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发明公开
CN110871896A 包括铰接罩盖的飞行器涡轮发动机组件及飞行器 有权

包括铰接罩盖的飞行器涡轮发动机组件及飞行器
摘要：
本发明涉及飞行器的包括短舱的涡轮发动机组件及飞行器，短舱包括具有用于将附接支柱附接的区域的结构体，形成进气口唇缘的第一罩盖，安排在短舱的上部、在第一罩盖与附接区域之间的铰接罩盖，铰接罩盖的铰链系统包括在短舱的中间平面的两侧的呈前后的前部杆件和后部杆件，每个杆件的两个端部在与中间平面平行的同一平面中，每个杆件的第一端部安装成铰接在铰接罩盖上，每个杆件的第二端部安装成铰接在结构体上，以及可以从短舱的外部在锁定位置与解锁位置之间致动的锁定系统。短舱还包括至少一个缸，缸的一个端部安装成铰接在结构体上且其另一端部安装成铰接在铰接罩盖上，并且缸安排成帮助打开铰接罩盖并确保铰接罩盖被固持在打开位置中。
摘要（英）：

An aircraft turbine engine assembly including a nacelle structure with a strut attachment zone, a first cover forming an air intake lip, a hinged cover arranged on the nacelle upper portion, between the first cover and the attachment zone, a hinge system of the cover comprising, on either side of a mid-plane of the nacelle, a front rod and a rear rod that are one in front of the other. The two ends of each rod are co-planar, parallel to the mid-plane. A first end of each rod is hinged on the cover. A second end of each rod is hinged on the structure. A locking system is actuatable from the outside of the nacelle between a locked and an unlocked positon. The nacelle comprises at least one cylinder with a first end mounted hinged on the structure and the other end mounted hinged on the cover.

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