发明名称 Pylon mounting arrangement for an aircraft engine
摘要 <p>The connector consists of a curved bar (16) with a central section fixed to the pylon (10) and two end sections attached to the engine by couplings (18), each of which incorporates a safety element (44) which transmits the engine weight to the bar in the event of a failure in another part of the coupling. The bar is made in two transverse sections joined by bolts (24) and connected separately to the pylon by traction bolts (30).</p>
申请公布号 EP0940337(A1) 申请公布日期 1999.09.08
申请号 EP19990400480 申请日期 1999.03.01
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 LE BLAYE, SEBASTIEN
分类号 B64D27/26;(IPC1-7):B64D27/26 主分类号 B64D27/26
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