发明名称 Mounting arrangement for an aircraft engine
摘要 <p>The mounting for an aircraft engine on a pylon (20) fixed to a wing or the fuselage comprises a fitting (26) fixed to the pylon by screws (34,36). Two connecting rods (28,30) connect the fitting to an engine structure part (22). Barrel nuts (38,40) in which the screws are screwed are placed in the same bores (42,43) as certain spindles connecting the connecting rods to the fitting.</p>
申请公布号 EP0934877(A1) 申请公布日期 1999.08.11
申请号 EP19990400223 申请日期 1999.02.02
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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