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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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