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rotor blade of helicopter KT-112 'kadet'

机译:直升机KT-112“学员”的旋翼

摘要

A helicopter rotor blade contains a longeron, a point of attachment of a blade to a rotor hub, a root fairing, a final fairing, an anti-flutter load, a balance weight located in the final fairing, a rear compartment, a covering, rubber and metallic anti-abrasive cover plates and a trimmer plate located in the rear compartment. For increasing the aerodynamic qualities with increase of strength and hardness the blade additionally contains a stiffener located in the tail section of the blade downstream of the rear compartment, an additional balance weight located in the root part of the blade, and clamps of basic and additional balance weights.
机译:直升机旋翼桨叶包括纵梁,桨叶与旋翼轮毂的连接点,根部整流罩,最终整流罩,抗颤振负载,位于最终整流罩中的平衡重,后舱,外罩,橡胶和金属的防磨盖板以及位于后车厢中的微调板。为了通过增加强度和硬度来提高空气动力学质量,叶片还包括位于叶片后部隔室下游的尾部中的加强筋,位于叶片根部的额外平衡重以及基本和附加的夹具平衡重。

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