An aircraft having a fixed structure (50), an engine pylon (100) and a fairing system (200), a slider (52) carrying a rear fairing and being translationally movable from an advanced position to a retracted position, a displacement system (250) having a guide (402a-b), a sliding element (404a-b) and a support (406a-b) on each side of a median plane (XZ) of the engine pylon (100), the guide being integral with the fixed structure (50), the sliding element (404a-b) being movable relative to the fixed structure (50), and the support (406a-b) being movable relative to the engine pylon (100). The sliding element is integral with the slider (52) and slides along each guide (402a-b) provided on the same side, and the support is integral with the fixed structure (50) and has a vane (408a-b) parallel to the translation direction on which a surface of the slider (52) parallel to the translation direction rests. The presence of the movable cowl particularly ensures easy access to the interior of the engine pylon and the system housed in the engine pylon.
一种飞行器,具有固定结构(50)、发动机挂架(100)和整流罩系统(200),滑动件(52)承载后整流罩并且能够从前进位置平移运动到缩回位置,位移系统(250)在发动机挂架(100)的中间平面(XZ)的各侧上具有引导件(402a-b)、滑动元件(404a-b)和支承件(406a-b),引导件与固定结构(50)成一体,滑动元件与滑动件(52)成一体并沿设置在同一侧上的每个引导件(402a-b)滑动,支承件与固定结构(50)成一体并具有平行于平移方向的叶片(408a-b),滑动件(52)的平行于平移方向的表面搁置在该叶片上。可动整流罩的存在尤其确保了容易通达发动机挂架的内部和容纳在发动机挂架中的系统。
Aircraft with movable fairing on engine pylon
发动机挂架带有可动整流罩的飞行器
2024-06-21
Patent
Electronic Resource
Chinese
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