发明名称 |
Suspension of a jet engine to an aircraft |
摘要 |
<p>The suspension has a front attachment (10) on an intermediate case (3), and a rear attachment (11) with two tie rods (114, 115) connected to an external ferrule (83) of an exhaust case (8). Pair of thrust transmission rods (12) is fixed to upstream of a hub of the case (3). A plane formed by two rods is inclined with respect to a plane of the case. The two tie rods connect the ends of a transversal beam to the external ferrule of the case (8).</p> |
申请公布号 |
EP2067698(A1) |
申请公布日期 |
2009.06.10 |
申请号 |
EP20080170679 |
申请日期 |
2008.12.04 |
申请人 |
SNECMA |
发明人 |
CHOUARD, PIERRE-ALAIN, JEAN-MARIE, PHILIPPE, HUGUE;LEFORT, GUILLAUME |
分类号 |
B64D27/26 |
主分类号 |
B64D27/26 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|