发明名称 |
Aerodynamically shaped support and/or cladding element in the bypass of a gas turbine engine |
摘要 |
<p>The element has a supporting structure radially extended between inner and outer walls of a bypass duct and including a front edge part (7) and a rear edge part (8). A connecting rod (9) connects the front and rear edge parts to form a recess that extends on two sides in a longitudinal direction of the supporting structure. A lining insert (11) is detachably attached with an aerodynamically-shaped outer contour by a fastener, and aligned with the front and rear edge parts. Cavities (14) are formed in the connecting rod for enclosing installations radially extended in the duct. The fastener is selected from a group consisting of a socket-head screw or countersunk screw and a plug-type connection. The lining insert is made of material that is lighter than that of the supporting structure with reduced sound reflection and sound-absorbing effect.</p> |
申请公布号 |
EP2365199(A2) |
申请公布日期 |
2011.09.14 |
申请号 |
EP20110001265 |
申请日期 |
2011.02.16 |
申请人 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
发明人 |
CLEMEN, CARSTEN |
分类号 |
F02C7/20;F01D9/02;F01D9/06;F02K3/06 |
主分类号 |
F02C7/20 |
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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