发明名称 Mounting for jet engines - has separate mountings provided for engine pod and bypass casing
摘要 <p>Separate mountings are provided for engine pod (22) and by-pass casing (24) in two broadly co-incident planes. In the forward plane the engine is supported from one bracket (30) and the casing from another (50); in the after plane a single bracket (40) carries the engine directly and the casing indirectly, via two struts (58, 60) with universally jointed ends running to brackets below and on either side of the casing axis, in the forward mounting plante. For turbofan engines, that part of the by-pass casing adjoining the fan (62) is supported (64) from the engine to minimise clearance variation. The joint with the main casing (66) is near the mounting plane.</p>
申请公布号 IT1058337(B) 申请公布日期 1982.04.10
申请号 IT19750030784 申请日期 1975.12.24
申请人 ROLLS ROYCE 1971 LTD 发明人
分类号 B64D;(IPC1-7):64D/ 主分类号 B64D
代理机构 代理人
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