发明名称 |
PROPULSION UNIT FOR AN AIRCRAFT |
摘要 |
<p>The present disclosure relates to a propulsion unit for an aircraft including a nacelle which surrounds a turbojet engine. The nacelle has an inner structure surrounding a downstream compartment of the turbojet engine, and the inner structure includes two annular half-portions. The propulsion unit also includes a rail/guide unit and to move the annular half-portions between a working position and a maintenance position. In particular, the rail/guide unit radially moves away the annular half-portions relative to a longitudinal axis of the nacelle, during a translation movement of the annular half-portions. The nacelle is provided with a connecting rod which is connected to the annular half-portions and to the turbojet engine and so that the connecting rod contributes to rotate the annular half-portions about the rail.</p> |
申请公布号 |
EP2931607(A1) |
申请公布日期 |
2015.10.21 |
申请号 |
EP20130820811 |
申请日期 |
2013.12.12 |
申请人 |
AIRCELLE;SNECMA SOCIÉTÉ ANONYME |
发明人 |
BOILEAU, PATRICK;CARUEL, PIERRE;ANCUTA, CARMEN;BEUTIN, BRUNO |
分类号 |
B64D29/08 |
主分类号 |
B64D29/08 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|