NACELLE FOR AN AIRCRAFT ENGINE INCLUDING MEANS PREVENTING THE DEFORMATION OF THE ARTICULATED FAN COVERS

    公开(公告)号:US20200070991A1

    公开(公告)日:2020-03-05

    申请号:US16558704

    申请日:2019-09-03

    Abstract: A nacelle including a fixed structure, a central cover mounted on the fixed structure, a fan cover mounted on and articulated to the central cover between an open position and a closed position, and locking means that are distributed between each fan cover and the fixed structure and that are designed to assume a locked position in which they lock the fan cover to the fixed structure and an unlocked position in which they do not lock the fan cover to the fixed structure, in which the locked position can be adopted only when the fan cover is in the closed position, and in which the unlocked position can be adopted whether the fan cover is in the open or closed position and wherein the locking means are locked and unlocked by a rotation around a longitudinal axis of the nacelle.

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