turboshaft engine casing and connecting same to a pylon, a rear suspension plane located at an exhaust casing of the turboshaft engine and connecting same to the pylon, and a failsafe intermediate suspension plane located between the front and rear planes and including at least one connecting rod connecting the turboshaft engine having a structural outer casing to the pylon, the connecting rod mounted on the turboshaft engine with a predetermined clearance that renders the connecting rod inoperable while the suspension system of the rear plane is operating. The connecting rod is advantageously arranged between the outer casing and the pylon, and an element made of a flexible material is combined with the connecting rod to create the predetermined clearance by an elastically deformable nature thereof.</p>
申请公布号 EP2580120(B1) 申请公布日期 2014.04.23
申请号 EP20110735475 申请日期 2011.06.09
申请人 SNECMA 发明人 BELLABAL, FRANCOIS;SEIZE, GUILHEM;VINCENT, THOMAS
分类号 B64D27/26 主分类号 B64D27/26
代理机构 代理人
主权项
地址